EA200801835A1 - Обойма винта вертолёта и способ её изготовления - Google Patents

Обойма винта вертолёта и способ её изготовления

Info

Publication number
EA200801835A1
EA200801835A1 EA200801835A EA200801835A EA200801835A1 EA 200801835 A1 EA200801835 A1 EA 200801835A1 EA 200801835 A EA200801835 A EA 200801835A EA 200801835 A EA200801835 A EA 200801835A EA 200801835 A1 EA200801835 A1 EA 200801835A1
Authority
EA
Eurasian Patent Office
Prior art keywords
attachment part
rack
inner edge
thickness
helicopter
Prior art date
Application number
EA200801835A
Other languages
English (en)
Inventor
Брайан К. Баскин
Original Assignee
Белл Хеликоптер Текстрон, Инк.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Белл Хеликоптер Текстрон, Инк. filed Critical Белл Хеликоптер Текстрон, Инк.
Publication of EA200801835A1 publication Critical patent/EA200801835A1/ru

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/33—Rotors having flexing arms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Braking Arrangements (AREA)

Abstract

Обойма винта включает часть для крепления лопасти, часть для крепления стойки и промежуточную часть, проходящую между частью для крепления лопасти и частью для крепления стойки. Промежуточная часть, часть для крепления лопасти и часть для крепления стойки ограничивают необязательную внутреннюю кромку, так что внутренняя кромка, если она имеется, ограничивает отверстие. Обойма винта, кроме того, содержит периферийную внешнюю кромку, проходящую вокруг части для крепления лопасти, промежуточной части и части для крепления стойки. По меньшей мере либо внешняя кромка, либо внутренняя кромка, если она имеется, содержит часть с уменьшенной толщиной, толщина которой меньше толщины прилегающей части обоймы винта.
EA200801835A 2006-02-24 2006-02-24 Обойма винта вертолёта и способ её изготовления EA200801835A1 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2006/006628 WO2007106064A2 (en) 2006-02-24 2006-02-24 Helicopter rotor yoke and method of making same

Publications (1)

Publication Number Publication Date
EA200801835A1 true EA200801835A1 (ru) 2009-02-27

Family

ID=38509906

Family Applications (1)

Application Number Title Priority Date Filing Date
EA200801835A EA200801835A1 (ru) 2006-02-24 2006-02-24 Обойма винта вертолёта и способ её изготовления

Country Status (11)

Country Link
US (1) US8147198B2 (ru)
EP (1) EP1986913B1 (ru)
JP (1) JP2009527417A (ru)
CN (1) CN101573269B (ru)
AU (1) AU2006340075A1 (ru)
BR (1) BRPI0621310A2 (ru)
CA (1) CA2637461C (ru)
DE (1) DE06844078T1 (ru)
EA (1) EA200801835A1 (ru)
MX (1) MX2008010891A (ru)
WO (1) WO2007106064A2 (ru)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101573269B (zh) * 2006-02-24 2013-03-13 贝尔直升机泰克斯特龙公司 直升机旋翼轭架及其制造方法
US8419375B2 (en) * 2008-01-31 2013-04-16 Textron Innovations Inc. Method of making a rotor yoke and rotor yoke thereof
JP5113734B2 (ja) * 2008-12-19 2013-01-09 川崎重工業株式会社 フレックスビームの断面決定方法およびフレックスビーム
CN101797851B (zh) * 2010-03-16 2011-08-03 天津博苑高新材料有限公司 激光打印机专用证卡片材及其制备方法
US9169010B2 (en) 2012-02-24 2015-10-27 Bell Helicopter Textron Inc. Offset stacked yoke hub for tiltrotor aircraft
US10336445B2 (en) * 2013-03-12 2019-07-02 Bell Helicopter Textron Inc. High flapping yoke hub assembly using a cylindrical elastomeric attachment to avoid holes
US9505490B2 (en) 2013-03-13 2016-11-29 Bell Helicopter Textron Inc. Composite rotor system using two race track style cantilevered yokes
US9505489B2 (en) 2013-03-13 2016-11-29 Bell Helicopter Textron Inc. Flexing clevis arrangement bolted joint attachment for flexible rotor hub with high offset and high flapping
US9714086B2 (en) 2013-03-13 2017-07-25 Bell Helicopter Textron Inc. Fiber orientation to allow for automated ply placement with composite rotor yokes
FR3031497B1 (fr) 2015-01-08 2017-01-06 Airbus Helicopters Rotor de giravion comportant un moyeu en materiaux composites issus de tissus de fibres de carbone poudrees d'une resine thermoplastique
US10513325B2 (en) 2016-02-08 2019-12-24 Bell Helicopter Textron Inc. Joint member for a composite wing structure
US10836121B2 (en) 2016-02-08 2020-11-17 Bell Helicopter Textron Inc. Methods of manufacture of a composite wing structure
US10589837B2 (en) 2016-02-08 2020-03-17 Bell Helicopter Textron Inc. Spar for a composite wing structure
US11020910B2 (en) * 2016-05-13 2021-06-01 Bell Helicopter Textron Inc. System and method of constructing composite structures without tooling dams
US11040771B2 (en) * 2018-05-08 2021-06-22 Avx Aircraft Company Rotor hub
CN113014013B (zh) * 2019-12-20 2023-06-09 新疆金风科技股份有限公司 转子支架、转子、电机及风力发电机组
CN112123617B (zh) * 2020-07-27 2022-02-25 青岛科技大学 一种啮合剪切式变间隙六棱转子

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4293276A (en) * 1978-10-27 1981-10-06 Textron Inc. Laminated composite rotor yoke
US4568245A (en) * 1983-03-22 1986-02-04 United Technologies Corporation Composite helicopter rotor hub
US4585393A (en) * 1983-03-22 1986-04-29 United Technologies Corporation Fiber reinforced/epoxy matrix composite helicopter rotor yoke
US5211538A (en) * 1991-11-27 1993-05-18 Bell Helicopter Textron Inc. Method for folding helicopter main rotor blades
US5358381A (en) * 1993-03-19 1994-10-25 Bell Helicopter Textron Inc. Yoke for helicopter rotor systems
US5690474A (en) 1996-07-18 1997-11-25 Sikorsky Aircraft Corporation Optimized composite flexbeam for helicopter tail rotors
US6708921B2 (en) * 2001-04-20 2004-03-23 Bell Helicopter Textron, Inc. Composite flapping flexure
DE10316095B4 (de) * 2003-04-08 2010-09-16 Eurocopter Deutschland Gmbh Drehflügelrotor
CN101573269B (zh) * 2006-02-24 2013-03-13 贝尔直升机泰克斯特龙公司 直升机旋翼轭架及其制造方法

Also Published As

Publication number Publication date
CA2637461A1 (en) 2007-09-20
CN101573269A (zh) 2009-11-04
US8147198B2 (en) 2012-04-03
US20100221119A1 (en) 2010-09-02
DE06844078T1 (de) 2009-02-19
WO2007106064A3 (en) 2009-04-16
WO2007106064A2 (en) 2007-09-20
AU2006340075A1 (en) 2007-09-20
BRPI0621310A2 (pt) 2011-12-06
EP1986913B1 (en) 2016-01-06
MX2008010891A (es) 2008-11-27
CA2637461C (en) 2011-04-19
EP1986913A4 (en) 2014-09-10
JP2009527417A (ja) 2009-07-30
EP1986913A2 (en) 2008-11-05
CN101573269B (zh) 2013-03-13

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