FR3005489B1 - Dispositif de commande d'une tuyere a section variable d'un aeronef - Google Patents
Dispositif de commande d'une tuyere a section variable d'un aeronefInfo
- Publication number
- FR3005489B1 FR3005489B1 FR1354201A FR1354201A FR3005489B1 FR 3005489 B1 FR3005489 B1 FR 3005489B1 FR 1354201 A FR1354201 A FR 1354201A FR 1354201 A FR1354201 A FR 1354201A FR 3005489 B1 FR3005489 B1 FR 3005489B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- controlling
- variable section
- section tube
- tube
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
- F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
-
- 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
- F05D2260/40—Transmission of power
-
- 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
- F05D2260/50—Kinematic linkage, i.e. transmission of position
- F05D2260/57—Kinematic linkage, i.e. transmission of position using servos, independent actuators, etc.
-
- 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
- F05D2260/84—Redundancy
-
- 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
- F05D2260/90—Braking
- F05D2260/902—Braking using frictional mechanical forces
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Multiple Motors (AREA)
- Control Of Position Or Direction (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1354201A FR3005489B1 (fr) | 2013-05-07 | 2013-05-07 | Dispositif de commande d'une tuyere a section variable d'un aeronef |
US14/269,815 US9657685B2 (en) | 2013-05-07 | 2014-05-05 | Device for controlling a nozzle of variable cross-section of an aircraft |
CN201410189843.0A CN104141554B (zh) | 2013-05-07 | 2014-05-07 | 用于控制航空器的具有可变横截面的喷嘴的装置 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1354201A FR3005489B1 (fr) | 2013-05-07 | 2013-05-07 | Dispositif de commande d'une tuyere a section variable d'un aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3005489A1 FR3005489A1 (fr) | 2014-11-14 |
FR3005489B1 true FR3005489B1 (fr) | 2017-03-17 |
Family
ID=48782476
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1354201A Expired - Fee Related FR3005489B1 (fr) | 2013-05-07 | 2013-05-07 | Dispositif de commande d'une tuyere a section variable d'un aeronef |
Country Status (3)
Country | Link |
---|---|
US (1) | US9657685B2 (fr) |
CN (1) | CN104141554B (fr) |
FR (1) | FR3005489B1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110823578A (zh) * | 2019-10-25 | 2020-02-21 | 中国航发北京航科发动机控制系统科技有限公司 | 一种航空发动机喷嘴的模拟试验装置 |
CN111852685B (zh) * | 2020-05-25 | 2021-09-24 | 北京动力机械研究所 | 一种直线运动构件的指定极限位置限制装置 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2986003A (en) * | 1957-04-04 | 1961-05-30 | Napier & Son Ltd | Fuel supply systems for compound ramjet-turborocket engines |
US3814537A (en) * | 1972-09-22 | 1974-06-04 | Gen Motors Corp | Turbine nozzle control |
FR2444505A1 (fr) | 1978-12-22 | 1980-07-18 | Air Ind | Procede et dispositif de deplacement alternatif d'appareils automatiques de projection de produits de revetement |
US4985666A (en) | 1988-08-30 | 1991-01-15 | Sony Corporation | Safety device for video cassette recorder |
US5467613A (en) | 1994-04-05 | 1995-11-21 | Carrier Corporation | Two phase flow turbine |
JPH09195853A (ja) | 1995-12-14 | 1997-07-29 | United Technol Corp <Utc> | 可変面積ファンエキゾーストノズル |
US6439504B1 (en) | 2001-06-15 | 2002-08-27 | Honeywell International, Inc. | System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system |
US6684623B2 (en) * | 2002-02-27 | 2004-02-03 | Honeywell International, Inc. | Gearless electric thrust reverser actuators and actuation system incorporating same |
US7127880B2 (en) * | 2003-08-29 | 2006-10-31 | The Nordam Group, Inc. | Induction coupled variable nozzle |
FR2925607B1 (fr) * | 2007-12-21 | 2013-05-10 | Aircelle Sa | Nacelle pour moteur d'aeronef a tuyere de section variable |
FR2927309B1 (fr) | 2008-02-13 | 2010-04-16 | Aircelle Sa | Systeme de commande pour nacelle de turboreacteur |
EP2239449B1 (fr) * | 2009-04-06 | 2015-09-30 | Rohr, Inc. | Ensemble de nacelle pour moteurs d'avion à réacteur à double flux |
GB201002315D0 (en) * | 2010-02-11 | 2010-03-31 | Goodrich Actuation Systems Ltd | Control system |
FR2960600B1 (fr) * | 2010-06-01 | 2013-10-25 | Aircelle Sa | Systeme d'actionnement d'un dispositif d'inversion de poussee |
FR2960917B1 (fr) * | 2010-06-03 | 2012-05-18 | Aircelle Sa | Inverseur de poussee a section de tuyere variable verrouillable |
US20120139531A1 (en) * | 2010-12-07 | 2012-06-07 | Hamilton Sundstrand Corporation | Position detecting system |
US8615982B2 (en) * | 2011-07-05 | 2013-12-31 | Hamilton Sundstrand Corporation | Integrated electric variable area fan nozzle thrust reversal actuation system |
FR3005488B1 (fr) | 2013-05-07 | 2015-05-29 | Airbus Operations Sas | Dispositif de commande d'une tuyere a section variable d'un aeronef |
-
2013
- 2013-05-07 FR FR1354201A patent/FR3005489B1/fr not_active Expired - Fee Related
-
2014
- 2014-05-05 US US14/269,815 patent/US9657685B2/en not_active Expired - Fee Related
- 2014-05-07 CN CN201410189843.0A patent/CN104141554B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN104141554B (zh) | 2017-07-11 |
US9657685B2 (en) | 2017-05-23 |
CN104141554A (zh) | 2014-11-12 |
FR3005489A1 (fr) | 2014-11-14 |
US20160003188A1 (en) | 2016-01-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLFP | Fee payment |
Year of fee payment: 5 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
ST | Notification of lapse |
Effective date: 20210105 |