发明名称 ACCELERATION CONTROL METHOD FOR BIAXIAL GAS TURBINE
摘要 PURPOSE:To improve response to a fluctuation in response through simple constitution by integrating a number of revolution difference signal between a set value and a present value for an output turbine shaft and adding number of revolutions signals for a gas generator shaft and an output turbine shaft to an integrating result. CONSTITUTION:When a load D of a biaxial gas turbine A is increased, a number of revolutions present value n2 of an output turbine shaft 5 is decreased. In which case, the detecting signal n2 from a detector 9 to detect the number of revolutions of an output turbine shaft 5 is applied on an adder 10 and compared with an input signal (a) for a number of revolutions set value N. Integration of a fluctuation component equivalent to a number of revolutions difference by an integrating circuit 11, an output signal (e) from a number of revolutions control circuit B is increased and the numbers of revolutions of a gas generator shaft 1 and the output turbine shaft 5 are increased. In this case, a detecting signal from a detector 16 to detect the number of revolutions of the gas generator shaft 1 is applied as a present value n1 of the number of revolutions on a proportional circuit 17, and an output signal (h) therefrom is applied on an adder 13. Namely, a function equivalent to a conventional differentiating circuit is provided for the circuits 16 and 17.
申请公布号 JPH0518272(A) 申请公布日期 1993.01.26
申请号 JP19910198659 申请日期 1991.07.12
申请人 KAWASAKI HEAVY IND LTD 发明人 TANAKA TAITARO;TORII HIDEAKI;OGAWA YASUHIRO;ASHIKAGA MITSUGI;NAGATOME YOICHI;SENOO NAGAYASU
分类号 F02C9/28;F02C3/10 主分类号 F02C9/28
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