FR2964945B1 - Helice et systeme d'helices contrarotatives comprenant des moyens ameliores de limitation du calage, et turbomachine les comprenant - Google Patents

Helice et systeme d'helices contrarotatives comprenant des moyens ameliores de limitation du calage, et turbomachine les comprenant

Info

Publication number
FR2964945B1
FR2964945B1 FR1057504A FR1057504A FR2964945B1 FR 2964945 B1 FR2964945 B1 FR 2964945B1 FR 1057504 A FR1057504 A FR 1057504A FR 1057504 A FR1057504 A FR 1057504A FR 2964945 B1 FR2964945 B1 FR 2964945B1
Authority
FR
France
Prior art keywords
propeller
timing
limiting
improved means
turbomachine including
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
FR1057504A
Other languages
English (en)
Other versions
FR2964945A1 (fr
Inventor
Pascal Marly
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 FR1057504A priority Critical patent/FR2964945B1/fr
Priority to US13/235,419 priority patent/US9260179B2/en
Publication of FR2964945A1 publication Critical patent/FR2964945A1/fr
Application granted granted Critical
Publication of FR2964945B1 publication Critical patent/FR2964945B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/38Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • B64C11/385Blade pitch-changing mechanisms fluid, e.g. hydraulic comprising feathering, braking or stopping systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/026Aircraft 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1057504A 2010-09-20 2010-09-20 Helice et systeme d'helices contrarotatives comprenant des moyens ameliores de limitation du calage, et turbomachine les comprenant Active FR2964945B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1057504A FR2964945B1 (fr) 2010-09-20 2010-09-20 Helice et systeme d'helices contrarotatives comprenant des moyens ameliores de limitation du calage, et turbomachine les comprenant
US13/235,419 US9260179B2 (en) 2010-09-20 2011-09-18 Propeller and system of counter-rotating propellers comprising improved means for limiting pitch, and a turbine engine comprising them

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1057504A FR2964945B1 (fr) 2010-09-20 2010-09-20 Helice et systeme d'helices contrarotatives comprenant des moyens ameliores de limitation du calage, et turbomachine les comprenant

Publications (2)

Publication Number Publication Date
FR2964945A1 FR2964945A1 (fr) 2012-03-23
FR2964945B1 true FR2964945B1 (fr) 2012-10-19

Family

ID=43923661

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1057504A Active FR2964945B1 (fr) 2010-09-20 2010-09-20 Helice et systeme d'helices contrarotatives comprenant des moyens ameliores de limitation du calage, et turbomachine les comprenant

Country Status (2)

Country Link
US (1) US9260179B2 (fr)
FR (1) FR2964945B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3011048B1 (fr) * 2013-09-24 2016-05-13 Snecma Dispositif d'alimentation en fluide hydraulique d'un verin et mecanisme de commande de pas des pales d'une helice de turbomoteur comportant le verin
US10472050B2 (en) 2016-08-31 2019-11-12 Honeywell International Inc. Propeller pitch control actuation system
US10747235B2 (en) * 2018-04-25 2020-08-18 The Boeing Company Pitch trim prediction for aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2309744A1 (fr) * 1975-04-30 1976-11-26 Ratier Sa Forest Dispositif de commande de variation du pas des pales d'un ventilateur
GB8723246D0 (en) * 1987-10-03 1987-11-04 Dowty Rotol Ltd Bladed rotor assemblies
US5242265A (en) * 1990-07-23 1993-09-07 General Electric Company Aircraft pitch change mechanism
DE4117735C1 (fr) * 1991-05-30 1992-10-29 Mercedes-Benz Aktiengesellschaft, 7000 Stuttgart, De
GB0821783D0 (en) 2008-12-01 2009-01-07 Rolls Royce Plc Blade pitch control system

Also Published As

Publication number Publication date
US20120070291A1 (en) 2012-03-22
US9260179B2 (en) 2016-02-16
FR2964945A1 (fr) 2012-03-23

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