DE1071421B - Brennkammer für Gasturbinen oder Raketenmotoren - Google Patents

Brennkammer für Gasturbinen oder Raketenmotoren

Info

Publication number
DE1071421B
DE1071421B DENDAT1071421D DE1071421DA DE1071421B DE 1071421 B DE1071421 B DE 1071421B DE NDAT1071421 D DENDAT1071421 D DE NDAT1071421D DE 1071421D A DE1071421D A DE 1071421DA DE 1071421 B DE1071421 B DE 1071421B
Authority
DE
Germany
Prior art keywords
combustion chamber
oxygen carrier
wall
fuel
around
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.)
Pending
Application number
DENDAT1071421D
Other languages
German (de)
English (en)
Inventor
Coventry Warwickshire Sidney Allen (Großbritannien)
Original Assignee
Armstrong Siddeley Motors Ltd., Coventry, Warwickshire (Großbritannien)
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.)
Publication date
Publication of DE1071421B publication Critical patent/DE1071421B/de
Pending 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • 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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/68—Decomposition chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hydrogen, Water And Hydrids (AREA)
  • Gas Burners (AREA)
DENDAT1071421D 1956-11-09 Brennkammer für Gasturbinen oder Raketenmotoren Pending DE1071421B (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3426856A GB847084A (en) 1956-11-09 1956-11-09 Combustion chamber for a gas turbine or rocket motor

Publications (1)

Publication Number Publication Date
DE1071421B true DE1071421B (de) 1959-12-17

Family

ID=10363522

Family Applications (1)

Application Number Title Priority Date Filing Date
DENDAT1071421D Pending DE1071421B (de) 1956-11-09 Brennkammer für Gasturbinen oder Raketenmotoren

Country Status (4)

Country Link
BE (1) BE562285A (enrdf_load_stackoverflow)
DE (1) DE1071421B (enrdf_load_stackoverflow)
FR (1) FR1187946A (enrdf_load_stackoverflow)
GB (1) GB847084A (enrdf_load_stackoverflow)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1297942B (de) * 1966-11-29 1969-06-19 Kayser Lutz T Anordnung zur Raketentriebwerkskuehlung
DE3213161A1 (de) * 1981-04-13 1982-11-25 Société Européenne de Propulsion, 92800 Puteaux, Hauts-de-Seine Brennkammer fuer raketentriebwerk
DE3728706A1 (de) * 1987-08-28 1988-10-27 Kurt Mannl Rotierendes einspritzsystem fuer raketentriebwerke
DE3923948A1 (de) * 1988-03-24 1991-01-24 Aerojet General Co Zweistufige raketenverbrennungskammer
DE102016208731A1 (de) * 2016-05-20 2017-11-23 Airbus Ds Gmbh Raketenantriebssystem und Verfahren zum Betreiben eines Raketenantriebssystems

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1164753B (de) * 1959-12-12 1964-03-05 Boelkow Entwicklungen Kg Raketentriebwerk fuer fluessige Treibstoffe
DE1142253B (de) * 1960-01-29 1963-01-10 Boelkow Entwicklungen Kg Brennkammer fuer Fluessigtreibstoffe
GB1196489A (en) * 1966-11-29 1970-06-24 Lutz Tilo Kayser Improvements in or relating to Rocket Engines
US3451223A (en) * 1966-12-06 1969-06-24 Howard Vern Main Rocket engine chamber cooling and injection system
DE2519538C2 (de) * 1975-05-02 1982-12-30 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verbindung zwischen dem Kühlmittel-Zulaufring und der Brennkammer-oder Schubdüsenwand eines Raketentriebwerks
US4840025A (en) * 1986-10-14 1989-06-20 General Electric Company Multiple-propellant air vehicle and propulsion system
US4841723A (en) * 1986-10-14 1989-06-27 General Electric Company Multiple-propellant air vehicle and propulsion system
US4835959A (en) * 1986-10-14 1989-06-06 General Electric Company Multiple-propellant air vehicle and propulsion system
US4817890A (en) * 1986-10-14 1989-04-04 General Electric Company Multiple-propellant air vehicle and propulsion system
US4811556A (en) * 1986-10-14 1989-03-14 General Electric Company Multiple-propellant air vehicle and propulsion system
CN111456866A (zh) * 2020-04-14 2020-07-28 合肥中科重明科技有限公司 一种液体火箭发动机的冷却液膜成型结构
CN112177801B (zh) * 2020-08-31 2021-12-24 西北工业大学 一种基于第三流体的过氧化氢/煤油火箭发动机推力室

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1297942B (de) * 1966-11-29 1969-06-19 Kayser Lutz T Anordnung zur Raketentriebwerkskuehlung
DE3213161A1 (de) * 1981-04-13 1982-11-25 Société Européenne de Propulsion, 92800 Puteaux, Hauts-de-Seine Brennkammer fuer raketentriebwerk
DE3728706A1 (de) * 1987-08-28 1988-10-27 Kurt Mannl Rotierendes einspritzsystem fuer raketentriebwerke
DE3923948A1 (de) * 1988-03-24 1991-01-24 Aerojet General Co Zweistufige raketenverbrennungskammer
DE102016208731A1 (de) * 2016-05-20 2017-11-23 Airbus Ds Gmbh Raketenantriebssystem und Verfahren zum Betreiben eines Raketenantriebssystems
US10968865B2 (en) 2016-05-20 2021-04-06 Arianegroup Gmbh Rocket propulsion system and method for operating a rocket propulsion system

Also Published As

Publication number Publication date
BE562285A (enrdf_load_stackoverflow)
GB847084A (en) 1960-09-07
FR1187946A (fr) 1959-09-17

Similar Documents

Publication Publication Date Title
DE1071421B (de) Brennkammer für Gasturbinen oder Raketenmotoren
DE69410424T2 (de) Brennstoff-Einspritzvorrichtung
DE2825431C2 (de) Vorrichtung zur Zufuhr von Luft und Brennstoff in die Brennkammer eines Gasturbinentriebwerkes
DE69412484T2 (de) Verbrennungskammer eines gasturbinenmotors
DE2442895C2 (de) Vorrichtung zur Zuführung von Luft und Brennstoff in eine Brennkammer
DE2833027C2 (enrdf_load_stackoverflow)
DE2131490A1 (de) Luftmischduese
DE833741C (de) Brennkammeraggregat fuer Gasturbinen
EP0438682B1 (de) Abgassystem mit einem Partikelfilter und einem Regenerierungsbrenner
DE3017034C2 (enrdf_load_stackoverflow)
DE69306291T2 (de) Einteiliger Aufsatz für eine Dualringbrennkammer
DE3007763A1 (de) Brenneinrichtung fuer gasturbinentriebwerke
DE2143012B2 (de) Brenneranordnung bei einer Gasturbinen-Brennkammer
DE1039784B (de) Brennkammer fuer Gasturbinen oder Strahltriebwerke
DE2739677A1 (de) Verbrennungseinrichtung fuer gasturbinentriebwerke
DE887286C (de) Nachbrennvorrichtung fuer Strahltriebwerke
DE69216990T2 (de) Gasturbinenbrennkammer für sehr grosse höhen
DE2116429A1 (de) Brennkammer fur Gasturbinenmaschinen
DE1198130B (de) Brenner fuer ringfoermige Brennkammern
DE2422362B2 (de) Ringbrennkammer für ein Gasturbinentriebwerk
DE1179767B (de) Brennkammer
DE1122776B (de) Flammhaltereinheit
DE10237604B4 (de) Nachverbrennungseinrichtung mit einem Brenner
DE2320594C3 (de) Zweikreis-Strahltriebwerk
DE1184562B (de) Zweistrom-Gasturbinenstrahltriebwerk