Patent GB-993558-A (GB)
Title: Engine fuel-flow control apparatus
Inventor: TYLER STANLEY RALPH
IPC: F02C9/32
Filed: 1961-03-28
Abstract: 993,558. Gas turbine engines. DOWTY FUEL SYSTEMS Ltd. March 27, 1962 [March 28, 1961; Oct. 2, 1961], Nos. 11341/61 and 35518/61. Heading F1G. [Also in Division G3] Gas turbine engine fuel-flow control apparatus comprises means for supplying fuel to the engine, means to control the rate of fuel flow to the engine and operable to maintain the engine at a predetermined speed, the control means being variable to effect positive or negative acceleration, limiting means responsive to engine operating conditions for limiting the rate of fuel flow to the engine during such acceleration, and adjusting means responsive to the rate of fuel flow required to maintain the engine at a predetermined speed arranged to continually adjust the limiting means in proportion to said rate of fuel flow. In one example the fuel supply to spill burners is controlled by a spill valve 6 the position of which is determined by a controller 7 comprising an all-speed governor 21 which controls a spool pilot valve 19 to control the supply of fuel under pressure to one of two pistons 17 which actuate a lever 15 which abuts a disc 14 on the stem of the spill valve 6. The lever 15 has a feedback connection to the spool valve 19 comprising a spring 28 and a pivoted lever 22 loaded by a spring 25 acting on a lever 26, an adjustable fulcrum being located between the levers 22, 26. Acceleration control means comprises a bellows 35 subject to a gas turbine pressure and acting on a bell-crank lever 34 carrying a leak-off valve 33 which controls the position of a piston 31 which actuates an acceleration control lever 16 one end of which is adjacent the disc 14. A spring 38 provides a feedback connection between the lever 16 and the bell-crank 34. If an acceleration is selected by moving the fulcrum 27 to the right to increase the loading on the spool valve 19 the lever 15 moves to allow closing movement of the spill valve 6 to an extent determined by the acceleration control lever 16. The bell-crank 34 is also subject to the action of a servo piston 41 the pressure on which is determined by the position of a leak-off valve 42 carried by a spring loaded lever 43 connected via a spring 44 to the stem of the spill valve 6 and via a spring 47 to the piston 31. A damper 49 ensures that movement of the piston 41 is at a slower rate than engine acceleration. The piston 41 may be emitted and the springs 44, 47 arranged to act directly on the lever 34. The action on the bell-crank lever 34 reduces the errors of the acceleration control resulting from e.g. variation in fuel density. The movement of spill valve 6 to a minimum engine fuel flow position during idling results in a valve 51 shutting off supply to the piston 41 to prevent adjustment of the spring 48. In another example, Fig. 3, an all speed governor 76 actuates a leak-off valve 75 to control a piston 71 connected by a rod 69 to a pivoted lever 64 the ball end 63 of which is located between flanges 62 on the stem 61 of the spill valve 6. The acceleration control means comprises a bellows 95 subject to an engine pressure and acting on a pivoted lever 92 controlling a leak-off valve 91 to control a piston 85 the rod 84 of which is connected to a pivoted lever 82 the end 66 of which forms an acceleration stop. The bellows 95 is connected by a pipe 96 to a chamber 103 leading via a Venturi 107 to a low pressure zone such as the engine nacelle. A pipe 106 carries engine compressor delivery pressure to a chamber 102 connected to the chamber 103 via an orifice 104 in which is located a tapered rod 105 downward movement of which is limited by a stop 113. The rod 105 is connected by a cage 114 to a rod 116 from which extends pins 117, 118. The pin 118 is embraced by the forked end of a pivoted lever 121 connected to a mechanical damper. A spring 125 extends between the levers 64 and 121 and a spring 126 between the levers 82, 121. If an acceleration is selected leak off valve 75 is closed and lever 64 is rocked to move spill valve 6 in a closing direction to an extent determined by the acceleration stop 66. It will be seen that in steady state conditions the position of the stop 66 as determined by the piston 85 is being continuously adjusted in accordance with the position of the lever 64. If e.g. the calorific value of the fuel falls engine speed is maintained by movement of the lever 64, this movement being transmitted to the rod 105 which opens the orifice 104 so that the pressure transmitted to the bellows 95 increases and the acceleration stop is adjusted accordingly. In another example the acceleration control is electrically operated. In another example the acceleration control includes a function generator which controls a three-dimensional cam which controls a servo mechanism controlling the acceleration flow stop and the minimum flow stop. The spill valve is replaced by a two-part metering valve, one part being linearly movable in accordance with an engine pressure and the other part being angularly movable in accordance with engine speed.