BRPI0908752A2 - Sistema de hélices contra-rotativas para turbomáquina de aeronave, turbomáquina para aeronave e processo de pilotagem de hélices contra-rotativas para turbomáquina de aeronave - Google Patents

Sistema de hélices contra-rotativas para turbomáquina de aeronave, turbomáquina para aeronave e processo de pilotagem de hélices contra-rotativas para turbomáquina de aeronave

Info

Publication number
BRPI0908752A2
BRPI0908752A2 BRPI0908752-4A BRPI0908752A BRPI0908752A2 BR PI0908752 A2 BRPI0908752 A2 BR PI0908752A2 BR PI0908752 A BRPI0908752 A BR PI0908752A BR PI0908752 A2 BRPI0908752 A2 BR PI0908752A2
Authority
BR
Brazil
Prior art keywords
counter
aircraft turbomachine
propeller
rotating
rotary
Prior art date
Application number
BRPI0908752-4A
Other languages
English (en)
Inventor
François Gallet
Original Assignee
Snecma
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 filed Critical Snecma
Publication of BRPI0908752A2 publication Critical patent/BRPI0908752A2/pt
Publication of BRPI0908752B1 publication Critical patent/BRPI0908752B1/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Discharge By Other Means (AREA)
  • Control Of Turbines (AREA)
  • Transmission Devices (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Retarders (AREA)
BRPI0908752-4A 2008-03-21 2009-03-20 Sistema de hélices contra-rotativas para turbomáquina de aeronave, turbomáquina para aeronave e processo de pilotagem de um sistema de hélices contra-rotativas para turbomáquina de aeronave BRPI0908752B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0851848A FR2928977B1 (fr) 2008-03-21 2008-03-21 Systeme d'helices contrarotatives disposant d'un dispositif de mise en drapeau des pales d'helices
FR08/51848 2008-03-21
PCT/EP2009/053280 WO2009115593A1 (fr) 2008-03-21 2009-03-20 Systeme d'helices contrarotatives disposant d'un dispositif de mise en drapeau des pales d'helices

Publications (2)

Publication Number Publication Date
BRPI0908752A2 true BRPI0908752A2 (pt) 2015-07-21
BRPI0908752B1 BRPI0908752B1 (pt) 2019-09-24

Family

ID=40349959

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0908752-4A BRPI0908752B1 (pt) 2008-03-21 2009-03-20 Sistema de hélices contra-rotativas para turbomáquina de aeronave, turbomáquina para aeronave e processo de pilotagem de um sistema de hélices contra-rotativas para turbomáquina de aeronave

Country Status (11)

Country Link
US (1) US8444388B2 (pt)
EP (1) EP2260197B1 (pt)
JP (1) JP5260725B2 (pt)
CN (1) CN101978150B (pt)
AT (1) ATE548554T1 (pt)
BR (1) BRPI0908752B1 (pt)
CA (1) CA2718619C (pt)
ES (1) ES2383270T3 (pt)
FR (1) FR2928977B1 (pt)
RU (1) RU2488520C2 (pt)
WO (1) WO2009115593A1 (pt)

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US8096750B2 (en) * 2009-03-30 2012-01-17 Ocean Renewable Power Company, Llc High efficiency turbine and method of generating power
CN102353512B (zh) * 2011-07-22 2014-10-01 北京航空航天大学 基于多台电机同步运行的攻角控制方法和多功能支撑装置
US9188355B1 (en) 2012-01-03 2015-11-17 Digital Control Systems, Inc. Fan array control system
WO2014066503A1 (en) * 2012-10-23 2014-05-01 General Electric Company Unducted thrust producing system
CN102935893B (zh) * 2012-11-29 2016-01-06 中国南方航空工业(集团)有限公司 发动机的顺桨停车保护方法和顺桨停车保护装置
CN103171760B (zh) * 2013-03-25 2015-12-23 贾小平 垂直升降陆空两用车螺旋桨变距装置
GB201408103D0 (en) * 2014-05-08 2014-06-25 Rolls Royce Plc A system
FR3024179B1 (fr) 2014-07-25 2016-08-26 Snecma Systeme d'alimentation en air sous pression installe dans une turbomachine d'aeronef comportant des moyens d'etancheite
CN104494811B (zh) * 2014-12-14 2018-02-06 惠阳航空螺旋桨有限责任公司 螺旋桨的伺服变距装置
CN104554708B (zh) * 2014-12-14 2018-02-06 惠阳航空螺旋桨有限责任公司 一种螺旋桨的电子变距装置的变距执行机构
EP3193006B1 (en) * 2016-01-12 2019-05-15 GE Renewable Technologies Device for reversing a blade of a runner unit
FR3050432B1 (fr) 2016-04-20 2018-04-13 Safran Aircraft Engines Systeme d'actionnement de pas pour une helice de turbomachine
FR3050431B1 (fr) * 2016-04-20 2018-04-27 Safran Aircraft Engines Systeme d'actionnement simplifie de pas pour une helice de turbomachine
US10843790B2 (en) * 2016-08-01 2020-11-24 Kitty Hawk Corporation Bistable pitch propeller system with bidirectional propeller rotation
FR3060523B1 (fr) * 2016-12-21 2019-05-17 Safran Aircraft Engines Systeme d'actionnement electromecanique de pas pour une helice de turbomachine
US9994305B1 (en) * 2017-04-14 2018-06-12 Swift Engineering, Inc. Coaxial drive propulsion system for aerial vehicles, and associated systems and methods
IT201900003999A1 (it) 2019-03-19 2020-09-19 Ge Avio Srl Valvola di comando combinato per sovra-velocita', messa in bandiera ed abilitazione di inversione per un gruppo elica
CN110040240B (zh) * 2019-05-24 2023-09-22 安阳市豪克航空科技有限公司 单驱动螺旋桨变距、顺桨、停桨位锁定系统
CN111114764B (zh) * 2020-02-10 2024-04-19 中国工程物理研究院总体工程研究所 无人机抛弃式螺旋桨变换装置
CN111706432B (zh) * 2020-05-28 2022-03-25 中国航发湖南动力机械研究所 桨扇发动机及具有其的推进装置
CN112429203A (zh) * 2020-11-20 2021-03-02 惠阳航空螺旋桨有限责任公司 一种螺旋桨变距连杆机构
FR3149295A1 (fr) * 2023-06-02 2024-12-06 Safran Electronics & Defense Module de soufflante pour une turbomachine d’aeronef

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SU1312A1 (ru) * 1925-02-07 1926-05-31 Бристольская Аэропланная Компания с огр. отв. Гребной винт с переменным шагом
FR50123E (fr) * 1938-08-17 1939-12-13 Propulseur à couple de réaction nul
FR985976A (fr) * 1943-11-22 1951-07-25 Mécanismes à engrenages permettant le décalage angulaire d'organes tournants et applications de tels mécanismes, notamment en aéronautique
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FR1114232A (fr) * 1953-12-04 1956-04-10 Gen Motors Corp Dispositif à hélices à pas variable tournant en sens inverse
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DE3941852A1 (de) * 1989-12-19 1991-06-20 Mtu Muenchen Gmbh Propfantriebwerk mit zwei entgegengesetzt drehenden fanrotoren
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RU2099242C1 (ru) * 1996-10-17 1997-12-20 Йелстаун Корпорейшн Н.В. Воздушный винт изменяемого шага и способ измерения углового положения его лопастей
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Also Published As

Publication number Publication date
CA2718619A1 (fr) 2009-09-24
EP2260197A1 (fr) 2010-12-15
RU2488520C2 (ru) 2013-07-27
BRPI0908752B1 (pt) 2019-09-24
US8444388B2 (en) 2013-05-21
CN101978150A (zh) 2011-02-16
WO2009115593A1 (fr) 2009-09-24
CN101978150B (zh) 2013-06-12
JP5260725B2 (ja) 2013-08-14
CA2718619C (fr) 2015-12-22
ES2383270T3 (es) 2012-06-19
FR2928977A1 (fr) 2009-09-25
RU2010143010A (ru) 2012-04-27
EP2260197B1 (fr) 2012-03-07
JP2011515265A (ja) 2011-05-19
FR2928977B1 (fr) 2010-04-09
US20110014046A1 (en) 2011-01-20
ATE548554T1 (de) 2012-03-15

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]