FR1486551A - Cooling structure for combustion chambers of gas turbine engines - Google Patents

Cooling structure for combustion chambers of gas turbine engines

Info

Publication number
FR1486551A
FR1486551A FR67563A FR67563A FR1486551A FR 1486551 A FR1486551 A FR 1486551A FR 67563 A FR67563 A FR 67563A FR 67563 A FR67563 A FR 67563A FR 1486551 A FR1486551 A FR 1486551A
Authority
FR
France
Prior art keywords
gas turbine
combustion chambers
cooling structure
turbine engines
engines
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
FR67563A
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.)
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
Priority to FR67563A priority Critical patent/FR1486551A/en
Application granted granted Critical
Publication of FR1486551A publication Critical patent/FR1486551A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
FR67563A 1966-06-30 1966-06-30 Cooling structure for combustion chambers of gas turbine engines Expired FR1486551A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR67563A FR1486551A (en) 1966-06-30 1966-06-30 Cooling structure for combustion chambers of gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR67563A FR1486551A (en) 1966-06-30 1966-06-30 Cooling structure for combustion chambers of gas turbine engines

Publications (1)

Publication Number Publication Date
FR1486551A true FR1486551A (en) 1967-06-30

Family

ID=8612152

Family Applications (1)

Application Number Title Priority Date Filing Date
FR67563A Expired FR1486551A (en) 1966-06-30 1966-06-30 Cooling structure for combustion chambers of gas turbine engines

Country Status (1)

Country Link
FR (1) FR1486551A (en)

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