GB864517A - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
GB864517A
GB864517A GB2395/58A GB239558A GB864517A GB 864517 A GB864517 A GB 864517A GB 2395/58 A GB2395/58 A GB 2395/58A GB 239558 A GB239558 A GB 239558A GB 864517 A GB864517 A GB 864517A
Authority
GB
United Kingdom
Prior art keywords
air
chamber
combustion
openings
turbine
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
GB2395/58A
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.)
Avco Manufacturing Corp
Original Assignee
Avco Manufacturing 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 Avco Manufacturing Corp filed Critical Avco Manufacturing Corp
Publication of GB864517A publication Critical patent/GB864517A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/145—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chamber being in the reverse flow-type

Abstract

864,517. Generating combustion products under pressure. AVCO MANUFACTURING CORPORATION. Jan. 24, 1958 [May 1, 1957], No. 2395/58. Class 51 (1). [Also in Group XXVI] The air discharge from the compressor 18 discharges through a radial flow diffuser 20a provided with vanes 21 into an annular air chamber 22 provided with vanes 21a to reduce the swirl. One half of this air flow is deflected by scoops 26 to form dilution air in the combustion chamber 25. The remainder of the air flows to the chamber 22a from whence it flows through openings in the wall 27 to form the primary air supply. Openings 29a, 29b, 29c are arranged so that the air flow through the openings is in the same direction as the gas flow in the combustion space. Primary air and fuel is provided by a number of fuel injection units 28 spaced around the chamber 25. The combustion gases make substantially a 180 degree turn 32 to enter the compressor driving turbine 34 and useful power turbine 36. The arrangement is such that the power turbine 36 together with the rear section of the annular combustion chamber may be removed by unbolting a flanged joint. The combustion chamber 25, passage 32 and turbine casing are connected by slip-joints for this purpose.
GB2395/58A 1957-05-01 1958-01-24 Gas turbine engine Expired GB864517A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US864517XA 1957-05-01 1957-05-01

Publications (1)

Publication Number Publication Date
GB864517A true GB864517A (en) 1961-04-06

Family

ID=22198651

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2395/58A Expired GB864517A (en) 1957-05-01 1958-01-24 Gas turbine engine

Country Status (1)

Country Link
GB (1) GB864517A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1206659B (en) * 1962-05-17 1965-12-09 Daimler Benz Ag Arrangement and drive of the lubricant units in gas turbine engines
DE1260232B (en) * 1962-08-02 1968-02-01 Daimler Benz Ag Device for converting mechanical control movements into hydraulic control pressures
JPS5469205U (en) * 1977-10-26 1979-05-17
EP0298014A1 (en) * 1987-06-29 1989-01-04 United Technologies Corporation Engine modularity

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1206659B (en) * 1962-05-17 1965-12-09 Daimler Benz Ag Arrangement and drive of the lubricant units in gas turbine engines
DE1260232B (en) * 1962-08-02 1968-02-01 Daimler Benz Ag Device for converting mechanical control movements into hydraulic control pressures
JPS5469205U (en) * 1977-10-26 1979-05-17
JPS5743058Y2 (en) * 1977-10-26 1982-09-22
EP0298014A1 (en) * 1987-06-29 1989-01-04 United Technologies Corporation Engine modularity

Similar Documents

Publication Publication Date Title
US3010281A (en) Toroidal combustion chamber
GB836088A (en) Improvements in turbojet engine afterburners
US2632299A (en) Precombustion chamber
GB947873A (en) An annular combustion chamber for gas turbines
GB801281A (en) Improvements in or relating to reaction turbines
GB1344359A (en) Combustion equipment for gas turbine engines
GB904142A (en) Improvements in or relating to gas-turbine engines
GB935903A (en) Gas turbine power plant having centripetal flow compressors and centrifugal flow turbines
GB864517A (en) Gas turbine engine
GB891278A (en) A gas turbine power unit
GB736823A (en) Engine combustion chambers
GB899213A (en) Combustion chambers
US2974487A (en) Combustion system for a gas turbine engine
GB694448A (en) Improvements in or relating to gas-turbine engines
GB1354333A (en) Regenerative gas turbine engines
GB1196168A (en) Combustion Assemblies for Gas-Turbine Engines
GB694414A (en) Improvements in or relating to internal combustion gas turbine engines
GB620270A (en) Improvements in or relating to turbine apparatus
GB543918A (en) Improvements and relating to combustion chambers
GB925349A (en) Improvements relating to prime movers incorporating gas turbines
GB866969A (en) Gas turbine engines
GB842677A (en) Improvements relating to gas turbine engines
GB898368A (en) Improved combustion chamber
GB791917A (en) Improvements in and relating to gas turbine plants
GB765175A (en) Improvements in and relating to the ignition of turbine engines having an annular combustion chamber