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FR2963605B1 - Helice pour aeronef - Google Patents

Helice pour aeronef

Info

Publication number
FR2963605B1
FR2963605B1 FR1156822A FR1156822A FR2963605B1 FR 2963605 B1 FR2963605 B1 FR 2963605B1 FR 1156822 A FR1156822 A FR 1156822A FR 1156822 A FR1156822 A FR 1156822A FR 2963605 B1 FR2963605 B1 FR 2963605B1
Authority
FR
France
Prior art keywords
helic
aircraft
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
FR1156822A
Other languages
English (en)
Other versions
FR2963605A1 (fr
Inventor
Michael Fedor Towkan
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.)
GE Aviation Systems Ltd
Original Assignee
GE Aviation Systems Ltd
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 GE Aviation Systems Ltd filed Critical GE Aviation Systems Ltd
Publication of FR2963605A1 publication Critical patent/FR2963605A1/fr
Application granted granted Critical
Publication of FR2963605B1 publication Critical patent/FR2963605B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48—Units of two or more coaxial propellers

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
FR1156822A 2010-08-06 2011-07-26 Helice pour aeronef Expired - Fee Related FR2963605B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1013261.1A GB2482545B (en) 2010-08-06 2010-08-06 Aircraft propellers with composite blades mounted to a single propeller hub

Publications (2)

Publication Number Publication Date
FR2963605A1 FR2963605A1 (fr) 2012-02-10
FR2963605B1 true FR2963605B1 (fr) 2014-08-29

Family

ID=42931302

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1156822A Expired - Fee Related FR2963605B1 (fr) 2010-08-06 2011-07-26 Helice pour aeronef

Country Status (8)

Country Link
US (1) US9527578B2 (fr)
JP (1) JP2012071823A (fr)
CN (1) CN102381469B (fr)
BR (1) BRPI1103825A2 (fr)
CA (1) CA2747457C (fr)
DE (1) DE102011052421A1 (fr)
FR (1) FR2963605B1 (fr)
GB (1) GB2482545B (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3011529B1 (fr) * 2013-10-09 2017-03-10 Snecma Pivot de pale d'helice aerienne
US10414486B2 (en) 2015-11-30 2019-09-17 General Electric Company Airfoil for a rotary machine including a propellor assembly
WO2017221387A1 (fr) * 2016-06-23 2017-12-28 株式会社プロドローン Aéronef sans pilote et son procédé de stockage
EP3323714B1 (fr) 2016-11-21 2019-07-03 Ratier-Figeac SAS Contrepoids d'équilibrage d'hélice
CN106741974A (zh) * 2016-12-12 2017-05-31 惠阳航空螺旋桨有限责任公司 一种螺旋桨用复合材料整流罩
CN206766327U (zh) * 2017-04-25 2017-12-19 深圳市大疆创新科技有限公司 螺旋桨、动力系统及无人飞行器
FR3070368B1 (fr) * 2017-08-29 2019-11-22 Safran Aircraft Engines Helice a calage variable
US11040767B2 (en) 2017-11-30 2021-06-22 General Electric Company Systems and methods for improved propeller design
FR3097835A1 (fr) 2019-06-27 2021-01-01 Airbus Helicopters Hélice d’avancement munie de pales interchangeables et procédé de montage de pales interchangeables sur une hélice d’avancement
US11401824B2 (en) 2019-10-15 2022-08-02 General Electric Company Gas turbine engine outlet guide vane assembly
US11506067B2 (en) 2019-10-15 2022-11-22 General Electric Company Gas turbine engine with clutch assembly
US20210108576A1 (en) 2019-10-15 2021-04-15 General Electric Company System and method for control for unducted engine
US12103702B2 (en) 2019-10-15 2024-10-01 General Electric Company Removeable fuselage shield for an aircraft
US11286795B2 (en) 2019-10-15 2022-03-29 General Electric Company Mount for an airfoil
US11505306B2 (en) 2021-04-05 2022-11-22 General Electric Company Variable pitch fan assembly with remote counterweights

Family Cites Families (66)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1868008A (en) * 1931-04-04 1932-07-19 Automotive Fan & Bearing Co Fan
US2043704A (en) * 1933-07-19 1936-06-09 Glen E Mcpherren Aircraft
US2087919A (en) * 1933-08-30 1937-07-27 Breeze Corp Propeller blade
US2382460A (en) * 1941-01-08 1945-08-14 Bell Aircraft Corp Aircraft
US2419787A (en) * 1941-04-09 1947-04-29 Muffly Glenn Aircraft engine and propeller unit
GB550117A (en) 1941-10-31 1942-12-23 Richard Walter Kloepfer Improvements in aerial propellers
US2407791A (en) * 1942-06-01 1946-09-17 Gen Motors Corp Governor valve
US2519762A (en) * 1945-07-09 1950-08-22 United Aircraft Corp Gyrodynamic damper
US2691419A (en) * 1950-03-10 1954-10-12 Andersen Charles Propeller
US2982361A (en) * 1958-12-19 1961-05-02 United Aircraft Corp Variable camber blading
GB872687A (en) * 1958-12-19 1961-07-12 United Aircraft Corp Improvements relating to propellers
US3219120A (en) * 1964-12-31 1965-11-23 Boeing Co Vibration absorbing system
US3298443A (en) * 1964-12-31 1967-01-17 Boeing Co Vibration absorbing system
GB1189444A (en) 1966-07-26 1970-04-29 Hawker Siddeley Dynamics Ltd Improvements in or relating to reversible pitch propellers
US3372758A (en) * 1967-02-15 1968-03-12 United Aircraft Corp Vibration absorber
US3540809A (en) * 1968-09-20 1970-11-17 United Aircraft Corp Vibration damped helicopter rotor
GB1302768A (fr) 1970-02-27 1973-01-10
US3867062A (en) * 1971-09-24 1975-02-18 Theodor H Troller High energy axial flow transfer stage
US3988074A (en) * 1975-11-13 1976-10-26 United Technologies Corporation Anhedral bifilar
US4097189A (en) * 1976-09-20 1978-06-27 Hartzell Propeller, Inc. Aircraft propeller and blade pitch control system
US4171183A (en) 1976-09-24 1979-10-16 United Technologies Corporation Multi-bladed, high speed prop-fan
US4407635A (en) 1979-01-08 1983-10-04 Trw Inc. Aircraft propeller assembly with composite blades
US4483658A (en) * 1979-12-11 1984-11-20 Levine Elliott M Rotational wake reaction steps for Foils
GB2066370B (en) * 1979-12-11 1983-09-14 Levine E M Rotational wake reaction synergetic staging for axial flow foils
JPS57164895A (en) 1981-03-31 1982-10-09 Kogyo Gijutsuin Variable pitch mechanism of rotor
CH659851A5 (de) * 1981-06-05 1987-02-27 Escher Wyss Ag Turbine.
US4446696A (en) * 1981-06-29 1984-05-08 General Electric Company Compound propulsor
US4483659A (en) * 1983-09-29 1984-11-20 Armstrong Richard J Axial flow impeller
JPS6058498U (ja) * 1983-09-29 1985-04-23 社団法人　日本航空宇宙工業会 可変ピツチプロペラのカウンタ−ウエイト機構
US4599041A (en) * 1984-12-19 1986-07-08 Stricker John G Variable camber tandem blade bow for turbomachines
US4883240A (en) * 1985-08-09 1989-11-28 General Electric Company Aircraft propeller noise reduction
GB2182727B (en) * 1985-11-12 1989-09-27 Gen Electric Propeller/fan pitch feathering apparatus
GB2190710B (en) * 1986-05-20 1990-10-24 Ronaldsway Aircraft Co Ltd Rotors for wind-driven machines
US4784575A (en) * 1986-11-19 1988-11-15 General Electric Company Counterrotating aircraft propulsor blades
DE3738785A1 (de) 1986-11-19 1988-05-26 Gen Electric Gegenlaeufig rotierende flugzeug-antriebsschaufeln
US5066195A (en) * 1987-10-26 1991-11-19 Deutsche Forschungsanstault Fur Luft- Und Raumfahrt e.V. Propeller for aircraft or the like
US5326223A (en) * 1988-07-07 1994-07-05 Speer Stephen R Automatic variable pitch marine propeller with mechanical holding means
US5240374A (en) * 1988-07-07 1993-08-31 Nautical Development, Inc. Damped automatic variable pitch marine propeller
US5061153A (en) * 1988-11-21 1991-10-29 Hartzell Propeller Inc. Aircraft propeller assembly with blade pitch reset for ground idle
US5551649A (en) * 1989-10-20 1996-09-03 Fokker Aircraft B.V. Propeller blade position controller
US5096383A (en) * 1989-11-02 1992-03-17 Deutsche Forschungsanstalt Fur Luft- Und Raumfahrt E.V. Propeller blades
US5190441A (en) * 1990-08-13 1993-03-02 General Electric Company Noise reduction in aircraft propellers
FR2685676B1 (fr) * 1991-12-27 1994-04-01 Aerospatiale Ste Nationale Indle Tete de rotor articule pour giravion.
FR2699497B1 (fr) * 1992-12-23 1995-03-10 Eurocopter France Dispositif de liaison pale-moyeu à attache feuilletée, pale de rotor munie d'une telle attache, et rotor équipé de telles pales.
JP2601209Y2 (ja) 1993-01-14 1999-11-15 アイワ株式会社 テープレコーダ等の可動シャーシの浮き防止機構
US5431539A (en) * 1993-10-28 1995-07-11 United Technologies Corporation Propeller pitch change mechanism
FR2719551B1 (fr) * 1994-05-04 1996-07-12 Eurocopter France Dispositif anti-couple à rotor et stator redresseur carénés, et à aubes redresseuses inclinées.
FR2719549B1 (fr) * 1994-05-04 1996-07-26 Eurocopter France Dispositif anti-couple à rotor caréné et modulation de phase des pales, pour hélicoptère.
US6155784A (en) 1997-01-09 2000-12-05 Cartercopters, Llc. Variable pitch aircraft propeller
US5820344A (en) * 1997-06-27 1998-10-13 Mcdonnell Douglas Corporation Contoured flexure strap for helicopter rotor system
US5836743A (en) * 1997-10-22 1998-11-17 United Technologies Corporation Variable pitch counterweighted propeller system with releasable hydraulic pitchlock
US6050778A (en) * 1998-09-24 2000-04-18 The Boeing Company Semi-articulated rotor system
JP2000352398A (ja) 1999-06-09 2000-12-19 Sumitomo Precision Prod Co Ltd 複合材製回転翼のシャンク部構造
US6439838B1 (en) * 1999-12-18 2002-08-27 General Electric Company Periodic stator airfoils
US7097427B2 (en) * 2002-08-02 2006-08-29 Bell Helicopter Textron Inc. Helicopter main rotor blade balance weight retention assembly
DE10305352A1 (de) * 2003-02-10 2004-09-02 Rolls-Royce Deutschland Ltd & Co Kg Turbopropantrieb mit mitläufigem Zweistufenhochleistungspropeller
RU2256585C1 (ru) 2004-01-20 2005-07-20 Общество С Ограниченной Ответственностью "Мидера-К" Воздушный винт
JP2008506582A (ja) * 2004-07-16 2008-03-06 ベル ヘリコプター テクストロン インコーポレイテッド ヘリコプタ用逆トルク装置
US7308869B2 (en) * 2005-09-23 2007-12-18 Nicholas Mathew Stone Radial compression-ignition engine
US7581929B2 (en) * 2005-10-13 2009-09-01 Hamilton Sundstrand Corporation Rotational airfoil balance system
GB2443482A (en) * 2006-11-02 2008-05-07 Smiths Group Plc Propeller blade retention
WO2009097850A2 (fr) 2008-02-05 2009-08-13 Bjarne Flytklint Rotor, en particulier pour des hélices ou des systèmes à énergie éolienne
EP2274203A4 (fr) * 2008-04-23 2014-10-15 Abe Karem Systèmes de moyeu de rotor et procédés associés
FR2935350B1 (fr) * 2008-08-27 2011-05-20 Snecma Methode de reduction des niveaux vibratoires d'une helice de turbomoteur.
FR2954274B1 (fr) * 2009-12-17 2012-02-24 Eurocopter France Mecanisme amortisseur de vibrations, et appareil volant muni d'une structure porteuse et d'un rotor muni d'un tel mecanisme
GB2482333A (en) * 2010-07-30 2012-02-01 Ge Aviat Systems Ltd Aircraft propeller

Also Published As

Publication number Publication date
FR2963605A1 (fr) 2012-02-10
US20120034095A1 (en) 2012-02-09
GB201013261D0 (en) 2010-09-22
GB2482545B (en) 2017-05-03
CA2747457A1 (fr) 2012-02-06
BRPI1103825A2 (pt) 2015-11-17
US9527578B2 (en) 2016-12-27
JP2012071823A (ja) 2012-04-12
CA2747457C (fr) 2018-09-04
CN102381469B (zh) 2016-01-27
CN102381469A (zh) 2012-03-21
DE102011052421A1 (de) 2012-02-09
GB2482545A (en) 2012-02-08

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