FR2872234B1 - Accouplement tolerant de forts deplacements angulaires et axiaux - Google Patents

Accouplement tolerant de forts deplacements angulaires et axiaux

Info

Publication number
FR2872234B1
FR2872234B1 FR0407091A FR0407091A FR2872234B1 FR 2872234 B1 FR2872234 B1 FR 2872234B1 FR 0407091 A FR0407091 A FR 0407091A FR 0407091 A FR0407091 A FR 0407091A FR 2872234 B1 FR2872234 B1 FR 2872234B1
Authority
FR
France
Prior art keywords
axial displacements
strong angular
tolerant coupling
tolerant
coupling
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
FR0407091A
Other languages
English (en)
Other versions
FR2872234A1 (fr
Inventor
Emmanuel Mermoz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0407091A priority Critical patent/FR2872234B1/fr
Priority to CNB2005100802376A priority patent/CN100417830C/zh
Priority to US11/167,110 priority patent/US7618326B2/en
Publication of FR2872234A1 publication Critical patent/FR2872234A1/fr
Application granted granted Critical
Publication of FR2872234B1 publication Critical patent/FR2872234B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/50—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
    • F16D3/72—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members with axially-spaced attachments to the coupling parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/50—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
    • F16D3/72—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members with axially-spaced attachments to the coupling parts
    • F16D3/725—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members with axially-spaced attachments to the coupling parts with an intermediate member made of fibre-reinforced resin

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Connection Of Plates (AREA)
  • Tires In General (AREA)
  • General Details Of Gearings (AREA)
FR0407091A 2004-06-28 2004-06-28 Accouplement tolerant de forts deplacements angulaires et axiaux Expired - Fee Related FR2872234B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR0407091A FR2872234B1 (fr) 2004-06-28 2004-06-28 Accouplement tolerant de forts deplacements angulaires et axiaux
CNB2005100802376A CN100417830C (zh) 2004-06-28 2005-06-28 可适应大的角度和轴向位移的联结器
US11/167,110 US7618326B2 (en) 2004-06-28 2005-06-28 Coupling capable of accommodating large angular and axial displacements

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0407091A FR2872234B1 (fr) 2004-06-28 2004-06-28 Accouplement tolerant de forts deplacements angulaires et axiaux

Publications (2)

Publication Number Publication Date
FR2872234A1 FR2872234A1 (fr) 2005-12-30
FR2872234B1 true FR2872234B1 (fr) 2007-11-30

Family

ID=34947884

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0407091A Expired - Fee Related FR2872234B1 (fr) 2004-06-28 2004-06-28 Accouplement tolerant de forts deplacements angulaires et axiaux

Country Status (3)

Country Link
US (1) US7618326B2 (fr)
CN (1) CN100417830C (fr)
FR (1) FR2872234B1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2446863A (en) * 2007-02-21 2008-08-27 Smiths Aerospace Ltd Diaphragm coupling with stops to limit range of movement
US8591345B2 (en) * 2011-09-09 2013-11-26 Goodrich Corporation Flexible diaphragm coupling for axial force loading
CN103591162A (zh) * 2013-11-25 2014-02-19 中国南方航空工业(集团)有限公司 联轴节组件
EP2990676B1 (fr) 2014-08-26 2021-04-07 Ellergon Antriebstechnik GmbH Couplage
KR101662535B1 (ko) * 2015-02-24 2016-10-14 현대자동차주식회사 베어링브라켓
GB2585712B (en) * 2019-07-09 2024-04-10 Crane John Uk Ltd Coupling members that join first and second rotary members
CN111577780B (zh) * 2020-05-22 2021-06-08 中国船舶科学研究中心 一种弹性膜片联轴器

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1392342A (en) * 1920-09-04 1921-10-04 Arthur M Laycock Universal joint
US2647380A (en) * 1949-06-24 1953-08-04 Bendix Aviat Corp Flexible shaft
US3500660A (en) * 1968-11-26 1970-03-17 James H Anderson Flexible couplings and hub mountings
DE3026104A1 (de) * 1980-07-10 1982-02-04 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor eines drehfluegelflugzeuges
US4666753A (en) * 1985-05-16 1987-05-19 United Technologies Corporation Filament wound structure for use as a torque drive
US5221232A (en) * 1989-01-12 1993-06-22 Zero-Max, Inc. Flexible disc-like coupling element
US5158504A (en) * 1989-05-12 1992-10-27 Lucas Aerospace Power Transmission Corp. Flexible coupling including a flexible diaphragm element contoured with its thinnest thickness near the center thereof
DE3936680C1 (fr) * 1989-11-03 1991-02-07 Bhs-Voith Getriebetechnik Gmbh, 8972 Sonthofen, De
US5000722A (en) * 1990-03-26 1991-03-19 Kop-Flex, Inc. Coupling member for rotatable shafts
JP3202410B2 (ja) * 1993-04-27 2001-08-27 三菱重工業株式会社 ダイアフラム継手の制振構造
GB2289742B (en) * 1994-05-27 1998-12-09 Western Atlas Uk Ltd Drive transmitting device
US20040005929A1 (en) * 2002-07-03 2004-01-08 Piasecki Frank N. Star flexible coupling
US20050255926A1 (en) * 2002-07-03 2005-11-17 Piasecki Frank N Star flexible coupling

Also Published As

Publication number Publication date
US20060003847A1 (en) 2006-01-05
CN1715696A (zh) 2006-01-04
US7618326B2 (en) 2009-11-17
CN100417830C (zh) 2008-09-10
FR2872234A1 (fr) 2005-12-30

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Legal Events

Date Code Title Description
CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20140602

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 17

ST Notification of lapse

Effective date: 20220205