FR2977862B1 - Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur - Google Patents

Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur

Info

Publication number
FR2977862B1
FR2977862B1 FR1156443A FR1156443A FR2977862B1 FR 2977862 B1 FR2977862 B1 FR 2977862B1 FR 1156443 A FR1156443 A FR 1156443A FR 1156443 A FR1156443 A FR 1156443A FR 2977862 B1 FR2977862 B1 FR 2977862B1
Authority
FR
France
Prior art keywords
turbopropulseur
orientation
controlling
blower blades
blower
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.)
Active
Application number
FR1156443A
Other languages
English (en)
Other versions
FR2977862A1 (fr
Inventor
Francois Gallet
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1156443A priority Critical patent/FR2977862B1/fr
Priority to GB1212050.7A priority patent/GB2492882B/en
Priority to US13/544,127 priority patent/US9090336B2/en
Publication of FR2977862A1 publication Critical patent/FR2977862A1/fr
Application granted granted Critical
Publication of FR2977862B1 publication Critical patent/FR2977862B1/fr
Active 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
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/32—Blade pitch-changing mechanisms mechanical
    • 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
    • B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers
    • 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
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • 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
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1156443A 2011-07-13 2011-07-13 Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur Active FR2977862B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1156443A FR2977862B1 (fr) 2011-07-13 2011-07-13 Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur
GB1212050.7A GB2492882B (en) 2011-07-13 2012-07-06 A device for controlling the pitch of turboprop fan blades
US13/544,127 US9090336B2 (en) 2011-07-13 2012-07-09 Device for controlling the pitch of turboprop fan blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1156443A FR2977862B1 (fr) 2011-07-13 2011-07-13 Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur

Publications (2)

Publication Number Publication Date
FR2977862A1 FR2977862A1 (fr) 2013-01-18
FR2977862B1 true FR2977862B1 (fr) 2013-08-23

Family

ID=46766256

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1156443A Active FR2977862B1 (fr) 2011-07-13 2011-07-13 Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur

Country Status (3)

Country Link
US (1) US9090336B2 (fr)
FR (1) FR2977862B1 (fr)
GB (1) GB2492882B (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3001264B1 (fr) * 2013-01-18 2017-03-17 Snecma Systeme pour changer le pas des pales d'une helice.
US9869190B2 (en) * 2014-05-30 2018-01-16 General Electric Company Variable-pitch rotor with remote counterweights
US10072510B2 (en) 2014-11-21 2018-09-11 General Electric Company Variable pitch fan for gas turbine engine and method of assembling the same
FR3036141B1 (fr) 2015-05-12 2019-08-09 Safran Aircraft Engines Arbre de commande radial pour dispositif de commande de l'orientation des pales de soufflante d'une turbomachine a soufflante non carenee et procede de montage d'un tel arbre.
FR3036092B1 (fr) * 2015-05-12 2017-06-02 Snecma Dispositif a arbre radial pour la commande de l'orientation des pales de soufflante d'une turbomachine a soufflante non carenee
PL226826B1 (pl) 2015-09-03 2017-09-29 Gen Electric Układ sterowania skokiem dozespołu wirnika, silnik turbospalinowy isposób sterowania katem skoku wielu łopat smigła
US10100653B2 (en) 2015-10-08 2018-10-16 General Electric Company Variable pitch fan blade retention system
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
US11674435B2 (en) 2021-06-29 2023-06-13 General Electric Company Levered counterweight feathering system
US11795964B2 (en) 2021-07-16 2023-10-24 General Electric Company Levered counterweight feathering system

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4657484A (en) * 1984-09-04 1987-04-14 General Electric Company Blade pitch varying means
GB2182727B (en) * 1985-11-12 1989-09-27 Gen Electric Propeller/fan pitch feathering apparatus
US4753572A (en) * 1986-10-02 1988-06-28 United Technologies Corporation Propeller pitch change actuation system
FR2937678B1 (fr) 2008-10-23 2013-11-22 Snecma Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur
FR2946012B1 (fr) * 2009-05-29 2011-06-24 Snecma Dispositif pour la commande de l'orientation des pales de soufflante d'un turbopropulseur
FR2946011B1 (fr) * 2009-05-29 2013-01-11 Snecma Dispositif a verin mobile pour la commande de l'orientation des pales de soufflante d'un turbopropulseur
FR2946010B1 (fr) * 2009-05-29 2011-06-24 Snecma Dispositif a verin fixe pour la commande des pales de soufflante d'un turbopropulseur
US8336290B2 (en) * 2010-09-30 2012-12-25 General Electric Company Pitch change apparatus for counter-rotating propellers

Also Published As

Publication number Publication date
US9090336B2 (en) 2015-07-28
GB2492882A (en) 2013-01-16
GB2492882B (en) 2017-06-28
FR2977862A1 (fr) 2013-01-18
GB201212050D0 (en) 2012-08-22
US20130017087A1 (en) 2013-01-17

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