CH383692A - Fuel supply adjustment installation for a gas turbine engine - Google Patents
Fuel supply adjustment installation for a gas turbine engineInfo
- Publication number
- CH383692A CH383692A CH2807555A CH2807555A CH383692A CH 383692 A CH383692 A CH 383692A CH 2807555 A CH2807555 A CH 2807555A CH 2807555 A CH2807555 A CH 2807555A CH 383692 A CH383692 A CH 383692A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas turbine
- fuel supply
- turbine engine
- supply adjustment
- adjustment installation
- Prior art date
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
- F02C9/32—Control of fuel supply characterised by throttling of fuel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/305—Blade pitch-changing mechanisms characterised by being influenced by other control systems, e.g. fuel supply
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- High-Pressure Fuel Injection Pump Control (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US476715A US2941601A (en) | 1954-12-21 | 1954-12-21 | Fuel control |
Publications (1)
Publication Number | Publication Date |
---|---|
CH383692A true CH383692A (en) | 1964-10-31 |
Family
ID=23892961
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH2807555A CH383692A (en) | 1954-12-21 | 1955-12-20 | Fuel supply adjustment installation for a gas turbine engine |
Country Status (2)
Country | Link |
---|---|
US (1) | US2941601A (en) |
CH (1) | CH383692A (en) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3034569A (en) * | 1956-04-09 | 1962-05-15 | Bendix Corp | Fuel feed and power control for gas turbine engines |
US3073328A (en) * | 1956-04-10 | 1963-01-15 | Curtiss Wright Corp | Helicopter speed control system |
US2996883A (en) * | 1957-11-15 | 1961-08-22 | United Aircraft Corp | Means for limiting torque in a turboprop engine or the like |
US3110348A (en) * | 1959-12-04 | 1963-11-12 | Escher Wyss Ag | Control device for adjusting a variablepitch marine propeller |
US3139894A (en) * | 1960-03-30 | 1964-07-07 | Bendix Corp | Power turbine speed control for turboprop engines |
GB1011055A (en) * | 1960-12-22 | 1965-11-24 | Dehavilland Aircraft | Improved engine fuel control system |
US3255586A (en) * | 1962-09-12 | 1966-06-14 | Dresser Ind | Gas turbine capable of rapidly accepting or rejecting a load with minimum speed deviation |
DE1201615B (en) * | 1962-10-27 | 1965-09-23 | Bmw Triebwerkbau Ges M B H | Device for controlling the drive unit for a jet helicopter |
US3159001A (en) * | 1962-12-21 | 1964-12-01 | Avco Corp | Fuel control air pressure multiplier and main metering valve |
US3174284A (en) * | 1963-02-19 | 1965-03-23 | United Aircraft Corp | Power management fuel control for plural gas turbine engines |
US3412648A (en) * | 1966-02-10 | 1968-11-26 | Woodward Governor Co | Isochronous-droop governor |
US3356152A (en) * | 1966-06-14 | 1967-12-05 | North American Aviation Inc | Aircraft propulsion system |
US4018045A (en) * | 1971-06-25 | 1977-04-19 | Motoren- Und Turbinen-Union Munchen Gmbh | Regulating device for a prime mover, more particularly for a single-spool gas turbine |
US3875849A (en) * | 1972-09-11 | 1975-04-08 | Applied Power Inc | Electro-hydraulic proportional servo actuator |
IT1087764B (en) * | 1976-10-13 | 1985-06-04 | Lucas Industries Ltd | FUEL CONTROL SYSTEM FOR A GAS TURBINE ENGINE |
US5005354A (en) * | 1989-04-11 | 1991-04-09 | United Technologies Corporation | Fuel control having reset of propeller overspeed and underspeed governors |
US8607576B1 (en) | 2012-06-07 | 2013-12-17 | United Technologies Corporation | Single turbine driving dual compressors |
WO2015053930A1 (en) * | 2013-10-11 | 2015-04-16 | Unison Industries, Llc | Method and apparatus for controlling a turboprop engine |
BR112017025854A2 (en) * | 2016-07-20 | 2018-08-28 | Deltahawk Engines Inc | simple input motor system and controller |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1976659A (en) * | 1934-05-03 | 1934-10-09 | Gen Electric | Governing mechanism for elastic fluid engines |
US2209987A (en) * | 1937-09-20 | 1940-08-06 | Woodward Governor Co | Cabinet type actuator governor |
US2168155A (en) * | 1938-02-12 | 1939-08-01 | Gen Electric | Governing system for elastic fluid engines |
US2350781A (en) * | 1938-04-09 | 1944-06-06 | Lichte August | Governor |
US2466438A (en) * | 1943-05-01 | 1949-04-05 | Kalin Albert | Governor |
US2560758A (en) * | 1943-12-03 | 1951-07-17 | Marquette Metal Products Co | Speed responsive pressure fluid servomotor |
US2489586A (en) * | 1945-03-03 | 1949-11-29 | Allischalmers Mfg Company | Acceleration control apparatus |
US2638993A (en) * | 1947-10-01 | 1953-05-19 | Niles Bement Pond Co | Hydraulic control apparatus for internal-combustion engines and variable pitch propellers |
-
1954
- 1954-12-21 US US476715A patent/US2941601A/en not_active Expired - Lifetime
-
1955
- 1955-12-20 CH CH2807555A patent/CH383692A/en unknown
Also Published As
Publication number | Publication date |
---|---|
US2941601A (en) | 1960-06-21 |
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