FR2605053A1 - Aeronef a combustibles multiples, et son systeme de propulsion - Google Patents

Aeronef a combustibles multiples, et son systeme de propulsion Download PDF

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Publication number
FR2605053A1
FR2605053A1 FR8713896A FR8713896A FR2605053A1 FR 2605053 A1 FR2605053 A1 FR 2605053A1 FR 8713896 A FR8713896 A FR 8713896A FR 8713896 A FR8713896 A FR 8713896A FR 2605053 A1 FR2605053 A1 FR 2605053A1
Authority
FR
France
Prior art keywords
fuel
channel
oxidant
combustion chamber
propulsion system
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.)
Withdrawn
Application number
FR8713896A
Other languages
English (en)
French (fr)
Inventor
George Albert Coffinberry
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2605053A1 publication Critical patent/FR2605053A1/fr
Withdrawn legal-status Critical Current

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)
FR8713896A 1986-10-14 1987-10-08 Aeronef a combustibles multiples, et son systeme de propulsion Withdrawn FR2605053A1 (fr)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
FR2605053A1 true FR2605053A1 (fr) 1988-04-15

Family

ID=25440002

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8713896A Withdrawn FR2605053A1 (fr) 1986-10-14 1987-10-08 Aeronef a combustibles multiples, et son systeme de propulsion

Country Status (8)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112298501A (zh) * 2020-10-20 2021-02-02 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
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

Families Citing this family (10)

* 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
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
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

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2526222A (en) * 1948-01-02 1950-10-17 Daniel And Florence Guggenheim Cooling and feeding means for rocket type combustion chambers
CH274976A (fr) * 1948-10-26 1951-04-30 Oerlikon Maschf Brûleur.
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
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
GB793300A (en) * 1953-06-19 1958-04-16 Havilland Engine Co Ltd Rocket motors
DE1085719B (de) * 1944-12-04 1960-07-21 Dr Eberhard Schneller Raketenantrieb und -ausbildung
US3067594A (en) * 1959-05-11 1962-12-11 Catacycle Company Cooling with endothermic chemical reactions
DE1626066A1 (de) * 1967-09-23 1970-06-11 Messerschmitt Boelkow Blohm Verfahren zum Aufbereiten eines fluessigen Monergols zum Betreiben eines Gaserzeugers,insbesondere fuer Raketentriebwerke,und Gaserzeuger zur Durchfuehrung des Verfahrens
EP0139851A2 (de) * 1983-09-19 1985-05-08 Rockwell International Corporation Verfahren zur Herstellung von engen Kanälen innerhalb eines Körpers

Family Cites Families (7)

* 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
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
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
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

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
CH274976A (fr) * 1948-10-26 1951-04-30 Oerlikon Maschf Brûleur.
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
US3067594A (en) * 1959-05-11 1962-12-11 Catacycle Company Cooling with endothermic chemical reactions
DE1626066A1 (de) * 1967-09-23 1970-06-11 Messerschmitt Boelkow Blohm Verfahren zum Aufbereiten eines fluessigen Monergols zum Betreiben eines Gaserzeugers,insbesondere fuer Raketentriebwerke,und Gaserzeuger zur Durchfuehrung des Verfahrens
EP0139851A2 (de) * 1983-09-19 1985-05-08 Rockwell International Corporation Verfahren zur Herstellung von engen Kanälen innerhalb eines Körpers

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
CN112298501A (zh) * 2020-10-20 2021-02-02 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

Also Published As

Publication number Publication date
NO874263L (no) 1988-04-15
CN87106913A (zh) 1988-07-13
GB8724107D0 (en) 1987-11-18
IT8722207A0 (it) 1987-10-09
SE464719B (sv) 1991-06-03
DE3734099A1 (de) 1988-04-21
JPS63120842A (ja) 1988-05-25
GB2196394B (en) 1991-06-26
SE8703970L (sv) 1988-04-15
NO874263D0 (no) 1987-10-13
IT1225459B (it) 1990-11-14
SE8703970D0 (sv) 1987-10-13
GB2196394A (en) 1988-04-27

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ER Errata listed in the french official journal (bopi)

Free format text: 15/88

ST Notification of lapse