JPS57501096A - - Google Patents
Info
- Publication number
- JPS57501096A JPS57501096A JP50185980A JP50185980A JPS57501096A JP S57501096 A JPS57501096 A JP S57501096A JP 50185980 A JP50185980 A JP 50185980A JP 50185980 A JP50185980 A JP 50185980A JP S57501096 A JPS57501096 A JP S57501096A
- Authority
- JP
- Japan
- 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.)
- Pending
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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/44—Control of fuel supply responsive to the speed of aircraft, e.g. Mach number control, optimisation of fuel consumption
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US1980/000786 WO1982000048A1 (en) | 1980-06-23 | 1980-06-23 | Supersonic airplane engine configuration |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS57501096A true JPS57501096A (en) | 1982-06-24 |
Family
ID=22154406
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP50185980A Pending JPS57501096A (en) | 1980-06-23 | 1980-06-23 |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0054555A4 (en) |
| JP (1) | JPS57501096A (en) |
| WO (1) | WO1982000048A1 (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6575406B2 (en) | 2001-01-19 | 2003-06-10 | The Boeing Company | Integrated and/or modular high-speed aircraft |
| US7644888B2 (en) | 2002-05-15 | 2010-01-12 | The Boeing Company | High-speed aircraft and methods for their manufacture |
| US6651928B1 (en) | 2002-09-05 | 2003-11-25 | The Boeing Company | Aircraft engine nacelles and methods for their manufacture |
| US10259565B2 (en) | 2016-08-11 | 2019-04-16 | General Electric Company | Inlet assembly for an aircraft aft fan |
| US10704418B2 (en) | 2016-08-11 | 2020-07-07 | General Electric Company | Inlet assembly for an aircraft aft fan |
| US10253779B2 (en) | 2016-08-11 | 2019-04-09 | General Electric Company | Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan |
| US10252790B2 (en) | 2016-08-11 | 2019-04-09 | General Electric Company | Inlet assembly for an aircraft aft fan |
| CN115680903B (en) * | 2022-08-31 | 2024-05-03 | 中国航发四川燃气涡轮研究院 | Recoverable bypass bleed air control method |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE469592A (en) * | 1945-12-05 | |||
| FR936706A (en) * | 1946-04-12 | 1948-07-28 | Air navigation device | |
| US2846846A (en) * | 1951-06-14 | 1958-08-12 | Bendix Aviat Corp | Fuel system for gas turbine engines having means for avoiding compressor instability |
| US2850871A (en) * | 1954-01-11 | 1958-09-09 | Marquardt Aircraft Co | Automatic constant mach number control system |
| US2997256A (en) * | 1955-01-14 | 1961-08-22 | James H Walker | Supersonic aircraft |
| US3129563A (en) * | 1955-02-02 | 1964-04-21 | Marquardt Corp | Pressure ratio sensing device |
| US3139727A (en) * | 1955-03-03 | 1964-07-07 | United Aircraft Corp | Fuel control for jet engines |
| US2982496A (en) * | 1956-01-11 | 1961-05-02 | English Electric Co Ltd | Aircraft |
| US2971328A (en) * | 1958-07-22 | 1961-02-14 | United Aircraft Corp | Control system for air inlet bypass |
| US3158996A (en) * | 1959-01-08 | 1964-12-01 | Power Jets Res & Dev Ltd | Control systems for gas turbine engines |
| US3067577A (en) * | 1960-01-25 | 1962-12-11 | North American Aviation Inc | Method and control system for sensing temperatured differentials of flowing gases |
| US3076312A (en) * | 1960-01-29 | 1963-02-05 | Lucas Industries Ltd | Fuel supply control for gas turbine engines |
| GB929842A (en) * | 1960-12-14 | 1963-06-26 | Rolls Royce | Gas turbine engine fuel system |
| US3181817A (en) * | 1962-12-19 | 1965-05-04 | United Aircraft Corp | Air inlet control |
| US3188022A (en) * | 1963-12-05 | 1965-06-08 | Svenska Aeroplan Ab | Delta wing canard aircraft |
| GB1228213A (en) * | 1968-04-16 | 1971-04-15 | ||
| US3680816A (en) * | 1969-12-29 | 1972-08-01 | Mc Donnell Douglas Corp | Aircraft having auxiliary airfoils |
| US3717163A (en) * | 1970-10-08 | 1973-02-20 | Cci Aerospace Corp | Precompression shroud for inlets |
| GB1423364A (en) * | 1972-06-21 | 1976-02-04 | Lucas Industries Ltd | Fuel control apparatus for gas turbine engine reheat system |
| US3813063A (en) * | 1972-07-21 | 1974-05-28 | United Aircraft Corp | Automatic aircraft engine pressure ratio control system |
| US3854287A (en) * | 1973-12-26 | 1974-12-17 | United Aircraft Corp | Self-trimming control for turbofan engines |
| US4275557A (en) * | 1978-01-25 | 1981-06-30 | General Electric Company | Method and apparatus for controlling thrust in a gas turbine engine |
| US4232515A (en) * | 1978-03-06 | 1980-11-11 | The Boeing Company | Supersonic cruise airplane and engine |
| US4294069A (en) * | 1978-04-26 | 1981-10-13 | United Technologies Corporation | Exhaust nozzle control and core engine fuel control for turbofan engine |
-
1980
- 1980-06-23 WO PCT/US1980/000786 patent/WO1982000048A1/en not_active Application Discontinuation
- 1980-06-23 EP EP19810901384 patent/EP0054555A4/en not_active Withdrawn
- 1980-06-23 JP JP50185980A patent/JPS57501096A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| EP0054555A4 (en) | 1983-11-11 |
| WO1982000048A1 (en) | 1982-01-07 |
| EP0054555A1 (en) | 1982-06-30 |