DE3144936C1 - Ventileinrichtung zum Steuern stroemender Medien hoher Temperatur,insbesondere zum Dosieren der Mengen brennstoffreicher Gase bei Staustrahl-Raketentriebwerken - Google Patents

Ventileinrichtung zum Steuern stroemender Medien hoher Temperatur,insbesondere zum Dosieren der Mengen brennstoffreicher Gase bei Staustrahl-Raketentriebwerken

Info

Publication number
DE3144936C1
DE3144936C1 DE3144936A DE3144936A DE3144936C1 DE 3144936 C1 DE3144936 C1 DE 3144936C1 DE 3144936 A DE3144936 A DE 3144936A DE 3144936 A DE3144936 A DE 3144936A DE 3144936 C1 DE3144936 C1 DE 3144936C1
Authority
DE
Germany
Prior art keywords
ball
fuel
combustion chamber
rich gases
valve device
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
Application number
DE3144936A
Other languages
German (de)
English (en)
Inventor
Ernst Dipl.-Ing. 8000 München Engl
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm 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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE3144936A priority Critical patent/DE3144936C1/de
Priority to FR8218953A priority patent/FR2516172A1/fr
Priority to GB08232094A priority patent/GB2109511A/en
Priority to US06/441,100 priority patent/US4483139A/en
Application granted granted Critical
Publication of DE3144936C1 publication Critical patent/DE3144936C1/de
Expired 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
    • 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
    • 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
    • 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
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00—Power plants
    • Y10S60/917—Solid fuel ramjet using pulverized fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Taps Or Cocks (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
DE3144936A 1981-11-12 1981-11-12 Ventileinrichtung zum Steuern stroemender Medien hoher Temperatur,insbesondere zum Dosieren der Mengen brennstoffreicher Gase bei Staustrahl-Raketentriebwerken Expired DE3144936C1 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE3144936A DE3144936C1 (de) 1981-11-12 1981-11-12 Ventileinrichtung zum Steuern stroemender Medien hoher Temperatur,insbesondere zum Dosieren der Mengen brennstoffreicher Gase bei Staustrahl-Raketentriebwerken
FR8218953A FR2516172A1 (fr) 1981-11-12 1982-11-10 Dispositif de soupape pour la commande de fluides en ecoulement a haute temperature, notamment pour le dosage des debits de gaz riches en combustible dans des moteurs-fusees du type statoreacteur
GB08232094A GB2109511A (en) 1981-11-12 1982-11-10 Valve apparatus for controlling high-temperature fluids
US06/441,100 US4483139A (en) 1981-11-12 1982-11-12 Valve construction particularly for ram jet rocket engines and to a ram jet rocket engine construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3144936A DE3144936C1 (de) 1981-11-12 1981-11-12 Ventileinrichtung zum Steuern stroemender Medien hoher Temperatur,insbesondere zum Dosieren der Mengen brennstoffreicher Gase bei Staustrahl-Raketentriebwerken

Publications (1)

Publication Number Publication Date
DE3144936C1 true DE3144936C1 (de) 1983-03-10

Family

ID=6146222

Family Applications (1)

Application Number Title Priority Date Filing Date
DE3144936A Expired DE3144936C1 (de) 1981-11-12 1981-11-12 Ventileinrichtung zum Steuern stroemender Medien hoher Temperatur,insbesondere zum Dosieren der Mengen brennstoffreicher Gase bei Staustrahl-Raketentriebwerken

Country Status (4)

Country Link
US (1) US4483139A (enExample)
DE (1) DE3144936C1 (enExample)
FR (1) FR2516172A1 (enExample)
GB (1) GB2109511A (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105736181A (zh) * 2014-12-09 2016-07-06 上海新力动力设备研究所 固体火箭发动机燃气流量调节装置环形多孔扰流结构

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3502673A1 (de) * 1985-01-26 1986-07-31 Rheinmetall GmbH, 4000 Düsseldorf Luftatmender feststoff-staustrahlantrieb
US5817968A (en) * 1987-08-03 1998-10-06 The United States Of America As Represented By The Secretary Of The Air Force Gas generation with high pressure sensitivity exponent propellant
US5172547A (en) * 1991-04-30 1992-12-22 The United States Of America As Represented By The Secretary Of The Air Force Electronic valve control for gas generator outflow
NO180467C (no) * 1994-11-04 1997-04-23 Rc Subsea As Strupeventil
US7287725B2 (en) * 2005-04-25 2007-10-30 Raytheon Company Missile control system and method
US7856806B1 (en) * 2006-11-06 2010-12-28 Raytheon Company Propulsion system with canted multinozzle grid
DE102007010349B4 (de) * 2007-03-03 2009-07-09 Lfk-Lenkflugkörpersysteme Gmbh Ventilsteuereinheit für Staustrahlantrieb sowie Lenkflugkörper mit einer solchen Ventilsteuereinheit
US8601790B2 (en) * 2008-02-28 2013-12-10 The Aerospace Corporation Buried radial flow rapid prototyping rocket motors
US8707676B2 (en) * 2008-02-28 2014-04-29 The Aerospace Corporation Radial flow rapid prototyping rocket motors
US8225507B2 (en) 2008-02-28 2012-07-24 The Aerospace Corporation Stereolithographic rocket motor manufacturing method
US8117847B2 (en) 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
US9038368B2 (en) 2011-08-01 2015-05-26 The Aerospace Corporation Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor
US9429104B2 (en) 2011-08-01 2016-08-30 The Aerospace Corporation Systems and methods for casting hybrid rocket motor fuel grains
US9127622B2 (en) * 2011-11-21 2015-09-08 United Technologies Corporation Reversible flow discharge orifice

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1311642A (en) * 1919-07-29 Check-valve
DE133326C (enExample) *
US2452441A (en) * 1944-06-17 1948-10-26 Alco Valve Co Regulator valve having a capillary tube expansion passage
US2948112A (en) * 1953-12-14 1960-08-09 Kenneth W Smith Combined rocket and ram-jet engine
US2935084A (en) * 1955-05-02 1960-05-03 Garrett Corp Air pressure regulator
US3065597A (en) * 1959-09-28 1962-11-27 Gen Electric Reignitable solid rocket motor
US3712058A (en) * 1961-08-14 1973-01-23 Northrop Carolina Inc Solid propellant controlled rocket motors
FR1378866A (fr) * 1963-07-11 1964-11-20 Onera (Off Nat Aerospatiale) Perfectionnements apportés aux générateurs de gaz chauds, notamment aux moteursfusées, à ergols fluide et solide hypergoliques
US3691770A (en) * 1966-12-02 1972-09-19 Us Navy Thrust control means for a solid propellant rocket motor
FR2109035A5 (enExample) * 1970-05-11 1972-05-26 Aquitaine Petrole
DE3005864A1 (de) * 1980-02-16 1981-09-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum steuern der stroemungsquerschnitte von kanaelen, insbesondere von gasleitrohren eines raketen-staustrahltriebwerks
DE3006298C2 (de) * 1980-02-20 1983-08-18 Daimler-Benz Ag, 7000 Stuttgart Elektrohydraulische Schalteinrichtung

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NICHTS-ERMITTELT *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105736181A (zh) * 2014-12-09 2016-07-06 上海新力动力设备研究所 固体火箭发动机燃气流量调节装置环形多孔扰流结构

Also Published As

Publication number Publication date
FR2516172B3 (enExample) 1984-11-30
GB2109511A (en) 1983-06-02
US4483139A (en) 1984-11-20
FR2516172A1 (fr) 1983-05-13

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Legal Events

Date Code Title Description
8100 Publication of the examined application without publication of unexamined application
D1 Grant (no unexamined application published) patent law 81
8364 No opposition during term of opposition
8320 Willingness to grant licences declared (paragraph 23)
8339 Ceased/non-payment of the annual fee