BE801230A - Paroi intermediaire pour moteurs de fusees - Google Patents

Paroi intermediaire pour moteurs de fusees

Info

Publication number
BE801230A
BE801230A BE132535A BE132535A BE801230A BE 801230 A BE801230 A BE 801230A BE 132535 A BE132535 A BE 132535A BE 132535 A BE132535 A BE 132535A BE 801230 A BE801230 A BE 801230A
Authority
BE
Belgium
Prior art keywords
intermediate wall
rocket engines
rocket
engines
wall
Prior art date
Application number
BE132535A
Other languages
English (en)
French (fr)
Original Assignee
Dynamit Nobel Ag
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 Dynamit Nobel Ag filed Critical Dynamit Nobel Ag
Publication of BE801230A publication Critical patent/BE801230A/xx

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
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/76—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
    • F02K9/763—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants with solid propellant
    • 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
    • F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/978—Closures for nozzles; Nozzles comprising ejectable or discardable elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K15/00—Check valves
    • F16K15/14—Check valves with flexible valve members
    • F16K15/1402—Check valves with flexible valve members having an integral flexible member cooperating with a plurality of seating surfaces
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K2200/00—Details of valves
    • F16K2200/20—Common housing having a single inlet, a single outlet and multiple valve members
    • F16K2200/203—Common housing having a single inlet, a single outlet and multiple valve members in parallel
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7734—Fluid opened valve requiring reset
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7837—Direct response valves [i.e., check valve type]
    • Y10T137/7838—Plural
    • Y10T137/7839—Dividing and recombining in a single flow path
    • Y10T137/784—Integral resilient member forms plural valves
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7837—Direct response valves [i.e., check valve type]
    • Y10T137/7859—Single head, plural ports in parallel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Testing Of Engines (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Nozzles (AREA)
  • Fuel-Injection Apparatus (AREA)
BE132535A 1972-06-22 1973-06-21 Paroi intermediaire pour moteurs de fusees BE801230A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2230457A DE2230457C3 (de) 1972-06-22 1972-06-22 Zwischenwand für Raketentriebwerke

Publications (1)

Publication Number Publication Date
BE801230A true BE801230A (fr) 1973-10-15

Family

ID=5848424

Family Applications (1)

Application Number Title Priority Date Filing Date
BE132535A BE801230A (fr) 1972-06-22 1973-06-21 Paroi intermediaire pour moteurs de fusees

Country Status (6)

Country Link
US (1) US3879942A (cs)
BE (1) BE801230A (cs)
DE (1) DE2230457C3 (cs)
FR (1) FR2189646B1 (cs)
GB (1) GB1401400A (cs)
IT (1) IT986191B (cs)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2458180A1 (de) * 1974-12-09 1976-06-10 Dynamit Nobel Ag Trennwand fuer raketentriebwerke
US4007685A (en) * 1975-07-30 1977-02-15 The United States Of America As Represented By The Secretary Of The Army Gas generator
US4028886A (en) * 1975-10-23 1977-06-14 Mcdonnell Douglas Corporation Passive chamber wall fragmenter
GB1537469A (en) * 1975-12-23 1978-12-29 Imi Kynoch Ltd Disintegrable member for controlling flow between pressure chambers
US4050243A (en) * 1976-05-17 1977-09-27 The United States Of America As Represented By The Secretary Of The Navy Combination solid fuel ramjet injector/port cover
FR2584456B1 (fr) * 1985-07-03 1987-10-02 Poudres & Explosifs Ste Nale Dispositif de fermeture temporaire d'un orifice interne d'un propulseur
US5201644A (en) * 1987-12-23 1993-04-13 3H Invent A/S Valve arrangement for pump or compressor
FR2631387B1 (fr) * 1988-05-10 1990-07-13 Poudres & Explosifs Ste Nale Propulseur sans tuyere de faible allongement
US5160070A (en) * 1988-08-11 1992-11-03 Fike Corporation Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor
US5311902A (en) * 1991-07-02 1994-05-17 Overfield Norbert W Reciprocating compressor valve
GB9206616D0 (en) * 1992-03-26 1997-09-17 Royal Ordnance Plc Improvements in or relating to combustion apparatus and valves therefor
ES2105242T3 (es) * 1992-04-02 1997-10-16 Procter & Gamble Articulo absorbente que tiene una lamina encimera no tejida con areas impermeables a los fluidos.
RU2161718C2 (ru) * 1999-01-27 2001-01-10 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Ракетный двигатель на твердом топливе
US8291691B2 (en) 2007-08-02 2012-10-23 Aerojet-General Corporation Multi-functional pulse-divided rocket
RU2362036C1 (ru) * 2008-02-07 2009-07-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Двухрежимный ракетный двигатель твердого топлива
US8117847B2 (en) * 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
RU2390646C1 (ru) * 2008-12-29 2010-05-27 Открытое акционерное общество "Машиностроительное конструкторское бюро "Искра" имени Ивана Ивановича Картукова" Двухрежимный ракетный двигатель твердого топлива
FR2945453B1 (fr) * 2009-05-14 2015-07-03 Airbus France Dispositif d'ejection d'un fluide.
US9032737B2 (en) 2009-12-30 2015-05-19 Rolls-Royce North American Technologies, Inc. Combustor added to a gas turbine engine to increase thrust
DE102014115722B4 (de) * 2014-10-29 2022-08-11 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Integriertes Flugkörperantriebssystem
CN104977168B (zh) * 2015-07-15 2017-09-08 江西洪都航空工业集团有限责任公司 一种堵盖释放装置
CN105445973B (zh) * 2015-12-31 2019-04-30 京东方科技集团股份有限公司 一种抽真空装置及采用该抽真空装置的操作方法
RU2704058C9 (ru) * 2018-11-20 2019-12-18 Акционерное общество "Машиностроительное конструкторское бюро "Искра" имени Ивана Ивановича Картукова" (АО "МКБ "Искра") Разделительное днище многоимпульсного ракетного двигателя на твердом топливе
CN110145412B (zh) * 2019-05-27 2020-11-03 北京理工大学 门式固体火箭发动机
CN110594038B (zh) * 2019-08-20 2021-11-09 西安航天动力技术研究所 一种多次脉冲激励装置
CN111762343B (zh) * 2020-06-09 2023-09-08 上海宇航系统工程研究所 一种航天器用可抛离双组元环形贮箱
CN117307359B (zh) * 2023-11-28 2024-03-19 西安现代控制技术研究所 一种固体火箭发动机喷管耐腐蚀唇型密封堵结构

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2835269A (en) * 1953-04-10 1958-05-20 Smith Corp A O Vessel closure
US2977879A (en) * 1957-09-18 1961-04-04 Atlantic Res Corp Rocket projectile
US3115008A (en) * 1959-02-03 1963-12-24 Cohen William Integral rocket ramjet missile propulsion system
US3040517A (en) * 1960-06-27 1962-06-26 Carl V Ryden Releasable rocket nozzle
US3112615A (en) * 1962-05-29 1963-12-03 Harold G Cook Electrical connector for boost sustained rocket motor
BE701665A (cs) * 1966-07-22 1968-01-02

Also Published As

Publication number Publication date
IT986191B (it) 1975-01-20
DE2230457A1 (de) 1974-01-10
DE2230457B2 (de) 1980-07-03
US3879942A (en) 1975-04-29
FR2189646A1 (cs) 1974-01-25
DE2230457C3 (de) 1981-05-27
GB1401400A (en) 1975-07-16
FR2189646B1 (cs) 1978-01-06

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