GB2021204A - Gas Turbine Combustion Chamber - Google Patents

Gas Turbine Combustion Chamber

Info

Publication number
GB2021204A
GB2021204A GB7916293A GB7916293A GB2021204A GB 2021204 A GB2021204 A GB 2021204A GB 7916293 A GB7916293 A GB 7916293A GB 7916293 A GB7916293 A GB 7916293A GB 2021204 A GB2021204 A GB 2021204A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
gas turbine
turbine combustion
flanges
apertures
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.)
Granted
Application number
GB7916293A
Other versions
GB2021204B (en
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB7916293A priority Critical patent/GB2021204B/en
Publication of GB2021204A publication Critical patent/GB2021204A/en
Application granted granted Critical
Publication of GB2021204B publication Critical patent/GB2021204B/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

Abstract

The combustion chamber wall 16 has a cooling ring 18 comprising two flanges 20, 22 defining between them an angle and a scoop ring 19a associated with the most downstream flange, apertures 24, 26 in the flanges being directed respectively upstream and downstream. Additional apertures 28 are also provided. <IMAGE>
GB7916293A 1978-05-20 1979-05-10 Gas turbinr combustion chamber Expired GB2021204B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7916293A GB2021204B (en) 1978-05-20 1979-05-10 Gas turbinr combustion chamber

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB2099078 1978-05-20
GB7916293A GB2021204B (en) 1978-05-20 1979-05-10 Gas turbinr combustion chamber

Publications (2)

Publication Number Publication Date
GB2021204A true GB2021204A (en) 1979-11-28
GB2021204B GB2021204B (en) 1982-10-13

Family

ID=26255031

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7916293A Expired GB2021204B (en) 1978-05-20 1979-05-10 Gas turbinr combustion chamber

Country Status (1)

Country Link
GB (1) GB2021204B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4463568A (en) * 1981-07-28 1984-08-07 Rolls-Royce Limited Fuel injector for gas turbine engines
US4893475A (en) * 1986-12-10 1990-01-16 Rolls-Royce Plc Combustion apparatus for a gas turbine
EP1489359A1 (en) * 2003-06-17 2004-12-22 Snecma Moteurs Annular combustion chamber for turbomachine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4463568A (en) * 1981-07-28 1984-08-07 Rolls-Royce Limited Fuel injector for gas turbine engines
US4893475A (en) * 1986-12-10 1990-01-16 Rolls-Royce Plc Combustion apparatus for a gas turbine
EP1489359A1 (en) * 2003-06-17 2004-12-22 Snecma Moteurs Annular combustion chamber for turbomachine
FR2856468A1 (en) * 2003-06-17 2004-12-24 Snecma Moteurs ANNULAR COMBUSTION CHAMBER OF TURBOMACHINE
US7155913B2 (en) 2003-06-17 2007-01-02 Snecma Moteurs Turbomachine annular combustion chamber

Also Published As

Publication number Publication date
GB2021204B (en) 1982-10-13

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee