FR2992685B1 - Procede de commande d'une section de tuyere variable d'un aeronef - Google Patents
Procede de commande d'une section de tuyere variable d'un aeronefInfo
- Publication number
- FR2992685B1 FR2992685B1 FR1256305A FR1256305A FR2992685B1 FR 2992685 B1 FR2992685 B1 FR 2992685B1 FR 1256305 A FR1256305 A FR 1256305A FR 1256305 A FR1256305 A FR 1256305A FR 2992685 B1 FR2992685 B1 FR 2992685B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- controlling
- pipe section
- variable pipe
- variable
- 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
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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
-
- 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/05—Purpose of the control system to affect the output of the engine
- F05D2270/051—Thrust
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Navigation (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1256305A FR2992685B1 (fr) | 2012-07-02 | 2012-07-02 | Procede de commande d'une section de tuyere variable d'un aeronef |
RU2015101781A RU2015101781A (ru) | 2012-07-02 | 2013-06-27 | Способ управления соплом переменного сечения летательного аппарата |
BR112014033049A BR112014033049A2 (pt) | 2012-07-02 | 2013-06-27 | método para controlar uma posição de uma seção de bocal variável de uma aeronave |
CN201380035244.7A CN104411959A (zh) | 2012-07-02 | 2013-06-27 | 用于控制航空器可变喷嘴截面的方法 |
PCT/FR2013/051498 WO2014006303A1 (fr) | 2012-07-02 | 2013-06-27 | Procédé de commande d'une section de tuyère variable d'un aéronef |
CA 2877836 CA2877836A1 (fr) | 2012-07-02 | 2013-06-27 | Procede de commande d'une section de tuyere variable d'un aeronef |
EP13744642.3A EP2867511A1 (fr) | 2012-07-02 | 2013-06-27 | Procédé de commande d'une section de tuyère variable d'un aéronef |
US14/584,435 US10036348B2 (en) | 2012-07-02 | 2014-12-29 | Method for controlling a variable nozzle section of an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1256305A FR2992685B1 (fr) | 2012-07-02 | 2012-07-02 | Procede de commande d'une section de tuyere variable d'un aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2992685A1 FR2992685A1 (fr) | 2014-01-03 |
FR2992685B1 true FR2992685B1 (fr) | 2016-05-27 |
Family
ID=46785698
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1256305A Active FR2992685B1 (fr) | 2012-07-02 | 2012-07-02 | Procede de commande d'une section de tuyere variable d'un aeronef |
Country Status (8)
Country | Link |
---|---|
US (1) | US10036348B2 (fr) |
EP (1) | EP2867511A1 (fr) |
CN (1) | CN104411959A (fr) |
BR (1) | BR112014033049A2 (fr) |
CA (1) | CA2877836A1 (fr) |
FR (1) | FR2992685B1 (fr) |
RU (1) | RU2015101781A (fr) |
WO (1) | WO2014006303A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106194494B (zh) * | 2016-08-09 | 2018-01-05 | 南京理工大学 | 一种用于微型涡喷发动机加力燃烧室的可调喷管 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4106730A (en) * | 1976-10-01 | 1978-08-15 | The Boeing Company | Engine out control system for STOL aircraft |
US5706649A (en) * | 1995-04-03 | 1998-01-13 | Boeing North American, Inc. | Multi axis thrust vectoring for turbo fan engines |
FR2927309B1 (fr) * | 2008-02-13 | 2010-04-16 | Aircelle Sa | Systeme de commande pour nacelle de turboreacteur |
FR2930973B1 (fr) * | 2008-05-06 | 2010-04-23 | Airbus France | Procede et dispositif de mise en oeuvre des inverseurs de poussee d'un aeronef |
FR2932226B1 (fr) * | 2008-06-06 | 2013-08-23 | Aircelle Sa | Procede de synchronisation des actionneurs d'un capot mobile d'inverseur de poussee |
FR2958910B1 (fr) * | 2010-04-20 | 2012-04-27 | Aircelle Sa | Nacelle pour moteur d'aeronef a tuyere de section variable |
US8978356B2 (en) * | 2010-12-03 | 2015-03-17 | The Boeing Company | Thrust reverser and variable area fan nozzle actuation system and method |
US8713911B2 (en) * | 2010-12-15 | 2014-05-06 | Woodward Hrt, Inc. | System and method for operating a thrust reverser for a turbofan propulsion system |
EP2466102A1 (fr) * | 2010-12-17 | 2012-06-20 | Ecopra | Dispositif de traitement d'un mélange gaz d'échappement/eau préalablement à son injection dans un moteur thermique et véhicule équipé d'un tel dispositif |
-
2012
- 2012-07-02 FR FR1256305A patent/FR2992685B1/fr active Active
-
2013
- 2013-06-27 BR BR112014033049A patent/BR112014033049A2/pt not_active IP Right Cessation
- 2013-06-27 CN CN201380035244.7A patent/CN104411959A/zh active Pending
- 2013-06-27 WO PCT/FR2013/051498 patent/WO2014006303A1/fr active Application Filing
- 2013-06-27 EP EP13744642.3A patent/EP2867511A1/fr not_active Withdrawn
- 2013-06-27 CA CA 2877836 patent/CA2877836A1/fr not_active Abandoned
- 2013-06-27 RU RU2015101781A patent/RU2015101781A/ru not_active Application Discontinuation
-
2014
- 2014-12-29 US US14/584,435 patent/US10036348B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN104411959A (zh) | 2015-03-11 |
RU2015101781A (ru) | 2016-08-20 |
BR112014033049A2 (pt) | 2017-06-27 |
CA2877836A1 (fr) | 2014-01-09 |
WO2014006303A1 (fr) | 2014-01-09 |
US20150108235A1 (en) | 2015-04-23 |
EP2867511A1 (fr) | 2015-05-06 |
FR2992685A1 (fr) | 2014-01-03 |
US10036348B2 (en) | 2018-07-31 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 4 |
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Year of fee payment: 5 |
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Year of fee payment: 6 |
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CD | Change of name or company name |
Owner name: SAFRAN NACELLES, FR Effective date: 20180125 |
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Year of fee payment: 7 |
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Year of fee payment: 11 |
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PLFP | Fee payment |
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