GB2289504B - Gas turbine propulsion unit - Google Patents
Gas turbine propulsion unitInfo
- Publication number
- GB2289504B GB2289504B GB9409381A GB9409381A GB2289504B GB 2289504 B GB2289504 B GB 2289504B GB 9409381 A GB9409381 A GB 9409381A GB 9409381 A GB9409381 A GB 9409381A GB 2289504 B GB2289504 B GB 2289504B
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- propulsion unit
- turbine propulsion
- unit
- gas
- 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 - Fee Related
Links
Classifications
-
- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Supercharger (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9409381A GB2289504B (en) | 1994-05-11 | 1994-05-11 | Gas turbine propulsion unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9409381A GB2289504B (en) | 1994-05-11 | 1994-05-11 | Gas turbine propulsion unit |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB9409381D0 GB9409381D0 (en) | 1994-06-29 |
| GB2289504A GB2289504A (en) | 1995-11-22 |
| GB2289504B true GB2289504B (en) | 1998-01-14 |
Family
ID=10754934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9409381A Expired - Fee Related GB2289504B (en) | 1994-05-11 | 1994-05-11 | Gas turbine propulsion unit |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2289504B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5881758A (en) * | 1996-03-28 | 1999-03-16 | The Boeing Company | Internal compression supersonic engine inlet |
| DE19962617C2 (en) * | 1999-12-23 | 2001-10-11 | Meyer Andreas Mathias | Turbo jet engine |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB622181A (en) * | 1947-03-11 | 1949-04-27 | Adrian Albert Lombard | Improvements relating to gas-turbine-engines |
| GB655871A (en) * | 1948-04-24 | 1951-08-08 | Devendra Nath Sharma | Improvements in or relating to internal combustion turbine power plants |
| GB706841A (en) * | 1948-07-17 | 1954-04-07 | Devendra Nath Sharma | Improvements relating to turbine jet propulsion power units |
| GB736503A (en) * | 1953-09-10 | 1955-09-07 | Rolls Royce | Improvements relating to gas-turbine engines |
| GB742242A (en) * | 1951-02-15 | 1955-12-21 | Power Jets Res & Dev Ltd | Improvements in the cooling of turbine rotors |
| GB757818A (en) * | 1954-04-06 | 1956-09-26 | Devendra Nath Sharma | Improvements relating to turbojet propulsion power units |
| GB1008886A (en) * | 1964-06-12 | 1965-11-03 | Rolls Royce | Gas turbine engine |
| GB2172056A (en) * | 1985-03-04 | 1986-09-10 | Gen Electric | Means and method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine |
| GB2206686A (en) * | 1984-12-17 | 1989-01-11 | Gen Electric | Gas-turbine augmentor |
| GB2216855A (en) * | 1988-04-07 | 1989-10-18 | Messerschmitt Boelkow Blohm | Propulsive unit arrangement for hypersonic flight vehicles |
| GB2264539A (en) * | 1992-02-21 | 1993-09-01 | Westinghouse Electric Corp | Heat transfer arrangement in a gas turbine |
-
1994
- 1994-05-11 GB GB9409381A patent/GB2289504B/en not_active Expired - Fee Related
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB622181A (en) * | 1947-03-11 | 1949-04-27 | Adrian Albert Lombard | Improvements relating to gas-turbine-engines |
| GB655871A (en) * | 1948-04-24 | 1951-08-08 | Devendra Nath Sharma | Improvements in or relating to internal combustion turbine power plants |
| GB706841A (en) * | 1948-07-17 | 1954-04-07 | Devendra Nath Sharma | Improvements relating to turbine jet propulsion power units |
| GB742242A (en) * | 1951-02-15 | 1955-12-21 | Power Jets Res & Dev Ltd | Improvements in the cooling of turbine rotors |
| GB736503A (en) * | 1953-09-10 | 1955-09-07 | Rolls Royce | Improvements relating to gas-turbine engines |
| GB757818A (en) * | 1954-04-06 | 1956-09-26 | Devendra Nath Sharma | Improvements relating to turbojet propulsion power units |
| GB1008886A (en) * | 1964-06-12 | 1965-11-03 | Rolls Royce | Gas turbine engine |
| GB2206686A (en) * | 1984-12-17 | 1989-01-11 | Gen Electric | Gas-turbine augmentor |
| GB2172056A (en) * | 1985-03-04 | 1986-09-10 | Gen Electric | Means and method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine |
| GB2216855A (en) * | 1988-04-07 | 1989-10-18 | Messerschmitt Boelkow Blohm | Propulsive unit arrangement for hypersonic flight vehicles |
| GB2264539A (en) * | 1992-02-21 | 1993-09-01 | Westinghouse Electric Corp | Heat transfer arrangement in a gas turbine |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2289504A (en) | 1995-11-22 |
| GB9409381D0 (en) | 1994-06-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0746680A4 (en) | Gas turbine generator set | |
| GB9415436D0 (en) | Auxiliary gas turbine engines | |
| GB2281356B (en) | Gas turbine engine turbine | |
| GB2287509B (en) | Air turbine | |
| SG104914A1 (en) | Gas turbine | |
| GB2295860B (en) | Turbine blade | |
| GB9606546D0 (en) | Gas turbine engine system | |
| GB2290833B (en) | Turbine blade | |
| GB9723022D0 (en) | Gas turbine apparatus | |
| GB2286431B (en) | Turbomachine rotor | |
| GB9608196D0 (en) | Gas turbine engine | |
| GB2319308B (en) | Gas turbine engine turbine system | |
| EP0770833A4 (en) | High-temperature gas generator | |
| GB9505452D0 (en) | Gas turbine engine | |
| GB9518424D0 (en) | Turbines | |
| GB9412550D0 (en) | Gas turbine system | |
| PL300467A1 (en) | Gas turbine unit | |
| GB2293628B (en) | Turbines | |
| PL320136A1 (en) | Liquefied gas generator | |
| GB2289504B (en) | Gas turbine propulsion unit | |
| BG99154A (en) | Gas turbine engine | |
| GB9610018D0 (en) | Gas turbine engine turbine | |
| GB2323896B (en) | Turbine blade units | |
| GB2435743B (en) | Gas turbine powerplant | |
| GB9513968D0 (en) | Gas turbine engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) | ||
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20030511 |