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NO874263D0 - Fremdriftssystem og luftfartoey med slikt system. - Google Patents

Fremdriftssystem og luftfartoey med slikt system.

Info

Publication number
NO874263D0
NO874263D0 NO874263A NO874263A NO874263D0 NO 874263 D0 NO874263 D0 NO 874263D0 NO 874263 A NO874263 A NO 874263A NO 874263 A NO874263 A NO 874263A NO 874263 D0 NO874263 D0 NO 874263D0
Authority
NO
Norway
Prior art keywords
aircraft
project
project system
Prior art date
Application number
NO874263A
Other languages
English (en)
Other versions
NO874263L (no
Inventor
George Albert Coffinberry
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of NO874263D0 publication Critical patent/NO874263D0/no
Publication of NO874263L publication Critical patent/NO874263L/no

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/10Plants 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
    • F02K7/18Composite ram-jet/rocket engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/10Plants 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
    • F02K7/14Plants 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 with external combustion, e.g. scram-jet engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/34Casings; Combustion chambers; Liners thereof
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/52Injectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/40Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Processing Of Solid Wastes (AREA)
  • Feeding Of Workpieces (AREA)
  • Vending Machines For Individual Products (AREA)
NO874263A 1986-10-14 1987-10-13 Fremdriftssystem og luftfartoey med slikt system. NO874263L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US91821786A 1986-10-14 1986-10-14

Publications (2)

Publication Number Publication Date
NO874263D0 true NO874263D0 (no) 1987-10-13
NO874263L NO874263L (no) 1988-04-15

Family

ID=25440002

Family Applications (1)

Application Number Title Priority Date Filing Date
NO874263A NO874263L (no) 1986-10-14 1987-10-13 Fremdriftssystem og luftfartoey med slikt system.

Country Status (8)

Country Link
JP (1) JPS63120842A (no)
CN (1) CN87106913A (no)
DE (1) DE3734099A1 (no)
FR (1) FR2605053A1 (no)
GB (1) GB2196394B (no)
IT (1) IT1225459B (no)
NO (1) NO874263L (no)
SE (1) SE464719B (no)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3911655C1 (en) * 1989-04-10 1990-06-07 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Cryogenic supersonic aircraft fuel tank - is surrounded by fuel pipe harness to permit heating or cooling
DE4437524C2 (de) * 1994-10-20 1997-04-24 Kunkel Klaus Dr Ing Verfahren zum Betreiben eines nach dem Rückstoßprinzip arbeitenden Antriebes eines Flugkörpers sowie Flugkörperantrieb
DE19927735B4 (de) * 1999-06-17 2005-10-06 Eads Space Transportation Gmbh Schubkammer-Anordnung für Raumfahrt-Triebwerke
RU2179256C2 (ru) * 1999-06-21 2002-02-10 Открытое акционерное общество Самарский научно-технический комплекс им. Н.Д. Кузнецова Газогенератор жрд
US7213392B2 (en) * 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
RU2344310C2 (ru) * 2005-12-02 2009-01-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт машиностроения" (ФГУП "НИИМаш") Способ внутреннего охлаждения двухкомпонентного жидкостного ракетного двигателя малой тяги и устройство для его осуществления
DE102014107316A1 (de) * 2014-05-23 2015-11-26 Airbus Operations Gmbh Tanksystem zur kryogenen Lagerung von Wasserstoff und Flugzeug mit einem Tanksystem zur kryogenen Lagerung von Wasserstoff
DE102017106758A1 (de) 2017-03-15 2018-09-20 Deutsches Zentrum für Luft- und Raumfahrt e.V. Schubkammervorrichtung und Verfahren zum Betreiben einer Schubkammervorrichtung
CN109162831A (zh) * 2018-09-05 2019-01-08 北京航空航天大学 固液动力发动机及应用其的火箭
RU2752960C1 (ru) * 2020-07-03 2021-08-11 Виктор Николаевич Исаков Камера сгорания с каталитическим покрытием для прямоточного воздушно-реактивного двигателя и способ нанесения каталитического покрытия
DE102020123422A1 (de) * 2020-09-08 2022-03-31 Deutsches Zentrum für Luft- und Raumfahrt e.V. Schubkammervorrichtung und Verfahren zum Betreiben einer Schubkammervorrichtung
CN112298501B (zh) * 2020-10-20 2023-06-16 广东石油化工学院 一种有翼电力挤压推进型智能水下无人航行器
CN112298502A (zh) * 2020-10-20 2021-02-02 广东石油化工学院 一种无翼电力挤压螺旋转动前进型智能水下无人航行器
CN113357052B (zh) * 2021-06-25 2022-07-19 中国科学院力学研究所 一种固液发动机药柱燃面均匀后退控制方法
CN119844240A (zh) * 2025-03-19 2025-04-18 中国空气动力研究与发展中心空天技术研究所 一种气体驱动的一体化支板脉冲喷注器及应用方法
CN119982251B (zh) * 2025-04-15 2025-08-29 深圳驭龙航天科技有限公司 直驱式液体火箭发动机

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE716175C (de) * 1935-02-09 1942-01-14 Eugen Saenger Dr Ing Raketenmotor
DE1085719B (de) * 1944-12-04 1960-07-21 Dr Eberhard Schneller Raketenantrieb und -ausbildung
US2526222A (en) * 1948-01-02 1950-10-17 Daniel And Florence Guggenheim Cooling and feeding means for rocket type combustion chambers
BE490776A (no) * 1948-10-26
US2695496A (en) * 1952-03-05 1954-11-30 Daniel And Florence Guggenheim Structure for feeding, intermingling, vaporizing, and igniting combustion liquids ina combustion chamber for rocket-type propulsion apparatus
GB793300A (en) * 1953-06-19 1958-04-16 Havilland Engine Co Ltd Rocket motors
US2749706A (en) * 1953-10-29 1956-06-12 Daniel And Florence Guggenheim Mechanism for cooling a combustion chamber in propulsion apparatus and for feeding combustion liquids thereto
GB800354A (en) * 1955-12-23 1958-08-27 Aerojet General Co Combustion chamber for gas generation provided with cooling means and a system for operating the same
GB865942A (en) * 1958-10-10 1961-04-26 Gen Motors Corp Improvements relating to exhaust ducts included in jet propulsion engines
US3067594A (en) * 1959-05-11 1962-12-11 Catacycle Company Cooling with endothermic chemical reactions
GB970222A (en) * 1962-04-17 1964-09-16 Anders Folke Anden Improvements in liquid fuel burning apparatus
GB1196489A (en) * 1966-11-29 1970-06-24 Lutz Tilo Kayser Improvements in or relating to Rocket Engines
DE1626066C3 (de) * 1967-09-23 1974-06-12 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Verfahren zum Erzeugen von Druckgas durch katalytische Zersetzung eines flüssigen Monergols und Vorrichtung zur Durchführung des Verfahrens
US4271675A (en) * 1977-10-21 1981-06-09 Rolls-Royce Limited Combustion apparatus for gas turbine engines
CA1159356A (en) * 1979-10-25 1983-12-27 Kurt Skoog Method and device for producing microdroplets of fluid
US4535518A (en) * 1983-09-19 1985-08-20 Rockwell International Corporation Method of forming small-diameter channel within an object

Also Published As

Publication number Publication date
JPS63120842A (ja) 1988-05-25
GB8724107D0 (en) 1987-11-18
CN87106913A (zh) 1988-07-13
NO874263L (no) 1988-04-15
FR2605053A1 (fr) 1988-04-15
SE464719B (sv) 1991-06-03
IT8722207A0 (it) 1987-10-09
GB2196394A (en) 1988-04-27
DE3734099A1 (de) 1988-04-21
IT1225459B (it) 1990-11-14
GB2196394B (en) 1991-06-26
SE8703970D0 (sv) 1987-10-13
SE8703970L (sv) 1988-04-15

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