Patent GB-1333135-A (GB)
Title: Gas turbine temperature adaptive control
IPC: F02C9/28
Filed: 1971-04-19
Abstract: 1333135 Gas turbine engine fuel systems GENERAL ELECTRIC CO 19 April 1971 [27 March 1970] 26256/71 Heading F1G [Also in Division G3] The present invention is directed to an improvement in a temperature control circuit described in Specification 1328356 wherein to avoid thermal shocks in a gas turbine when starting from cold, the fuel input is controlled to control the rate of increase in temperature of the turbine, the exhaust gas temperature being sensed as an indication of turbine temperature. During this "warm-up" period the temperature control overrides all other controls of the turbine, to limit the fuel input thereto and maintain the rate of temperature rise at a predetermined level. For this purpose the control system includes a minimum value gate Fig.1 (not shown) which allows that circuit such as the temperature, start-up or speed control circuit, which has the least positive output, to assume control of the turbine. The temperature adaptive control circuit Fig.3 comprises a summer junction 25 having three inputs and an output via an amplifier 33 and diode 145 to the minimum value gate. One input via line 21 is from the temperature sensors (not shown) and ranges from a predetermined positive value representing the highest temperature to a predetermined negative value representing the lowest temperature sensed. Another input is a negative reference signal representing the maximum allowable temperature and is pre-set by R41. Thus on starting from cold; if only these two input signals were present the amplifier 33 would go into positive saturation so that the temperature control circuit would be ineffective to control the turbine. However a third signal is applied via a diode 65 to the summer in opposition to the negative reference signal and has the effect of suppressing the maximum allowable temperature to a value determined by the positive voltage level of the third signal, which voltage level initially varies indirectly in proportion to the turbine exhaust temperature in the warm up period and allows the turbine temperature to increase at a controlled rate to the maximum set by R41. This third signal is continually varied in dependence upon the degree of feedback from amplifier 33 to a voltage divider R47, R39, R37, the essential effect of which is to vary the degree of conduction of a transistor Tr 31 by controlling the conduction of a transistor Tr29. When the turbine is cold the amplifier feedback is such that Tr29 fully conducts and Tr31 will be held off so that the suppression signal will be maximum. As the sensed temperature increases after "flame on", the summer output and hence the amplifier feedback will be such that Tr29 is less conductive and Tr31 conducts. When conducting, Tr31 diverts some current from and hence decreases the suppression signal to the summer 25, depending upon the degree of conduction of Tr31, which decrease causes a change in the amplifier output and feedback. In this manner continual correction of the degree of conduction of Tr29 + Tr31 is effected as a function of turbine temperature. The amplifier 33 tends to be in positive saturation and on the verge of assuming control of the turbine. At the end of the warm up period a timed signal causes a zero level voltage at an input Z which turns off Tr29 and current is diverted from Tr31 via R51 and a diode 43. Tr31 remains conducting via R59 and its degree of conduction increases gradually at a uniform rate determined by R59 C57 until eventually the suppression signal is eliminated and the amplifier output is dependent upon the actual temperature and reference temperature signals only; whereupon the speed control will predominate to control the turbine.