NL267395A - - Google Patents

Info

Publication number
NL267395A
NL267395A NL267395DA NL267395A NL 267395 A NL267395 A NL 267395A NL 267395D A NL267395D A NL 267395DA NL 267395 A NL267395 A NL 267395A
Authority
NL
Netherlands
Application number
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.)
Publication of NL267395A publication Critical patent/NL267395A/xx

Links

Classifications

    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means
    • 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
    • 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
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
NL267395D 1960-07-22 NL267395A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US44586A US3086363A (en) 1960-07-22 1960-07-22 Annular transition duct

Publications (1)

Publication Number Publication Date
NL267395A true NL267395A (ja)

Family

ID=21933179

Family Applications (1)

Application Number Title Priority Date Filing Date
NL267395D NL267395A (ja) 1960-07-22

Country Status (5)

Country Link
US (1) US3086363A (ja)
BE (1) BE606411A (ja)
CH (1) CH402517A (ja)
GB (1) GB924333A (ja)
NL (1) NL267395A (ja)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4411134A (en) * 1981-10-26 1983-10-25 Moir David L Apparatus for the repair and replacement of transition ducts on jet engines and bracket therefor
US4720236A (en) * 1984-12-21 1988-01-19 United Technologies Corporation Coolable stator assembly for a gas turbine engine
US5274991A (en) * 1992-03-30 1994-01-04 General Electric Company Dry low NOx multi-nozzle combustion liner cap assembly
EP0564181B1 (en) * 1992-03-30 1996-11-20 General Electric Company Combustor dome construction
EP1284391A1 (de) * 2001-08-14 2003-02-19 Siemens Aktiengesellschaft Brennkammeranordnung für Gasturbinen
GB2402714A (en) * 2003-06-12 2004-12-15 Rolls Royce Plc Cannular combustor with directly associated nozzle guide vanes
FR2887588B1 (fr) * 2005-06-24 2011-06-03 Snecma Moteurs Interface ventilee entre une chambre de combustion et un distributeur haute pression de turboreacteur et turboreacteur comportant cette interface
US8091365B2 (en) * 2008-08-12 2012-01-10 Siemens Energy, Inc. Canted outlet for transition in a gas turbine engine
EP2206885A1 (de) * 2009-01-08 2010-07-14 Siemens Aktiengesellschaft Gasturbine
US8381526B2 (en) * 2010-02-15 2013-02-26 General Electric Company Systems and methods of providing high pressure air to a head end of a combustor
FR3047544B1 (fr) * 2016-02-10 2018-03-02 Safran Aircraft Engines Chambre de combustion de turbomachine
GB2571591B (en) * 2018-03-03 2020-08-05 Rolls Royce Plc Rear outer discharge nozzle

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE487768A (ja) * 1947-03-14
US2670600A (en) * 1947-06-17 1954-03-02 Bristol Aeroplane Co Ltd Air distribution system for flame tubes of gas turbine engines
US2609663A (en) * 1951-07-21 1952-09-09 United Aircraft Corp Rotatable combustion apparatus for aligning individual flame tubes with access partsor manholes
US2916874A (en) * 1957-01-31 1959-12-15 United Aircraft Corp Engine construction

Also Published As

Publication number Publication date
US3086363A (en) 1963-04-23
BE606411A (fr) 1962-01-22
GB924333A (en) 1963-04-24
CH402517A (de) 1965-11-15

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