FR1556914A - - Google Patents
Info
- Publication number
- FR1556914A FR1556914A FR1556914DA FR1556914A FR 1556914 A FR1556914 A FR 1556914A FR 1556914D A FR1556914D A FR 1556914DA FR 1556914 A FR1556914 A FR 1556914A
- Authority
- FR
- France
- 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
- 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
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 |
---|---|---|---|
GB15224/67A GB1118898A (en) | 1967-04-03 | 1967-04-03 | Fluid flow machine |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1556914A true FR1556914A (en) | 1969-02-07 |
Family
ID=10055250
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1556914D Expired FR1556914A (en) | 1967-04-03 | 1968-03-25 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3494539A (en) |
DE (1) | DE1751094A1 (en) |
FR (1) | FR1556914A (en) |
GB (1) | GB1118898A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2636375A1 (en) * | 1988-08-15 | 1990-03-16 | Gen Electric | REINFORCEMENT RING FOR LOW PRESSURE STAGE OF A COMPRESSOR |
WO2015049548A1 (en) * | 2013-10-03 | 2015-04-09 | Franco Tosi Meccanica S.P.A. | Rotor stage of axial turbine with improved chord/pitch ratio |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1428365A (en) * | 1972-03-15 | 1976-03-17 | Rolls Royce | Fluid flow machines |
GB1485032A (en) * | 1974-08-23 | 1977-09-08 | Rolls Royce | Gas turbine engine casing |
US4012165A (en) * | 1975-12-08 | 1977-03-15 | United Technologies Corporation | Fan structure |
GB1549422A (en) * | 1976-10-19 | 1979-08-08 | Rolls Royce | Axial flow gas turbine engine compressor |
GB2192238B (en) * | 1986-07-02 | 1990-05-23 | Rolls Royce Plc | Gas turbine engine power turbine |
GB2192237B (en) * | 1986-07-02 | 1990-05-16 | Rolls Royce Plc | Gas turbine engine power turbine |
US5224341A (en) * | 1992-01-06 | 1993-07-06 | United Technologies Corporation | Separable fan strut for a gas turbofan powerplant |
US5358382A (en) * | 1993-07-21 | 1994-10-25 | Eaton Corporation | Fan and fan drive assembly |
US5649419A (en) * | 1995-01-27 | 1997-07-22 | The Boeing Company | Rotating acoustically lined inlet splitter for a turbo-fan engine |
US7094033B2 (en) * | 2004-01-21 | 2006-08-22 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
GB2455785B (en) * | 2007-12-21 | 2009-11-11 | Rolls Royce Plc | Annular component |
US8667775B1 (en) * | 2009-08-05 | 2014-03-11 | The Boeing Company | Reverse flow engine core having a ducted fan with integrated secondary flow blades |
US8813864B2 (en) | 2011-09-09 | 2014-08-26 | Jack D. Layton | Support system for a box blade attached to a tractor |
GB201705732D0 (en) * | 2017-04-10 | 2017-05-24 | Rolls Royce Plc | Acoustic attenuation in gas turbine engines |
US20200017229A1 (en) * | 2018-07-13 | 2020-01-16 | Bell Helicopter Textron Inc. | Fan clutch for convertible engine |
GB202216057D0 (en) * | 2022-10-31 | 2022-12-14 | Rolls Royce Plc | Flow splitter |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3216654A (en) * | 1965-11-09 | Tureeofan engine | ||
US3037742A (en) * | 1959-09-17 | 1962-06-05 | Gen Motors Corp | Compressor turbine |
US3070284A (en) * | 1960-10-07 | 1962-12-25 | Gen Electric | Turbo-fan rotor |
GB1003313A (en) * | 1960-11-17 | 1965-09-02 | Bristol Siddeley Engines Ltd | Improvements in blades for ducted axial flow machines |
GB981476A (en) * | 1963-11-04 | 1965-01-27 | Rolls Royce | Gas turbine engine vane assembly |
-
1967
- 1967-04-03 GB GB15224/67A patent/GB1118898A/en not_active Expired
-
1968
- 1968-03-14 US US712986A patent/US3494539A/en not_active Expired - Lifetime
- 1968-03-25 FR FR1556914D patent/FR1556914A/fr not_active Expired
- 1968-04-02 DE DE19681751094 patent/DE1751094A1/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2636375A1 (en) * | 1988-08-15 | 1990-03-16 | Gen Electric | REINFORCEMENT RING FOR LOW PRESSURE STAGE OF A COMPRESSOR |
WO2015049548A1 (en) * | 2013-10-03 | 2015-04-09 | Franco Tosi Meccanica S.P.A. | Rotor stage of axial turbine with improved chord/pitch ratio |
Also Published As
Publication number | Publication date |
---|---|
GB1118898A (en) | 1968-07-03 |
US3494539A (en) | 1970-02-10 |
DE1751094A1 (en) | 1970-08-13 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
TP | Transmission of property | ||
ST | Notification of lapse |