FR1214261A - Gas turbojet channel wall - Google Patents

Gas turbojet channel wall

Info

Publication number
FR1214261A
FR1214261A FR1214261DA FR1214261A FR 1214261 A FR1214261 A FR 1214261A FR 1214261D A FR1214261D A FR 1214261DA FR 1214261 A FR1214261 A FR 1214261A
Authority
FR
France
Prior art keywords
channel wall
gas
gas turbojet
turbojet channel
turbojet
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
Other languages
French (fr)
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.)
Canadian Patents and Development Ltd
Original Assignee
Canadian Patents and Development Ltd
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 Canadian Patents and Development Ltd filed Critical Canadian Patents and Development Ltd
Application granted granted Critical
Publication of FR1214261A publication Critical patent/FR1214261A/en
Expired legal-status Critical Current

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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infra-red radiation suppressors
    • 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
FR1214261D 1957-10-28 1958-10-22 Gas turbojet channel wall Expired FR1214261A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1214261XA 1957-10-28 1957-10-28

Publications (1)

Publication Number Publication Date
FR1214261A true FR1214261A (en) 1960-04-07

Family

ID=22396655

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1214261D Expired FR1214261A (en) 1957-10-28 1958-10-22 Gas turbojet channel wall

Country Status (1)

Country Link
FR (1) FR1214261A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2556410A1 (en) * 1983-12-07 1985-06-14 Snecma DEVICE FOR CENTERING THE INSIDE RING OF A VARIABLE TIMING FINS STATOR
EP0216721A1 (en) * 1985-07-03 1987-04-01 United Technologies Corporation Liner construction
ITTO20080578A1 (en) * 2008-07-28 2010-01-29 Ansaldo Energia Spa CONNECTION GROUP TO CONNECT A PALLET TO A SUPPORT RING, IN PARTICULAR TO AN INTERNAL RING OF A COMPRESSOR STATOR

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2556410A1 (en) * 1983-12-07 1985-06-14 Snecma DEVICE FOR CENTERING THE INSIDE RING OF A VARIABLE TIMING FINS STATOR
EP0146449A1 (en) * 1983-12-07 1985-06-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Arrangement for centering an inner stator shroud supported by changeable blades
US4604030A (en) * 1983-12-07 1986-08-05 Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. Compressor with variable incidence stator vanes
EP0216721A1 (en) * 1985-07-03 1987-04-01 United Technologies Corporation Liner construction
ITTO20080578A1 (en) * 2008-07-28 2010-01-29 Ansaldo Energia Spa CONNECTION GROUP TO CONNECT A PALLET TO A SUPPORT RING, IN PARTICULAR TO AN INTERNAL RING OF A COMPRESSOR STATOR
EP2149678A1 (en) * 2008-07-28 2010-02-03 Ansaldo Energia S.P.A. Connection assembly for connecting a blade to a support ring

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