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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
Application number
FR0856971A
Other languages
English (en)
Other versions
FR2937092A1 (fr
Inventor
Gonidec Serge Le
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 FR0856971A priority Critical patent/FR2937092B1/fr
Priority to DE102009045704A priority patent/DE102009045704A1/de
Priority to ITTO2009A000781A priority patent/IT1396075B1/it
Priority to US12/578,809 priority patent/US8364374B2/en
Priority to JP2009254416A priority patent/JP5528771B2/ja
Publication of FR2937092A1 publication Critical patent/FR2937092A1/fr
Application granted granted Critical
Publication of FR2937092B1 publication Critical patent/FR2937092B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/56Control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/56Control
    • F02K9/563Control of propellant feed pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/94Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/95Rocket-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)
FR0856971A 2008-10-15 2008-10-15 Procede et dispositif de calcul d'une sequence de demarrage ou d'arret d'un moteur. Active FR2937092B1 (fr)

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)

* Cited by examiner, † Cited by third party
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

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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

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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