PL3313730T3 - Urządzenie sterujące śmigłem silnika turbośmigłowego z łopatami o zmiennym nastawieniu - Google Patents

Urządzenie sterujące śmigłem silnika turbośmigłowego z łopatami o zmiennym nastawieniu

Info

Publication number
PL3313730T3
PL3313730T3 PL16736531T PL16736531T PL3313730T3 PL 3313730 T3 PL3313730 T3 PL 3313730T3 PL 16736531 T PL16736531 T PL 16736531T PL 16736531 T PL16736531 T PL 16736531T PL 3313730 T3 PL3313730 T3 PL 3313730T3
Authority
PL
Poland
Prior art keywords
regulating device
variable pitch
pitch blades
turboprop propeller
turboprop
Prior art date
Application number
PL16736531T
Other languages
English (en)
Inventor
Antoine MOUTAUX
Jean-Michel PRESSE
Original Assignee
Safran Helicopter Engines
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 Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL3313730T3 publication Critical patent/PL3313730T3/pl

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
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • 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
    • 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
    • B64C11/303—Blade pitch-changing mechanisms characterised by comprising a governor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00—Details of servomotor systems ; Valves for servomotor systems
    • F15B13/10—Special arrangements for operating the actuated device with or without using fluid pressure, e.g. for emergency use
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/16—Systems essentially having two or more interacting servomotors, e.g. multi-stage
    • F15B9/17—Systems essentially having two or more interacting servomotors, e.g. multi-stage with electrical control means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B21/00—Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
    • F15B21/08—Servomotor systems incorporating electrically operated control means
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Transmission Devices (AREA)
  • Supercharger (AREA)
  • Operation Control Of Excavators (AREA)
PL16736531T 2015-06-23 2016-06-17 Urządzenie sterujące śmigłem silnika turbośmigłowego z łopatami o zmiennym nastawieniu PL3313730T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1555734A FR3037922B1 (fr) 2015-06-23 2015-06-23 Dispositif de regulation d'une helice a pales a calage variable d'un turbopropulseur
EP16736531.1A EP3313730B1 (fr) 2015-06-23 2016-06-17 Dispositif de régulation d'une hélice à pales à calage variable d'un turbopropulseur
PCT/FR2016/051476 WO2016207522A1 (fr) 2015-06-23 2016-06-17 Dispositif de régulation d'une hélice à pales à calage variable d'un turbopropulseur

Publications (1)

Publication Number Publication Date
PL3313730T3 true PL3313730T3 (pl) 2019-07-31

Family

ID=54066058

Family Applications (1)

Application Number Title Priority Date Filing Date
PL16736531T PL3313730T3 (pl) 2015-06-23 2016-06-17 Urządzenie sterujące śmigłem silnika turbośmigłowego z łopatami o zmiennym nastawieniu

Country Status (10)

Country Link
US (1) US10421530B2 (pl)
EP (1) EP3313730B1 (pl)
JP (1) JP6782257B2 (pl)
KR (1) KR102526448B1 (pl)
CN (1) CN107709156B (pl)
CA (1) CA2988633C (pl)
FR (1) FR3037922B1 (pl)
PL (1) PL3313730T3 (pl)
RU (1) RU2711848C2 (pl)
WO (1) WO2016207522A1 (pl)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11118464B2 (en) 2018-10-11 2021-09-14 General Electric Company Aircraft gas turbine engine blade pitch change mechanism
KR102558225B1 (ko) 2021-09-08 2023-07-20 한국항공우주연구원 프로펠러 구동 항공기용 자동 패더링 장치
US20230322367A1 (en) * 2022-04-11 2023-10-12 Category, LLC Monocopter

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4588354A (en) * 1983-08-05 1986-05-13 United Technologies Corporation Engine speed control in propeller pitch control systems
US4909709A (en) * 1988-06-22 1990-03-20 Raisbeck James D Throttle/propeller mixer cam
US4986734A (en) * 1988-10-27 1991-01-22 Sundstrand Corporation Overspeed protection system for aircraft fan engine
US4893989A (en) * 1989-03-07 1990-01-16 United Technologies Corporation Variable propeller system incorporating a forward transfer bearing
US5037271A (en) * 1989-12-26 1991-08-06 United Technologies Corporation Pitch control system
US5042966A (en) * 1989-12-26 1991-08-27 United Technologies Corporation Pitch control system
US5141399A (en) * 1990-10-18 1992-08-25 United Technologies Corporation Pitch change control system
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
US6511292B2 (en) * 2001-06-27 2003-01-28 Hamilton Sundstrand Corporation Backup governing system for a variable pitch propeller
US8267656B2 (en) * 2006-03-08 2012-09-18 Hamilton Sundstrand Corporation Propeller pitch lock system
FR2911644B1 (fr) * 2007-01-23 2012-06-01 Snecma Turbopropulseur comportant une helice formee de pales a orientation reglable.
FR2911930A1 (fr) * 2007-01-26 2008-08-01 Snecma Sa Turbopropulseur a helice a pas reglable
FR2946010B1 (fr) * 2009-05-29 2011-06-24 Snecma Dispositif a verin fixe pour la commande des pales de soufflante d'un turbopropulseur
US9718536B2 (en) * 2010-05-18 2017-08-01 Hamilton Sundstrand Corporation Counter-rotating open-rotor (CROR)
US8726787B2 (en) * 2011-03-18 2014-05-20 General Electric Company Rotary hydraulic actuator with hydraulically controlled position limits
US9169783B2 (en) * 2012-05-30 2015-10-27 Woodward, Inc. Electrohydraulic propeller governor
RU2527798C2 (ru) * 2012-11-28 2014-09-10 Михаил Никитович Алексенко Устройство управления вектором тяги реактивного двигателя

Also Published As

Publication number Publication date
CA2988633A1 (fr) 2016-12-29
EP3313730B1 (fr) 2019-03-13
CN107709156B (zh) 2021-09-10
WO2016207522A1 (fr) 2016-12-29
RU2017143152A3 (pl) 2019-11-22
KR102526448B1 (ko) 2023-04-27
US10421530B2 (en) 2019-09-24
EP3313730A1 (fr) 2018-05-02
JP2018518416A (ja) 2018-07-12
RU2017143152A (ru) 2019-07-24
FR3037922A1 (fr) 2016-12-30
KR20180058658A (ko) 2018-06-01
FR3037922B1 (fr) 2017-07-07
RU2711848C2 (ru) 2020-01-22
JP6782257B2 (ja) 2020-11-11
CA2988633C (fr) 2024-02-27
CN107709156A (zh) 2018-02-16
US20180354608A1 (en) 2018-12-13

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