FR1232288A - Improvements to combustion chambers - Google Patents

Improvements to combustion chambers

Info

Publication number
FR1232288A
FR1232288A FR802843A FR802843A FR1232288A FR 1232288 A FR1232288 A FR 1232288A FR 802843 A FR802843 A FR 802843A FR 802843 A FR802843 A FR 802843A FR 1232288 A FR1232288 A FR 1232288A
Authority
FR
France
Prior art keywords
combustion chambers
chambers
combustion
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
FR802843A
Other languages
French (fr)
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.)
Bristol Siddeley Engines Ltd
Original Assignee
Bristol Siddeley Engines 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 claimed from GB19541/57A external-priority patent/GB851448A/en
Application filed by Bristol Siddeley Engines Ltd filed Critical Bristol Siddeley Engines Ltd
Priority to FR802843A priority Critical patent/FR1232288A/en
Application granted granted Critical
Publication of FR1232288A publication Critical patent/FR1232288A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion or thrust chambers having cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR802843A 1957-06-21 1959-08-14 Improvements to combustion chambers Expired FR1232288A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR802843A FR1232288A (en) 1957-06-21 1959-08-14 Improvements to combustion chambers

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB19541/57A GB851448A (en) 1957-06-21 1957-06-21 Improvements in and relating to combustion chambers
FR802843A FR1232288A (en) 1957-06-21 1959-08-14 Improvements to combustion chambers

Publications (1)

Publication Number Publication Date
FR1232288A true FR1232288A (en) 1960-10-06

Family

ID=26184295

Family Applications (1)

Application Number Title Priority Date Filing Date
FR802843A Expired FR1232288A (en) 1957-06-21 1959-08-14 Improvements to combustion chambers

Country Status (1)

Country Link
FR (1) FR1232288A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2309729A1 (en) * 1975-05-02 1976-11-26 Messerschmitt Boelkow Blohm Cooling medium collection ring for rocket propulsion - having connecting flange with one sided dove tail joint to prevent displacement
FR2471486A1 (en) * 1979-12-08 1981-06-19 Messerschmitt Boelkow Blohm DEVICE FOR COOLING THE PUSHING TUYER OF A SPUTTER PROPELLER

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2309729A1 (en) * 1975-05-02 1976-11-26 Messerschmitt Boelkow Blohm Cooling medium collection ring for rocket propulsion - having connecting flange with one sided dove tail joint to prevent displacement
FR2471486A1 (en) * 1979-12-08 1981-06-19 Messerschmitt Boelkow Blohm DEVICE FOR COOLING THE PUSHING TUYER OF A SPUTTER PROPELLER

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