FR1214261A - Gas turbojet channel wall - Google Patents
Gas turbojet channel wallInfo
- 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
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; Infrared 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
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)
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 |
-
1958
- 1958-10-22 FR FR1214261D patent/FR1214261A/en not_active Expired
Cited By (6)
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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