GB806349A - Improvements relating to combustion chambers - Google Patents

Improvements relating to combustion chambers

Info

Publication number
GB806349A
GB806349A GB28163/56A GB2816356A GB806349A GB 806349 A GB806349 A GB 806349A GB 28163/56 A GB28163/56 A GB 28163/56A GB 2816356 A GB2816356 A GB 2816356A GB 806349 A GB806349 A GB 806349A
Authority
GB
United Kingdom
Prior art keywords
segment
shroud portion
segments
combustion
air
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
GB28163/56A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB806349A publication Critical patent/GB806349A/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
    • F23R3/10—Air inlet arrangements for primary air

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

806,349. Generating combustion products under pressure. GENERAL ELECTRIC CO. Sept. 14, 1956 [Sept. 15, 1955], No. 28163/56. Class 51 (1). Combustion equipment for a gas turbine engine comprises an outer casing and an inner flame tube 4, the flame tube having an end cap 1 comprising a part-spherical annular shroud portion 13 defining ports 15 for the metering of air therethrough, and two coaxial annular segments 16, 17 of different mean diameters mounted within the shroud portion in partly overlapping relation. The segments are resiliently connected together by means of flexible metal connectors 19 and the smaller segment 17 is disposed upstream of the larger segment 16. The outer edge of the segment 16 is in slidable contact with the shroud portion 13 while the smaller segment 17 is resiliently connected to the shroud portion 13 by means of a ring member 21 secured by welding to the segment 17 and by means of clips 22 to the shroud. A fuel nozzle mounting ring 23 is secured to the inner edge of the smaller segment 17. The outer segment 16 has a plurality of louvres 25 in staggered formation in concentric rows therein for directing combustion air into the combustion space in a generally circumferential direction from the space between the shroud portion and the larger segment. The segments 16, 17 in the embodiment shown are each of frusto-conical form and the louvres in the segment 16 have arcuate slits arranged in a generally radial direction. The nozzle mounting ring 23 is formed with recesses 24 in its inner periphery so as to provide passages for the flow of cooling air over the nozzle. Air also flows radially inwardly through the annular gap 18 between the segments 16, 17. U.S.A. Specification 2,801,134 is referred to. Reference has been directed, by the Comptroller to Specification 677,602.
GB28163/56A 1955-09-15 1956-09-14 Improvements relating to combustion chambers Expired GB806349A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US534455A US2840989A (en) 1955-09-15 1955-09-15 End cap for combustor

Publications (1)

Publication Number Publication Date
GB806349A true GB806349A (en) 1958-12-23

Family

ID=24130111

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28163/56A Expired GB806349A (en) 1955-09-15 1956-09-14 Improvements relating to combustion chambers

Country Status (4)

Country Link
US (1) US2840989A (en)
CH (1) CH351800A (en)
DE (1) DE1043719B (en)
GB (1) GB806349A (en)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2990108A (en) * 1957-03-04 1961-06-27 Curtiss Wright Corp Compressor with annular discharge diffuser
US3316714A (en) * 1963-06-20 1967-05-02 Rolls Royce Gas turbine engine combustion equipment
US3391535A (en) * 1966-08-31 1968-07-09 United Aircraft Corp Burner assemblies
US3916619A (en) * 1972-10-30 1975-11-04 Hitachi Ltd Burning method for gas turbine combustor and a construction thereof
US4077205A (en) * 1975-12-05 1978-03-07 United Technologies Corporation Louver construction for liner of gas turbine engine combustor
US4199936A (en) * 1975-12-24 1980-04-29 The Boeing Company Gas turbine engine combustion noise suppressor
US4365470A (en) * 1980-04-02 1982-12-28 United Technologies Corporation Fuel nozzle guide and seal for a gas turbine engine
JPS5966619A (en) * 1982-10-06 1984-04-16 Hitachi Ltd Gas turbine combustor
US4848081A (en) * 1988-05-31 1989-07-18 United Technologies Corporation Cooling means for augmentor liner
US5407133A (en) * 1989-12-26 1995-04-18 United Technologies Corporation Cooled thin metal liner
US5129231A (en) * 1990-03-12 1992-07-14 United Technologies Corporation Cooled combustor dome heatshield
US5077969A (en) * 1990-04-06 1992-01-07 United Technologies Corporation Cooled liner for hot gas conduit
US7260936B2 (en) * 2004-08-27 2007-08-28 Pratt & Whitney Canada Corp. Combustor having means for directing air into the combustion chamber in a spiral pattern
US8171736B2 (en) * 2007-01-30 2012-05-08 Pratt & Whitney Canada Corp. Combustor with chamfered dome
FR2948988B1 (en) * 2009-08-04 2011-12-09 Snecma TURBOMACHINE COMBUSTION CHAMBER COMPRISING ENHANCED AIR INLET ORIFICES
JP2011102669A (en) * 2009-11-10 2011-05-26 Mitsubishi Heavy Ind Ltd Gas turbine combustor and gas turbine
CN103930218B (en) 2011-10-27 2017-08-29 固瑞克明尼苏达有限公司 Sprayer fluid feed system with collapsible bushing pipe
WO2013063294A1 (en) 2011-10-27 2013-05-02 Graco Minnesota Inc. Melter cartridge
DE102013221286B4 (en) 2013-10-21 2021-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Combustion chamber, in particular gas turbine combustion chamber, e.g. B. for an aircraft engine
US9796492B2 (en) 2015-03-12 2017-10-24 Graco Minnesota Inc. Manual check valve for priming a collapsible fluid liner for a sprayer
TW202110541A (en) 2019-05-31 2021-03-16 美商葛萊兒明尼蘇達股份有限公司 Handheld fluid sprayer
US11920790B2 (en) * 2021-11-03 2024-03-05 General Electric Company Wavy annular dilution slots for lower emissions

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE478436A (en) * 1943-09-03 1948-01-31 Gen Electric
US2458497A (en) * 1945-05-05 1949-01-11 Babcock & Wilcox Co Combustion chamber
FR962862A (en) * 1946-10-26 1950-06-22
US2657531A (en) * 1948-01-22 1953-11-03 Gen Electric Wall cooling arrangement for combustion devices
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner
GB677602A (en) * 1950-03-24 1952-08-20 British Thomson Houston Co Ltd Improvements in and relating to fluid fuel combustion chambers
US2555965A (en) * 1950-03-24 1951-06-05 Gen Electric End cap for fluid fuel combustors

Also Published As

Publication number Publication date
CH351800A (en) 1961-01-31
US2840989A (en) 1958-07-01
DE1043719B (en) 1958-11-13

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