GB830007A - Fuel control for gas turbine engine - Google Patents
Fuel control for gas turbine engineInfo
- Publication number
- GB830007A GB830007A GB34358/56A GB3435856A GB830007A GB 830007 A GB830007 A GB 830007A GB 34358/56 A GB34358/56 A GB 34358/56A GB 3435856 A GB3435856 A GB 3435856A GB 830007 A GB830007 A GB 830007A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- piston
- pump
- leak
- fuel
- 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.)
- Expired
Links
Classifications
-
- 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)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
830,007. Gas-turbine jet-propulsion plant. BENDIX AVIATION CORPORATION. Nov. 9, 1956 [Dec. 15, 1955], No. 34358/56. Class 110 (3). [Also in Group XXIX] Control apparatus for gas-turbine engines with afterburner fuel control means 44 comprises a fluid-operated device 109 controlling fuel supply through the control means 44, and two devices controlling fluid supply to the device 109, one 65 being manually actuated and the other 79 being actuated in response to engine speed to permit fluid flow for a range of speeds above a predetermined value. A pump 36 supplies fuel through a main fuel control 34 to the main burners 26 and also up to a piston valve 64 and past a pressure regulator 126 to a cylinder 122 having a leak-off valve 120. A manual throttle lever 54 for the control 34 opens the valve 64 through a cam 56 allowing the pump discharge pressure to pass to a normally closed piston valve 79. On the engine speed reaching a predetermined minimum value set by an adjustment 140, an engine speed sensitive flyweight 112 acts through lever 116 to close the leak-off valve 120 whereby the piston 129 spring connected to the leak-off valve, moves upwards and through its cam 134 closes a leak-off valve 96 whereby the pump discharge pressure builds up beneath a piston 80. As the piston moves up, direct pump pressure is suddenly applied via passage 86 and opens the piston valve 79 to allow pump discharge pressure to pass to the left-hand side of a piston 103 which moves to open the valve 107 allowing fuel to pass through a pump 48 and fuel control 44 to after burners 50. The piston valve 79 is hydraulically locked in its raised position regardless of subsequent engine speed changes. When the lever 54 is moved to allow the valve 65 to close, pump discharge pressure is cut-off at 76 and 86 and spring 82 moves the piston valve 79 downwards to close line 98 and connect both sides of the piston 103 to pump intake pressure via pipe 110 so that spring 105 closes valve 107.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US830007XA | 1955-12-15 | 1955-12-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB830007A true GB830007A (en) | 1960-03-09 |
Family
ID=22174809
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34358/56A Expired GB830007A (en) | 1955-12-15 | 1956-11-09 | Fuel control for gas turbine engine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB830007A (en) |
-
1956
- 1956-11-09 GB GB34358/56A patent/GB830007A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB991729A (en) | Fuel control for combustion engine | |
US3021827A (en) | Carburetor governor | |
GB845269A (en) | Improvements in fuel flow control apparatus for gas turbine engines | |
GB830007A (en) | Fuel control for gas turbine engine | |
GB538229A (en) | Improvements in or relating to automatic control devices, suitable for use with internal combustion engines | |
GB888328A (en) | Improvements in fuel systems for aircraft gas turbine engines | |
GB897091A (en) | Gas turbine engine fuel system | |
GB840456A (en) | Fuel control apparatus for gas turbine engines | |
GB687183A (en) | Improvements in apparatus for supplying liquid fuel to continuous combustion turbine engines | |
GB654263A (en) | Speed governor mechanisms for aircraft internal combustion turbine engines | |
GB806207A (en) | Improvements in or relating to governors, more particularly for gas turbine engines | |
GB833496A (en) | Improvements in reheat control systems for gas turbine engines | |
GB694316A (en) | Improvements in speed limiting mechanism for continuous combustion turbine engines | |
GB564303A (en) | Improvements in regulating devices for controlling the supply of fuel to internal combustion engines | |
GB856215A (en) | Gas turbine engine control | |
GB696758A (en) | Improved method of feeding liquid fuel to gas turbines and notably to jet turbine and propellor turbine engines | |
GB723546A (en) | Improvements in liquid fuel supply systems for re-heat burners of gas turbine engines | |
GB718104A (en) | Liquid fuel control means for jet-propulsion engines or gas turbines | |
GB800511A (en) | Fuel supply and associated apparatus for internal combustion engines | |
GB740457A (en) | Improvements relating to fuel supply systems for gas turbine engines | |
GB825054A (en) | Fuel feed and power control system for gas turbine engines | |
GB692202A (en) | Improvements in all-speed governing mechanisms for continuous combustion turbine engines | |
GB750472A (en) | Co-ordinated fuel feed and exhaust jet control for jet engines | |
GB1171312A (en) | Fuel Systems for Gas Turbine Engines | |
GB663532A (en) | Improvements in or relating to fuel supply systems for internal combustion engines |