GB1082232A - Gas turbine engine and rotary fuel injection means therefor - Google Patents

Gas turbine engine and rotary fuel injection means therefor

Info

Publication number
GB1082232A
GB1082232A GB3648664A GB3648664A GB1082232A GB 1082232 A GB1082232 A GB 1082232A GB 3648664 A GB3648664 A GB 3648664A GB 3648664 A GB3648664 A GB 3648664A GB 1082232 A GB1082232 A GB 1082232A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
therefor
fuel injection
fuel
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
GB3648664A
Inventor
Carl Francis Bachle
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.)
Continental Aviation and Engineering Corp
Original Assignee
Continental Aviation and Engineering Corp
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 Continental Aviation and Engineering Corp filed Critical Continental Aviation and Engineering Corp
Priority to GB3648664A priority Critical patent/GB1082232A/en
Publication of GB1082232A publication Critical patent/GB1082232A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means

Abstract

1,082,232. Burners. CONTINENTAL AVIATION & ENGINEERING CORPORATION. Sept. 5, 1964, No. 36486/64. Heading F4T. [Also in Division F1] The combustion zone 18 of a gas turbine engine annular combustion chamber is supplied with fuel through angularly spaced injection orifices 27 in an annular fuel slinger 25 rotating with the compressor drive-shaft 11. The fuel flows to the orifices 27 from a chamber 30 within the slinger supplied through ports 34 from an annular passageway 32 within a fixed distributing member 33. Figs. 4 to 7 (not shown) illustrate slightly modified slingers and distributing members.
GB3648664A 1964-09-05 1964-09-05 Gas turbine engine and rotary fuel injection means therefor Expired GB1082232A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3648664A GB1082232A (en) 1964-09-05 1964-09-05 Gas turbine engine and rotary fuel injection means therefor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3648664A GB1082232A (en) 1964-09-05 1964-09-05 Gas turbine engine and rotary fuel injection means therefor

Publications (1)

Publication Number Publication Date
GB1082232A true GB1082232A (en) 1967-09-06

Family

ID=10388601

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3648664A Expired GB1082232A (en) 1964-09-05 1964-09-05 Gas turbine engine and rotary fuel injection means therefor

Country Status (1)

Country Link
GB (1) GB1082232A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2602003A1 (en) * 1986-07-28 1988-01-29 Teledyne Ind FUEL PUMP IN THE TREE OF A TURBINE
WO2005036058A1 (en) * 2003-10-08 2005-04-21 Honeywell International Inc. Auxiliary power unit having a rotary fuel slinger

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2602003A1 (en) * 1986-07-28 1988-01-29 Teledyne Ind FUEL PUMP IN THE TREE OF A TURBINE
WO2005036058A1 (en) * 2003-10-08 2005-04-21 Honeywell International Inc. Auxiliary power unit having a rotary fuel slinger
US7036321B2 (en) 2003-10-08 2006-05-02 Honeywell International, Inc. Auxiliary power unit having a rotary fuel slinger

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