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DE60206424T2 - Rohrverschlussvorrichtung, insbesondere für Luftrohre in einem Staustrahlantrieb - Google Patents

Rohrverschlussvorrichtung, insbesondere für Luftrohre in einem Staustrahlantrieb Download PDF

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Publication number
DE60206424T2
DE60206424T2 DE60206424T DE60206424T DE60206424T2 DE 60206424 T2 DE60206424 T2 DE 60206424T2 DE 60206424 T DE60206424 T DE 60206424T DE 60206424 T DE60206424 T DE 60206424T DE 60206424 T2 DE60206424 T2 DE 60206424T2
Authority
DE
Germany
Prior art keywords
orifice
duct
closure device
air pipes
shutter
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.)
Expired - Lifetime
Application number
DE60206424T
Other languages
English (en)
Other versions
DE60206424D1 (de
Inventor
Laurent Carton
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.)
Aerospatiale Matra Missiles SA
Original Assignee
Aerospatiale Matra Missiles SA
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 Aerospatiale Matra Missiles SA filed Critical Aerospatiale Matra Missiles SA
Publication of DE60206424D1 publication Critical patent/DE60206424D1/de
Application granted granted Critical
Publication of DE60206424T2 publication Critical patent/DE60206424T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Compressor (AREA)
  • Pipe Accessories (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Testing Of Engines (AREA)
DE60206424T 2001-01-12 2002-01-07 Rohrverschlussvorrichtung, insbesondere für Luftrohre in einem Staustrahlantrieb Expired - Lifetime DE60206424T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0100383A FR2819556B1 (fr) 2001-01-12 2001-01-12 Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur

Publications (2)

Publication Number Publication Date
DE60206424D1 DE60206424D1 (de) 2005-11-10
DE60206424T2 true DE60206424T2 (de) 2006-06-14

Family

ID=8858739

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60206424T Expired - Lifetime DE60206424T2 (de) 2001-01-12 2002-01-07 Rohrverschlussvorrichtung, insbesondere für Luftrohre in einem Staustrahlantrieb

Country Status (8)

Country Link
US (1) US6725664B2 (de)
EP (1) EP1225326B1 (de)
AT (1) ATE306017T1 (de)
CA (1) CA2366044C (de)
DE (1) DE60206424T2 (de)
ES (1) ES2250595T3 (de)
FR (1) FR2819556B1 (de)
RU (1) RU2219362C2 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2840029B1 (fr) * 2002-05-27 2004-08-13 Mbdam Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur
US9032737B2 (en) 2009-12-30 2015-05-19 Rolls-Royce North American Technologies, Inc. Combustor added to a gas turbine engine to increase thrust
RU2739449C1 (ru) * 2019-10-31 2020-12-24 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Воздухозаборное устройство со сбрасываемой заглушкой беспилотного летательного аппарата с воздушно-реактивным двигателем
RU197363U1 (ru) * 2019-11-13 2020-04-23 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Сбрасываемый пиропривод с заглушкой для воздухозаборных устройств беспилотных летательных аппаратов с воздушно-реактивным двигателем
IL297942A (en) * 2020-05-05 2023-01-01 Atlantis Res Labs Inc Multi-mode drive system
CN111948334B (zh) * 2020-07-20 2022-07-15 西安近代化学研究所 一种推进剂燃烧速度测试装置
CN112627983B (zh) * 2020-12-25 2022-02-22 中国人民解放军国防科技大学 一种rbcc发动机内流道及rbcc发动机
CN113202655B (zh) * 2021-06-07 2022-05-24 北京理工大学 一种固液冲压组合发动机
CN115107968B (zh) * 2022-06-13 2023-04-18 南昌航空大学 一种低航速水下冲压发动机及其设计方法

Family Cites Families (24)

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Publication number Priority date Publication date Assignee Title
US3038303A (en) * 1958-01-02 1962-06-12 Robert O Gose Thrust termination in solid propellant rockets
US3137408A (en) * 1962-07-09 1964-06-16 Rubbermaid Inc Pail with lid and latching mechanism
US3768255A (en) * 1967-03-06 1973-10-30 Texaco Inc Inlet port covers for reaction vehicle
DE1626069B1 (de) * 1967-10-18 1970-10-08 Messerschmitt Boelkow Blohm Kombinationstriebwerk
US3901028A (en) * 1972-09-13 1975-08-26 Us Air Force Ramjet with integrated rocket boost motor
US4028886A (en) * 1975-10-23 1977-06-14 Mcdonnell Douglas Corporation Passive chamber wall fragmenter
US4022352A (en) * 1976-04-26 1977-05-10 Pehr Harold T Container cover and safety closure
US4047495A (en) * 1976-05-03 1977-09-13 Polytop Corporation Child resistant dispensing closures
US4441312A (en) * 1979-06-22 1984-04-10 The United States Of America As Represented By The Secretary Of The Air Force Combined cycle ramjet engine
DE3003004C2 (de) 1980-01-29 1982-06-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Deckel aus leicht zerstörbarem Material zum Verschließen der in die Brennkammer von kombinierten Staustrahl-Raketentriebwerken einmündenden Lufteinlauföffnungen, und Schlagvorrichtung zum Zerstören des Deckels
DE3242585C2 (de) * 1982-11-18 1985-01-10 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verschlußeinrichtung für einen in die Brennkammer von Staustrahl-Raketentriebwerken einmündenden Lufteinlaufkanal
FR2629136B1 (fr) * 1985-09-17 1990-11-09 Aerospatiale Statoreacteur pourvu d'une pluralite de manches d'alimentation en air carbure et missile pourvu d'un tel statoreacteur
FR2591664B1 (fr) * 1985-12-13 1988-03-25 Aerospatiale Systeme d'injection de carburant pour statoreacteur, statoreacteur pourvu d'un tel systeme d'injection et missile propulse par ce statoreacteur
DE3738703A1 (de) * 1987-05-27 1988-12-08 Mtu Muenchen Gmbh Kombiniertes, umschaltbares strahltriebwerk zum antrieb von flugzeugen und raumfahrzeugen
US4865267A (en) * 1988-02-25 1989-09-12 Sundstrand Corporation Ram air flow system for aircraft
JPH079216B2 (ja) 1989-07-24 1995-02-01 防衛庁技術研究本部長 ラムロケット
US6003302A (en) * 1996-05-10 1999-12-21 Feldman; Peter Ramjet with adjustable working duct casings
FR2755182B1 (fr) * 1996-10-30 1998-12-31 Aerospatiale Systeme d'obturation pour un orifice d'entree d'air dans la chambre de combustion d'un statoreacteur
US5784877A (en) * 1996-11-08 1998-07-28 Atlantic Research Corporation Rocket-ramjet engine casing port closure
JPH10314027A (ja) * 1997-05-19 1998-12-02 P-Kotsuku Mahobin Kogyo Kk 容器の蓋取付け構造
US6058846A (en) * 1998-06-03 2000-05-09 Lockhead Martin Corporation Rocket and ramjet powered hypersonic stealth missile having alterable radar cross section
FR2810642B1 (fr) * 2000-06-26 2003-02-07 Seb Sa Dispositif de verrouillage de couvercle
US6568554B2 (en) * 2000-07-21 2003-05-27 H-Tech, Inc. Hydraulic or pneumatic safety device for fluid handling apparatus
FR2813344B1 (fr) * 2000-08-28 2002-11-29 Aerospatiale Matra Missiles Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur

Also Published As

Publication number Publication date
DE60206424D1 (de) 2005-11-10
US20040050062A1 (en) 2004-03-18
CA2366044A1 (fr) 2002-07-12
FR2819556B1 (fr) 2003-04-04
US6725664B2 (en) 2004-04-27
CA2366044C (fr) 2008-10-07
EP1225326B1 (de) 2005-10-05
ES2250595T3 (es) 2006-04-16
RU2219362C2 (ru) 2003-12-20
EP1225326A1 (de) 2002-07-24
FR2819556A1 (fr) 2002-07-19
ATE306017T1 (de) 2005-10-15

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