CH411465A - Chambre de combustion comprenant des tubes de flamme reliés entre eux par des tubes de jonction - Google Patents

Chambre de combustion comprenant des tubes de flamme reliés entre eux par des tubes de jonction

Info

Publication number
CH411465A
CH411465A CH744364A CH744364A CH411465A CH 411465 A CH411465 A CH 411465A CH 744364 A CH744364 A CH 744364A CH 744364 A CH744364 A CH 744364A CH 411465 A CH411465 A CH 411465A
Authority
CH
Switzerland
Prior art keywords
tubes
combustion chamber
junction
interconnected
flame
Prior art date
Application number
CH744364A
Other languages
English (en)
Inventor
Leo Mulcahey Robert
Original Assignee
United Aircraft 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 Aircraft Corp filed Critical United Aircraft Corp
Publication of CH411465A publication Critical patent/CH411465A/fr

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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes

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)
CH744364A 1963-06-18 1964-06-08 Chambre de combustion comprenant des tubes de flamme reliés entre eux par des tubes de jonction CH411465A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US288823A US3184918A (en) 1963-06-18 1963-06-18 Cooling arrangement for crossover tubes

Publications (1)

Publication Number Publication Date
CH411465A true CH411465A (fr) 1966-04-15

Family

ID=23108790

Family Applications (1)

Application Number Title Priority Date Filing Date
CH744364A CH411465A (fr) 1963-06-18 1964-06-08 Chambre de combustion comprenant des tubes de flamme reliés entre eux par des tubes de jonction

Country Status (7)

Country Link
US (1) US3184918A (fr)
BE (1) BE648950A (fr)
CH (1) CH411465A (fr)
FR (1) FR1398352A (fr)
GB (1) GB1037955A (fr)
NL (1) NL6406585A (fr)
SE (1) SE302221B (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1500110A (fr) * 1966-07-08 1967-11-03 Snecma Perfectionnements aux turbo-réacteurs
US3391535A (en) * 1966-08-31 1968-07-09 United Aircraft Corp Burner assemblies
GB1104599A (en) * 1966-12-16 1968-02-28 Rolls Royce Gas turbine engine combustion chamber
US3811274A (en) * 1972-08-30 1974-05-21 United Aircraft Corp Crossover tube construction
US3995422A (en) * 1975-05-21 1976-12-07 General Electric Company Combustor liner structure
US4887432A (en) * 1988-10-07 1989-12-19 Westinghouse Electric Corp. Gas turbine combustion chamber with air scoops
DE4309131A1 (de) * 1993-03-22 1994-09-29 Abb Management Ag Verfahren und Vorrichtung zur Nachlaufbeeinflussung bei Brennkammereinbauten
US5402635A (en) * 1993-09-09 1995-04-04 Westinghouse Electric Corporation Gas turbine combustor with cooling cross-flame tube connector
US20130333389A1 (en) * 2012-06-15 2013-12-19 General Electric Company Cross fire tube retention system for a gas turbine engine
US10161635B2 (en) 2014-06-13 2018-12-25 Rolls-Royce Corporation Combustor with spring-loaded crossover tubes
JP6325930B2 (ja) * 2014-07-24 2018-05-16 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
JP6521283B2 (ja) * 2014-09-25 2019-05-29 三菱日立パワーシステムズ株式会社 燃焼器、ガスタービン
US20170059165A1 (en) 2015-08-28 2017-03-02 Rolls-Royce High Temperature Composites Inc. Cmc cross-over tube
FR3096114B1 (fr) * 2019-05-13 2022-10-28 Safran Aircraft Engines Chambre de combustion comprenant des moyens de refroidissement d’une zone d’enveloppe annulaire en aval d’une cheminée

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
US2851859A (en) * 1952-07-16 1958-09-16 Onera (Off Nat Aerospatiale) Improvements in combustion chambers for turbo-jet, turbo-prop and similar engines
US2979893A (en) * 1958-04-02 1961-04-18 United Aircraft Corp Thrust reverser

Also Published As

Publication number Publication date
BE648950A (fr) 1964-10-01
SE302221B (fr) 1968-07-08
FR1398352A (fr) 1965-05-07
US3184918A (en) 1965-05-25
GB1037955A (en) 1966-08-03
NL6406585A (fr) 1964-12-21

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