IL62558A0 - Combustor liner construction for gas turbine engines - Google Patents

Combustor liner construction for gas turbine engines

Info

Publication number
IL62558A0
IL62558A0 IL62558A IL6255881A IL62558A0 IL 62558 A0 IL62558 A0 IL 62558A0 IL 62558 A IL62558 A IL 62558A IL 6255881 A IL6255881 A IL 6255881A IL 62558 A0 IL62558 A0 IL 62558A0
Authority
IL
Israel
Prior art keywords
gas turbine
turbine engines
combustor liner
liner construction
construction
Prior art date
Application number
IL62558A
Other languages
English (en)
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of IL62558A0 publication Critical patent/IL62558A0/xx

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
    • F23R3/002—Wall structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)
IL62558A 1980-04-02 1981-04-02 Combustor liner construction for gas turbine engines IL62558A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/136,652 US4414816A (en) 1980-04-02 1980-04-02 Combustor liner construction

Publications (1)

Publication Number Publication Date
IL62558A0 true IL62558A0 (en) 1981-06-29

Family

ID=22473775

Family Applications (1)

Application Number Title Priority Date Filing Date
IL62558A IL62558A0 (en) 1980-04-02 1981-04-02 Combustor liner construction for gas turbine engines

Country Status (7)

Country Link
US (1) US4414816A (xx)
JP (1) JPS57426A (xx)
DE (1) DE3113383A1 (xx)
FR (1) FR2479900A1 (xx)
GB (1) GB2074308A (xx)
IL (1) IL62558A0 (xx)
SE (1) SE8102133L (xx)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4912922A (en) * 1972-12-19 1990-04-03 General Electric Company Combustion chamber construction
GB2118710B (en) * 1981-12-31 1985-05-22 Secr Defence Improvements in or relating to combustion chamber wall cooling
US4567730A (en) * 1983-10-03 1986-02-04 General Electric Company Shielded combustor
US4796423A (en) * 1983-12-19 1989-01-10 General Electric Company Sheet metal panel
GB2160964B (en) * 1984-06-25 1988-04-07 Gen Electric Combustion chamber construction
FR2567250A1 (fr) * 1984-07-06 1986-01-10 Gen Electric Chambre de combustion pour moteur a turbine a gaz
DE3535442A1 (de) * 1985-10-04 1987-04-09 Mtu Muenchen Gmbh Ringbrennkammer fuer gasturbinentriebwerke
US4854122A (en) * 1988-01-28 1989-08-08 The United States Of America As Represented By The Secretary Of The Air Force Augmentor curtain liner assembly for sharing tensile loading
US5144795A (en) * 1991-05-14 1992-09-08 The United States Of America As Represented By The Secretary Of The Air Force Fluid cooled hot duct liner structure
US5653110A (en) * 1991-07-22 1997-08-05 General Electric Company Film cooling of jet engine components
US5201887A (en) * 1991-11-26 1993-04-13 United Technologies Corporation Damper for augmentor liners
CA2089285C (en) * 1992-03-30 2002-06-25 Stephen Winthrop Falls Segmented centerbody for a double annular combustor
GB2267736B (en) * 1992-06-09 1995-08-09 Gen Electric Segmented turbine flowpath assembly
US5318402A (en) * 1992-09-21 1994-06-07 General Electric Company Compressor liner spacing device
DE59208713D1 (de) 1992-11-09 1997-08-21 Asea Brown Boveri Gasturbinen-Brennkammer
JPH06234628A (ja) * 1993-02-09 1994-08-23 Kao Corp 皮膚外用剤
US5327727A (en) * 1993-04-05 1994-07-12 General Electric Company Micro-grooved heat transfer combustor wall
US5337568A (en) * 1993-04-05 1994-08-16 General Electric Company Micro-grooved heat transfer wall
US5363654A (en) * 1993-05-10 1994-11-15 General Electric Company Recuperative impingement cooling of jet engine components
FR2708086B1 (fr) * 1993-06-30 1995-09-01 Snecma Structure tubulaire sectorisée travaillant à l'implosion.
FR2710968B1 (fr) * 1993-10-06 1995-11-03 Snecma Chambre de combustion à double paroi.
US5524438A (en) * 1994-12-15 1996-06-11 United Technologies Corporation Segmented bulkhead liner for a gas turbine combustor
US5680767A (en) * 1995-09-11 1997-10-28 General Electric Company Regenerative combustor cooling in a gas turbine engine
JP2890033B2 (ja) * 1996-11-05 1999-05-10 科学技術庁航空宇宙技術研究所長 ガスタービン燃焼器
CN1246638C (zh) * 2001-04-27 2006-03-22 西门子公司 燃烧室、尤其是燃气轮机的燃烧室
US7578134B2 (en) * 2006-01-11 2009-08-25 General Electric Company Methods and apparatus for assembling gas turbine engines
DE102011007562A1 (de) * 2011-04-18 2012-10-18 Man Diesel & Turbo Se Brennkammergehäuse und damit ausgerüstete Gasturbine
GB201113249D0 (en) 2011-08-02 2011-09-14 Rolls Royce Plc A combustion chamber
US9163837B2 (en) * 2013-02-27 2015-10-20 Siemens Aktiengesellschaft Flow conditioner in a combustor of a gas turbine engine
WO2015017180A1 (en) 2013-08-01 2015-02-05 United Technologies Corporation Attachment scheme for a ceramic bulkhead panel
GB201322838D0 (en) 2013-12-23 2014-02-12 Rolls Royce Plc A combustion chamber
GB201501817D0 (en) 2015-02-04 2015-03-18 Rolls Royce Plc A combustion chamber and a combustion chamber segment
US10101029B2 (en) * 2015-03-30 2018-10-16 United Technologies Corporation Combustor panels and configurations for a gas turbine engine
US10816212B2 (en) 2016-04-22 2020-10-27 Rolls-Royce Plc Combustion chamber having a hook and groove connection
GB201613110D0 (en) * 2016-07-29 2016-09-14 Rolls Royce Plc A combustion chamber
CN117091162A (zh) * 2022-05-13 2023-11-21 通用电气公司 具有稀释孔结构的燃烧器
CN117091159A (zh) * 2022-05-13 2023-11-21 通用电气公司 燃烧器衬里

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH255541A (de) * 1947-05-12 1948-06-30 Bbc Brown Boveri & Cie Gekühlte metallische Brennkammer zur Erzeugung von Heiz- und Treibgasen.
GB700004A (en) * 1949-12-12 1953-11-25 Babcock & Wilcox Ltd Improvements in or relating to combustion apparatus
BE535497A (xx) * 1954-02-26
NL113358C (xx) * 1957-02-18
CH428324A (de) * 1964-05-21 1967-01-15 Prvni Brnenska Strojirna Brennkammer
US3422620A (en) * 1967-05-04 1969-01-21 Westinghouse Electric Corp Combustion apparatus
US3706203A (en) * 1970-10-30 1972-12-19 United Aircraft Corp Wall structure for a gas turbine engine
US4132066A (en) * 1977-09-23 1979-01-02 United Technologies Corporation Combustor liner for gas turbine engine
US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
US4253301A (en) * 1978-10-13 1981-03-03 General Electric Company Fuel injection staged sectoral combustor for burning low-BTU fuel gas

Also Published As

Publication number Publication date
US4414816A (en) 1983-11-15
DE3113383A1 (de) 1982-04-08
JPS57426A (en) 1982-01-05
SE8102133L (sv) 1981-10-03
GB2074308A (en) 1981-10-28
FR2479900A1 (fr) 1981-10-09

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