BR7904241A - Rotor de helicoptero com travessao e amortecedor de facil reposicao - Google Patents

Rotor de helicoptero com travessao e amortecedor de facil reposicao

Info

Publication number
BR7904241A
BR7904241A BR7904241A BR7904241A BR7904241A BR 7904241 A BR7904241 A BR 7904241A BR 7904241 A BR7904241 A BR 7904241A BR 7904241 A BR7904241 A BR 7904241A BR 7904241 A BR7904241 A BR 7904241A
Authority
BR
Brazil
Prior art keywords
shock absorber
easy replacement
helicopter rotor
helicopter
rotor
Prior art date
Application number
BR7904241A
Other languages
English (en)
Inventor
W Noehren
D Ferris
P Ogle
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of BR7904241A publication Critical patent/BR7904241A/pt

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Dampers (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Springs (AREA)
BR7904241A 1978-07-12 1979-07-05 Rotor de helicoptero com travessao e amortecedor de facil reposicao BR7904241A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/924,110 US4244677A (en) 1978-07-12 1978-07-12 Cross-beam helicopter rotor with readily replaceable snubber

Publications (1)

Publication Number Publication Date
BR7904241A true BR7904241A (pt) 1980-04-15

Family

ID=25449720

Family Applications (1)

Application Number Title Priority Date Filing Date
BR7904241A BR7904241A (pt) 1978-07-12 1979-07-05 Rotor de helicoptero com travessao e amortecedor de facil reposicao

Country Status (12)

Country Link
US (1) US4244677A (pt)
AU (1) AU523370B2 (pt)
BE (1) BE877614A (pt)
BR (1) BR7904241A (pt)
CA (1) CA1110606A (pt)
CH (1) CH637890A5 (pt)
DE (1) DE2927263A1 (pt)
FR (1) FR2430885A1 (pt)
GB (1) GB2025340B (pt)
IL (1) IL57704A (pt)
IT (1) IT1122106B (pt)
NO (1) NO146273C (pt)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2903524C2 (de) * 1979-01-31 1982-02-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schlag- und schwenkgelenkloser Anschluß von Rotorblättern eines Drehflügelflugzeuges
US4332525A (en) * 1979-12-03 1982-06-01 United Technologies Corporation Matched stiffness rotor flexbeam and blade system
US4381902A (en) * 1979-12-20 1983-05-03 Hughes Helicopters, Inc. Helicopter tail rotor of the elastomerically-mounted composite flexbeam type
DE3241754C2 (de) * 1982-11-11 1986-02-06 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor, insbesondere eines Drehflügelflugzeuges
US4695227A (en) * 1985-02-27 1987-09-22 Hughes Helicopters Inc. All composite, constant speed universal joint for use in a shaft driven tiltable main rotor for a helicopter
DE3526470C1 (de) * 1985-07-24 1987-01-02 Messerschmitt Boelkow Blohm Rotor,insbesondere eines Drehfluegelflugzeugs
JP2667176B2 (ja) * 1987-11-10 1997-10-27 富士重工業株式会社 ヘリコプタのピッチ変更及びリードラグ減衰装置
DE3824816A1 (de) * 1988-07-21 1990-01-25 Messerschmitt Boelkow Blohm Federelement zur drehwinkelbeweglichen verbindung zweiter bauteile
DE3824815A1 (de) * 1988-07-21 1990-01-25 Messerschmitt Boelkow Blohm Rotor, insbesondere eines drehfluegelflugzeugs, abstuetzung einer blattsteuerhuelle
GB8922338D0 (en) * 1989-10-04 1989-11-22 Westland Helicopters Helicopter rotors
US5092738A (en) * 1990-04-06 1992-03-03 United Technologies Corporation Flexbeam helicopter rotor with improved snubber-vibration damper between the torque tube and the flexible spar member
CA2055202C (en) * 1990-12-17 1992-06-18 Francis E. Byrnes Snubber-bearing with combined elastomer laminates
US5188513A (en) * 1990-12-17 1993-02-23 United Technologies Corporation Snubber-bearing with combined elastomer laminates
US5340279A (en) * 1992-06-22 1994-08-23 United Technologies Corporation Snubber assembly for a rotor assembly having ducted, coaxial counter-rotating rotors
WO1994015113A1 (en) * 1992-12-23 1994-07-07 United Technologies Corporation Tubular elastomer damper
US5913659A (en) * 1993-11-22 1999-06-22 United Technologies Corporation Apparatus and method for adjusting rotor blade tracking
US5499903A (en) * 1994-10-18 1996-03-19 United Technologies Corporation Snubber bearing mounting assembly for bearingless rotors
US5460487A (en) * 1994-11-09 1995-10-24 United Technologies Corporation Pitch adjustment assembly for bearingless main rotors
FR2728540A1 (fr) * 1994-12-22 1996-06-28 Eurocopter France Rotor sans articulation a anneaux intermediaires de commande de pas
US6024325A (en) * 1997-01-09 2000-02-15 Cartercopters, Llc Rotor for rotary wing aircraft
FR2775951B1 (fr) * 1998-03-16 2001-09-07 Rene Mouille Pale de rotor, notamment pour le rotor arriere anticouple d'un helicoptere
FR2778165B1 (fr) * 1998-04-29 2000-07-13 Eurocopter France Rotor sans articulation avec demi-paliers precomprimes d'appui des manchettes de pied de pale sur des lames torsibles d'emplanture des pales
DE19915085C2 (de) * 1998-05-28 2002-03-14 Eurocopter Deutschland Rotorblatt für einen lagerlosen Rotor eines Hubschraubers
ITMI991124A1 (it) 1998-05-28 2000-11-21 Eurocopter Deutschland Pala per un rotore privo di supporto di un elicottero
ITMI991127A1 (it) * 1998-05-28 2000-11-21 Eurocopter Deutschland Pala per un rotore privo di supporto di un elicottero
EP1070662B1 (de) 1999-07-20 2003-06-11 Eurocopter Deutschland GmbH Rotorblatt für einen lagerlosen Rotor eines Hubschraubers
US6371681B1 (en) * 1999-09-20 2002-04-16 Bell Helicopter Textron Inc. Anti-rotation clip
US20020113349A1 (en) * 2001-02-09 2002-08-22 Rivin Evgeny I. Nonlinear and adjustable bushings
US6588967B2 (en) * 2001-04-06 2003-07-08 Evgeny I. Rivin Joint
FR2839945B1 (fr) 2002-05-24 2004-08-13 Hutchinson Dispositif combine amortisseur-rotule pour rotor d'helicoptere
US6695583B2 (en) * 2002-05-30 2004-02-24 Sikorsky Aircraft Corporation Snubber-vibration damper system for a bearingless main rotor
US6827553B2 (en) * 2003-01-15 2004-12-07 Lord Corporation Flexbeam damper assembly having transition shim clamp device
US6848886B2 (en) * 2003-04-18 2005-02-01 Sikorsky Aircraft Corporation Snubber
CN1842422A (zh) * 2003-08-27 2006-10-04 贝尔直升机泰克斯特龙公司 双弹簧刚度阻尼器
DE102007035970A1 (de) * 2007-07-30 2009-02-12 Ims Gear Gmbh Elektrische Lenkvorrichtung für Kraftfahrzeuge
US8122586B2 (en) 2008-11-18 2012-02-28 The Boeing Company Method for connecting a tension-torsion strap
US9884680B2 (en) * 2008-12-11 2018-02-06 Sikorsky Aircraft Corporation Elastomeric bearing system motion limiter
US9068621B1 (en) 2010-11-23 2015-06-30 Lord Corporation Rotary wing aircraft bearing for rotary wing aircraft motions
EP2504231B1 (en) * 2009-11-23 2017-03-15 LORD Corporation Elastomeric high capacity laminated rotary wing aircraft bearing
EP3333075B1 (en) * 2009-11-23 2019-07-10 LORD Corporation Rotary wing aircraft bearing for rotary wing aircraft motions
CN103900801B (zh) * 2012-12-25 2016-12-28 中国直升机设计研究所 一种叉形件疲劳试验装置
US9682773B2 (en) 2013-06-25 2017-06-20 The Boeing Company Systems and methods for blade attachment
US10793264B2 (en) * 2014-06-27 2020-10-06 Sikorsky Aircraft Corporation Flex beam clamp for rotor assembly
WO2017079014A1 (en) * 2015-11-02 2017-05-11 Sikorsky Aircraft Corporation Rotor blade snubber retainer for a rotary wing aircraft

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3484174A (en) * 1968-04-08 1969-12-16 Kaman Corp Rotary wing system
US3700352A (en) * 1971-03-05 1972-10-24 Lord Corp Rotor system
CA951301A (en) * 1971-04-08 1974-07-16 United Aircraft Corporation Helicopter rotor system
US3874815A (en) * 1973-11-15 1975-04-01 Boeing Co Rotary head assembly for rotary wing aircraft
US3874820A (en) * 1974-04-08 1975-04-01 United Aircraft Corp Hingeless in-plane rotor blade design
FR2285298A1 (fr) * 1974-09-19 1976-04-16 Aerospatiale Agencement de rotor de queue pour giravions
US4008980A (en) * 1975-06-26 1977-02-22 United Technologies Corporation Composite helicopter spar and means to alleviate stress concentration
US4093400A (en) * 1976-12-15 1978-06-06 United Technologies Corporation Cross beam rotor
US4087203A (en) * 1977-01-07 1978-05-02 United Technologies Corporation Cross beam rotor
FR2397325A1 (fr) * 1977-07-13 1979-02-09 Aerospatiale Moyeu de rotor, en particulier pour le rotor principal d'un helicoptere

Also Published As

Publication number Publication date
AU4880879A (en) 1980-01-17
IT1122106B (it) 1986-04-23
DE2927263A1 (de) 1980-01-24
FR2430885B1 (pt) 1983-10-28
NO146273C (no) 1982-09-01
GB2025340B (en) 1982-09-02
BE877614A (fr) 1979-11-05
NO146273B (no) 1982-05-24
DE2927263C2 (pt) 1989-11-02
IL57704A (en) 1982-09-30
CA1110606A (en) 1981-10-13
CH637890A5 (de) 1983-08-31
NO792286L (no) 1980-01-15
FR2430885A1 (fr) 1980-02-08
IT7924241A0 (it) 1979-07-10
AU523370B2 (en) 1982-07-22
US4244677A (en) 1981-01-13
GB2025340A (en) 1980-01-23

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