TR201903517T4 - Gaz Tahliye Bölümünün Modülasyonu için Tertibat. - Google Patents

Gaz Tahliye Bölümünün Modülasyonu için Tertibat. Download PDF

Info

Publication number
TR201903517T4
TR201903517T4 TR2019/03517T TR201903517T TR201903517T4 TR 201903517 T4 TR201903517 T4 TR 201903517T4 TR 2019/03517 T TR2019/03517 T TR 2019/03517T TR 201903517 T TR201903517 T TR 201903517T TR 201903517 T4 TR201903517 T4 TR 201903517T4
Authority
TR
Turkey
Prior art keywords
setup
modulation
gas discharge
discharge section
propellants
Prior art date
Application number
TR2019/03517T
Other languages
English (en)
Inventor
Clermont Mathieu
Remigi Alain
Larrieu Jean-Michel
Marlin Philippe
Original Assignee
Arianegroup 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 Arianegroup Sas filed Critical Arianegroup Sas
Publication of TR201903517T4 publication Critical patent/TR201903517T4/tr

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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/26—Burning control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Plasma Technology (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

Gaz Tahliye Bölümünün Modülasyonu için Tertibat. Mevcut buluş füze, fırlatıcı veya uydu gibi uzay araçlarının pilotajı için gaz reaksiyonu veya tahliyesi yoluyla itme ilkesini kullanarak itme meydana getirecek yapıdaki iticilerin veya roket motorlarının genel alanına ilişkindir. Buluş daha özel olarak, katı yakıtlı iticilerle donatılı sabit ıraksak bölümlü nozülleri amaçlar.
TR2019/03517T 2013-03-07 2014-03-04 Gaz Tahliye Bölümünün Modülasyonu için Tertibat. TR201903517T4 (tr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1300515A FR3002982B1 (fr) 2013-03-07 2013-03-07 Dispositif de modulation de section d'ejection de gaz.

Publications (1)

Publication Number Publication Date
TR201903517T4 true TR201903517T4 (tr) 2019-04-22

Family

ID=48795597

Family Applications (1)

Application Number Title Priority Date Filing Date
TR2019/03517T TR201903517T4 (tr) 2013-03-07 2014-03-04 Gaz Tahliye Bölümünün Modülasyonu için Tertibat.

Country Status (8)

Country Link
US (1) US9541031B2 (tr)
EP (1) EP2964947B1 (tr)
JP (1) JP6285967B2 (tr)
KR (1) KR102137785B1 (tr)
FR (1) FR3002982B1 (tr)
IL (1) IL240899B (tr)
TR (1) TR201903517T4 (tr)
WO (1) WO2014135789A1 (tr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3030634B1 (fr) 2014-12-17 2021-09-24 Herakles Dispositif de modulation de section d'ejection de gaz

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2583570A (en) * 1945-06-28 1952-01-29 Clarence N Hickman Nozzle for rocket motors
US2637973A (en) * 1949-04-01 1953-05-12 Reaction Motors Inc Rocket engine having turbine located in nozzle for driving auxiliaries
US3073112A (en) * 1959-09-21 1963-01-15 Olin Mathieson Rocket motor control system
US3230704A (en) * 1961-10-30 1966-01-25 Thiokol Chemical Corp Rocket engine
US3150485A (en) * 1961-11-24 1964-09-29 Frederick R Hickerson Variable thrust rocket engine
US3608312A (en) * 1969-10-22 1971-09-28 Us Navy Self-actuated dual area annular nozzle
GB2156290B (en) * 1984-03-27 1988-06-02 British Aerospace Rockets and rocket motors
JPH0658090B2 (ja) * 1988-03-28 1994-08-03 防衛庁技術研究本部長 ロケットエンジン燃焼ガス流量の制御方法
US5491973A (en) * 1994-10-17 1996-02-20 Aerojet General Corporation Self-actuating control for rocket motor nozzle
FR2740105B1 (fr) * 1995-10-20 1998-01-16 Europ Propulsion Dispositif de pilotage d'un vehicule spatial par vannage de gaz

Also Published As

Publication number Publication date
US20160010591A1 (en) 2016-01-14
EP2964947B1 (fr) 2018-12-12
IL240899B (en) 2018-04-30
EP2964947A1 (fr) 2016-01-13
IL240899A0 (en) 2015-10-29
KR102137785B1 (ko) 2020-07-27
KR20150122793A (ko) 2015-11-02
FR3002982B1 (fr) 2015-04-10
US9541031B2 (en) 2017-01-10
JP2016513769A (ja) 2016-05-16
JP6285967B2 (ja) 2018-02-28
WO2014135789A1 (fr) 2014-09-12
FR3002982A1 (fr) 2014-09-12

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