DE1526824A1 - Brennstoffregelanlage fuer Nachbrenner von Duesentriebwerken - Google Patents
Brennstoffregelanlage fuer Nachbrenner von DuesentriebwerkenInfo
- Publication number
 - DE1526824A1 DE1526824A1 DE19661526824 DE1526824A DE1526824A1 DE 1526824 A1 DE1526824 A1 DE 1526824A1 DE 19661526824 DE19661526824 DE 19661526824 DE 1526824 A DE1526824 A DE 1526824A DE 1526824 A1 DE1526824 A1 DE 1526824A1
 - Authority
 - DE
 - Germany
 - Prior art keywords
 - fuel
 - thrust
 - afterburner
 - pressure
 - engine
 - 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.)
 - Pending
 
Links
- 239000000446 fuel Substances 0.000 title claims description 156
 - 238000002485 combustion reaction Methods 0.000 claims description 14
 - 239000000203 mixture Substances 0.000 claims description 2
 - 238000000605 extraction Methods 0.000 claims 1
 - 230000006870 function Effects 0.000 description 10
 - 239000007789 gas Substances 0.000 description 10
 - 239000000567 combustion gas Substances 0.000 description 3
 - 230000008859 change Effects 0.000 description 2
 - 230000001419 dependent effect Effects 0.000 description 2
 - 230000001771 impaired effect Effects 0.000 description 2
 - 230000007704 transition Effects 0.000 description 2
 - 101100286286 Dictyostelium discoideum ipi gene Proteins 0.000 description 1
 - 235000008694 Humulus lupulus Nutrition 0.000 description 1
 - 244000025221 Humulus lupulus Species 0.000 description 1
 - 241000269319 Squalius cephalus Species 0.000 description 1
 - 230000008901 benefit Effects 0.000 description 1
 - 239000000969 carrier Substances 0.000 description 1
 - 238000010586 diagram Methods 0.000 description 1
 - 239000002828 fuel tank Substances 0.000 description 1
 - 230000004941 influx Effects 0.000 description 1
 - 230000001960 triggered effect Effects 0.000 description 1
 
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 | 
|---|---|
| DE1526824A1 true DE1526824A1 (de) | 1970-02-12 | 
Family
ID=24094049
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date | 
|---|---|---|---|
| DE19661526824 Pending DE1526824A1 (de) | 1966-02-07 | 1966-10-12 | Brennstoffregelanlage fuer Nachbrenner von Duesentriebwerken | 
Country Status (4)
| Country | Link | 
|---|---|
| US (1) | US3331204A (OSRAM) | 
| BE (1) | BE689296A (OSRAM) | 
| DE (1) | DE1526824A1 (OSRAM) | 
| GB (1) | GB1122290A (OSRAM) | 
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| CN113864067A (zh) * | 2020-06-30 | 2021-12-31 | 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 | 
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 | 
| 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 | 
| CN119641510B (zh) * | 2024-12-12 | 2025-09-02 | 西北工业大学 | 一种航空涡扇发动机飞行包线右边界加力供油方法及装置 | 
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 GB GB49486/66A patent/GB1122290A/en not_active Expired
 - 1966-11-04 BE BE689296D patent/BE689296A/xx unknown
 
 
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| CN113864067A (zh) * | 2020-06-30 | 2021-12-31 | 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 | 
| 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 | 
Also Published As
| Publication number | Publication date | 
|---|---|
| US3331204A (en) | 1967-07-18 | 
| BE689296A (OSRAM) | 1967-05-05 | 
| GB1122290A (en) | 1968-08-07 | 
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