GB699865A - Improvements in or relating to gas turbines - Google Patents

Improvements in or relating to gas turbines

Info

Publication number
GB699865A
GB699865A GB2708350A GB2708350A GB699865A GB 699865 A GB699865 A GB 699865A GB 2708350 A GB2708350 A GB 2708350A GB 2708350 A GB2708350 A GB 2708350A GB 699865 A GB699865 A GB 699865A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
air
nov
air inlet
relating
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
GB2708350A
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.)
ARTHUR WILLIAM POPE
W H Allen Sons & Co Ltd
Original Assignee
ARTHUR WILLIAM POPE
W H Allen Sons & Co 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 ARTHUR WILLIAM POPE, W H Allen Sons & Co Ltd filed Critical ARTHUR WILLIAM POPE
Priority to GB2708350A priority Critical patent/GB699865A/en
Publication of GB699865A publication Critical patent/GB699865A/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

699,865. Generating combustion products under pressure. ALLEN, SONS & CO., Ltd., W. H., SMITH, F. S., and POPE, A. W. Nov. 6, 1951 [Nov. 6, 1950], No. 27083/50. Class 51(i) [Also in Group XXVI] An air jacketed, annular combustion chamber 13 of octagonal or circular cross-section has a diffuser ring 5 which is divided by plates 6, 7 to form main and subsidiary air inlet passages 9, 10 respectively and a fuel and air inlet passage 8. The inner walls 25, 23 of the combustion chamber are made of heat resisting alloy steel and are provided with air openings or formed by guide or vane elements. The air openings are more closely spaced towards the inner diameter of the combustion chamber which has an intermediate wall 26 defining an annular discharge passage 22.
GB2708350A 1950-11-06 1950-11-06 Improvements in or relating to gas turbines Expired GB699865A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2708350A GB699865A (en) 1950-11-06 1950-11-06 Improvements in or relating to gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2708350A GB699865A (en) 1950-11-06 1950-11-06 Improvements in or relating to gas turbines

Publications (1)

Publication Number Publication Date
GB699865A true GB699865A (en) 1953-11-18

Family

ID=10253897

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2708350A Expired GB699865A (en) 1950-11-06 1950-11-06 Improvements in or relating to gas turbines

Country Status (1)

Country Link
GB (1) GB699865A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1000189B (en) * 1955-06-28 1957-01-03 Bmw Studiengesellschaft Fuer T Gas turbine, in particular small gas turbine
DE1108516B (en) * 1956-04-03 1961-06-08 Bristol Siddeley Engines Ltd burning device
DE1130646B (en) * 1954-08-19 1962-05-30 Laval Steam Turbine Co Diagonal gas turbine power plant
US3103325A (en) * 1960-06-13 1963-09-10 Leutzinger Rudolph Leslie Radial jet engine
US3163003A (en) * 1954-10-25 1964-12-29 Garrett Corp Gas turbine compressor
DE1184561B (en) * 1958-08-01 1964-12-31 Bmw Triebwerkbau Gmbh Jet engine for short or vertical take-off aircraft, in particular for installation in the wings of airplanes
DE1278794B (en) * 1960-11-04 1968-09-26 Rudolph Birmann Verpuffungsgasturbinenanlage
GB2197911A (en) * 1986-07-28 1988-06-02 Teledyne Ind Fuel supply path in a gas turbine engine

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1130646B (en) * 1954-08-19 1962-05-30 Laval Steam Turbine Co Diagonal gas turbine power plant
US3163003A (en) * 1954-10-25 1964-12-29 Garrett Corp Gas turbine compressor
DE1000189B (en) * 1955-06-28 1957-01-03 Bmw Studiengesellschaft Fuer T Gas turbine, in particular small gas turbine
US2924937A (en) * 1955-06-28 1960-02-16 Bmw Triebwerkbau Ges Mit Besch Gas turbine
DE1108516B (en) * 1956-04-03 1961-06-08 Bristol Siddeley Engines Ltd burning device
DE1184561B (en) * 1958-08-01 1964-12-31 Bmw Triebwerkbau Gmbh Jet engine for short or vertical take-off aircraft, in particular for installation in the wings of airplanes
US3103325A (en) * 1960-06-13 1963-09-10 Leutzinger Rudolph Leslie Radial jet engine
DE1278794B (en) * 1960-11-04 1968-09-26 Rudolph Birmann Verpuffungsgasturbinenanlage
GB2197911A (en) * 1986-07-28 1988-06-02 Teledyne Ind Fuel supply path in a gas turbine engine
GB2197911B (en) * 1986-07-28 1991-03-20 Teledyne Ind Turbine shaft fuel pump

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