BE608937A - Rotor pour turbo-ventilateur - Google Patents
Rotor pour turbo-ventilateurInfo
- Publication number
- BE608937A BE608937A BE608937A BE608937A BE608937A BE 608937 A BE608937 A BE 608937A BE 608937 A BE608937 A BE 608937A BE 608937 A BE608937 A BE 608937A BE 608937 A BE608937 A BE 608937A
- Authority
- BE
- Belgium
- Prior art keywords
- turbo
- rotor
- fan
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
-
- 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
- F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
-
- 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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US61248A US3070284A (en) | 1960-10-07 | 1960-10-07 | Turbo-fan rotor |
Publications (1)
Publication Number | Publication Date |
---|---|
BE608937A true BE608937A (fr) | 1962-02-01 |
Family
ID=22034583
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE608937A BE608937A (fr) | 1960-10-07 | 1961-10-06 | Rotor pour turbo-ventilateur |
Country Status (3)
Country | Link |
---|---|
US (1) | US3070284A (fr) |
BE (1) | BE608937A (fr) |
GB (1) | GB950527A (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3404831A (en) * | 1966-12-07 | 1968-10-08 | Gen Electric | Turbine bucket supporting structure |
GB1118898A (en) * | 1967-04-03 | 1968-07-03 | Rolls Royce | Fluid flow machine |
GB2192237B (en) * | 1986-07-02 | 1990-05-16 | Rolls Royce Plc | Gas turbine engine power turbine |
US5108259A (en) * | 1988-12-19 | 1992-04-28 | General Electric Company | Flexible connector for use in aircraft |
US6454535B1 (en) | 2000-10-31 | 2002-09-24 | General Electric Company | Blisk |
WO2015049548A1 (fr) * | 2013-10-03 | 2015-04-09 | Franco Tosi Meccanica S.P.A. | Étage de rotor de turbine axiale avec rapport de corde/pas amélioré |
US10119403B2 (en) * | 2014-02-13 | 2018-11-06 | United Technologies Corporation | Mistuned concentric airfoil assembly and method of mistuning same |
GB2571176B (en) * | 2017-12-14 | 2022-07-20 | Safran Aircraft Engines | Damping device |
CN110439623B (zh) * | 2019-08-14 | 2024-05-14 | 上海两擎机电科技合伙企业(有限合伙) | 飞机发动机风扇叶片用金属包边、加工工装及加工方法 |
US20240286757A1 (en) * | 2023-02-23 | 2024-08-29 | ESS 2 Tech, LLC | Fluid accelerator |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA584125A (fr) * | 1959-09-29 | E. Moss Charles | Ailes pour moteurs a turbine a gaz | |
US2429681A (en) * | 1942-02-27 | 1947-10-28 | Griffith Alan Arnold | Thrust balancing construction for turbines, compressors, and the like |
US2391623A (en) * | 1943-12-08 | 1945-12-25 | Armstrong Siddeley Motors Ltd | Bladed rotor |
US2518660A (en) * | 1944-09-07 | 1950-08-15 | Wright Aeronautical Corp | Internal-combustion engine and exhaust gas turbine therefor |
US2625365A (en) * | 1949-02-26 | 1953-01-13 | Curtiss Wright Corp | Shrouded impeller |
US2868439A (en) * | 1954-05-07 | 1959-01-13 | Goodyear Aircraft Corp | Plastic axial-flow compressor for gas turbines |
US2819870A (en) * | 1955-04-18 | 1958-01-14 | Oleh A Wayne | Sheet metal blade base |
-
1960
- 1960-10-07 US US61248A patent/US3070284A/en not_active Expired - Lifetime
-
1961
- 1961-09-26 GB GB34417/61A patent/GB950527A/en not_active Expired
- 1961-10-06 BE BE608937A patent/BE608937A/fr unknown
Also Published As
Publication number | Publication date |
---|---|
GB950527A (en) | 1964-02-26 |
US3070284A (en) | 1962-12-25 |
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