FR2937092B1 - Procede et dispositif de calcul d'une sequence de demarrage ou d'arret d'un moteur. - Google Patents
Procede et dispositif de calcul d'une sequence de demarrage ou d'arret d'un moteur.Info
- Publication number
- FR2937092B1 FR2937092B1 FR0856971A FR0856971A FR2937092B1 FR 2937092 B1 FR2937092 B1 FR 2937092B1 FR 0856971 A FR0856971 A FR 0856971A FR 0856971 A FR0856971 A FR 0856971A FR 2937092 B1 FR2937092 B1 FR 2937092B1
- Authority
- FR
- France
- Prior art keywords
- stopping
- calculating
- engine
- starting
- sequence
- 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
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/56—Control
-
- 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/56—Control
- F02K9/563—Control of propellant feed pumps
-
- 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
- F02K9/94—Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants
-
- 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
- F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0856971A FR2937092B1 (fr) | 2008-10-15 | 2008-10-15 | Procede et dispositif de calcul d'une sequence de demarrage ou d'arret d'un moteur. |
DE102009045704A DE102009045704A1 (de) | 2008-10-15 | 2009-10-14 | Verfahren und Vorrichtung zur Berechnung einer Start- oder Stopsequenz eines Motors |
ITTO2009A000781A IT1396075B1 (it) | 2008-10-15 | 2009-10-14 | Metodo e dispositivo per calcolare una sequenza di avviamento o di arresto per un motore |
US12/578,809 US8364374B2 (en) | 2008-10-15 | 2009-10-14 | Method and a device for calculating a starting or stop sequence for an engine |
JP2009254416A JP5528771B2 (ja) | 2008-10-15 | 2009-10-15 | エンジンの始動シーケンス又は停止シーケンスの計算方法及び装置 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0856971A FR2937092B1 (fr) | 2008-10-15 | 2008-10-15 | Procede et dispositif de calcul d'une sequence de demarrage ou d'arret d'un moteur. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2937092A1 FR2937092A1 (fr) | 2010-04-16 |
FR2937092B1 true FR2937092B1 (fr) | 2010-12-10 |
Family
ID=40677743
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0856971A Active FR2937092B1 (fr) | 2008-10-15 | 2008-10-15 | Procede et dispositif de calcul d'une sequence de demarrage ou d'arret d'un moteur. |
Country Status (5)
Country | Link |
---|---|
US (1) | US8364374B2 (fr) |
JP (1) | JP5528771B2 (fr) |
DE (1) | DE102009045704A1 (fr) |
FR (1) | FR2937092B1 (fr) |
IT (1) | IT1396075B1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2604839B1 (fr) * | 2011-12-16 | 2016-05-25 | Astrium GmbH | Moteur |
FR2991072B1 (fr) * | 2012-05-28 | 2014-06-20 | Snecma | Systeme et methode de traitement d'informations pour la surveillance d'un systeme complexe |
FR2997454B1 (fr) * | 2012-10-30 | 2014-12-12 | Snecma | Procede et systeme de detection d'allumage |
FR3016412B1 (fr) * | 2014-01-10 | 2016-02-05 | Snecma | Procede de commande d'ensemble propulsif |
FR3042227B1 (fr) * | 2015-10-08 | 2020-04-03 | Arianegroup Sas | Procede et circuit de regulation de moteur-fusee |
US11181076B2 (en) * | 2016-03-03 | 2021-11-23 | Kevin Michael Weldon | Rocket engine bipropellant supply system including an electrolyzer |
DE102016208729A1 (de) | 2016-05-20 | 2017-11-23 | Airbus Ds Gmbh | Verfahren zum Betreiben eines Raketenantriebssystems und Raketenantriebssystem |
RU2674112C1 (ru) * | 2017-12-25 | 2018-12-04 | Акционерное общество "Корпорация "Московский институт теплотехники" (АО "Корпорация "МИТ") | Способ экспериментального определения параметров запуска двигателя при стендовых испытаниях |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3171250A (en) * | 1961-02-06 | 1965-03-02 | Aerojet General Co | Malfunction control system |
US3851157A (en) * | 1973-07-09 | 1974-11-26 | United Aircraft Corp | Self-correcting feedback control system |
JPS60195333A (ja) * | 1984-03-15 | 1985-10-03 | Sanyo Denki Seisakusho:Kk | ガスタ−ビンエンジンの自動制御装置 |
US4618931A (en) * | 1984-03-21 | 1986-10-21 | The United States Of America As Represented By The Secretary Of The Air Force | Gas generator fuel flow throttle control system |
JPS62261652A (ja) * | 1986-05-07 | 1987-11-13 | Natl Space Dev Agency Japan<Nasda> | 液体ロケツトエンジン |
US5070691A (en) * | 1988-08-03 | 1991-12-10 | Thiokol Corporation | Solid propellant canister loaded multiple pulsed or staged rocket |
JPH03210608A (ja) * | 1990-01-16 | 1991-09-13 | Mitsubishi Heavy Ind Ltd | タンク圧力制御装置 |
US5148674A (en) * | 1990-01-26 | 1992-09-22 | Morris Brian G | Method and apparatus for providing real-time control of a gaseous propellant rocket propulsion system |
JP2799792B2 (ja) * | 1991-10-05 | 1998-09-21 | 川崎重工業株式会社 | ガスタービン起動制御方式 |
FR2697587B1 (fr) * | 1992-11-04 | 1995-01-20 | Europ Propulsion | Système optimisé d'alimentation de moteur fusée réallumable. |
US5873240A (en) * | 1993-04-14 | 1999-02-23 | Adroit Systems, Inc. | Pulsed detonation rocket engine |
JPH10238408A (ja) * | 1997-02-21 | 1998-09-08 | Ishikawajima Harima Heavy Ind Co Ltd | エキスパンダサイクルエンジン |
US6321721B1 (en) * | 1999-01-29 | 2001-11-27 | Denso Corporation | Apparatus for detecting the fuel property for an internal combustion engine |
US7542885B1 (en) * | 1999-05-07 | 2009-06-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method and apparatus for predicting unsteady pressure and flow rate distribution in a fluid network |
US20080000215A1 (en) * | 2000-03-02 | 2008-01-03 | Duncan Ronnie J | Engine systems and methods |
US6619031B1 (en) * | 2000-04-27 | 2003-09-16 | Vladimir V. Balepin | Multi-mode multi-propellant liquid rocket engine |
WO2003008792A1 (fr) * | 2001-07-18 | 2003-01-30 | Jae-Chang Lee | Turboreacteur utilisant des gaz d'echappement |
US7997060B2 (en) * | 2002-03-15 | 2011-08-16 | Pratt & Whitney Rocketdyne, Inc. | Rocket engine power cycle |
US6968695B2 (en) * | 2002-09-13 | 2005-11-29 | The Boeing Company | Compact lightweight ramjet engines incorporating swirl augmented combustion with improved performance |
US6907724B2 (en) * | 2002-09-13 | 2005-06-21 | The Boeing Company | Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance |
US20050151107A1 (en) * | 2003-12-29 | 2005-07-14 | Jianchao Shu | Fluid control system and stem joint |
US7685973B2 (en) * | 2004-01-26 | 2010-03-30 | Anju Nelson | Water engine and method |
US20050160735A1 (en) * | 2004-01-26 | 2005-07-28 | Anju Nelson | Water hydrogen engine system |
JP4092405B2 (ja) * | 2004-08-04 | 2008-05-28 | 防衛省技術研究本部長 | ラムロケットエンジンの二次燃焼着火制御方法及びラムロケットエンジンを搭載した高速飛しょう体 |
FR2917799B1 (fr) * | 2007-06-19 | 2009-10-02 | Snecma Sa | Vanne a longue course de regulation avec fonction d'arret. |
US8612107B2 (en) * | 2008-06-10 | 2013-12-17 | The Regents Of The University Of Michigan | Method, control apparatus and powertrain system controller for real-time, self-learning control based on individual operating style |
-
2008
- 2008-10-15 FR FR0856971A patent/FR2937092B1/fr active Active
-
2009
- 2009-10-14 DE DE102009045704A patent/DE102009045704A1/de not_active Ceased
- 2009-10-14 US US12/578,809 patent/US8364374B2/en not_active Expired - Fee Related
- 2009-10-14 IT ITTO2009A000781A patent/IT1396075B1/it active
- 2009-10-15 JP JP2009254416A patent/JP5528771B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
IT1396075B1 (it) | 2012-11-09 |
US20100094522A1 (en) | 2010-04-15 |
FR2937092A1 (fr) | 2010-04-16 |
JP5528771B2 (ja) | 2014-06-25 |
US8364374B2 (en) | 2013-01-29 |
ITTO20090781A1 (it) | 2010-04-16 |
JP2010096183A (ja) | 2010-04-30 |
DE102009045704A1 (de) | 2010-04-29 |
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