BE755508A - Rotor pour moteurs a turbine a gaz - Google Patents
Rotor pour moteurs a turbine a gazInfo
- Publication number
- BE755508A BE755508A BE755508DA BE755508A BE 755508 A BE755508 A BE 755508A BE 755508D A BE755508D A BE 755508DA BE 755508 A BE755508 A BE 755508A
- Authority
- BE
- Belgium
- Prior art keywords
- rotor
- gas turbine
- turbine engines
- engines
- gas
- Prior art date
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
- 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
- F01D5/021—Blade-carrying members, e.g. rotors for flow machines or engines with only one axial stage
-
- 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
- F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
- F01D5/087—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor in the radial passages of the rotor disc
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US55119066A | 1966-05-16 | 1966-05-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE755508A true BE755508A (fr) | 1971-02-01 |
Family
ID=24200221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE755508D BE755508A (fr) | 1966-05-16 | Rotor pour moteurs a turbine a gaz |
Country Status (2)
Country | Link |
---|---|
US (1) | US3588277A (fr) |
BE (1) | BE755508A (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3832090A (en) * | 1972-12-01 | 1974-08-27 | Avco Corp | Air cooling of turbine blades |
US3982852A (en) * | 1974-11-29 | 1976-09-28 | General Electric Company | Bore vane assembly for use with turbine discs having bore entry cooling |
US4102603A (en) * | 1975-12-15 | 1978-07-25 | General Electric Company | Multiple section rotor disc |
US4820122A (en) * | 1988-04-25 | 1989-04-11 | United Technologies Corporation | Dirt removal means for air cooled blades |
US4820123A (en) * | 1988-04-25 | 1989-04-11 | United Technologies Corporation | Dirt removal means for air cooled blades |
US20090169385A1 (en) * | 2004-12-01 | 2009-07-02 | Suciu Gabriel L | Fan-turbine rotor assembly with integral inducer section for a tip turbine engine |
WO2006060001A1 (fr) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Rotor de ventilateur pour moteur a turbine de bout |
WO2006060003A2 (fr) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Pale de ventilateur comprenant une section de diffuseur integrale et une section de pale de turbine a aube destine a une moteur a turbine a aube |
WO2006072193A1 (fr) * | 2005-01-05 | 2006-07-13 | New Noah Technology (Shenzhen) Co., Ltd. | Systeme de transition d'informations a distance pour machine portative d'apprentissage reseau multimedia et procede correspondant |
US8079802B2 (en) * | 2008-06-30 | 2011-12-20 | Mitsubishi Heavy Industries, Ltd. | Gas turbine |
GB201000982D0 (en) * | 2010-01-22 | 2010-03-10 | Rolls Royce Plc | A rotor disc |
-
0
- BE BE755508D patent/BE755508A/fr unknown
-
1966
- 1966-05-16 US US551190A patent/US3588277A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US3588277A (en) | 1971-06-28 |
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