发明名称 GAS TURBINE ENGINE AND METHOD FOR STARTING SAME
摘要 A starting method for a gas turbine engine includes a primary warming step of warming up the gas turbine engine while a constant primary warm-up rotation speed is maintained by an inverter motor and a secondary warming step of warming up the gas turbine engine while a constant secondary warm-up rotation speed is maintained by further increasing the speed of the inverter motor. The primary warming step terminates when an electric power required by the inverter motor attains a predetermined preset electric power value. The preset electric power value is so chosen as to decrease as the intake air temperature is low.
申请公布号 US2014298820(A1) 申请公布日期 2014.10.09
申请号 US201414307954 申请日期 2014.06.18
申请人 KAWASAKI JUKOGYO KABUSHIKI KAISHA 发明人 YAMASAKI Yoshihiro;UEMURA Daisuke;KUROSAKA Soh;MATSUO Kazuya
分类号 F02C7/26 主分类号 F02C7/26
代理机构 代理人
主权项 1. A method of starting a gas turbine engine including a compressor to compress an intake air to thereby generate a compressed gas, a combustor to burn the compressed gas to thereby generate a high temperature, high pressure combustion gas, a turbine driven by the combustion gas, and a starter device in the form of a rotating machine which concurrently serves as an electric power generator driven by the turbine, the starter device including an inverter motor, which method comprises: a primary warming step of warming up the gas turbine engine while a constant primary warm-up rotation speed is maintained by the inverter motor; and a secondary warming step of warming up the gas turbine engine while a constant secondary warm-up rotation speed is maintained by further increasing the speed of the inverter motor.
地址 Kobe-shi JP