SE8703970D0 - Framdrivningssystem for luftfarkost - Google Patents

Framdrivningssystem for luftfarkost

Info

Publication number
SE8703970D0
SE8703970D0 SE8703970A SE8703970A SE8703970D0 SE 8703970 D0 SE8703970 D0 SE 8703970D0 SE 8703970 A SE8703970 A SE 8703970A SE 8703970 A SE8703970 A SE 8703970A SE 8703970 D0 SE8703970 D0 SE 8703970D0
Authority
SE
Sweden
Prior art keywords
fuel
oxidizer
passageway
injection holes
combustion chamber
Prior art date
Application number
SE8703970A
Other languages
English (en)
Other versions
SE8703970L (sv
SE464719B (sv
Inventor
G A 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 SE8703970D0 publication Critical patent/SE8703970D0/sv
Publication of SE8703970L publication Critical patent/SE8703970L/sv
Publication of SE464719B publication Critical patent/SE464719B/sv

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
    • 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
    • F02K7/14—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 with external combustion, e.g. scram-jet 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • 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
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/40—Continuous 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)
SE8703970A 1986-10-14 1987-10-13 Framdrivningssystem SE464719B (sv)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
SE8703970D0 true SE8703970D0 (sv) 1987-10-13
SE8703970L SE8703970L (sv) 1988-04-15
SE464719B SE464719B (sv) 1991-06-03

Family

ID=25440002

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8703970A SE464719B (sv) 1986-10-14 1987-10-13 Framdrivningssystem

Country Status (8)

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

Families Citing this family (12)

* 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
US7213392B2 (en) 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
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
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
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
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

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 (sv) * 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
DK102875C (da) * 1962-04-17 1965-10-18 Anders Folke Anden Brænder til flydende brændsel.
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
FR2605053A1 (fr) 1988-04-15
IT1225459B (it) 1990-11-14
GB2196394A (en) 1988-04-27
SE8703970L (sv) 1988-04-15
GB2196394B (en) 1991-06-26
SE464719B (sv) 1991-06-03
NO874263L (no) 1988-04-15
DE3734099A1 (de) 1988-04-21
GB8724107D0 (en) 1987-11-18
IT8722207A0 (it) 1987-10-09
NO874263D0 (no) 1987-10-13
CN87106913A (zh) 1988-07-13
JPS63120842A (ja) 1988-05-25

Similar Documents

Publication Publication Date Title
SE8703970L (sv) Framdrivningssystem for luftfarkost
US8544280B2 (en) Continuous detonation wave engine with quenching structure
US4771599A (en) Tripropellant rocket engine with injector
US3595022A (en) Thermodynamic reaction drive
US5253474A (en) Apparatus for supersonic combustion in a restricted length
US3535881A (en) Combination rocket and ram jet engine
JP2812710B2 (ja) 二液型推進剤ロケットエンジンの構造体
US3695041A (en) Two-stage hydrazine rocket motor
US5224344A (en) Variable-cycle storable reactants engine
US3570249A (en) Method of operating a rocket combustion chamber and combustion chamber system for performing the method
US3712059A (en) Reverse flow internally-cooled rocket engine
US3166898A (en) Liquid injection system
US3286469A (en) Rocket nozzle cooling and thrust recovery device
US3286473A (en) Fixed injector and turbopump assembly
US3355891A (en) Ram jet engine and fuel injection system therefor
GB1475354A (en) Thermal reactor
US3295323A (en) Means for vaporizing liquid propellants
US2978868A (en) Concentric combustion system with cooled dividing partition
US3518828A (en) Hybrid rocket motor ignition system
US4381642A (en) Ramjet engine
JP4183475B2 (ja) ハイブリッドロケットエンジンの固体モータとその燃焼方法
US3170294A (en) Oxygen injection system
WO2021091613A3 (en) Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber
US3451223A (en) Rocket engine chamber cooling and injection system
Schadow et al. Water tunnel and windowed combustion as tools for ducted rocket development

Legal Events

Date Code Title Description
NUG Patent has lapsed

Ref document number: 8703970-7

Effective date: 19930510

Format of ref document f/p: F