FR2683789B1 - Interrupteur de limite inferieure du pas, a commande hydraulique, pour un dispositif de variation du pas d'une helice. - Google Patents

Interrupteur de limite inferieure du pas, a commande hydraulique, pour un dispositif de variation du pas d'une helice.

Info

Publication number
FR2683789B1
FR2683789B1 FR9212977A FR9212977A FR2683789B1 FR 2683789 B1 FR2683789 B1 FR 2683789B1 FR 9212977 A FR9212977 A FR 9212977A FR 9212977 A FR9212977 A FR 9212977A FR 2683789 B1 FR2683789 B1 FR 2683789B1
Authority
FR
France
Prior art keywords
limit switch
propeller
hydraulically controlled
variation device
controlled lower
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
FR9212977A
Other languages
English (en)
Other versions
FR2683789A1 (fr
Inventor
William J Bagge
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.)
Raytheon Technologies Corp
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 FR2683789A1 publication Critical patent/FR2683789A1/fr
Application granted granted Critical
Publication of FR2683789B1 publication Critical patent/FR2683789B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • 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
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
FR9212977A 1991-10-25 1992-10-23 Interrupteur de limite inferieure du pas, a commande hydraulique, pour un dispositif de variation du pas d'une helice. Expired - Fee Related FR2683789B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/782,835 US5186608A (en) 1991-10-25 1991-10-25 Hydraulic low pitch switch for propeller pitch change system

Publications (2)

Publication Number Publication Date
FR2683789A1 FR2683789A1 (fr) 1993-05-21
FR2683789B1 true FR2683789B1 (fr) 1994-05-27

Family

ID=25127318

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9212977A Expired - Fee Related FR2683789B1 (fr) 1991-10-25 1992-10-23 Interrupteur de limite inferieure du pas, a commande hydraulique, pour un dispositif de variation du pas d'une helice.

Country Status (3)

Country Link
US (1) US5186608A (fr)
FR (1) FR2683789B1 (fr)
GB (1) GB2261707B (fr)

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US5498135A (en) * 1995-01-17 1996-03-12 Newport News Shipbuilding And Dry Dock Company Actuator for a variable pitch propeller
US6059528A (en) * 1996-11-22 2000-05-09 United Technologies Corporation Electronic propeller control system
US5897293A (en) * 1996-11-22 1999-04-27 United Technologies Corporation Counterweighted propeller control system
US6077040A (en) * 1998-05-01 2000-06-20 United Technologies Corporation Control system for blades for a variable pitch propeller
FR2796457B1 (fr) * 1999-07-16 2001-10-05 Lucas Aerospace Fcs Perfectionnements aux capteurs de deplacement pour verins de servo-commande
JP2003194036A (ja) 2001-12-28 2003-07-09 Honda Motor Co Ltd オイルレシーバ
US7118336B2 (en) * 2003-12-19 2006-10-10 Pratt & Whitney Canada Corp. Pressurized oil supply for propeller engine system
US7172391B2 (en) * 2004-08-03 2007-02-06 Hamilton Sundstrand Propeller actuation system
US8267656B2 (en) * 2006-03-08 2012-09-18 Hamilton Sundstrand Corporation Propeller pitch lock system
US8545178B2 (en) * 2006-03-08 2013-10-01 Hamilton Sundstrand Corporation Controlled propeller pitch lock actuation system
US7758310B2 (en) * 2007-01-15 2010-07-20 Sikorsky Aircraft Corporation Translational thrust system for a rotary wing aircraft
EP2050670A3 (fr) * 2008-01-11 2011-11-23 MT-Propeller Entwicklung GmbH Régulateur d'hélice hydroélectrique
FR2931797B1 (fr) * 2008-05-29 2010-07-30 Snecma Systeme simplifie de commande de calage de pale d'une helice d'un turbomoteur pour aeronef
US8162611B2 (en) * 2008-07-15 2012-04-24 Hamilton Sundstrand Corporation Controllable pitch propeller with electrical power generation
FR2939098B1 (fr) * 2008-12-01 2016-07-29 Eurocopter France Distributeur hydraulique, helicoptere hybride muni d'un tel distributeur hydraulique et procede mis en oeuvre par ce distributeur hydraulique
US8277182B2 (en) * 2009-07-02 2012-10-02 Hamilton Sundstrand Corporation Remote pitch controller for a variable pitch propeller
US8496436B2 (en) * 2010-01-11 2013-07-30 Hamilton Sundstrand Corporation Torque compensation for propeller pitch change mechanism
GB201007569D0 (en) 2010-05-06 2010-06-23 Rolls Royce Plc Pitch control mechanism
GB201007567D0 (en) 2010-05-06 2010-06-23 Rolls Royce Plc BAck-up featherer
GB201007565D0 (en) 2010-05-06 2010-06-23 Rolls Royce Plc Pitch control mechanism
GB201007564D0 (en) 2010-05-06 2010-06-23 Rolls Royce Plc Back-up featherer
US8535007B2 (en) 2010-05-18 2013-09-17 Hamilton Sundstrand Corporation Hydraulic actuator locking device
US8784055B2 (en) * 2010-11-30 2014-07-22 Hamilton Sundstrand Corporation Propeller pitchlock un-locking device
US8726787B2 (en) 2011-03-18 2014-05-20 General Electric Company Rotary hydraulic actuator with hydraulically controlled position limits
FR2978953B1 (fr) * 2011-08-08 2013-09-20 Snecma Systeme de commande hydraulique de l'orientation de pales de soufflante
FR2980452B1 (fr) * 2011-09-23 2013-10-11 Eurocopter France Systeme de commande de la variation de pas des pales d'une helice, helice et aeronef
FR2992696B1 (fr) * 2012-06-28 2015-04-10 Eurocopter France Distributeur hydraulique, dispositif de reglage du pas de pales, aeronef muni d'un tel distributeur hydraulique
CN102765473B (zh) * 2012-08-13 2015-04-15 中国南方航空工业(集团)有限公司 螺旋桨变距用分油装置
CN103046969B (zh) * 2013-01-09 2014-09-24 于魁江 一种气动叶轮
US9381997B2 (en) * 2013-08-13 2016-07-05 Hamilton Sundstrand Corporation Propeller pitchlock system with a rotating interface
BR112016005998A2 (pt) * 2013-10-07 2017-08-01 Ge Aviat Systems Ltd conjunto de controle de afastamento
PL226824B1 (pl) * 2015-09-07 2017-09-29 Gen Electric Układ isposób regulacji skoku smigła
PL226825B1 (pl) 2015-09-07 2017-09-29 Gen Electric Układ isposób regulacji skoku smigła
GB2548085B (en) 2016-02-29 2019-12-25 Ge Aviation Systems Llc A system and method for coordinating a propeller with an electronic engine control
EP3239041A1 (fr) * 2016-04-29 2017-11-01 Ratier-Figeac SAS Systèmes d'actionnement hydraulique
US10683082B2 (en) 2016-04-29 2020-06-16 Ratier-Figeac Sas Hydraulic actuation systems
FR3055308B1 (fr) * 2016-08-26 2018-08-17 Safran Aircraft Engines Moyen de commande d'un systeme de changement de pas comprenant un dispositif anti-rotation, systeme de changement de pas equipe dudit moyen de commande et turbomachine correspondante
US10793256B2 (en) * 2016-09-12 2020-10-06 Pratt & Whitney Canada Corp. Propeller blade angle control system
EP3354562A1 (fr) * 2017-01-30 2018-08-01 Ge Avio S.r.l. Dispositif d'écrasement de palier de transfert
US10247579B2 (en) * 2017-03-01 2019-04-02 Honeywell International Inc. Linear variable differential transformer (LVDT) calibration mechanism for precision rigging with vibration and accuracy tracking robustness
US20180340501A1 (en) * 2017-05-23 2018-11-29 Weishun Willaim Ni Variable displacement fuel pump with position sensor
US10577080B2 (en) * 2017-08-23 2020-03-03 Hamilton Sundstrand Corporation Dual valve systems for actuator control
US11312476B2 (en) * 2017-09-25 2022-04-26 Woodward, Inc. Propeller control unit
FR3072714B1 (fr) * 2017-10-24 2019-09-27 Safran Transmission Systems Tube de transfert d'huile pour un systeme de commande de regulation du pas d'une helice de turbomachine
US11118464B2 (en) 2018-10-11 2021-09-14 General Electric Company Aircraft gas turbine engine blade pitch change mechanism
EP3670333A1 (fr) * 2018-12-18 2020-06-24 Hamilton Sundstrand Corporation Commande en boucle fermée d'angle de pale d'hélice par modulation de solénoïde
US11554850B2 (en) * 2019-04-25 2023-01-17 Pratt & Whitney Canada Corp. Blade angle position feedback system with offset sensors

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1185041A (en) * 1966-04-12 1970-03-18 Dowty Rotol Ltd Adjustable Bladed Rotors
SE312497B (fr) * 1968-05-03 1969-07-14 Karlstad Mekaniska Ab
US3820917A (en) * 1972-10-10 1974-06-28 Titovi Zavodi Litostroj Safety device for preventing the excessive speed of water turbines
US3873235A (en) * 1973-10-01 1975-03-25 Gen Electric Variable pitch turbofan engine
US4348156A (en) * 1980-03-17 1982-09-07 United Technologies Corporation Blade pitch actuation system
US4523891A (en) * 1983-06-15 1985-06-18 United Technologies Corporation Propeller pitch change actuation system
GB2180892B (en) * 1985-09-28 1990-03-07 Dowty Rotol Ltd A control system for a bladed rotor assembly
GB8916714D0 (en) * 1989-07-21 1989-09-06 Dowty Rotol Ltd A propeller blade pitch control mechanism
US5141399A (en) * 1990-10-18 1992-08-25 United Technologies Corporation Pitch change control system

Also Published As

Publication number Publication date
GB2261707B (en) 1994-10-12
GB9222010D0 (en) 1992-12-02
US5186608A (en) 1993-02-16
GB2261707A (en) 1993-05-26
FR2683789A1 (fr) 1993-05-21

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20100630