CH268285A - Gasturbomaschine mit einem Kranz von Verbrennungskammern. - Google Patents

Gasturbomaschine mit einem Kranz von Verbrennungskammern.

Info

Publication number
CH268285A
CH268285A CH268285DA CH268285A CH 268285 A CH268285 A CH 268285A CH 268285D A CH268285D A CH 268285DA CH 268285 A CH268285 A CH 268285A
Authority
CH
Switzerland
Prior art keywords
ring
gas turbine
turbine engine
combustion chambers
chambers
Prior art date
Application number
Other languages
German (de)
English (en)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH268285A publication Critical patent/CH268285A/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F23R3/60—Support structures; Attaching or mounting means
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
CH268285D 1947-03-14 1948-03-12 Gasturbomaschine mit einem Kranz von Verbrennungskammern. CH268285A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB268285X 1947-03-14

Publications (1)

Publication Number Publication Date
CH268285A true CH268285A (de) 1950-05-15

Family

ID=10249898

Family Applications (1)

Application Number Title Priority Date Filing Date
CH268285D CH268285A (de) 1947-03-14 1948-03-12 Gasturbomaschine mit einem Kranz von Verbrennungskammern.

Country Status (5)

Country Link
US (1) US2594808A (fr)
BE (1) BE487768A (fr)
CH (1) CH268285A (fr)
FR (1) FR963256A (fr)
GB (1) GB622384A (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836959A (en) * 1950-01-11 1958-06-03 Gen Motors Corp Gas turbine engine supporting frame
US2702454A (en) * 1951-06-07 1955-02-22 United Aircraft Corp Transition piece providing a connection between the combustion chambers and the turbine nozzle in gas turbine power plants
NL267395A (fr) * 1960-07-22
US3116604A (en) * 1962-05-17 1964-01-07 Gen Electric Engine exhaust system
US3750398A (en) * 1971-05-17 1973-08-07 Westinghouse Electric Corp Static seal structure
US4573315A (en) * 1984-05-15 1986-03-04 A/S Kongsberg Vapenfabrikk Low pressure loss, convectively gas-cooled inlet manifold for high temperature radial turbine
US5414999A (en) * 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
EP0718468B1 (fr) * 1994-12-20 2001-10-31 General Electric Company Cadre de renforcement pour un élément de transition d'une chambre de combustion
WO1998016764A1 (fr) * 1996-10-16 1998-04-23 Siemens Westinghouse Power Corporation Joint a brosse toroidal pour interface de transition du dispositif combustor et de la turbine a gaz
US6116013A (en) * 1998-01-02 2000-09-12 Siemens Westinghouse Power Corporation Bolted gas turbine combustor transition coupling
US6886343B2 (en) * 2003-01-15 2005-05-03 General Electric Company Methods and apparatus for controlling engine clearance closures
WO2009103636A1 (fr) * 2008-02-20 2009-08-27 Alstom Technology Ltd. Machine thermique
US8616007B2 (en) * 2009-01-22 2013-12-31 Siemens Energy, Inc. Structural attachment system for transition duct outlet
JP2012145098A (ja) * 2010-12-21 2012-08-02 Toshiba Corp トランジションピースおよびガスタービン
US8938976B2 (en) * 2011-05-20 2015-01-27 Siemens Energy, Inc. Structural frame for gas turbine combustion cap assembly
US9404421B2 (en) 2014-01-23 2016-08-02 Siemens Energy, Inc. Structural support bracket for gas flow path

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445114A (en) * 1948-07-13 Arrangement of jet propulsion
US1794454A (en) * 1928-09-08 1931-03-03 Huron Ind Inc Sealing ring for rotating machines or cylinders
US1852279A (en) * 1929-05-16 1932-04-05 Superheater Co Ltd Means for securing tubes to headers
US2479573A (en) * 1943-10-20 1949-08-23 Gen Electric Gas turbine power plant
BE487120A (fr) * 1946-03-25

Also Published As

Publication number Publication date
BE487768A (fr)
FR963256A (fr) 1950-07-05
GB622384A (en) 1949-05-02
US2594808A (en) 1952-04-29

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