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Bewise Inc. www.tool-tool.com Reference source from the internet.

熱処理作業について学習を行う前に、今までにお話ししてきた中で出てきた金属組織について、その特徴を若干解説しておきましょう。

フェライト

純鉄に微量(常温で0.00004%、723℃で00218%)のCを固溶したα-固溶体のことで、組織学上フェライトと云います。また、α-鉄、地鉄と呼ばれることもあります。ラテン語の鉄Ferrum(フェルーム)からきています。bccの結晶構造を持ち、A変態点でγ-鉄に変わります。軟らかく延性に優れ、常温から780℃までは強磁性体です。顕微鏡的にはオーステナイトと同様、多角形状の集合体で腐食されにくい組織です。硬さは70~100HVです。

セメンタイト

FeとC(6.69%)の金属間化合物です。炭化物とも呼ばれFeCで表されます。金属光沢を有し硬くてもろく、常温では強磁性体ですが、213℃(A変 態:キューリ点)で磁性を失います。顕微鏡的には層状、球状、網状、針状を呈し、特に球状をしたものを球状セメンタイトと呼んでいます。耐摩耗性が要求さ れる工具や軸受けなどではなくてはならない組織の一つです。通常は腐食され難く、白色を呈していますが、ピクリン酸ソーダのアルカリ溶液で煮沸すると黒色 になります。また、FeCは比較的不安定な化合物で、900℃程度の温度で、長時間加熱すると黒鉛(グラファイト)に分解します。硬さは1200HV程度です。

パーライト

0.77%Cの鋼がA変態点で生じた共析晶です。フェライトとFeC が極く薄い層で交互に並んだもので、一見パール(真珠貝)のような色合いを示すことから、パーライトと呼んでいます。パーライトはオーステナイト状態の鋼 を、ゆっくり冷やした時に得られる組織で、冷却速度の相違によって層間隔が異なるため、3つに分類しています。普通パーライト(粗パーライト)は100倍 程度で層状が認められ、一般的に観察されるものです。中パーライトは1000倍位で認められず、2000倍で層間隔がわかる程度です。また、微細パーライ トは焼入れ冷却途中で、S曲線の鼻にかかり、生じたもので、2000倍でも層状が認めがたい組織です。硬さは240HV程度です。

マルテンサイト

1891 年ドイツのマルテンスによって発見された組織で、Cを固溶したα-固溶体のことです。オーステナイトを急冷したとき無拡散変態、つまり、焼入れした時に得 られる組織で結晶構造は、体心正方晶及び体心立方晶とがあります。組織的には麻の葉状又は針状を呈しています。鋼の熱処理の内で最も硬くもろい組織で、強 磁性を示します。このマルテンサイトを100~200℃で焼戻しを行うと、FeCが析出し、若干粘り強くなりますが腐食されやすくなります。この状態のマルテンサイトを焼入れの場合と区別し、焼戻マルテンサイトと呼んでいます。硬さは0.2%Cで500HV、0.8%Cで850HV程度です。

歡迎來到Bewise Inc.的世界,首先恭喜您來到這接受新的資訊讓產業更有競爭力,我們是提供專業刀具製造商,應對客戶高品質的刀具需求,我們可以協助客戶滿足您對產業的不同要求,我們有能力達到非常卓越的客戶需求品質,這是現有相關技術無法比擬的,我們成功的滿足了各行各業的要求,包括:精密HSS DIN切削刀具協助客戶設計刀具流程DIN or JIS 鎢鋼切削刀具設計NAS986 NAS965 NAS897 NAS937orNAS907 航太切削刀具,NAS航太刀具設計超高硬度的切削刀具BW捨棄式鑽石V卡刀BW捨棄式金屬圓鋸片木工捨棄式金屬圓鋸片PCD木工圓鋸片醫療配件刀具設計汽車業刀具設計電子產業鑽石刀具全鎢鋼V卡刀-電路版專用全鎢鋼鋸片焊刃式側銑刀焊刃式千鳥側銑刀焊刃式T型銑刀焊刃式千鳥T型銑刀焊刃式螺旋機械鉸刀全鎢鋼斜邊刀電路版專用鎢鋼焊刃式高速鉸刀超微粒鎢鋼機械鉸刀超微粒鎢鋼定點鑽焊刃式帶柄角度銑刀焊刃式螺旋立銑刀焊刃式帶柄倒角銑刀焊刃式角度銑刀焊刃式筒型平面銑刀木工產業鑽石刀具等等。我們的產品涵蓋了從民生刀具到工業級的刀具設計;從微細刀具到大型刀具;從小型生產到大型量產;全自動整合;我們的技術可提供您連續生產的效能,我們整體的服務及卓越的技術,恭迎您親自體驗!!

BW Bewise Inc. Willy Chen willy@tool-tool.com bw@tool-tool.com www.tool-tool.com skype:willy_chen_bw mobile:0937-618-190 Head &Administration Office No.13,Shiang Shang 2nd St., West Chiu Taichung,Taiwan 40356 http://www.tool-tool..com / FAX:+886 4 2471 4839 N.Branch 5F,No.460,Fu Shin North Rd.,Taipei,Taiwan S.Branch No.24,Sec.1,Chia Pu East Rd.,Taipao City,Chiayi Hsien,Taiwan

Welcome to BW tool world! We are an experienced tool maker specialized in cutting tools. We focus on what you need and endeavor to research the best cutter to satisfy users demand. Our customers involve wide range of industries, like mold & die, aerospace, electronic, machinery, etc. We are professional expert in cutting field. We would like to solve every problem from you. Please feel free to contact us, its our pleasure to serve for you. BW product including: cutting toolaerospace tool .HSS DIN Cutting toolCarbide end millsCarbide cutting toolNAS Cutting toolNAS986 NAS965 NAS897 NAS937orNAS907 Cutting Tools,Carbide end milldisc milling cutter,Aerospace cutting toolhss drillФрезерыCarbide drillHigh speed steelMilling cutterCVDD(Chemical Vapor Deposition Diamond )’PCBN (Polycrystalline Cubic Boron Nitride) Core drillTapered end millsCVD Diamond Tools Inserts’PCD Edge-Beveling Cutter(Golden FingerEdge modifying knifeSolid carbide saw blade-V typeV-type locking-special use for PC boardMetal Slitting SawaCarbide Side milling CuttersCarbide Side Milling Cutters With Staggered TeethCarbide T-Slot Milling CuttersCarbide T-Slot Milling Cutters With Staggered TeethCarbide Machine ReamersHigh speed reamer-standard typeHigh speed reamer-long type’’PCD V-CutterPCD Wood toolsPCD Cutting toolsPCD Circular Saw BladePVDD End Millsdiamond tool V-type locking-special use for PC board Single Crystal Diamond Metric end millsMiniature end millsСпециальные режущие инструменты Пустотелое сверло Pilot reamerFraisesFresas con mango PCD (Polycrystalline diamond) ‘FreseElectronics cutterStep drillMetal cutting sawDouble margin drillGun barrelAngle milling cutterCarbide burrsCarbide tipped cutterChamfering toolIC card engraving cutterSide cutterNAS toolDIN or JIS toolSpecial toolMetal slitting sawsShell end millsSide and face milling cuttersSide chip clearance sawsLong end millsStub roughing end millsDovetail milling cuttersCarbide slot drillsCarbide torus cuttersAngel carbide end millsCarbide torus cuttersCarbide ball-nosed slot drillsMould cutterTool manufacturer.

Bewise Inc. www.tool-tool.com

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情報を受け取って頂き、もっと各産業に競争力プラス展開。

弊社は専門なエンドミルの製造メーカーで、客先に色んな分野のニーズ

豊富なパリエーションを満足させ、特にハイテク品質要求にサポート致します。

弊社は各領域に供給できる内容は:

(1)精密HSSエンドミルのR&D

(2)Carbide Cutting tools設計

(3)鎢鋼エンドミル設計

(4)航空エンドミル設計

(5)超高硬度エンドミル

(6)ダイヤモンドエンドミル

(7)医療用品エンドミル設計

(8)自動車部品&材料加工向けエンドミル設計

弊社の製品の供給調達機能は:

(1)生活産業~ハイテク工業までのエンドミル設計

(2)ミクロエンドミル~大型エンドミル供給

(3)小Lot生産~大量発注対応供給

(4)オートメーション整備調達

(5)スポット対応~流れ生産対応

弊社の全般供給体制及び技術自慢の総合専門製造メーカーに貴方のご体験を御待ちしております。

BW специализируется в научных исследованиях и разработках, и снабжаем самым высокотехнологичным карбидовым материалом для поставки режущих / фрезеровочных инструментов для почвы, воздушного пространства и электронной индустрии. В нашу основную продукцию входит твердый карбид / быстрорежущая сталь, а также двигатели, микроэлектрические дрели, IC картонорезальные машины, фрезы для гравирования, режущие пилы, фрезеры-расширители, фрезеры-расширители с резцом, дрели, резаки форм для шлицевого вала / звездочки роликовой цепи, и специальные нано инструменты. Пожалуйста, посетите сайт www.tool-tool.com для получения большей информации.

BW is specialized in R&D and sourcing the most advanced carbide material with high-tech coating to supply cutting / milling tool for mould & die, aero space and electronic industry. Our main products include solid carbide / HSS end mills, micro electronic drill, IC card cutter, engraving cutter, shell end mills, cutting saw, reamer, thread reamer, leading drill, involute gear cutter for spur wheel, rack and worm milling cutter, thread milling cutter, form cutters for spline shaft/roller chain sprocket, and special tool, with nano grade. Please visit our web www.tool-tool.com for more info.

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Bewise Inc. www.tool-tool.com Reference source from the internet.

オー ステナイト状態に加熱した鋼を、連続的に しかも等速で冷却した時に生ずる変態の様相及び組織の変化を図示したものが連続冷却変態曲線又はC.C.T曲線と云います。S曲線と同様横軸に時間 (log)を取ったもので、S曲線と併記してあります。例えば完全焼なましの場合は、パーライト変態がaで開始し、bで終了します。また、油焼入れの場合は、a、aと交わったところで一部パーライト変態を起こしますが、a、bの変態中止線で変態を中止し、残りはMs点と交わるところで、マルテンサイトを生じます。したがって、得られる組織は微細なパーライトとマルテンサイトの混合組織です。この曲線もS曲線同様大切ですから、是非頭の中に入れておいて下さい。

歡迎來到Bewise Inc.的世界,首先恭喜您來到這接受新的資訊讓產業更有競爭力,我們是提供專業刀具製造商,應對客戶高品質的刀具需求,我們可以協助客戶滿足您對產業的不同要求,我們有能力達到非常卓越的客戶需求品質,這是現有相關技術無法比擬的,我們成功的滿足了各行各業的要求,包括:精密HSS DIN切削刀具協助客戶設計刀具流程DIN or JIS 鎢鋼切削刀具設計NAS986 NAS965 NAS897 NAS937orNAS907 航太切削刀具,NAS航太刀具設計超高硬度的切削刀具BW捨棄式鑽石V卡刀BW捨棄式金屬圓鋸片木工捨棄式金屬圓鋸片PCD木工圓鋸片醫療配件刀具設計汽車業刀具設計電子產業鑽石刀具全鎢鋼V卡刀-電路版專用全鎢鋼鋸片焊刃式側銑刀焊刃式千鳥側銑刀焊刃式T型銑刀焊刃式千鳥T型銑刀焊刃式螺旋機械鉸刀全鎢鋼斜邊刀電路版專用鎢鋼焊刃式高速鉸刀超微粒鎢鋼機械鉸刀超微粒鎢鋼定點鑽焊刃式帶柄角度銑刀焊刃式螺旋立銑刀焊刃式帶柄倒角銑刀焊刃式角度銑刀焊刃式筒型平面銑刀木工產業鑽石刀具等等。我們的產品涵蓋了從民生刀具到工業級的刀具設計;從微細刀具到大型刀具;從小型生產到大型量產;全自動整合;我們的技術可提供您連續生產的效能,我們整體的服務及卓越的技術,恭迎您親自體驗!!

BW Bewise Inc. Willy Chen willy@tool-tool.com bw@tool-tool.com www.tool-tool.com skype:willy_chen_bw mobile:0937-618-190 Head &Administration Office No.13,Shiang Shang 2nd St., West Chiu Taichung,Taiwan 40356 http://www.tool-tool..com / FAX:+886 4 2471 4839 N.Branch 5F,No.460,Fu Shin North Rd.,Taipei,Taiwan S.Branch No.24,Sec.1,Chia Pu East Rd.,Taipao City,Chiayi Hsien,Taiwan

Welcome to BW tool world! We are an experienced tool maker specialized in cutting tools. We focus on what you need and endeavor to research the best cutter to satisfy users demand. Our customers involve wide range of industries, like mold & die, aerospace, electronic, machinery, etc. We are professional expert in cutting field. We would like to solve every problem from you. Please feel free to contact us, its our pleasure to serve for you. BW product including: cutting toolaerospace tool .HSS DIN Cutting toolCarbide end millsCarbide cutting toolNAS Cutting toolNAS986 NAS965 NAS897 NAS937orNAS907 Cutting Tools,Carbide end milldisc milling cutter,Aerospace cutting toolhss drillФрезерыCarbide drillHigh speed steelMilling cutterCVDD(Chemical Vapor Deposition Diamond )’PCBN (Polycrystalline Cubic Boron Nitride) Core drillTapered end millsCVD Diamond Tools Inserts’PCD Edge-Beveling Cutter(Golden FingerEdge modifying knifeSolid carbide saw blade-V typeV-type locking-special use for PC boardMetal Slitting SawaCarbide Side milling CuttersCarbide Side Milling Cutters With Staggered TeethCarbide T-Slot Milling CuttersCarbide T-Slot Milling Cutters With Staggered TeethCarbide Machine ReamersHigh speed reamer-standard typeHigh speed reamer-long type’’PCD V-CutterPCD Wood toolsPCD Cutting toolsPCD Circular Saw BladePVDD End Millsdiamond tool V-type locking-special use for PC board Single Crystal Diamond Metric end millsMiniature end millsСпециальные режущие инструменты Пустотелое сверло Pilot reamerFraisesFresas con mango PCD (Polycrystalline diamond) ‘FreseElectronics cutterStep drillMetal cutting sawDouble margin drillGun barrelAngle milling cutterCarbide burrsCarbide tipped cutterChamfering toolIC card engraving cutterSide cutterNAS toolDIN or JIS toolSpecial toolMetal slitting sawsShell end millsSide and face milling cuttersSide chip clearance sawsLong end millsStub roughing end millsDovetail milling cuttersCarbide slot drillsCarbide torus cuttersAngel carbide end millsCarbide torus cuttersCarbide ball-nosed slot drillsMould cutterTool manufacturer.

Bewise Inc. www.tool-tool.com

ようこそBewise Inc.の世界へお越し下さいませ、先ず御目出度たいのは新たな

情報を受け取って頂き、もっと各産業に競争力プラス展開。

弊社は専門なエンドミルの製造メーカーで、客先に色んな分野のニーズ

豊富なパリエーションを満足させ、特にハイテク品質要求にサポート致します。

弊社は各領域に供給できる内容は:

(1)精密HSSエンドミルのR&D

(2)Carbide Cutting tools設計

(3)鎢鋼エンドミル設計

(4)航空エンドミル設計

(5)超高硬度エンドミル

(6)ダイヤモンドエンドミル

(7)医療用品エンドミル設計

(8)自動車部品&材料加工向けエンドミル設計

弊社の製品の供給調達機能は:

(1)生活産業~ハイテク工業までのエンドミル設計

(2)ミクロエンドミル~大型エンドミル供給

(3)小Lot生産~大量発注対応供給

(4)オートメーション整備調達

(5)スポット対応~流れ生産対応

弊社の全般供給体制及び技術自慢の総合専門製造メーカーに貴方のご体験を御待ちしております。

BW специализируется в научных исследованиях и разработках, и снабжаем самым высокотехнологичным карбидовым материалом для поставки режущих / фрезеровочных инструментов для почвы, воздушного пространства и электронной индустрии. В нашу основную продукцию входит твердый карбид / быстрорежущая сталь, а также двигатели, микроэлектрические дрели, IC картонорезальные машины, фрезы для гравирования, режущие пилы, фрезеры-расширители, фрезеры-расширители с резцом, дрели, резаки форм для шлицевого вала / звездочки роликовой цепи, и специальные нано инструменты. Пожалуйста, посетите сайт www.tool-tool.com для получения большей информации.

BW is specialized in R&D and sourcing the most advanced carbide material with high-tech coating to supply cutting / milling tool for mould & die, aero space and electronic industry. Our main products include solid carbide / HSS end mills, micro electronic drill, IC card cutter, engraving cutter, shell end mills, cutting saw, reamer, thread reamer, leading drill, involute gear cutter for spur wheel, rack and worm milling cutter, thread milling cutter, form cutters for spline shaft/roller chain sprocket, and special tool, with nano grade. Please visit our web www.tool-tool.com for more info.

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Bewise Inc. www.tool-tool.com Reference source from the internet.

UH-1 Iroquois

Bell UH-1D Huey of the United States Army

Type Multipurpose utility helicopter
Manufacturer Bell Helicopter Textron
Maiden flight 22 October 1956 (XH-40)
Introduction 1959
Primary users United States Army
Japan Ground Self-Defense Force
Australian Army
Armed Forces of the Philippines
Number built >16,000
Variants UH-1N Twin Huey
AH-1 Cobra
Bell 204/205
Bell 212
Bell 214

The Bell Helicopter Textron UH-1 Iroquois, commonly (or officially in the United States Marine Corps) known as the "Huey", is a multipurpose military helicopter, famous for its use in the Vietnam War. The "U" stands for utility, in contrast to attack or cargo helicopters.

The UH-1 was developed from 1955 US Army trials with the Bell Model 204. The initial designation of HU-1 (helicopter utility) led to its nickname, Huey. The nickname became so popular that Bell started putting the Huey name on the anti-torque pedals.[1]

The aircraft was first used by the military in 1959 and went into tri-service production in 1962 as the UH-1. The last were produced in 1976 with more than 16,000 made in total,[2] of which about 7,000 saw use during the Vietnam War.

In Vietnam, 2,202 Huey pilots were killed and approximately 2,500 aircraft were lost, roughly half to combat and the rest to operational accidents.

[edit] Development

Earlier helicopters had been powered by piston engines. By the early 1950s, however, turbine engines were being used in many fixed-wing aircraft and aircraft designers began to consider using them for rotary-wing use. Turbines, though expensive to build, were long-lived, durable, and extremely light for their power output in comparison to piston-powered engines.

[edit] XH-40 and YH-40

A Bell XH-40, a prototype of the UH-1

A Bell XH-40, a prototype of the UH-1

The first Bell helicopter to use a turbine engine was a modified Model 47 (designated the XH-13F), first flown in October 1954. In 1955, anxious to obtain a powerful medical evacuation helicopter, the U.S. Army awarded Bell a contract to develop the next generation turbine-powered helicopter, designated the XH-40 (Bell company designation was the Model 204). The first XH-40 flew on 22 October 1956. Two more prototypes were built in 1957, and six YH-40 prototypes were tested in 1958.

Bell believed the YH-40 was ideal for troop transport and cargo carrying as well as the medevac role, a view soon adopted by the Army, who found the pre-production aircraft so much better in service than previous piston-powered helicopters they soon ordered more of them.

[edit] UH-1A

The HU-1A (later redesignated the UH-1A) was the first turbine-equipped U.S. helicopter to go into production, and production models first entered service with the 101st Airborne Division at Fort Lewis, Washington, the 82nd Airborne Division and the 57th Medical Detachment. Although they were intended for evaluation only, the Army quickly pressed them into operational service and Hueys with the 57th Medical Detachment arrived in Vietnam in March 1962.[3]

The helicopter was originally designated the HU-1A, which is where it received its nickname - "Huey." The official U.S. Army designation Iroquois (Army helicopters are traditionally given Native American names) was almost never used in practice.[4]

Fourteen of the original order of UH-1As were designated as TH-1A which were used for crew training and a single aircraft was redesignated XH-1A for grenade launcher testing in 1960.[3]

The first UH-1As to arrive in Vietnam after the 57th Medical Detachment were with a new test unit, the US Army's Utility Tactical Transport Company (UTTCO). UTTCO had 20 "Alpha" Hueys and deployed to Vietnam in the fall of 1962.[5] These aircraft were used as armed escorts to the existing H-21 Shawnees and H-34 Choctaws troop carriers.[4][3]

In use the UH-1A proved under-powered with their Lycoming T53-L-1 powerplants of just 860 shp and indicated the need for improved follow-on models of the Huey.[4][3]

[edit] UH-1B

A UH-1B on display at Lackland AFB, San Antonio, Texas.

A UH-1B on display at Lackland AFB, San Antonio, Texas.

The HU-1B was an improved model that was equipped with the Lycoming T53-L-5 engine of 960 shp, revised main rotor blades of 44 foot diameter and 21 inch chord, 13 inch higher rotor mast and a longer cabin that could accommodate seven passengers.[4][3] This version was redesignated UH-1B in 1962.

Later production UH-1Bs were equipped with Lycoming T53-L-9 and L-11 engines of 1100 shp. Gross weight was 8,500 lbs and the standard empty weight was 4513 lbs.[4][3]

Army testing of the "B" model started in November, 1960 with first production aircraft arriving in March, 1961. A total of 1010 "Bravo" models were delivered to the US Army. First deployment was in November 1963 when eleven were sent to Vietnam to join the "Alpha" models already in use by UTTCO.[3]

One NUH-1B was produced for test purposes.[3]

Bell certified a civil version of the UH-1B incorporating some minor safety improvements, such as improved door locks. The aircraft was marketed as the Bell 204B.[3]

[edit] UH-1C

The UH-1C was specifically developed as a gunship version until the "interim" attack helicopter, the Bell AH-1G Huey Cobra was available and to correct the deficiencies of the UH-1B when it was used in the armed role. The UH-1C was widely referred to as the "Huey Hog" in US Army service.[4][3]

The "Charlie" model was fitted with the 1100 shp T53-L-9 or L-11 engine to provide the power needed to lift the weapons systems in use or under development at the time. It incorporated the new Bell 540 rotor system with 27 inch chord blades. The increased power lead Bell's engineers to design a new tailboom for the "C" which incorporated a wider chord fin on a longer boom and larger synchronized elevators. The "C" also introduced a dual hydraulic control system for redundancy in battle and an improved inlet filter system for the dusty conditions found in southeast Asia. Fuel was increased to 242 US gallons and gross weight to 9500 lbs, giving a nominal useful load of 4673 lbs.[4][3]

Development on the "C" model had commenced in 1960, with production starting in June 1966. A total of 766 "C" models was completed, including five for the Royal Australian Navy, designated N9 and five for Norway. The balance went to the US Army.[4][3]

Many UH-1Cs were later re-engined with the 1400 shp Lycoming T53-L-13 powerplant. With this engine they were redesignated UH-1M.[4][3]

[edit] UH-1D

The earlier "short-body" Hueys were a success, especially in the gunship role, but lacked the cabin space to be an effective troop transport. The US Army wanted a version that could carry a crew of four (two pilots and two door gunners) and also deliver an infantry section of eight-ten soldiers. Bell's solution was to stretch the UH-1B fuselage by 41 inches (105 cm) and use the extra space to fit two sideways-facing seats on either side of the transmission. This brought the total seating capacity to 15, including crew seats.[4][3]

The new Huey was designated UH-1D by the US Army and as the Model 205 by Bell. The enlarged cabin could also accommodate six stretchers, double that of the earlier models, making the "Delta" a good MEDEVAC aircraft. In place of the earlier model's sliding side doors with a single window, larger doors were fitted which had two windows, plus a small "hinged panel" with an optional window, providing access to the cabin. The doors and hinged panels were quickly removable and the Huey could be flown in that configuration.[3]

The first YUH-1D prototype flew in August 1960. Seven YUH-1Ds were delivered and tested at Edwards AFB starting in March 1961. The YUH-1D was initially equipped with a 44 ft main rotor and a Lycoming T53-L-9 engine. Testing revealed that more power was required and so the rotor was lengthened to 48 ft with a chord of 21 inches and the engine was upgraded to the Lycoming T53-L-11 engine of 1,100 shp. A longer tailboom was designed to accommodate the longer rotor blades. Gross weight was 9,500 lbs. Later production "Deltas" had the Lycoming T53-L-13 powerplant of 1,400 shp installed and redesignated as "Hotel" models.[4][3]

The first Army unit deliveries of the "Delta" model were on 9 August 1963 when the 11th Air Assault Division (Test) at Fort Benning Georgia received two. This unit was renamed the 1st Cavalry Division and deployed to Vietnam with its "Delta" Hueys.[4][3]

A total of 2008 UH-1Ds were delivered to the US Army between 1962 and 1966. The model was widely exported and served with the armed forces of Australia and South Vietnam among others. A grand total of 2,561 UH-1Ds were built, including 352 constructed by Dornier for the West German armed forces.[4][3]

The HH-1D was a base rescue/fire-fighting version for the US Army that had a 50 gallon water and foam spray system that could be discharged via an extendable 16 foot boom.[3]

Upgrading the UH-1D to the Lycoming T53-L-13 engine, plus relocating the pitot tube from the nose to the roof resulted in a new model, the UH-1H, which was to become the most produced variant of the Huey family.[4][3]

[edit] UH-1E

In 1962 the US Marines held a competition to choose a new assault support helicopter to replace the Cessna O-1 and Kaman OH-43D helicopter. The winner was the UH-1B which was already then in service with the US Army.[4]

The UH-1B was developed into a special model, designated UH-1E, to meet Marine Corps requirements. The major changes included the use of all-aluminum construction for corrosion resistance (earlier UH-1s had some magnesium components), special avionics that were compatible with Marine Corps ground frequencies, a rotor brake to stop the rotor quickly on shutdown for shipboard use and a roof-mounted rescue hoist.[4][3]

The UH-1E was first flown on 7 October 1963 and deliveries commenced 21 February 1964, with 192 aircraft completed. Due to production line realities at Bell the UH-1E was produced in two different versions, both with the same UH-1E designation. The first 34 built were essentially UH-1B airframes with the Lycoming T53-L-11 of 1,100 shp. Because Bell was switching Army production to the UH-1C the UH-1E production line was converted to commonality with the “C”. This meant the later “Echo” Hueys were completed with the “Charlie” style tailboom including the larger fin, the 540 rotor system and a gross weight of 8,500 lbs.[3]

The Marines used the UH-1E as both a gunship and troop transport. Many were upgraded to the Lycoming T53-L-13 engine which produced 1,400 shp, making these “Echos” similar to the Army “Mike” models. At least 126 UH-1Es survived their Vietnam service and were still in use more than a decade later.[4][3]

There was a Marine Corps training version of the UH-1E, which was based on the UH-1C variant and was designated TH-1E. Twenty were delivered in 1965.[3]

[edit] UH-1F

Bell Helicopters was the winner of a 1963 United States Air Force competition for a support helicopter for use on its missile bases.[3]

Bell had proposed the UH-1B for the competition but the USAF asked Bell to develop a special version of the "Bravo" in using the General Electric T58 turboshaft as a powerplant. The USAF already had a large inventory of these engines for its fleet of Sikorsky HH-3 Jolly Green Giant rescue helicopters and wanted to have commonality between the types. This engine was capable of 1,250 hp (932 kW) compared to the UH-1B's 1,100 hp (820 kW) Lycoming T53-L11.[3][4]

In response Bell proposed an upgraded version of the UH-1B with the T58 engine installed. The resulting UH-1F had the shorter cabin of the "Bravo" Huey, but with the longer tail boom, rotor and transmission of the UH-1D.[3]

Due to the Huey's configuration, Bell installed the T58 engine backwards compared to the HH-3. The Huey's engine is behind the transmission, whereas the HH-3's engines are in front of the transmission. Externally, the only visible differences from UH-1B were the engine exhaust, which exited to the right side of the engine and the longer tail boom.[3]

The UH-1F was introduced into the USAF inventory on 20 February 1964. The USAF took delivery of 119 with production ending in 1967. Many of the aircraft served in southeast Asia with the 20th Special Operations Squadron and some were converted to the armed UH-1P configuration.[3][4]

In Italy, Agusta produced a similar model by re-engining the 204B with the 1,225 hp (914 kW) Rolls-Royce Gnome turboshaft and later the UH-1F's General Electric engine. The Italian version was exported to the military of the Netherlands, Denmark, Austria, and Switzerland. It had a rescue hoist located at the right side of the cabin.

The last UH-1F was retired from the USAF in the early 1980s when it was replaced by the UH-1N. many of these aircraft later served as forest fire fighting aircraft with various US state governments and agencies.[3]

There was a TH-1F trainer also built for the USAF. The first TH-1F was flown in January 1967 and deliveries ran from April to July of that year with 27 completed.[3]

[edit] UH-1H

A Canadian CH 118 with 417 Squadron in the Rocky Mountains of British Columbia, January 1992

A Canadian CH 118 with 417 Squadron in the Rocky Mountains of British Columbia, January 1992
A US Army UH-1H serving with the Multinational Force and Observers South Camp, Naama Bay, Sinai, Egypt, 1989

A US Army UH-1H serving with the Multinational Force and Observers South Camp, Naama Bay, Sinai, Egypt, 1989

The UH-1H was an improved UH-1D, with the Lycoming T53-L-13 engine of 1,400 shp installed, plus the pitot tube relocated from the nose to the roof, to reduce ground damage to it. "Hotel" models were created by upgrading "Deltas" with the more powerful engine. The first YUH-1H flew in 1966 with deliveries of production models starting in September 1967.[4][3]

The "Hotel" model Huey was produced in larger numbers than any other model, with 4,850 delivered to the US Army alone.[4] The "Hotel" model was widely exported and was also built under licence in Germany, Italy, Japan and Taiwan.[3]

Ten were sold to Canada for use under the designation CUH-1H with the first one was delivered on 6 March 1968. These were evaluated by the Canadian Forces and found unsuitable for Canadian tactical use, which resulted in the Canadian government sponsoring the development of the twin-engined version of the "Hotel", the UH-1N Twin Huey. The ten CUH-1Hs were re-equipped for search and rescue use, redesignated CH-118 and served until 1995.[4][3]

The "Hotel" model Huey was also the basis for a number of sub-variants:

  • HH-1H was a UH-1H equipped for base rescue duties. Thirty were delivered to the USAF between 1970-73.[4][3]
  • EH-1H was a UH-1H modified under Project Quick Fix in 1976 and used as communications jamming aircraft with the US Army. Twenty-two aircraft were modified to this configuration beginning in 1976. Initial aircraft were fielded to the 82nd Airborne Division and the 2nd Armored Division. The 82nd fielded the type during the invasion of Grenada (Operation Urgent Fury) in 1983.[4][3]
  • EH-1X was an improved EH-1H communications jammer and DF aircraft.[3]
  • JUH-1 was a UH-1H equipped with retractable skid gear and an AN/APS 94 radar boom mounted on the belly.[3]
  • UH-1V was a MEDEVAC version of the "Hotel", with upgraded avionics.[3]
  • TH-1H: Modified UH-1Hs for use as basic helicopter flight trainers by the USAF.

Bell developed a certified version of the UH-1H for the civil market. The aircraft incorporated minor changes for safety, such as dual sliding door locks and a baggage compartment in the tailboom. It was marketed by Bell as the Model 205A and later the improved 205A-1.[3]

[edit] HH-1K

Bell was awarded a contract by the US Navy in December 1968 for a new search and rescue helicopter. The aircraft was designated the HH-1K and was basically a UH-1E with different avionics and the Lycoming T53-L-13 powerplant of 1,400 shp.[4][3]

Deliveries of the “Kilo” Huey started in May 1970 and by November of that year three had been sent to Vietnam to serve with US Navy squadron HA(L)-3. A total of 27 HH-1Ks were produced.[3]

[edit] UH-1L

With deliveries of the UH-1E underway to the US Marines the US Navy tested a few and found that the type would suit their uses as a utility helicopter. On 16 May 1968, the US Navy ordered eight aircraft under the designation UH-1L.[4][3]

The “Lima” Huey was basically a UH-1E, of the later production type based on the Army's UH-1C, equipped with a rescue hoist and intake particle screen. The “Ls” were delivered without the armour or armament installed and were equipped with the Lycoming T53-L-13 powerplant of 1,400 shp.[4][3]

The first four “Limas” were delivered in November 1969 and sent to Vietnam to equip the US Navy HA(L)-3 detachment assigned to Operation Sealords. In Vietnam the aircraft were modified with weapons and armour and were fitted to carry 500 lb bombs and 500 lb Fuel-Air Explosive munitions.[3]

There was a TH-1L version of the UH-1L for the Navy to replace the H-34 and the borrowed Army UH-1Ds used in the training role, including for pilot aircraft carrier qualification training. Forty-five TH-1Ls were delivered starting in November 1969.[3]

[edit] UH-1M

The "Mike" model Huey was a conversion of the existing UH-1C by re-engining it with the 1,400 shp Lycoming T53-L-13 powerplant used in the UH-1H. This provided more power to the "C" model for its role as a gunship and also provided engine commonality between the attack and transport helicopters in use in Vietnam at that time.[4][3]

[edit] UH-1N

Main article: UH-1N Twin Huey
Canadian Forces CH-135 Twin Huey, 1987

Canadian Forces CH-135 Twin Huey, 1987

Bell flew the first twin-engined Huey in April 1965, calling it the Model 208. It was powered by two Continental Motors engines. The Canadian government provided the incentive for Bell to continue development of the Twin Huey using Pratt & Whitney Canada PT6 engines. The project attracted orders from the Canadian Forces, US Marine Corps, US Navy and USAF, but not the US Army.[4][3]

The new aircraft was designated UH-1N Iroquois in US service and CUH-1N Twin Huey in Canadian Forces use. The Canadian designation was later changed to CH-135 Twin Huey. There was an HH-1N version produced for the USAF as a base rescue helicopter and for use by the 20th Special Operations Squadron in the counter-insurgency role using the call sign Green Hornet. Some Marine Corps UH-1Ns were converted to VH-1Ns as VIP transports, including six for Presidential use.[4][3]

The UH-1N was widely produced and exported to a large number of countries and licence-built by Agusta in Italy and the People's Republic of China. Bell certified a civil version as the Model 212 in October 1970.[4]

[edit] UH-1P

An unknown number of UH-1Fs were modified to UH-1P configuration by the USAF for use by the their 20th Special Operations Squadron, The Green Hornets, based in southeast Asia during the Vietnam War.[3][4]

Official USAF sources state that these aircraft were used for a classified psychological warfare role, but this is incorrect. The "Papa" Hueys were in fact modified and employed as gunships armed with machine guns and rocket launchers.[3]

[edit] UH-1V

The UH-1V is a version of the UH-1H converted by the US Army Electronics Command for MEDEVAC use. The aircraft have several upgrades including a radar altimeter, DME, ILS and a rescue hoist. The first aircraft were supplied to the New Hampshire National Guard.[3]

[edit] EH-1X

The EH-1X was an improved EH-1H that was equipped with the AN/ALQ-151 system and configured for the airborne jamming, radio intercept and DF role. Ten EH-1Xs were built starting in late 1976 under Project Quick Fix IIA.[3]

[edit] UH-1Y

Main article: UH-1Y Venom

The UH-1Y Venom is an upgraded UH-1N Twin Huey for the US Marines that was first flown on November 18 2006.

[edit] JUH-1 SOTAS

The JUH-1 was a modified UH-1H an AN/APS 94 radar system mounted in a rotating boom on the belly, where the cargo hook had been. The aircraft's skid landing gear was modified to retract allowing the radar antennae to rotate while in flight. The JUH-1s also incorporated an autopilot and improved navigation avionics. The radar system was connected by datalink to a ground station for analysis of the radar images.[3]

At least four UH-1Hs were modified to JUH-1s for use by the US Army in Europe and Korea for use as technology demonstrators in the Stand Off Target Acquisition System (SOTAS) program. They were first deployed in 1975 but by 1986 they had been replaced by the EH-60 Black Hawk.[3]

[edit] Operational history

[edit] Service in Vietnam

A UH-1D "Huey" seen offloading troops during the Vietnam War.

A UH-1D "Huey" seen offloading troops during the Vietnam War.

The UH-1 has long become a symbol of US involvement in Southeast Asia in general and Vietnam in particular, and as a result of that conflict, has become one of the world's most recognized helicopters. In Vietnam primary missions included general support, air assault, cargo transport, aeromedical evacuation, search and rescue, electronic warfare, and later, ground attack. During the conflict, the craft was upgraded, notably to a larger version based on the Model 205. This version was initially designated the UH-1D and flew operationally from 1963.

Helicopters played an integral part in the U.S military's land and air operations. Here UH-1Ds airlift members of the 2nd Battalion, 14th Infantry Regiment from the Filhol Rubber Plantation area to a new staging area, in 1966.

Helicopters played an integral part in the U.S military's land and air operations. Here UH-1Ds airlift members of the 2nd Battalion, 14th Infantry Regiment from the Filhol Rubber Plantation area to a new staging area, in 1966.

During service in the Vietnam War, the UH-1 was used for various purposes and various terms for each task abounded. UH-1s tasked with a ground attack or armed escort role were outfitted with rocket launchers, grenade launchers, and machine guns. These gunship UH-1s were commonly referred to as Hogs if they carried rockets, and Cobras if they had guns.[6] While UH-1s tasked for troop transport were often called Slicks due to an absence of weapons pods. Slicks did have door gunners, but for the most part they were strictly troop carriers and medevacs.[4][3] In the US Navy and USMC the difference between gunships were referred to as Sharks, troop transport aircraft, Dolphins.

USS Garrett County (AGP-786) at anchor in the Mekong Delta, South Vietnam, date unknown. On her deck are two Navy Helicopter Attack (Light) Squadron Three (HAL-3) "Seawolf" UH-1B Huey gunships from the squadrons Det Four or Det Six assigned to the ship.

USS Garrett County (AGP-786) at anchor in the Mekong Delta, South Vietnam, date unknown. On her deck are two Navy Helicopter Attack (Light) Squadron Three (HAL-3) "Seawolf" UH-1B Huey gunships from the squadrons Det Four or Det Six assigned to the ship.

UH-1s also flew hunter-killer teams with observation helicopters, namely the Bell OH-58A Kiowa and the Hughes OH-6 Cayuse (Loach).[4][3]

Towards the end of the conflict, the UH-1 was tested with TOW missiles, and two UH-1B helicopters equipped with the XM26 Armament Subsystem were deployed to help counter the 1972 Easter Invasion.[7] USAF Lieutenant James P. Fleming piloted a UH-1F on a 26 November 1968 mission that won him the Medal of Honor.

UH-1 troop transports were designated by Blue teams, hence the nickname for troops carried in by these Hueys as the Blues. The reconnaissance or observation teams were White teams. The attack ships were called Red teams. Over the duration of the conflict the tactics used by the military evolved and teams were mixed for more effective results. Purple teams with one or two Blue slicks dropping off the troops, while a Red attack team provided protection until the troops could defend themselves. Another highly effective team was the Pink Recon/Attack team, which offered the capability of carrying out assaults upon areas where the enemy was known to be present but could not be pinpointed.[4]

During the course of the War, the UH-1 went through several upgrades. The UH-1A, B, and C models (short fuselage, Bell 204) and the UH-1D and H models (stretched-fuselage, Bell 205) each had improved performance and load-carrying capabilities. The UH-1B and C performed the gunship and some of the transport duties until 1967, when the new AH-1 Cobra arrived on the scene. The newer Cobra, a purpose-built attack helicopter based on the UH-1 was faster, sleeker, harder to hit, and could carry more ordinance. The increasing intensity and sophistication of NVA anti-aircraft defenses made continued use of gunships based on the UH-1 impractical, and after Vietnam the Cobra was adopted as the Army's main attack helicopter. Devotees of the UH-1 in the gunship role cite its ability to act as an impromptu dustoff if the need arose, as well as the superior observational capabilities of the larger Huey cockpit, which allowed return fire from door gunners to the rear and sides of the aircraft.[4]

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An-225 Mriya

The Antonov-225 at Munich Airport

Type Strategic airlifter
Manufacturer Antonov
Maiden flight 21 December 1988
Status Operational
Primary user Antonov Airlines (1)
Produced 1988
Number built 2
Developed from Antonov An-124

The An-225 Mriya (Ukrainian: Антонов Ан-225 Мрія, NATO reporting name: Cossack) is a strategic airlift transport aircraft which was built by the Antonov Design Bureau, and is the largest flying airplane ever built by the most commonly accepted measure,[1] maximum gross takeoff weight. The design, built to transport the Buran orbiter, was an enlargement of the successful An-124 Ruslan. Mriya (Мрія) means "Dream" (Inspiration) in Ukrainian.

With a maximum gross weight of 640 tonnes (1,411,000 lb), the An-225 is the world's heaviest and largest aircraft. The Hughes H-4 Hercules, known to most as the "Spruce Goose", had a greater wingspan and a greater overall height, but was considerably shorter, and due to the materials used in its construction, also lighter. In addition, the Hercules only flew once and never climbed above 21.3 m (70 ft), making the An-225 the largest aircraft in the world to take off multiple times.[2] The An-225 is also larger than the Airbus A380 airliner, and considerably bigger than the Antonov An-124, Boeing 747 Large Cargo Freighter, and Lockheed C-5 Galaxy, the nearest equivalent heavy airlifters.

In November 2004, FAI placed the An-225 in the Guinness Book of Records for its 240 records.

The Antonov An-225 is commercially available for flying any over-sized payload due the unique size of its cargo deck. Currently there is only one aircraft operating but a second mothballed airframe is being reconditioned and is scheduled for completion around mid to late 2008.[3]

[edit] Development

Space shuttle Buran being carried by the An-225

Space shuttle Buran being carried by the An-225

The An-225 was designed for the Soviet space program as a replacement for the Myasishchev VM-T. Able to airlift the Energia rocket's boosters and the Buran space shuttle, its mission and objectives are almost identical to that of the Airbus Beluga and the United States' Shuttle Carrier Aircraft.[4]

The An-225 is an extension of Antonov's earlier An-124. To meet the needs of its new role, fuselage barrel extensions were added fore and aft of the wings, which received root extensions.[4] Two more Lotarev D-18 turbofan engines were added to the new wing roots, bringing the total to six, and an increased-capacity landing gear system with 32 wheels was designed. The An-124’s rear cargo door and ramp were removed to save weight, and the empennage was changed from a single vertical stabilizer to a twin tail with an oversized horizontal stabilizer. The twin tail was made necessary by the requirement to carry very large and heavy external loads, which would disturb the aerodynamics of a conventional tail. Unlike the An-124, the An-225 was not intended for tactical airlifting and is not designed for short-field operation.[4]

The An-225 first flew on December 21, 1988. The aircraft was on static display at the Paris Air Show in 1989. Two aircraft were ordered, but only one An-225 (tail number UR-82060[5]) is currently in service. It is commercially available for carrying ultra-heavy and oversize freight, up to 250,000 kg (550,000 lb) internally[4] or 200,000 kg (440,000 lb) on the upper fuselage. Cargo on the upper fuselage can be 70 m long.[6] A second An-225 was partially built during the late 1980s for use by the Soviet space program. Following the collapse of the Soviet Union in 1990 and the cancellation of the Buran space program, the lone operational An-225 was placed in storage. The six Lotarev engines were removed for use on An-124s, and the second An-225 airframe (nearing completion and awaiting engines) was also mothballed.

[edit] Operational service

In the late 1980s, efforts were begun by the Soviet government to generate revenue from its military assets. In 1989, a holding company was set up by the Antonov Design Bureau as a heavy airlift shipping corporation under the name "Antonov Airlines", based in Kiev, Ukraine and operating from London Luton Airport in partnership with Air Foyle HeavyLift.[6][7].

The company initiated operations with a fleet of four An-124-100s and three Antonov An-12s, but by the late 1990s a need for aircraft larger than the An-124 became apparent. In response, the original An-225 was re-engined, modified for heavy cargo transport, and placed back in service under the management of Antonov Airlines.

On May 23, 2001, the An-225 received its type certificate from the Interstate Aviation Committee Aviation Register (IAC AR).[8] The type's first flight in commercial service departed from Stuttgart, Germany on January 3, 2002, and flew to Thumrait, Oman with 216,000 prepared meals for American military personnel based in the region. This vast amount of ready meals was transported on some 375 pallets and weighed 187.5 tons.[9] Since then, the An-225 has become the major workhorse of the Antonov Airlines fleet, transporting objects once thought impossible to move by air, such as locomotives and 150-ton generators, and has become a valuable asset to international relief organizations for its ability to quickly transport huge quantities of emergency supplies during disaster relief operations.[10]

By 2000, it had become apparent that the demand for the An-225 had exceeded the airline's booking capacity, and in September 2006 the decision was made to complete the second An-225. Assembly is scheduled to complete in 2008.[11]

Beginning in June 2003, the An-225, along with An-124s, delivered over 800 tons of equipment to aid humanitarian efforts in Iraq.[12]

The An-225 has also been contracted by the Canadian and U.S. governments to transport military supplies to the Middle East in support of Coalition forces.[10]

The An-225 and Buran at Le Bourget Airport 1989

The An-225 and Buran at Le Bourget Airport 1989
An-225 main landing gear

An-225 main landing gear
The An-225 at Manchester Airport in 2006

The An-225 at Manchester Airport in 2006

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C-130 Hercules

USAF C-130E

Type STOL military transport aircraft
Manufacturer Lockheed
Maiden flight 23 August 1954
Introduction December 1956
Status In production
Primary users United States Air Force
United States Marine Corps
Royal Air Force
Canadian Forces
Produced 2,262 as of 2006[1]
Variants C-130J Super Hercules
AC-130 Spectre/Spooky
Lockheed DC-130
Lockheed EC-130
Lockheed HC-130
Lockheed LC-130
Lockheed MC-130
Lockheed WC-130

The Lockheed C-130 Hercules is an American four-engine turboprop military transport aircraft built by Lockheed and the main tactical airlifter for many military forces worldwide. Over 40 models and variants of the Hercules serve with more than 50 nations. In December 2006, the C-130 became the fourth aircraft—after the English Electric Canberra in May 2001, the B-52 Stratofortress in January 2005 and the Tupolev Tu-95 in January 2006 – to mark 50 years of continuous use with its original primary customer, in this case the United States Air Force. The C-130 remains in production as the updated C-130J Super Hercules.

Capable of short takeoffs and landings from unprepared runways, the C-130 was originally designed as a troop, medical evacuation and cargo transport aircraft. The versatile airframe has found uses in a variety of other roles, including as a gunship, and for airborne assault, search and rescue, scientific research support, weather reconnaissance, aerial refuelling and aerial firefighting. The Hercules family has the longest continuous production run of any military aircraft in history. During more than 50 years of service the family has participated in military, civilian and humanitarian aid operations.

[edit] Development

The two YC-130 prototypes; the blunt nose was replaced with radar on later production models.

The two YC-130 prototypes; the blunt nose was replaced with radar on later production models.

The Korean War, which began in June, 1950, showed that World War II-era transports—C-119 Flying Boxcars, C-47 Skytrains and C-46 Commandos—were inadequate for modern warfare. Thus, on February 2, 1951, the United States Air Force issued a General Operating Requirement (GOR) for a new transport to Boeing, Douglas, Fairchild, Lockheed, Martin, Chase Aircraft, North American Northrop, and Airlifts Inc. The new transport would have a capacity for 92 passengers, 72 combat troops or 64 paratroopers, a range of 1,100 nautical miles (2,000 km), takeoff capability from short and unprepared strips, and the ability to fly with one engine shut down.

Fairchild, North American, Martin and Northrop declined to participate. The remaining five companies tendered a total of ten designs: Lockheed two, Boeing one, Chase three, Douglas three, Airlifts Inc one. The contest was a close affair between the lighter of the two Lockheed (preliminary project designation L-206) proposals and a four-turboprop Douglas design. The Lockheed design team was led by Willis Hawkins starting with a 130 page proposal for the Lockheed L-206 and another two-turboprop and heavier one.[2] Hall Hibbard, Lockheed vice president and chief engineer, saw the proposal and directed it to Kelly Johnson, who remarked when he saw the proposal, "If you sign that letter, you will destroy the Lockheed Company."[clarify] Both Hibbard and Johnson signed the proposal and the company won the contract for the now-designated Model 82 on July 2, 1951.[3]

[edit] First flight

The first flight of the YC-130 prototype was made on August 23, 1954 from the Lockheed plant in Burbank, California. The aircraft, serial number 53-3397, was the second prototype but the first of the two to fly. The YC-130 was piloted by Stanley Beltz and Roy Wimmer on its 61-minute flight to Edwards Air Force Base; Jack Real and Dick Stanton served as flight engineers. Kelly Johnson flew chase in a P2V Neptune.[4]

[edit] Production

C-130 Hercules flight deck

C-130 Hercules flight deck

After the two prototypes were completed, production began in Marietta, Georgia, where more than 2,000 C-130s have been built.[1]

The initial production model, the C-130A, was powered by Allison T56-A-9 turboprops with three-blade propellers. Deliveries began in December 1956, continuing until the introduction of the C-130B model in 1959. Some A models were re-designated C-130D after being equipped with skis. The newer C-130B had ailerons with increased boost — 3,000 versus 2,050 lbf/in² (21 versus 14 MPa) — as well as uprated engines and four-bladed propellers that were standard until the "J" model's introduction.

[edit] C-130A Model

The first production C-130s were designated as A-models, with deliveries to the 463rd Troop Carrier Wing at Ardmore AFB, Oklahoma and the 314th Troop Carrier Wing at Sewart AFB, Tennessee. Six additional squadrons were assigned to the 322nd Air Division in Europe and the 315th Air Division in the Far East. Additional airplanes were modified for electronics intelligence work and assigned to Rhein-Main Air Base, Germany while modified RC-130As were assigned to the Military Air Transport Service (MATS) photo-mapping division. Airplanes equipped with giant skis were designated as C-130Ds, but were essentially A-models except for the conversion. As the C-130A became operational with Tactical Air Command (TAC), the airplane's lack of range became apparent and additional fuel capacity was added in the form of external pylon-mounted tanks at the end of the wings. The A-model continued in service through the Vietnam War, where the airplanes assigned to the four squadrons at Naha AB, Okinawa and one at Tachikawa AB, Japan performed yeoman's service, including operating highly classified special operations missions such as the BLIND BAT FAC/Flare mission and FACT SHEET leaflet mission over Laos and North Vietnam.

[edit] C-130B Model

The C-130B model was developed to complement the A-models that had previously been delivered,and incorporated new features, particularly increased fuel capacity in the form of auxiliary tanks built into the center wing section and an AC electrical system. Four-bladed Hartzell propellers replaced the Aero Product three-bladed propellers that distinguished the earlier A-models. B-models replaced A-models in the 314th and 463rd Troop Carrier Wings. During the Vietnam War four squadrons assigned to the 463rd Troop Carrier/Tactical Airlift Wing based at Clark and Mactan Air Fields in the Philippines were used primarily for tactical airlift operations in South Vietnam. In the spring of 1969 463rd crews commenced COMMANDO VAULT bombing missions dropping M-121 10,000 pound bombs to clear "instant LZs" for helicopters. As the Vietnam War wound down, the 463rd B-models and A-models of the 374th Tactical Airlift Wing were transferred back to the United States where most were assigned to Air Force Reserve and Air National Guard units. Another prominent role for the B-model was with the United States Marine Corps, where Hercules initially designated as GV-1s replaced C-119s. After Air Force C-130Ds proved the type's usefulness in Antarctica, the US Navy purchased a number of B-models equipped with skis that were designated as LC-130s.

[edit] C-130E model

The extended range C-130E model entered service in 1962 after it developed as an interim long-range transport for the Military Air Transport Service. Essentially a B-model, the new designation was the result of the installation of 5,150 liter (1,360 US gallon) fuel tanks under each wing. (center-section) wing-mounted auxiliary fuel tanks and more powerful Allison T-56-A-7A turboprops. The E model also featured structural improvements, avionics upgrades and a higher gross weight.

The KC-130 tankers, originally C-130Fs procured for the US Marine Corps (USMC) in 1958 (under the designation GV-1) are equipped with a removable 13,626 liter (3600 US gallon) stainless steel fuel tank carried inside the cargo compartment. The two wing-mounted hose and drogue aerial refueling pods each transfer up to 19 liters per second (equivalent to 300 US gallons per minute) to two aircraft simultaneously, allowing for rapid cycle times of multiple-receiver aircraft formations, (a typical tanker formation of four aircraft in less than 30 minutes). The US Navy's C-130G has increased structural strength allowing higher gross weight operation.

[edit] C-130H model

The C-130H model has updated Allison T56-A-15 turboprops, a redesigned outer wing, updated avionics and other minor improvements. Later H models had a new, fatigue-life-improved, center wing that was retro-fitted to many earlier H-models. The H model remains in widespread use with the US Air Force (USAF) and many foreign air forces. Initial deliveries began in 1964 (to the RNZAF), remaining in production until 1996. An improved C-130H was introduced in 1974.

From 1992 to 1996 the C-130H was described as a C-130H3 by the USAF. The 3 denoting the third variation in design for the H series. Improvements included a partial glass cockpit (ADI and HSI instruments), a more capable APN-241 color radar, night vision device compatible instrument lighting and an improved electrical system using Bus Switching Units to provide 'clean' power to the more sensitive upgraded components.

[edit] C-130K model

Royal Air Force C-130K (C.3)

Royal Air Force C-130K (C.3)

The equivalent model for export to the UK is the C-130K, known by the Royal Air Force (RAF) as the Hercules C.1. The C-130H-30 (Hercules C.3 in RAF service) is a stretched version of the original Hercules, achieved by inserting a 100-inch (2.54 m) plug aft of the cockpit and an 80-inch (2.03 m) plug at the rear of the fuselage. A single C-130K was purchased by the Met Office for use by its Meteorological Research Flight. This aircraft was heavily modified (with its most prominent feature being the long red and white striped atmospheric probe on the nose) to the extent that it was given the designation W.2, to differentiate it from the ordinary C.1. This aircraft, named Snoopy, was withdrawn in 2001. The C-130K is used by the RAF Falcons for parachute drops. Three C-130K (Hercules C Mk.1P) where upgraded and sold to the Austrian Air Force in 2002.[5]

[edit] Later C-130 models & variants

USAF HC-130P refuels an HH-60G Pavehawk helicopter

USAF HC-130P refuels an HH-60G Pavehawk helicopter

The HC-130N & P are long range search and rescue variants used by the USAF, to include the Air Force Reserve Command and the Air National Guard. Equipped for deep deployment of pararescue men (PJs), survival equipment, and aerial refueling of combat rescue helicopters, HC-130s are usually the on-scene command aircraft for combat SAR missions. Early versions were equipped with the Fulton surface-to-air recovery system, designed to pull a person off the ground using a wire strung from a helium balloon. The John Wayne movie The Green Berets features its use. The Fulton system was later removed when aerial refueling of helicopters proved safer and more versatile. The movie The Perfect Storm depicts a real life SAR mission involving aerial refueling of a New York Air National Guard HH-60G by an Air National Guard HC-130P.

The C-130R and C-130T are US Navy and USMC models, both equipped with underwing external fuel tanks. The C-130T is similar, but has numerous avionics improvements over the R model and is fully night-vision system compatible. In both models, USMC aircraft are equipped with Allison T-56-A-16 engines. The USMC versions are designated KC-130R or KC-130T when equipped with underwing refueling pods and pylons.

The RC-130 is a reconnaissance version. A single example is used by the Islamic Republic of Iran Air Force, the aircraft having originally been sold to the former Imperial Iranian Air Force.

[edit] Civilian models

L-382 of Tepper Aviation at Mojave Spaceport

L-382 of Tepper Aviation at Mojave Spaceport

The Lockheed L-100 (L-382) is a civilian variant, equivalent to a C-130E model without pylon tanks or military equipment. The L-100 also has 2 stretched versions: the L-100-20 has an 8.3 ft (2.5 m) fuselage stretch and the L-100-30 is stretched by 15 ft (4.6 m). The L-100 has not seen widespread use in the civilian market.

[edit] Next generation

In the 1970s Lockheed proposed a C-130 variant with turbofan engines rather than turboprops, but the US Air Force preferred the takeoff performance of the existing aircraft. In the 1980s the C-130 was intended to be replaced by the Advanced Medium STOL Transport project. The project was canceled and the C-130 has remained in production.

[edit] C-130J model

Main article: C-130J Super Hercules

The C-130J Super Hercules is the newest version of the Hercules and the only model still produced. Externally similar to the classic Hercules in general appearance, the J model has new turboprops, digital avionics, and other new systems.

[edit] Operational history

A Hercules deploying flares, sometimes referred as to 'Angel Flares' due to the characteristic shape

A Hercules deploying flares, sometimes referred as to 'Angel Flares' due to the characteristic shape
C-130 Hercules performing takeoffs and landings aboard the aircraft carrier USS Forrestal (CVA-59) in 1963. This aircraft is currently on display at the National Museum of Naval Aviation.

C-130 Hercules performing takeoffs and landings aboard the aircraft carrier USS Forrestal (CVA-59) in 1963. This aircraft is currently on display at the National Museum of Naval Aviation.

The Hercules holds the record for the largest and heaviest aircraft to land on an aircraft carrier. In October and November 1963, a USMC KC-130F (BuNo 149798), bailed to the US Naval Air Test Center, made 21 unarrested landings and take-offs on the USS Forrestal at a number of different weights. The pilot, LT (later RADM) James Flatley III, USN, was awarded the Distinguished Flying Cross for his participation. The tests were highly successful, but the idea was considered too risky for routine "Carrier Onboard Delivery" (COD) operations. Instead, the C-2 Greyhound was developed as a dedicated COD aircraft. (The Hercules used in the test, most recently in service with Marine Aerial Refueler Squadron 352 (VMGR-352) until 2005, is now part of the collection of the National Museum of Naval Aviation at NAS Pensacola, Florida.)

While the C-130 is involved in cargo and resupply operations daily, it has been a part of some notable offensive operations:

The MC-130 Combat Talon variant carries and deploys what are currently the world's largest conventional bombs, the BLU-82 "Daisy Cutter" and GBU-43/B Massive Ordnance Air Blast bomb, also known as the MOAB. Daisy Cutters were used during the Vietnam War to clear landing zones for helicopters and to eliminate minefields and have recently even been proposed for anti-personnel use. The weight and size of the weapons make it impossible or impractical to load them on conventional bombers. The GBU-43/B MOAB is a successor to the BLU-82 and can perform the same function, as well as perform strike functions against hardened targets in a low air threat environment.

In the Indo-Pakistani War of 1965, the Pakistan Air Force modified/improvised several aircraft for use as heavy bombers, and attacks were made on enemy bridges and troop concentrations with some notable successes. No aircraft were lost in the operations, though one was slightly damaged.[6]

It was also used in the 1976 Entebbe raid in which Israeli commando forces carried a surprise assault to rescue 103 passengers of an airliner hijacked by Palestinian and German terrorists at Entebbe Airport, Uganda. The rescue force — 200 soldiers, jeeps, and a black Mercedes-Benz (intended to resemble Ugandan Dictator Idi Amin's vehicle of state) — was flown 4,000 kilometres (2,160 nmi) from Israel to Entebbe by five Israeli Air Force (IAF) Hercules aircraft without mid-air refueling (on the way back, the planes refueled in Nairobi, Kenya).

During the Falklands War of 1982, Argentine Air Force C-130s undertook highly dangerous, daily re-supply flights to the Argentine garrison on the Falkland Islands (Malvinas). Only one was lost during the war. Argentina also operated two KC-130s refuellers during the war, and these refueled the Skyhawk attack planes which sank the British frigate HMS Antelope. The British also used their C-130s to support their logistical operations.

During the Gulf War of 1991, the C-130 Hercules was used operationally by the US Air Force, US Navy and US Marine Corps, and the air forces of Australia, New Zealand, Saudi Arabia, South Korea and the UK.

During the invasion of Afghanistan and in support of the International Security Assistance Force, the C-130 Hercules was used operationally by Australia, Belgium, Canada, France, Italy, the Netherlands, New Zealand, Norway, South Korea, Spain, the UK and the United States.

During the 2003 invasion of Iraq, the C-130 Hercules was used operationally by Australia, the UK and the United States. After the initial invasion, C-130 operators as part of the Multinational force in Iraq used their C-130s to support their forces in Iraq.

USMC C-130T Fat Albert

USMC C-130T Fat Albert

A prominent C-130T aircraft is Fat Albert, the support aircraft for the US Navy Blue Angels flight demonstration team. Although Fat Albert supports a Navy squadron, it is operated by the US Marine Corps (USMC) and its crew consists solely of USMC personnel. At some air shows featuring the team, Fat Albert takes part, performing flyovers and sometimes demonstrating its jet-assisted takeoff (JATO) capabilities.

[edit] Civilian uses

In the late 1980s, 22 retired USAF C-130As were removed from storage at Davis-Monthan Air Force Base and transferred to the U.S. Forest Service who then sold them to six private companies to be converted into airtankers for use in fighting wildfires (see U.S. Forest Service airtanker scandal). After two of these aircraft crashed due to wing separation in flight as a result of fatigue stress cracking, the entire fleet of C-130A airtankers was permanently grounded in 2004. (See 2002 airtanker crashes.)

An Australian defence force Hercules plane was hired to carry a 530 lb (240 kg) patient because there were no ambulances or planes big enough to transport her. Even though the woman was deemed well enough to travel by road from Mt Isa to Townsville, the Queensland Ambulance Service had no vehicles to carry her.[7]

[edit] Variants

[edit] Military variants

Significant military variants of the C-130 include:

[edit] Civilian variants

  • L-100 - Civilian version, equivalent to the C-130E
  • L-100-20 - Civilian version, stretched 8.3 feet (2.5 m)
  • L-100-30 - Civilian version, stretched 15 feet (5 m)

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Diagram of a gas turbine jet engine

Diagram of a gas turbine jet engine

Turbojets are the oldest kind of general purpose jet engines. Two engineers, Frank Whittle in the United Kingdom and Hans von Ohain in Germany, developed the concept independently during the late 1930s, although credit for the first turbojet is given to Whittle.

Turbojets consist of an air inlet, an air compressor, a combustion chamber, a gas turbine (that drives the air compressor) and a nozzle. The air is compressed into the chamber, heated and expanded by the fuel combustion and then allowed to expand out through the turbine into the nozzle where it is accelerated to high speed to provide propulsion.

Turbojets are quite inefficient (if flown below about Mach 2) and very noisy. Most modern aircraft use turbofans instead for economic reasons. Turbojets are still very common in medium range cruise missiles, due to their high speed, low frontal area and relative simplicity.

[edit] History

Heinkel He 178, the world's first aircraft to fly purely on turbojet power

Heinkel He 178, the world's first aircraft to fly purely on turbojet power

On 27 August 1939 the Heinkel He 178 became the world's first aircraft to fly under turbojet power, thus becoming the first practical jet plane. The first two operational turbojet aircraft, the Messerschmitt Me 262 and the Gloster Meteor entered service towards the end of World War II in 1944.

A turbojet engine is used primarily to propel aircraft. Air is drawn into the rotating compressor via the intake and is compressed to a higher pressure before entering the combustion chamber. Fuel is mixed with the compressed air and ignited by a flame in the eddy of a flame holder. This combustion process significantly raises the temperature of the gas. Hot combustion products leaving the combustor expand through the turbine where power is extracted to drive the compressor. Although this expansion process reduces the turbine exit gas temperature and pressure, both parameters are usually still well above ambient conditions. The gas stream exiting the turbine expands to ambient pressure via the propelling nozzle, producing a high velocity jet in the exhaust plume. If the momentum of the exhaust stream exceeds the momentum of the intake stream, the impulse is positive, thus, there is a net forward thrust upon the airframe.

Early generation jet engines were pure turbojets with either an axial or centrifugal compressor. They were used because they were able to achieve very high altitudes and speeds, much higher than propeller engines, because of a better compression ratio. However they were not very fuel efficient. Modern jet engines are mainly turbofans, where a proportion of the air entering the intake bypasses the combustor; this proportion depends on the engine's bypass ratio. This makes turbofans much more efficient than turbojets.

Although ramjet engines are simpler in design as they have virtually no moving parts, they are incapable of operating at low flight speeds.

[edit] Air intake

An animation of an axial compressor. The darker colored blades are the stators.

An animation of an axial compressor. The darker colored blades are the stators.
Schematic diagram showing the operation of a centrifugal flow turbojet engine. The compressor is driven via the turbine stage and throws the air outwards, requiring it to be redirected parallel to the axis of thrust.

Schematic diagram showing the operation of a centrifugal flow turbojet engine. The compressor is driven via the turbine stage and throws the air outwards, requiring it to be redirected parallel to the axis of thrust.
Schematic diagram showing the operation of an axial flow turbojet engine. Here, the compressor is again driven by the turbine, but the air flow remains parallel to the axis of thrust.

Schematic diagram showing the operation of an axial flow turbojet engine. Here, the compressor is again driven by the turbine, but the air flow remains parallel to the axis of thrust.

Preceding the compressor is the air intake (or inlet). It is designed to be as efficient as possible at recovering the ram pressure of the air streamtube approaching the intake. The air leaving the intake then enters the compressor. The stators (stationary blades) guide the airflow of the compressed gases.

[edit] Compressor

The compressor is driven by the turbine. The compressor rotates at very high speed, adding energy to the airflow and at the same time squeezing (compressing) it into a smaller space. Compressing the air increases its pressure and temperature.

In most turbojet-powered aircraft, bleed air is extracted from the compressor section at various stages to perform a variety of jobs including air conditioning/pressurization, engine inlet anti-icing and turbine cooling. Bleeding air off decreases the overall efficiency of the engine, but the usefulness of the compressed air outweighs the loss in efficiency.

Several types of compressor are used in turbojets and gas turbines in general: axial, centrifugal, axial-centrifugal, double-centrifugal, etc.

Early turbojet compressors had overall pressure ratios as low as 5:1 (as do a lot of simple auxiliary power units and small propulsion turbojets today). Aerodynamic improvements, plus splitting the compression system into two separate units and/or incorporating variable compressor geometry, enabled later turbojets to have overall pressure ratios of 15:1 or more. For comparison, modern civil turbofan engines have overall pressure ratios as high as 44:1 or more.

After leaving the compressor section, the compressed air enters the combustion chamber.

[edit] Combustion chamber

The burning process in the combustor is significantly different from that in a piston engine. In a piston engine the burning gases are confined to a small volume and, as the fuel burns, the pressure increases dramatically. In a turbojet the air and fuel mixture passes unconfined through the combustion chamber. As the mixture burns its temperature increases dramatically, but the pressure actually decreases a few percent.

The fuel-air mixture must be brought almost to a stop so that a stable flame can be maintained.
This occurs just after the start of the combustion chamber. The aft part of this flame front is allowed to progress rearward. This ensures that all of the fuel is burned, as the flame becomes hotter when it leans out, and because of the shape of the combustion chamber the flow is accelerated rearwards. Some pressure drop is required, as it is the reason why the expanding gases travel out the rear of the engine rather than out the front. Less than 25% of the air is involved in combustion, in some engines as little as 12%, the rest acting as a reservoir to absorb the heating effects of the burning fuel.

Another difference between piston engines and jet engines is that the peak flame temperature in a piston engine is experienced only momentarily in a small portion of the full cycle. The combustor in a jet engine is exposed to the peak flame temperature continuously and operates at a pressure high enough that a stoichiometric fuel-air ratio would melt the can and everything downstream. Instead, jet engines run a very lean mixture, so lean that it would not normally support combustion. A central core of the flow (primary airflow) is mixed with enough fuel to burn readily. The cans are carefully shaped to maintain a layer of fresh unburned air between the metal surfaces and the central core. This unburned air (secondary airflow) mixes into the burned gases to bring the temperature down to something a turbine can tolerate.

[edit] Turbine

Hot gases leaving the combustor are allowed to expand through the turbine. In the first stage the turbine is largely an impulse turbine (similar to a pelton wheel) and rotates because of the impact of the hot gas stream. Later stages are convergent ducts that accelerate the gas rearward and gain energy from that process. Pressure drops, and energy is transferred into the shaft. The turbine's rotational energy is used primarily to drive the compressor. Some shaft power is extracted to drive accessories, like fuel, oil, and hydraulic pumps. Because of its significantly higher entry temperature, the turbine pressure ratio is much lower than that of the compressor. In a turbojet almost two thirds of all the power generated by burning fuel is used by the compressor to compress the air for the engine.

[edit] Nozzle

After the turbine, the gases are allowed to expand through the exhaust nozzle to atmospheric pressure, producing a high velocity jet in the exhaust plume. In a convergent nozzle, the ducting narrows progressively to a throat. The nozzle pressure ratio on a turbojet is usually high enough for the expanding gases to reach Mach 1.0 and choke the throat. Normally, the flow will go supersonic in the exhaust plume outside the engine.

If, however, a convergent-divergent "de Laval" nozzle is fitted, the divergent (increasing flow area) section allows the gases to reach supersonic velocity within the nozzle itself. This is slightly more efficient on thrust than using a convergent nozzle. There is, however, the added weight and complexity, since the con-di nozzle must be fully variable to cope basically with engine throttling.

[edit] Net thrust

An equation for calculating the approximate net thrust of a turbojet is given by:

F_n = \dot{m} (V_{jfe} - V_a)

where:

\dot{m} is the intake mass flow rate
Vjfe is the fully-expanded jet velocity (in the exhaust plume)

\dot{m} V_{jfe} represents the nozzle gross thrust

\dot{m} V_a represents the ram drag of the intake.

Obviously, the jet velocity must exceed that of the flight velocity if there is to be a net forward thrust on the airframe.

[edit] Thrust to power ratio

A simple turbojet engine will produce thrust of approximately: 2.5 pounds force per horsepower (15 mN/W).

[edit] Afterburner

An afterburner or "reheat jetpipe" is a device added to the rear of the jet engine. It provides a means of spraying fuel directly into the hot exhaust, where it ignites and boosts available thrust significantly; a drawback is its very high fuel consumption rate. Afterburners are used mostly on military aircraft, but the two supersonic civilian transports, the Concorde and the TU-144, also utilized afterburners, as does Scaled Composites White Knight, a carrier aircraft for the experimental SpaceShipOne suborbital spacecraft.

[edit] Thrust reverser

A thrust reverser is, essentially, a pair of clamshell doors mounted at the rear of the engine which, when deployed, divert thrust normal to the jet engine flow to help slow an aircraft upon landing. They are often used in conjunction with spoilers. The accidental deployment of a thrust reverser during flight is a dangerous event that can lead to loss of control and destruction of the aircraft. Thrust reversers are more convenient than drogue parachutes.

[edit] Cycle improvements

Thermodynamics of a Jet Engine is modelled approximately by a Brayton Cycle.

Increasing the overall pressure ratio of the compression system raises the combustor entry temperature. Therefore, at a fixed fuel flow and airflow, there is an increase in turbine inlet temperature. Although the higher temperature rise across the compression system, implies a larger temperature drop over the turbine system, the nozzle temperature is unaffected, because the same amount of heat is being added to the system. There is, however, a rise in nozzle pressure, because overall pressure ratio increases faster than the turbine expansion ratio. Consequently, net thrust increases, while specific fuel consumption (fuel flow/net thrust) decreases.

Thus turbojets can be made more fuel efficient by raising overall pressure ratio and turbine inlet temperature in union. However, better turbine materials and/or improved vane/blade cooling are required to cope with increases in both turbine inlet temperature and compressor delivery temperature. Increasing the latter requires better compressor materials.

By Increasing the useful work to system , by minimizing the heat losses by conduction etc and minimizing the inlet temperature ratio up to a certain level will increase the themal efficiency of the turbo jet engine.

[edit] Early designs

Early German engines had serious problems controlling the turbine inlet temperature. A lack of suitable alloys due to war shortages meant the turbine rotor and stator blades would sometimes disintegrate on first operation and never lasted long. Their early engines averaged 10-25 hours of operation before failing—often with chunks of metal flying out the back of the engine when the turbine overheated. British engines tended to fare better, running for 150 hours between overhauls. A few of the original fighters still exist with their original engines, but many have been re-engined with more modern engines with greater fuel efficiency and a longer TBO (such as the reproduction Me-262 powered by General Electric J85s).

The United States had the best materials because of their reliance on turbo/supercharging in high altitude bombers of World War II. For a time some US jet engines included the ability to inject water into the engine to cool the compressed flow before combustion, usually during takeoff. The water would tend to prevent complete combustion and as a result the engine ran cooler again, but the planes would take off leaving a huge plume of smoke.

Today these problems are much better handled, but temperature still limits turbojet airspeeds in supersonic flight. At the very highest speeds, the compression of the intake air raises the temperatures throughout the engine to the point that the turbine blades would melt, forcing a reduction in fuel flow to lower temperatures, but giving a reduced thrust and thus limiting the top speed. Ramjets and scramjets do not have turbine blades; therefore they are able to fly faster.

At lower speeds, better materials have increased the critical temperature, and automatic fuel management controls have made it nearly impossible to overheat the engine.

歡迎來到Bewise Inc.的世界,首先恭喜您來到這接受新的資訊讓產業更有競爭力,我們是提供專業刀具製造商,應對客戶高品質的刀具需求,我們可以協助客戶滿足您對產業的不同要求,我們有能力達到非常卓越的客戶需求品質,這是現有相關技術無法比擬的,我們成功的滿足了各行各業的要求,包括:精密HSS DIN切削刀具協助客戶設計刀具流程DIN or JIS 鎢鋼切削刀具設計NAS986 NAS965 NAS897 NAS937orNAS907 航太切削刀具,NAS航太刀具設計超高硬度的切削刀具BW捨棄式鑽石V卡刀BW捨棄式金屬圓鋸片木工捨棄式金屬圓鋸片PCD木工圓鋸片醫療配件刀具設計汽車業刀具設計電子產業鑽石刀具全鎢鋼V卡刀-電路版專用全鎢鋼鋸片焊刃式側銑刀焊刃式千鳥側銑刀焊刃式T型銑刀焊刃式千鳥T型銑刀焊刃式螺旋機械鉸刀全鎢鋼斜邊刀電路版專用鎢鋼焊刃式高速鉸刀超微粒鎢鋼機械鉸刀超微粒鎢鋼定點鑽焊刃式帶柄角度銑刀焊刃式螺旋立銑刀焊刃式帶柄倒角銑刀焊刃式角度銑刀焊刃式筒型平面銑刀木工產業鑽石刀具等等。我們的產品涵蓋了從民生刀具到工業級的刀具設計;從微細刀具到大型刀具;從小型生產到大型量產;全自動整合;我們的技術可提供您連續生產的效能,我們整體的服務及卓越的技術,恭迎您親自體驗!!

BW Bewise Inc. Willy Chen willy@tool-tool.com bw@tool-tool.com www.tool-tool.com skype:willy_chen_bw mobile:0937-618-190 Head &Administration Office No.13,Shiang Shang 2nd St., West Chiu Taichung,Taiwan 40356 http://www.tool-tool..com / FAX:+886 4 2471 4839 N.Branch 5F,No.460,Fu Shin North Rd.,Taipei,Taiwan S.Branch No.24,Sec.1,Chia Pu East Rd.,Taipao City,Chiayi Hsien,Taiwan

Welcome to BW tool world! We are an experienced tool maker specialized in cutting tools. We focus on what you need and endeavor to research the best cutter to satisfy users demand. Our customers involve wide range of industries, like mold & die, aerospace, electronic, machinery, etc. We are professional expert in cutting field. We would like to solve every problem from you. Please feel free to contact us, its our pleasure to serve for you. BW product including: cutting toolaerospace tool .HSS DIN Cutting toolCarbide end millsCarbide cutting toolNAS Cutting toolNAS986 NAS965 NAS897 NAS937orNAS907 Cutting Tools,Carbide end milldisc milling cutter,Aerospace cutting toolhss drillФрезерыCarbide drillHigh speed steelMilling cutterCVDD(Chemical Vapor Deposition Diamond )’PCBN (Polycrystalline Cubic Boron Nitride) Core drillTapered end millsCVD Diamond Tools Inserts’PCD Edge-Beveling Cutter(Golden FingerEdge modifying knifeSolid carbide saw blade-V typeV-type locking-special use for PC boardMetal Slitting SawaCarbide Side milling CuttersCarbide Side Milling Cutters With Staggered TeethCarbide T-Slot Milling CuttersCarbide T-Slot Milling Cutters With Staggered TeethCarbide Machine ReamersHigh speed reamer-standard typeHigh speed reamer-long type’’PCD V-Cutter%2

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Bewise Inc. www.tool-tool.com Reference source from the internet.

同一材質の圧入荷重

入力項目 (数値は半角入力で)
締め代(半径)(δ):mm
軸側内径(D1):mm
軸側外径(D2):mm
穴側外径(D3):mm
嵌合幅(B):mm
摩擦係数(μ):
材質: ヤング率(E):MPa
計算結果
圧入荷重(F):N
せん断応力(軸):MPa
せん断応力(穴):MPa
http://www.hk.sun-ip.or.jp/ynaoki/atunyudouitu.htm

同一材質の圧入荷重

入力項目 (数値は半角入力で)
締め代(半径)(δ): mm
軸側内径(D1): mm
軸側外径(D2): mm
穴側外径(D3): mm
嵌合幅(B): mm
摩擦係数(μ):
材質: ヤング率(E): MPa
計算結果
圧入荷重(F): N
せん断応力(軸): MPa
せん断応力(穴): MPa
http://www.hajimeteno.ne.jp/engineer/calclib/press1-1.html

異種材質の圧入荷重

入力項目 (数値は半角入力で)
締め代(半径)(δ): mm
軸側内径(D1): mm
軸側外径(D2): mm
穴側外径(D3): mm
嵌合幅(B): mm
摩擦係数(μ):
材質(軸): ヤング率(E): MPa ポアソン比:
材質(穴): ヤング率(E): MPa ポアソン比:
計算結果
圧入荷重(F): N
せん断応力(軸): MPa
せん断応力(穴): MPa
http://www.hajimeteno.ne.jp/engineer/calclib/press2-1.html

歡迎來到Bewise Inc.的世界,首先恭喜您來到這接受新的資訊讓產業更有競爭力,我們是提供專業刀具製造商,應對客戶高品質的刀具需求,我們可以協助客戶滿足您對產業的不同要求,我們有能力達到非常卓越的客戶需求品質,這是現有相關技術無法比擬的,我們成功的滿足了各行各業的要求,包括:精密HSS DIN切削刀具協助客戶設計刀具流程DIN or JIS 鎢鋼切削刀具設計NAS986 NAS965 NAS897 NAS937orNAS907 航太切削刀具,NAS航太刀具設計超高硬度的切削刀具BW捨棄式鑽石V卡刀BW捨棄式金屬圓鋸片木工捨棄式金屬圓鋸片PCD木工圓鋸片醫療配件刀具設計汽車業刀具設計電子產業鑽石刀具全鎢鋼V卡刀-電路版專用全鎢鋼鋸片焊刃式側銑刀焊刃式千鳥側銑刀焊刃式T型銑刀焊刃式千鳥T型銑刀焊刃式螺旋機械鉸刀全鎢鋼斜邊刀電路版專用鎢鋼焊刃式高速鉸刀超微粒鎢鋼機械鉸刀超微粒鎢鋼定點鑽焊刃式帶柄角度銑刀焊刃式螺旋立銑刀焊刃式帶柄倒角銑刀焊刃式角度銑刀焊刃式筒型平面銑刀木工產業鑽石刀具等等。我們的產品涵蓋了從民生刀具到工業級的刀具設計;從微細刀具到大型刀具;從小型生產到大型量產;全自動整合;我們的技術可提供您連續生產的效能,我們整體的服務及卓越的技術,恭迎您親自體驗!!

BW Bewise Inc. Willy Chen willy@tool-tool.com bw@tool-tool.com www.tool-tool.com skype:willy_chen_bw mobile:0937-618-190 Head &Administration Office No.13,Shiang Shang 2nd St., West Chiu Taichung,Taiwan 40356 http://www.tool-tool..com / FAX:+886 4 2471 4839 N.Branch 5F,No.460,Fu Shin North Rd.,Taipei,Taiwan S.Branch No.24,Sec.1,Chia Pu East Rd.,Taipao City,Chiayi Hsien,Taiwan

Welcome to BW tool world! We are an experienced tool maker specialized in cutting tools. We focus on what you need and endeavor to research the best cutter to satisfy users demand. Our customers involve wide range of industries, like mold & die, aerospace, electronic, machinery, etc. We are professional expert in cutting field. We would like to solve every problem from you. Please feel free to contact us, its our pleasure to serve for you. BW product including: cutting toolaerospace tool .HSS DIN Cutting toolCarbide end millsCarbide cutting toolNAS Cutting toolNAS986 NAS965 NAS897 NAS937orNAS907 Cutting Tools,Carbide end milldisc milling cutter,Aerospace cutting toolhss drillФрезерыCarbide drillHigh speed steelMilling cutterCVDD(Chemical Vapor Deposition Diamond )’PCBN (Polycrystalline Cubic Boron Nitride) Core drillTapered end millsCVD Diamond Tools Inserts’PCD Edge-Beveling Cutter(Golden FingerEdge modifying knifeSolid carbide saw blade-V typeV-type locking-special use for PC boardMetal Slitting SawaCarbide Side milling CuttersCarbide Side Milling Cutters With Staggered TeethCarbide T-Slot Milling CuttersCarbide T-Slot Milling Cutters With Staggered TeethCarbide Machine ReamersHigh speed reamer-standard typeHigh speed reamer-long type’’PCD V-CutterPCD Wood toolsPCD Cutting toolsPCD Circular Saw BladePVDD End Millsdiamond tool V-type locking-special use for PC board Single Crystal Diamond Metric end millsMiniature end millsСпециальные режущие инструменты Пустотелое сверло Pilot reamerFraisesFresas con mango PCD (Polycrystalline diamond) ‘FreseElectronics cutterStep drillMetal cutting sawDouble margin drillGun barrelAngle milling cutterCarbide burrsCarbide tipped cutterChamfering toolIC card engraving cutterSide cutterNAS toolDIN or JIS toolSpecial toolMetal slitting sawsShell end millsSide and face milling cuttersSide chip clearance sawsLong end millsStub roughing end millsDovetail milling cuttersCarbide slot drillsCarbide torus cuttersAngel carbide end millsCarbide torus cuttersCarbide ball-nosed slot drillsMould cutterTool manufacturer.

Bewise Inc. www.tool-tool.com

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BW специализируется в научных исследованиях и разработках, и снабжаем самым высокотехнологичным карбидовым материалом для поставки режущих / фрезеровочных инструментов для почвы, воздушного пространства и электронной индустрии. В нашу основную продукцию входит твердый карбид / быстрорежущая сталь, а также двигатели, микроэлектрические дрели, IC картонорезальные машины, фрезы для гравирования, режущие пилы, фрезеры-расширители, фрезеры-расширители с резцом, дрели, резаки форм для шлицевого вала / звездочки роликовой цепи, и специальные нано инструменты. Пожалуйста, посетите сайт www.tool-tool.com для получения большей информации.

BW is specialized in R&D and sourcing the most advanced carbide material with high-tech coating to supply cutting / milling tool for mould & die, aero space and electronic industry. Our main products include solid carbide / HSS end mills, micro electronic drill, IC card cutter, engraving cutter, shell end mills, cutting saw, reamer, thread reamer, leading drill, involute gear cutter for spur wheel, rack and worm milling cutter, thread milling cutter, form cutters for spline shaft/roller chain sprocket, and special tool, with nano grade. Please visit our web www.tool-tool.com for more info.

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