ATE531923T1 - Einspritzvorrichtung für monoergol mit starker durchflussmodulation - Google Patents

Einspritzvorrichtung für monoergol mit starker durchflussmodulation

Info

Publication number
ATE531923T1
ATE531923T1 AT09164989T AT09164989T ATE531923T1 AT E531923 T1 ATE531923 T1 AT E531923T1 AT 09164989 T AT09164989 T AT 09164989T AT 09164989 T AT09164989 T AT 09164989T AT E531923 T1 ATE531923 T1 AT E531923T1
Authority
AT
Austria
Prior art keywords
wall
monoergol
injection device
channel
flow modulation
Prior art date
Application number
AT09164989T
Other languages
English (en)
Inventor
Herve Goislot
Original Assignee
Snecma
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 filed Critical Snecma
Application granted granted Critical
Publication of ATE531923T1 publication Critical patent/ATE531923T1/de

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
    • F02K9/52—Injectors
    • 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
    • F02K9/58—Propellant feed valves
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
    • 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
    • F05D2260/52—Kinematic linkage, i.e. transmission of position involving springs

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Massaging Devices (AREA)
  • Surgical Instruments (AREA)
  • Infusion, Injection, And Reservoir Apparatuses (AREA)
AT09164989T 2008-07-11 2009-07-09 Einspritzvorrichtung für monoergol mit starker durchflussmodulation ATE531923T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0854777A FR2933741B1 (fr) 2008-07-11 2008-07-11 Dispositif d'injection de monoergol a forte modulation du debit.

Publications (1)

Publication Number Publication Date
ATE531923T1 true ATE531923T1 (de) 2011-11-15

Family

ID=40429914

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09164989T ATE531923T1 (de) 2008-07-11 2009-07-09 Einspritzvorrichtung für monoergol mit starker durchflussmodulation

Country Status (4)

Country Link
US (1) US8596039B2 (de)
EP (1) EP2143928B1 (de)
AT (1) ATE531923T1 (de)
FR (1) FR2933741B1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100968878B1 (ko) * 2010-04-02 2011-05-31 (주)제이제이테크 추진기관의 추진제 처리장비
CN101956981B (zh) * 2010-07-08 2012-05-23 中国航天科技集团公司第六研究院第十一研究所 一种气液组元高室压大范围变工况燃烧器
US8966879B1 (en) * 2012-02-15 2015-03-03 Orbital Technologies Corporation Acoustic igniter
KR101631891B1 (ko) 2014-12-18 2016-06-20 한국항공우주연구원 핀틀-스월 혼합형 추진제 분사장치
DE102020122337A1 (de) * 2020-08-26 2022-03-03 LabOrbital GmbH Heißgaserzeugungsvorrichtung mit monergolem ionischen Treibstoff und Niederspannungsanzündung
KR102472925B1 (ko) 2020-11-25 2022-11-30 한국항공우주연구원 핀틀 분사기
CN114607530B (zh) * 2022-03-31 2024-04-19 西安航天动力研究所 一种采用机械调节喷注面积的针栓式喷注器
CN115355107B (zh) * 2022-03-31 2024-08-09 西安航天动力研究所 一种实现快速优化调整的栓式喷注器中心路装置
CN115419519B (zh) * 2022-11-03 2023-02-07 西安航天动力研究所 一种变推力针栓式喷注器

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3074231A (en) * 1960-03-30 1963-01-22 Klein David Marshall Annular stream variable area injector
US3431733A (en) 1966-07-05 1969-03-11 Joseph T Hamrick Two-step rocket propellant injection system
US3464633A (en) * 1967-11-16 1969-09-02 Trw Inc Multiple fluid controlling shear valve
US3897008A (en) * 1969-09-24 1975-07-29 Us Navy Liquid fuel injector system
US3742701A (en) * 1971-06-16 1973-07-03 Us Navy Propellant injector assembly
US4000613A (en) * 1975-02-13 1977-01-04 The United States Of America As Represented By The Secretary Of The Navy Dual mode fluid management system
FR2933742A1 (fr) * 2008-07-11 2010-01-15 Snecma Dispositif d'injection de monoergol a debit modulable avec vitesse d'injection stable.

Also Published As

Publication number Publication date
US20100005779A1 (en) 2010-01-14
EP2143928B1 (de) 2011-11-02
FR2933741B1 (fr) 2011-06-03
FR2933741A1 (fr) 2010-01-15
EP2143928A1 (de) 2010-01-13
US8596039B2 (en) 2013-12-03

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