BE689296A - - Google Patents
Info
- Publication number
- BE689296A BE689296A BE689296DA BE689296A BE 689296 A BE689296 A BE 689296A BE 689296D A BE689296D A BE 689296DA BE 689296 A BE689296 A BE 689296A
- Authority
- BE
- Belgium
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
- F02K1/16—Control or regulation conjointly with another control
- F02K1/17—Control or regulation conjointly with another control with control of fuel supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
- F02K1/16—Control or regulation conjointly with another control
-
- 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
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US525639A US3331204A (en) | 1966-02-07 | 1966-02-07 | Standby afterburner operation system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE689296A true BE689296A (es) | 1967-05-05 |
Family
ID=24094049
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE689296D BE689296A (es) | 1966-02-07 | 1966-11-04 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3331204A (es) |
| BE (1) | BE689296A (es) |
| DE (1) | DE1526824A1 (es) |
| GB (1) | GB1122290A (es) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1126809A (en) * | 1967-07-04 | 1968-09-11 | Rolls Royce | Gas turbine engine |
| US3747344A (en) * | 1970-07-20 | 1973-07-24 | Gen Electric | Variable nozzle area control system |
| US4095420A (en) * | 1977-04-26 | 1978-06-20 | The United States Of America As Represented By The Secretary Of The Air Force | Augmentor outer segment lockout and fan upmatch |
| US4134259A (en) * | 1977-05-20 | 1979-01-16 | United Technologies Corporation | Fuel manifold prefill |
| US4242865A (en) * | 1978-01-25 | 1981-01-06 | Curtiss-Wright Corporation | Turbojet afterburner engine with two-position exhaust nozzle |
| US4244183A (en) * | 1978-04-27 | 1981-01-13 | United Technologies Corporation | Control means for an augmentor for a gas turbine engine |
| US7762078B2 (en) * | 2006-09-13 | 2010-07-27 | Aerojet-General Corporation | Nozzle with temperature-responsive throat diameter |
| US20120174559A1 (en) * | 2011-01-07 | 2012-07-12 | Honeywell International Inc. | System and method for controlling a gas turbine engine afterburner |
| CN102878130A (zh) * | 2011-07-11 | 2013-01-16 | 上海立新液压有限公司 | 电调制比例节流控制阀 |
| GB201819748D0 (en) | 2018-10-12 | 2019-01-16 | Rolls Royce Plc | Afterburner system |
| CN113864067B (zh) * | 2020-06-30 | 2022-08-02 | 中国航发商用航空发动机有限责任公司 | 一种滚动优化预测闭环控制器及系统 |
| CN114136628B (zh) * | 2021-10-20 | 2023-06-30 | 中国航发四川燃气涡轮研究院 | 一种航空发动机试验角度可调的油门杆限位装置 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2774215A (en) * | 1949-04-22 | 1956-12-18 | Bendix Aviat Corp | Tailpipe or afterburning control for turbojet engines |
| US2737775A (en) * | 1950-09-15 | 1956-03-13 | Solar Aircraft Co | Afterburner electric controls |
| US2737016A (en) * | 1950-09-15 | 1956-03-06 | Solar Aircraft Co | Afterburner controls |
| US2958186A (en) * | 1955-05-25 | 1960-11-01 | Bendix Corp | Fuel feed and exhaust nozzle control for gas turbine engines |
| US3243955A (en) * | 1960-09-13 | 1966-04-05 | Gen Electric | Afterburner fuel control mechanism |
| US3060683A (en) * | 1960-10-26 | 1962-10-30 | Gen Electric | Afterburner fuel and nozzle area control |
-
1966
- 1966-02-07 US US525639A patent/US3331204A/en not_active Expired - Lifetime
- 1966-10-12 DE DE19661526824 patent/DE1526824A1/de active Pending
- 1966-11-04 BE BE689296D patent/BE689296A/xx unknown
- 1966-11-04 GB GB49486/66A patent/GB1122290A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB1122290A (en) | 1968-08-07 |
| US3331204A (en) | 1967-07-18 |
| DE1526824A1 (de) | 1970-02-12 |