GB847084A - Combustion chamber for a gas turbine or rocket motor - Google Patents

Combustion chamber for a gas turbine or rocket motor

Info

Publication number
GB847084A
GB847084A GB3426856A GB3426856A GB847084A GB 847084 A GB847084 A GB 847084A GB 3426856 A GB3426856 A GB 3426856A GB 3426856 A GB3426856 A GB 3426856A GB 847084 A GB847084 A GB 847084A
Authority
GB
United Kingdom
Prior art keywords
supplied
inlet
tubes
fuel
space
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
GB3426856A
Other languages
English (en)
Inventor
Sidney Allen
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors Ltd
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
Priority to BE562285D priority Critical patent/BE562285A/xx
Priority to DENDAT1071421D priority patent/DE1071421B/de
Application filed by Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB3426856A priority patent/GB847084A/en
Priority to FR1187946D priority patent/FR1187946A/fr
Publication of GB847084A publication Critical patent/GB847084A/en
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
    • F02K9/42—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)
GB3426856A 1956-11-09 1956-11-09 Combustion chamber for a gas turbine or rocket motor Expired GB847084A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BE562285D BE562285A (enrdf_load_stackoverflow) 1956-11-09
DENDAT1071421D DE1071421B (de) 1956-11-09 Brennkammer für Gasturbinen oder Raketenmotoren
GB3426856A GB847084A (en) 1956-11-09 1956-11-09 Combustion chamber for a gas turbine or rocket motor
FR1187946D FR1187946A (fr) 1956-11-09 1957-11-08 Chambre de combustion

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
GB847084A true GB847084A (en) 1960-09-07

Family

ID=10363522

Family Applications (1)

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

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 (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3451223A (en) * 1966-12-06 1969-06-24 Howard Vern Main Rocket engine chamber cooling and injection system
US3462956A (en) * 1966-11-29 1969-08-26 Lutz T Kayser Rocket drive cooling arrangement
GB2196392A (en) * 1986-10-14 1988-04-27 Gen Electric Multiple-propellant propulsion apparatus & method
GB2196391A (en) * 1986-10-14 1988-04-27 Gen Electric Prolpusion apparatus & method
US4817890A (en) * 1986-10-14 1989-04-04 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
US4840025A (en) * 1986-10-14 1989-06-20 General Electric Company Multiple-propellant air vehicle and propulsion system
CN112177801A (zh) * 2020-08-31 2021-01-05 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

Families Citing this family (9)

* 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
DE1297942B (de) * 1966-11-29 1969-06-19 Kayser Lutz T Anordnung zur Raketentriebwerkskuehlung
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
FR2503794B1 (fr) * 1981-04-13 1986-04-25 Europ Propulsion Chambre de combustion de propulseur-fusee a divergent multiple
DE3728706A1 (de) * 1987-08-28 1988-10-27 Kurt Mannl Rotierendes einspritzsystem fuer raketentriebwerke
US4882904A (en) * 1988-03-24 1989-11-28 Aerojet-General Corporation Two stage rocket combustor
DE102016208731A1 (de) 2016-05-20 2017-11-23 Airbus Ds Gmbh Raketenantriebssystem und Verfahren zum Betreiben eines Raketenantriebssystems
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

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3462956A (en) * 1966-11-29 1969-08-26 Lutz T Kayser Rocket drive cooling arrangement
US3451223A (en) * 1966-12-06 1969-06-24 Howard Vern Main Rocket engine chamber cooling and injection system
GB2196392A (en) * 1986-10-14 1988-04-27 Gen Electric Multiple-propellant propulsion apparatus & method
GB2196391A (en) * 1986-10-14 1988-04-27 Gen Electric Prolpusion apparatus & method
US4811556A (en) * 1986-10-14 1989-03-14 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
US4835959A (en) * 1986-10-14 1989-06-06 General Electric Company Multiple-propellant air vehicle and propulsion system
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
GB2196391B (en) * 1986-10-14 1991-06-26 Gen Electric Rocket propulsion system.
GB2196392B (en) * 1986-10-14 1991-06-26 Gen Electric Rocket propulsion system.
CN112177801A (zh) * 2020-08-31 2021-01-05 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

Also Published As

Publication number Publication date
FR1187946A (fr) 1959-09-17
DE1071421B (de) 1959-12-17
BE562285A (enrdf_load_stackoverflow)

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