Patent GB-1107681-A (GB)
Title: Combustion engine fuel control
IPC: F02C9/16
Filed: 1966-08-25
Abstract: 1,107,681. Gas turbine engine fuel systems. BENDIX CORPORATION. Aug. 25, 1966 [Sept. 3, 1965], No. 38228/66. Heading F1G. The fuel supply to a gas turbine engine is controlled by a control unit 58, Figs. 3, 4 and 5, and a control unit 60, Fig. 8, the two control units being connected in series. A manual lever movable over a range of positions including shut off, start, idle and maximum is connected to a lever 70, Fig. 4, whereby a cam 140, see also Fig. 5, is rotated to act through a roller 138, a pivoted bracket 136, an adjustable stop 134, a follower 132, a shaft 128 and a forked lever 126 to vary the compression of a spring 118 acting on a tubular valve member 114 in opposition to governor weights 102, the governor being driven by a shaft 108 of the engine-driven fuel pump 80. The valve member 114 co-operates with a valve orifice 146 to variably throttle the delivery of the fuel pump 80 in accordance with variations in engine speed. A further throttle valve downstream of the throttle valve 114, 146 comprises a valve member 338, Fig. 8, co-operating with a valve orifice 336, the valve member 338 being actuated in accordance with the temperature of the compressed air entering the combustion chamber of the engine from an exhaust gas pre-heater as sensed by a temperature sensor 348, and further actuated in accordance with atmospheric pressure P a  as sensed by a bellows 370. The fuel delivery is varied by a by-pass valve connected across the fuel pump 80 and comprising a ball valve 160, Fig. 3, co-operating with a by-pass passage 164. The ball valve 160 is controlled by a lever 172 pivoted at 176 and acted on by diaphragms 184 and 294. Fuel is bled from the discharge side of the fuel pump 80 to a point downstream of the control unit 60 via restricted passages 198, 196 connected in series. Diaphragm 184 is exposed on one side to the pump discharge press P 1  and on the other side to the pressure P 3  obtaining at the junction between the passages 198, 196. Diaphragm 294 is exposed on one side to the atmospheric pressure P a  and on the other side to the discharge pressure P c  of the engine air compressor communicated through duct 300. Since the pressure drop P 1 -P 3  sensed by the diaphragm 184 is proportional to the total pressure drop across the governor orifice 146 and the orifice 336, the diaphragm 184 controls the by-pass valve 160 in accordance with the variables controlling the orifices 146, 336, i.e., engine speed, temperature of the compressed air entering the combustion chamber, and atmospheric pressure. The spindle 316 transmitting force from the diaphragm 294 to the level 172 is not connected direct to the lever but is instead connected to it through a linkage which, at values of the pressure differential P c -P a  obtaining at speeds above the selected idle speed, introduces a compensation for variations of the compressor inlet air temperature between -20F. and +100F., whereby the fuel flow for a given value of P c -P a  increases with increasing temperature within those limits. As fuel flows above a predetermined value, the torque exerted on the lever 172 by the diaphragm 184 is reduced to a fixed fraction of the torque which would otherwise have been exerted. This weakening of the controlling effect of the diaphragm 184 causes the slope of the curve of fuel flow against P c -P a  to become steeper above this point to provide enrichment for further acceleration. For this purpose, the connection between the diaphragm 184 and the lever 172 involves a lever 218 pivoted to the lever 172 at 220 and constrained by a spring 232 to move with the lever 172, the diaphragm 184 being connected to the lever 218 through a link 200. When an extension 236 of the lever 218 comes against a stop 238, further movement of diaphragm 184 to the left causes lever 218 to pivot about the stop 238 and to act on the lever 172 through the pivot 220. This reduces the torque exerted on the lever 172 by the diaphragm 184. When the engine has accelerated to the speed set by the manual control, the weights 102 move the valve member 114 to reduce the opening of orifice 146, and the fuel flow reduces to the value needed to maintain that speed.