GB1150344A - Combustion Apparatus for Gas Turbine Engines - Google Patents

Combustion Apparatus for Gas Turbine Engines

Info

Publication number
GB1150344A
GB1150344A GB3362065A GB3362065A GB1150344A GB 1150344 A GB1150344 A GB 1150344A GB 3362065 A GB3362065 A GB 3362065A GB 3362065 A GB3362065 A GB 3362065A GB 1150344 A GB1150344 A GB 1150344A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
walls
air
annular
combustion apparatus
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
GB3362065A
Inventor
Kenneth Greenwood
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Joseph Lucas Industries 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
Application filed by Lucas Industries Ltd, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB3362065A priority Critical patent/GB1150344A/en
Publication of GB1150344A publication Critical patent/GB1150344A/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones

Abstract

1,150,344. Gas turbine engine combustion chambers. JOSEPH LUCAS (INDUSTRIES) Ltd. Aug. 3, 1966 [Aug. 5, 1965], No.33620/65. Heading F1L. Combustion apparatus for a gas turbine engine comprises an annular flame tube having inner and outer walls 12, 13. Disposed downstream of the inlet 26 is a flare plate 25 which, as shown, may be divided into two parts by an annular hollow wall 24 which also divides the inlet into two parts. Annular baffle plates 23 deflect the gases away from the walls 12, 13, 24 upstream of a row of openings 22 for the entry of secondary combustion air and dilution air. The baffle plates 23 on the walls 12, 13 may be replaced by a row of small holes in each wall 12, 13 affording access for a stream of air which itself forms a baffle for the gases.
GB3362065A 1965-08-05 1965-08-05 Combustion Apparatus for Gas Turbine Engines Expired GB1150344A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3362065A GB1150344A (en) 1965-08-05 1965-08-05 Combustion Apparatus for Gas Turbine Engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3362065A GB1150344A (en) 1965-08-05 1965-08-05 Combustion Apparatus for Gas Turbine Engines

Publications (1)

Publication Number Publication Date
GB1150344A true GB1150344A (en) 1969-04-30

Family

ID=10355285

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3362065A Expired GB1150344A (en) 1965-08-05 1965-08-05 Combustion Apparatus for Gas Turbine Engines

Country Status (1)

Country Link
GB (1) GB1150344A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2838258A1 (en) * 1977-09-02 1979-03-15 Snecma COMBUSTION CHAMBER ARRANGEMENT
EP0488557A1 (en) * 1990-11-26 1992-06-03 General Electric Company Double dome combustor
GB2263733A (en) * 1992-01-28 1993-08-04 Snecma Turbomachine with removable combustion chamber.
US5479774A (en) * 1991-04-30 1996-01-02 Rolls-Royce Plc Combustion chamber assembly in a gas turbine engine
US5490380A (en) * 1992-06-12 1996-02-13 United Technologies Corporation Method for performing combustion

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2838258A1 (en) * 1977-09-02 1979-03-15 Snecma COMBUSTION CHAMBER ARRANGEMENT
EP0488557A1 (en) * 1990-11-26 1992-06-03 General Electric Company Double dome combustor
US5479774A (en) * 1991-04-30 1996-01-02 Rolls-Royce Plc Combustion chamber assembly in a gas turbine engine
GB2263733A (en) * 1992-01-28 1993-08-04 Snecma Turbomachine with removable combustion chamber.
GB2263733B (en) * 1992-01-28 1995-01-18 Snecma Turbomachine with removable combustion chamber
US5490380A (en) * 1992-06-12 1996-02-13 United Technologies Corporation Method for performing combustion

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Legal Events

Date Code Title Description
PS Patent sealed
PE Patent expired