Patent GB-847594-A (GB)
Title: Improvements in or relating to gas turbine engine controls
IPC: F02C9/22
Filed: 1957-06-14
Abstract: 847,594. Gas-turbine plant ; centrifugal compressors. GARRETT CORPORATION. June 14, 1957 [June 15, 1956], No. 18903/57. Classes 110 (1) and 110 (3). [Also in Group XXIX] A gas-turbine plant comprising a compressor supplying air to a combustion chamber feeding a turbine driving the compressor has means responsive to the Mach. No. at a point in the flow path through the compressor and the compression ratio across the compressor controlling variable area-nozzle mechanism at the turbine inlet. The invention is described with reference to a gasturbine plant comprising a mixed axial-radial flow compressor which supplies air to an external user and to a combustion chamber feeding a radial flow turbine driving the compressor. The turbine has variable area inlet nozzles which are controlled by mechanism 25, Fig. 3. A non- return valve 32, Fig. 2, is provided between the compressor discharge and the inlet to the combustion chamber. Air is led from the compressor discharge through ducts 38 to the plenum 17 from which air is taken to the external user and to a blowoff valve 126 in a duct 27, Fig. 5. The ducts 38 are arranged in front of the valve 32. Air from the compressor discharge is led from a pressure regulator to a compressor flow sensing mechanism 28, Fig. 4, through a pipe 58 and orifice 60. A bleed-off valve 61 varies the pressure in the control output tube 62. The valve 61 is urged towards the open position by a spring 63 and the movement is controlled by a stem 64 attached to a diaphragm 65. The diaphragm 65 is responsive to the difference between the total and static pressures in the intake of the compressor 11 and the loading of the spring 73. A smaller diaphragm 75 is connected to the diaphragm 65 by a link 74. The diaphragm 75 is responsive to the pressure drop across a Venturi-shaped orifice 83 and the loading of a spring 79. The loading of the spring 79 is adjusted by the screw 80 to balance that of the spring 73. The orifice 83 is arranged in series with a variable area sharp-edged nozzle 84 in a conduit connecting the discharge of the compressor to its inlet or atmosphere. The orifice 83 is choked and its effective area remains constant regardless of changes in inlet pressure. The orifice 84 when subject to a varied pressure experiences a change in its effective area. The diaphragm 75 is therefore subject to a pressure difference substantially proportional to the compressor discharge pressure but is varied slightly from linear proportionality therewith by the correspondence of the effective area of the sharp edged orifice 84 with the compressor pressure ratio. The tube 62 is used to control the variable area inlet nozzles to the turbine so that this area is increased as the flow through the compressor falls. The pressure in the tube 62 is caused to act on a spring-loaded diaphragm 87, Fig. 3, to actuate a rod 92 carrying valve members 93, 94 which control the supply of pressure oil to and from chambers 108, 109 separated by a piston 110 having a rod 111 connected to the variable area nozzles. The rod 111 carries a second piston 113 which separates two chambers 115, 116 connected to chambers 119, 120 on each side of a diaphragm 121 connected to the rod 92. Two capillary tubes 122, 123 connect the chambers 119, 120 to the tube 58. This arrangement returns the rod 92 gradually to the neutral position and prevents overtravel of the rod 111. If the opening of these nozzles is not sufficient to prevent surging of the compressor the blow-off valve 126, Fig. 5, is actuated. The pressure in the tube 62 acts on a spring-loaded diaphragm 142 to position a piston valve 139 and so control the leak off through ports 151 in a sleeve 140. This causes a change in the pressure acting on a diaphragm 129 which opens or closes the blow-off valve 126. The valve 126 is connected to the sleeve 140 to provide follow up. During starting the blow-off valve 126 must be closed and remain closed until the turbine has reached 75% of its operating speed. The pressure at the discharge 155 of the oil pump is supplied to a chamber 156 through a passage 168 controlled by a valve 167. During starting the pressure on the piston 158 moves the diaphragm 129 downwards and closes the valve 126. The valve 167 is attached to a spring-loaded diaphragm 166. The chamber 165 is connected by the conduit 164 to the tube 58 connected to the compressor discharge. When the compressor discharge pressure reaches a predetermined value the valve 167 cuts-off the connection to the chamber 156 from the conduit 155 and connects the chamber 156 to drain 176. The piston 158 then rises under the action of the spring 163 and the valve 126 is then controlled by the diaphragm 129 in response to movements of the piston 139. Additional air from another engine may be supplied to the turbine inlet 19, Fig. 2, by a duct 29 the flow through which is controlled by a butterfly valve controlled by a mechanism 30. This arrangement is described and claimed in Specification 847,595. Specifications 770,563 and 775,454 also are referred to.