GB636624A - Improvements in or relating to high temperature gas ducts - Google Patents

Improvements in or relating to high temperature gas ducts

Info

Publication number
GB636624A
GB636624A GB22241/47A GB2224147A GB636624A GB 636624 A GB636624 A GB 636624A GB 22241/47 A GB22241/47 A GB 22241/47A GB 2224147 A GB2224147 A GB 2224147A GB 636624 A GB636624 A GB 636624A
Authority
GB
United Kingdom
Prior art keywords
air
holes
chamber
gas
walls
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
GB22241/47A
Other languages
English (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.)
RAYMOND ARTHUR BOULTER
WALTER FREDERICK SHILLING
Power Jets Research and Development Ltd
Original Assignee
RAYMOND ARTHUR BOULTER
WALTER FREDERICK SHILLING
Power Jets Research and Development 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 RAYMOND ARTHUR BOULTER, WALTER FREDERICK SHILLING, Power Jets Research and Development Ltd filed Critical RAYMOND ARTHUR BOULTER
Publication of GB636624A publication Critical patent/GB636624A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Gas Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB22241/47A 1947-08-11 1947-08-11 Improvements in or relating to high temperature gas ducts Expired GB636624A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB275237X 1947-08-11

Publications (1)

Publication Number Publication Date
GB636624A true GB636624A (en) 1950-05-03

Family

ID=10260976

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22241/47A Expired GB636624A (en) 1947-08-11 1947-08-11 Improvements in or relating to high temperature gas ducts

Country Status (5)

Country Link
US (1) US2664702A (US08197722-20120612-C00042.png)
CH (1) CH275237A (US08197722-20120612-C00042.png)
FR (1) FR988963A (US08197722-20120612-C00042.png)
GB (1) GB636624A (US08197722-20120612-C00042.png)
NL (1) NL74196C (US08197722-20120612-C00042.png)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2872971A (en) * 1959-02-10 Combustion chambers for jet propulsion
GB694484A (en) * 1949-06-30 1953-07-22 Rolls Royce Improvements relating to combustion equipment for gas turbine engines
US2722180A (en) * 1950-05-12 1955-11-01 Oran T Mcilvaine Fuel burners
US2815069A (en) * 1951-06-29 1957-12-03 Orr & Sembower Inc Burner apparatus
US2958194A (en) * 1951-09-24 1960-11-01 Power Jets Res & Dev Ltd Cooled flame tube
GB721209A (en) * 1951-09-24 1955-01-05 Power Jets Res & Dev Ltd Combustion apparatus
GB736699A (en) * 1952-09-10 1955-09-14 Ca Nat Research Council Pulsating torch igniter for combustion chambers
GB736823A (en) * 1953-01-19 1955-09-14 Lucas Industries Ltd Engine combustion chambers
US2972230A (en) * 1954-01-13 1961-02-21 Gen Motors Corp Automobile gas turbine
DE1032622B (de) * 1955-09-22 1958-06-19 Power Jets Res & Dev Ltd Leitung zur Fuehrung eines heissen, stroemenden Mediums
US2988139A (en) * 1956-11-14 1961-06-13 Sebac Nouvelie S A Spraying device
US3031012A (en) * 1957-12-27 1962-04-24 Gen Thermique Procedes Brola S Combustion apparatus
US3175361A (en) * 1959-08-05 1965-03-30 Phillips Petroleum Co Turbojet engine and its operation
US3316714A (en) * 1963-06-20 1967-05-02 Rolls Royce Gas turbine engine combustion equipment
GB1073335A (en) * 1965-06-21 1967-06-21 Rolls Royce Gas turbine engine combustion chamber
US4012902A (en) * 1974-03-29 1977-03-22 Phillips Petroleum Company Method of operating a gas turbine combustor having an independent airstream to remove heat from the primary combustion zone
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
US4199936A (en) * 1975-12-24 1980-04-29 The Boeing Company Gas turbine engine combustion noise suppressor
US4122674A (en) * 1976-12-27 1978-10-31 The Boeing Company Apparatus for suppressing combustion noise within gas turbine engines
US4419863A (en) * 1981-09-30 1983-12-13 United Technologies Corporation Fuel-air mixing apparatus
US4475344A (en) * 1982-02-16 1984-10-09 Westinghouse Electric Corp. Low smoke combustor for land based combustion turbines
US4687436A (en) * 1986-08-05 1987-08-18 Tadao Shigeta Gasified fuel combustion apparatus
US5220795A (en) * 1991-04-16 1993-06-22 General Electric Company Method and apparatus for injecting dilution air
JP3924136B2 (ja) * 2001-06-27 2007-06-06 三菱重工業株式会社 ガスタービン燃焼器
JP4709433B2 (ja) * 2001-06-29 2011-06-22 三菱重工業株式会社 ガスタービン燃焼器
US6568187B1 (en) * 2001-12-10 2003-05-27 Power Systems Mfg, Llc Effusion cooled transition duct
US8522557B2 (en) * 2006-12-21 2013-09-03 Siemens Aktiengesellschaft Cooling channel for cooling a hot gas guiding component
US20080264035A1 (en) * 2007-04-25 2008-10-30 Ricciardo Mark J Coolant flow swirler for a rocket engine
FR2948988B1 (fr) * 2009-08-04 2011-12-09 Snecma Chambre de combustion de turbomachine comprenant des orifices d'entree d'air ameliores
US20140331678A1 (en) * 2013-05-08 2014-11-13 Solar Turbines Incorporated System for distributing compressed air in a combustor

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB433631A (en) * 1934-02-19 1935-08-19 George Roddam Improvements in or relating to internal combustion turbines
GB539069A (en) * 1939-01-30 1941-08-27 Bbc Brown Boveri & Cie Improvements in and relating to pipes, containers, casings or the like for gases of high temperature
NL70682C (US08197722-20120612-C00042.png) * 1939-12-09
US2398654A (en) * 1940-01-24 1946-04-16 Anglo Saxon Petroleum Co Combustion burner
US2396068A (en) * 1941-06-10 1946-03-05 Youngash Reginald William Turbine
BE446918A (US08197722-20120612-C00042.png) * 1941-07-12
GB588086A (en) * 1943-04-01 1947-05-14 Power Jets Ltd Improvements relating to combustion apparatus
US2382564A (en) * 1943-09-16 1945-08-14 Laval Steam Turbine Co Turbine system
GB579424A (en) * 1943-09-29 1946-08-02 Lucas Ltd Joseph Improvements relating to liquid fuel combustion apparatus for generating gases for power purposes
BE489359A (US08197722-20120612-C00042.png) * 1944-10-05
US2447482A (en) * 1945-04-25 1948-08-24 Westinghouse Electric Corp Turbine apparatus
US2458497A (en) * 1945-05-05 1949-01-11 Babcock & Wilcox Co Combustion chamber
US2581999A (en) * 1946-02-01 1952-01-08 Gen Electric Hemispherical combustion chamber end dome having cooling air deflecting means
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner

Also Published As

Publication number Publication date
US2664702A (en) 1954-01-05
NL74196C (US08197722-20120612-C00042.png)
CH275237A (de) 1951-05-15
FR988963A (fr) 1951-09-03

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