CA1031973A - Chambre de combustion pour moteur a turbine a gaz - Google Patents

Chambre de combustion pour moteur a turbine a gaz

Info

Publication number
CA1031973A
CA1031973A CA228,697A CA228697A CA1031973A CA 1031973 A CA1031973 A CA 1031973A CA 228697 A CA228697 A CA 228697A CA 1031973 A CA1031973 A CA 1031973A
Authority
CA
Canada
Prior art keywords
combustion chamber
gas turbine
turbine engine
engine
gas
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
CA228,697A
Other languages
English (en)
Other versions
CA228697S (fr
Inventor
John A. Irwin
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.)
Motors Liquidation Co
Original Assignee
General Motors 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 General Motors Corp filed Critical General Motors Corp
Application granted granted Critical
Publication of CA1031973A publication Critical patent/CA1031973A/fr
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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CA228,697A 1974-10-24 1975-06-06 Chambre de combustion pour moteur a turbine a gaz Expired CA1031973A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/517,807 US3990231A (en) 1974-10-24 1974-10-24 Interconnections between ceramic rings permitting relative radial movement

Publications (1)

Publication Number Publication Date
CA1031973A true CA1031973A (fr) 1978-05-30

Family

ID=24061311

Family Applications (1)

Application Number Title Priority Date Filing Date
CA228,697A Expired CA1031973A (fr) 1974-10-24 1975-06-06 Chambre de combustion pour moteur a turbine a gaz

Country Status (3)

Country Link
US (1) US3990231A (fr)
CA (1) CA1031973A (fr)
GB (1) GB1512439A (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2845588A1 (de) * 1978-10-19 1980-04-24 Motoren Turbinen Union Brennkammer fuer gasturbinentriebwerke
US4380896A (en) * 1980-09-22 1983-04-26 The United States Of America As Represented By The Secretary Of The Army Annular combustor having ceramic liner
US4363208A (en) * 1980-11-10 1982-12-14 General Motors Corporation Ceramic combustor mounting
JPS58138927A (ja) * 1982-02-15 1983-08-18 Nissan Motor Co Ltd 燃焼器の支持装置
US6182451B1 (en) 1994-09-14 2001-02-06 Alliedsignal Inc. Gas turbine combustor waving ceramic combustor cans and an annular metallic combustor
US7007480B2 (en) * 2003-04-09 2006-03-07 Honeywell International, Inc. Multi-axial pivoting combustor liner in gas turbine engine
FR2914707B1 (fr) * 2007-04-05 2009-10-30 Snecma Propulsion Solide Sa Procede d'assemblage avec recouvrement de deux pieces ayant des coefficients de dilatation differents et assemblage ainsi obtenu
EP3002519B1 (fr) * 2014-09-30 2020-05-27 Ansaldo Energia Switzerland AG Agencement de chambre de combustion avec système de fixation pour pièces de chambre de combustion
US10989413B2 (en) * 2019-07-17 2021-04-27 General Electric Company Axial retention assembly for combustor components of a gas turbine engine
US12173900B2 (en) * 2021-11-11 2024-12-24 General Electric Company Combustion liner having a dilution passage

Family Cites Families (7)

* 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.
US2725929A (en) * 1951-11-24 1955-12-06 Selas Corp Of America Combustion chamber type burner
US2858673A (en) * 1955-06-28 1958-11-04 Gen Electric Sectional liner structure for combustor
US2877623A (en) * 1956-11-27 1959-03-17 Klompas Nicholas Annular fairing structure for the rear frame housing of a gas turbine engine
US2933895A (en) * 1957-12-31 1960-04-26 Gen Electric Combustion chamber
US3485043A (en) * 1968-02-01 1969-12-23 Gen Electric Shingled combustion liner
GB1240009A (en) * 1968-07-27 1971-07-21 Leyland Gas Turbines Ltd Flame tube

Also Published As

Publication number Publication date
GB1512439A (en) 1978-06-01
US3990231A (en) 1976-11-09

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