CH313849A - Axialströmungsmaschine - Google Patents
AxialströmungsmaschineInfo
- Publication number
- CH313849A CH313849A CH313849DA CH313849A CH 313849 A CH313849 A CH 313849A CH 313849D A CH313849D A CH 313849DA CH 313849 A CH313849 A CH 313849A
- Authority
- CH
- Switzerland
- Prior art keywords
- axial flow
- flow machine
- machine
- axial
- flow
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/023—Details or means for fluid extraction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23637/51A GB712051A (en) | 1951-10-10 | 1951-10-10 | Improvements in or relating to axial-flow fluid machines |
Publications (1)
Publication Number | Publication Date |
---|---|
CH313849A true CH313849A (de) | 1956-05-15 |
Family
ID=10198865
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH313849D CH313849A (de) | 1951-10-10 | 1952-10-09 | Axialströmungsmaschine |
Country Status (4)
Country | Link |
---|---|
US (1) | US2910268A (de) |
CH (1) | CH313849A (de) |
FR (1) | FR1068974A (de) |
GB (1) | GB712051A (de) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3085400A (en) * | 1959-03-23 | 1963-04-16 | Gen Electric | Cooling fluid impeller for elastic fluid turbines |
US3034763A (en) * | 1959-08-20 | 1962-05-15 | United Aircraft Corp | Rotor construction |
US3398881A (en) * | 1967-01-10 | 1968-08-27 | United Aircraft Corp | Compressor bleed device |
GB1217807A (en) * | 1969-07-19 | 1970-12-31 | Rolls Royce | Gas turbine engine |
US3609059A (en) * | 1969-10-03 | 1971-09-28 | Gen Motors Corp | Isothermal wheel |
US3647313A (en) * | 1970-06-01 | 1972-03-07 | Gen Electric | Gas turbine engines with compressor rotor cooling |
US3632221A (en) * | 1970-08-03 | 1972-01-04 | Gen Electric | Gas turbine engine cooling system incorporating a vortex shaft valve |
US3897168A (en) * | 1974-03-05 | 1975-07-29 | Westinghouse Electric Corp | Turbomachine extraction flow guide vanes |
FR2401320A1 (fr) * | 1977-08-26 | 1979-03-23 | Snecma | Perfectionnements au refroidissement des turbines a gaz |
GB2075123B (en) * | 1980-05-01 | 1983-11-16 | Gen Electric | Turbine cooling air deswirler |
US4541774A (en) * | 1980-05-01 | 1985-09-17 | General Electric Company | Turbine cooling air deswirler |
FR2491549B1 (fr) * | 1980-10-08 | 1985-07-05 | Snecma | Dispositif de refroidissement d'une turbine a gaz, par prelevement d'air au niveau du compresseur |
FR2552164B1 (fr) * | 1983-09-21 | 1986-12-26 | Snecma | Disque de compresseur avec accelerateur centripete integre pour l'aspiration d'air dans un dispositif de refroidissement d'une turbine a gaz |
US4759688A (en) * | 1986-12-16 | 1988-07-26 | Allied-Signal Inc. | Cooling flow side entry for cooled turbine blading |
FR2609500B1 (fr) * | 1987-01-14 | 1991-04-12 | Snecma | Disque de compresseur de turbomachine avec accelerateur centripete pour l'aspiration d'air de refroidissement de la turbine |
GB2207465B (en) * | 1987-07-18 | 1992-02-19 | Rolls Royce Plc | A compressor and air bleed arrangement |
DE19617539B4 (de) * | 1996-05-02 | 2006-02-09 | Alstom | Rotor für eine thermische Turbomaschine |
US5997244A (en) * | 1997-05-16 | 1999-12-07 | Alliedsignal Inc. | Cooling airflow vortex spoiler |
FR2834758B1 (fr) * | 2002-01-17 | 2004-04-02 | Snecma Moteurs | Dispositif pour redresser l'air d'alimentation d'un prelevement centripete dans un compresseur |
FR2834753B1 (fr) * | 2002-01-17 | 2004-09-03 | Snecma Moteurs | Disque de compresseur axial de turbomachine a prelevement d'air centripete |
US8047768B2 (en) * | 2009-01-12 | 2011-11-01 | General Electric Company | Split impeller configuration for synchronizing thermal response between turbine wheels |
US8348599B2 (en) * | 2010-03-26 | 2013-01-08 | General Electric Company | Turbine rotor wheel |
US20120003091A1 (en) * | 2010-06-30 | 2012-01-05 | Eugenio Yegro Segovia | Rotor assembly for use in gas turbine engines and method for assembling the same |
US9145772B2 (en) | 2012-01-31 | 2015-09-29 | United Technologies Corporation | Compressor disk bleed air scallops |
EP2732145B1 (de) | 2012-02-10 | 2016-06-08 | General Electric Company | Gasturbine mit einem druckbeaufschlagten sumpf |
US9121413B2 (en) * | 2012-03-22 | 2015-09-01 | General Electric Company | Variable length compressor rotor pumping vanes |
US10208668B2 (en) | 2015-09-30 | 2019-02-19 | Rolls-Royce Corporation | Turbine engine advanced cooling system |
US10415465B2 (en) * | 2017-12-21 | 2019-09-17 | United Technologies Corporation | Axial compressor with inter-stage centrifugal compressor |
CN112360761A (zh) * | 2021-01-12 | 2021-02-12 | 中国航发上海商用航空发动机制造有限责任公司 | 向心增压引气装置及系统 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB479427A (en) * | 1935-05-31 | 1938-01-31 | Gyoergy Jendrassik | Improvements in rotary compressors |
US2177159A (en) * | 1938-03-11 | 1939-10-24 | Edward A Stalker | Pumping machinery |
US2294586A (en) * | 1941-08-04 | 1942-09-01 | Del Conveyor & Mfg Company | Axial flow fan structure |
US2419669A (en) * | 1942-05-08 | 1947-04-29 | Fed Reserve Bank | Diffuser for centrifugal compressors |
BE488010A (de) * | 1947-03-11 | 1900-01-01 | ||
US2618433A (en) * | 1948-06-23 | 1952-11-18 | Curtiss Wright Corp | Means for bleeding air from compressors |
DE838188C (de) * | 1950-08-12 | 1952-05-05 | Köln Dipl.-Ing. Max Adolf Müller | Radial von außen nach innen durchströmter Tragflügelverdichter |
-
1951
- 1951-10-10 GB GB23637/51A patent/GB712051A/en not_active Expired
-
1952
- 1952-10-08 US US313746A patent/US2910268A/en not_active Expired - Lifetime
- 1952-10-09 CH CH313849D patent/CH313849A/de unknown
- 1952-10-10 FR FR1068974D patent/FR1068974A/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB712051A (en) | 1954-07-14 |
FR1068974A (fr) | 1954-07-02 |
US2910268A (en) | 1959-10-27 |
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