IL57120A - Exhaust nozzle and fuel flow control means for turbofan engine - Google Patents
Exhaust nozzle and fuel flow control means for turbofan engineInfo
- Publication number
- IL57120A IL57120A IL57120A IL5712079A IL57120A IL 57120 A IL57120 A IL 57120A IL 57120 A IL57120 A IL 57120A IL 5712079 A IL5712079 A IL 5712079A IL 57120 A IL57120 A IL 57120A
- Authority
- IL
- Israel
- Prior art keywords
- control means
- flow control
- fuel flow
- exhaust nozzle
- turbofan engine
- Prior art date
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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Jet Pumps And Other Pumps (AREA)
- Supercharger (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/900,384 US4294069A (en) | 1978-04-26 | 1978-04-26 | Exhaust nozzle control and core engine fuel control for turbofan engine |
Publications (1)
Publication Number | Publication Date |
---|---|
IL57120A true IL57120A (en) | 1982-02-28 |
Family
ID=25412424
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL57120A IL57120A (en) | 1978-04-26 | 1979-04-23 | Exhaust nozzle and fuel flow control means for turbofan engine |
Country Status (7)
Country | Link |
---|---|
US (1) | US4294069A (xx) |
EP (1) | EP0005135B1 (xx) |
JP (1) | JPS54142411A (xx) |
CA (1) | CA1130888A (xx) |
DK (1) | DK171579A (xx) |
IL (1) | IL57120A (xx) |
NO (1) | NO791308L (xx) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1982000048A1 (en) * | 1980-06-23 | 1982-01-07 | Co Boeing | Supersonic airplane engine configuration |
US4414807A (en) * | 1980-12-08 | 1983-11-15 | United Technologies Corporation | Method and apparatus for controlling a gas turbine engine |
US4441156A (en) * | 1981-01-21 | 1984-04-03 | Teledyne Industries, Inc. | Integrated fuel management system |
US4697238A (en) * | 1981-01-21 | 1987-09-29 | Teledyne Industries, Inc. | Integrated fuel management system |
US4813226A (en) * | 1987-01-12 | 1989-03-21 | Grosselfinger Robert A | Demand control of variable geometry gas turbine power plant |
US4809500A (en) * | 1987-02-03 | 1989-03-07 | United Technologies Corporation | Transient control system for gas turbine engine |
US4959955A (en) * | 1989-02-27 | 1990-10-02 | United Technologies Corporation | Method of operating gas turbine engine with fan damage |
US5072580A (en) * | 1989-02-27 | 1991-12-17 | United Technologies Corporation | System for operating gas turbine jet engine with fan damage |
US5197280A (en) * | 1989-03-20 | 1993-03-30 | General Electric Company | Control system and method for controlling a gas turbine engine |
JPH02267328A (ja) * | 1989-03-20 | 1990-11-01 | General Electric Co <Ge> | ガスタービンエンジンの制御装置および制御方法 |
US5269136A (en) * | 1992-03-30 | 1993-12-14 | United Technologies Corporation | Sub-idle stability enhancement and rotating stall recovery |
US5267435A (en) * | 1992-08-18 | 1993-12-07 | General Electric Company | Thrust droop compensation method and system |
US5394689A (en) * | 1993-09-22 | 1995-03-07 | General Electric Company | Gas turbine engine control system having integral flight Mach number synthesis method |
US5463458A (en) * | 1993-12-16 | 1995-10-31 | General Electric Company | Optical sensor for duct fan discharge mach numbers |
US5622045A (en) * | 1995-06-07 | 1997-04-22 | Allison Engine Company, Inc. | System for detecting and accommodating gas turbine engine fan damage |
US5791138A (en) * | 1996-01-11 | 1998-08-11 | Burbank Aeuronautical Corporation Ii | Turbofan engine with reduced noise |
US6000215A (en) * | 1997-12-23 | 1999-12-14 | United Technologies Corporation | Method of operating a gas turbine engine |
GB9918092D0 (en) * | 1999-08-03 | 1999-10-06 | Rolls Royce Plc | Ducted fan gas turbine engine control system |
US6459963B1 (en) * | 2000-07-31 | 2002-10-01 | General Electric Company | Methods and apparatus for trimming engine control systems |
US6748744B2 (en) | 2001-11-21 | 2004-06-15 | Pratt & Whitney Canada Corp. | Method and apparatus for the engine control of output shaft speed |
WO2006059982A1 (en) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Remote engine fuel control and electronic engine control for turbine engine |
JP4745767B2 (ja) * | 2005-09-08 | 2011-08-10 | 三菱重工業株式会社 | 燃料流量制御装置及び発電システム並びに燃料流量制御方法 |
US8313280B2 (en) * | 2006-10-12 | 2012-11-20 | United Technologies Corporation | Method and device to avoid turbo instability in a gas turbine engine |
EP2074301B1 (en) * | 2006-10-12 | 2016-02-24 | United Technologies Corporation | Turbofan engine with thrust vectoring for starting and landing |
US8308423B2 (en) | 2006-10-12 | 2012-11-13 | United Technologies Corporation | Variable area fan nozzle for accommodating a foreign object strike event |
EP2064434B1 (en) | 2006-10-12 | 2012-06-27 | United Technologies Corporation | Operational line management of low pressure compressor in a turbofan engine |
US7921634B2 (en) * | 2006-10-31 | 2011-04-12 | General Electric Company | Turbofan engine assembly and method of assembling same |
GB0720703D0 (en) * | 2007-10-23 | 2007-12-05 | Rolls Royce Plc | Gas turbine engine reheat fuel system |
US20090226303A1 (en) * | 2008-03-05 | 2009-09-10 | Grabowski Zbigniew M | Variable area fan nozzle fan flutter management system |
US7871455B1 (en) * | 2009-06-19 | 2011-01-18 | Vintage Capital Group, Llc | Jet engine protection system |
US20110120079A1 (en) * | 2009-11-24 | 2011-05-26 | Schwark Jr Fred W | Variable area fan nozzle stiffeners and placement |
US8290683B2 (en) * | 2010-02-16 | 2012-10-16 | Telectro-Mek, Inc. | Apparatus and method for reducing aircraft fuel consumption |
US8517612B2 (en) | 2011-06-30 | 2013-08-27 | United Technologies Corporation | Bearing oiling system |
US9932121B2 (en) | 2012-06-22 | 2018-04-03 | United Technologies Corporation | Turbomachine flow stability enhancement device control |
FR2996254B1 (fr) * | 2012-10-03 | 2014-09-12 | Snecma | Methode de surveillance d'un defaut de poussee d'un turboreacteur d'aeronef |
US8616777B1 (en) | 2012-11-16 | 2013-12-31 | Pratt & Whitney Canada Corp. | Bearing assembly with inner ring |
CN115875138B (zh) * | 2023-02-06 | 2023-05-16 | 中国航发沈阳发动机研究所 | 一种航空燃气涡轮发动机分域分时控制方法及装置 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR941556A (fr) * | 1947-02-06 | 1949-01-14 | Procédé de réglage de turbo-réacteurs et appareils pour la mise en oeuvre de ce procédé | |
GB906653A (xx) * | 1959-01-08 | |||
US3401524A (en) * | 1967-04-21 | 1968-09-17 | United Aircraft Corp | Control for ducted fan engine |
US3797233A (en) * | 1973-06-28 | 1974-03-19 | United Aircraft Corp | Integrated control for a turbopropulsion system |
US3854287A (en) * | 1973-12-26 | 1974-12-17 | United Aircraft Corp | Self-trimming control for turbofan engines |
US4130872A (en) * | 1975-10-10 | 1978-12-19 | The United States Of America As Represented By The Secretary Of The Air Force | Method and system of controlling a jet engine for avoiding engine surge |
US4159625A (en) * | 1977-02-01 | 1979-07-03 | United Technologies Corporation | Control for gas turbine engine |
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 |
-
1978
- 1978-04-26 US US05/900,384 patent/US4294069A/en not_active Expired - Lifetime
-
1979
- 1979-04-20 NO NO791308A patent/NO791308L/no unknown
- 1979-04-23 EP EP79930004A patent/EP0005135B1/en not_active Expired
- 1979-04-23 IL IL57120A patent/IL57120A/xx unknown
- 1979-04-24 CA CA326,217A patent/CA1130888A/en not_active Expired
- 1979-04-24 JP JP5132079A patent/JPS54142411A/ja active Pending
- 1979-04-25 DK DK171579A patent/DK171579A/da active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
JPS54142411A (en) | 1979-11-06 |
US4294069A (en) | 1981-10-13 |
NO791308L (no) | 1979-10-29 |
EP0005135B1 (en) | 1983-11-23 |
DK171579A (da) | 1979-12-03 |
CA1130888A (en) | 1982-08-31 |
EP0005135A1 (en) | 1979-10-31 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IL57120A (en) | Exhaust nozzle and fuel flow control means for turbofan engine | |
DE2964890D1 (en) | Internal combustion engine and valve control means therefor | |
IL65659A (en) | Exhaust nozzle for gas turbine engine | |
JPS5720539A (en) | Exhaust nozzle for gas turbine engine | |
JPS5575535A (en) | Fuel injection apparatus for gas turbine engine | |
JPS5641436A (en) | Exhaust nozzle for gas turbine engines | |
IL65660A0 (en) | Exhaust nozzle for gas turbine engine | |
GB2102936B (en) | Fuel injector for gas turbine engines | |
GB2035461B (en) | Fuel control for gas turbine engines | |
JPS57186028A (en) | Fuel controller for gas turbine engine | |
GB2019494B (en) | Gas turbine engine fuel system | |
JPS5449410A (en) | Fuel nozzle assembly for gas turbine engine | |
GB2045471B (en) | Gas turbine engine fuel control systems | |
GB2163105B (en) | Vectorable exhaust nozzle for gas turbine engine | |
GB2035540B (en) | Gas turbine engine fuel injector | |
GB2057577B (en) | Gas turbine fuel flow control | |
GB2164613B (en) | Vectorable exhaust nozzle for gas turbine engines | |
JPS5477821A (en) | Shuttoff valve device and fuel control system for gas turbine engine | |
JPS5652526A (en) | Gas turbine engine fuel controlling system | |
JPS51146612A (en) | Method and device for controlling gas turbine engine fuel | |
JPS54118908A (en) | Fuel control device for reheating system of gas turbine engine | |
JPS57198348A (en) | Thrust reversal/exhaust gas nozzle assemblage for gas turbine engine | |
JPS5792609A (en) | Fuel nozzle for gas turbine engine | |
GB2057576B (en) | Gas turbine fuel flow control | |
DE2961611D1 (en) | Fuel injection system for an internal combustion engine and air/fuel ratio controller therefor |