发明名称 AIR ASSIST PUMP DRIVE CIRCUIT FOR GAS TURBINE ENGINE
摘要 PURPOSE:To use a gas turbine starting battery as the power source for an air assist pump, by inserting a voltage drop resistor in series with a drive motor for an air assist pump at the final stage of starting operation. CONSTITUTION:Upon turning on of a contact 1, a startor functions to drop the battery voltage considerably while simultaneously relays 2, 4 function to turn on the contacts 2a, 4a and magnet relays 5, 6 function to turn on the contacts 5a, 6a to connect an air assist pump 8 to a battery 9 thus to start operation. The battery voltage will recover gradually as the turbine rotation increases while upon reaching to the maximum allowable terminal voltage of a drive motor 11 for the pump 8, the contact 3 will turn off to be energize the relay 4 thus to turn off the contact 4a while a magnet relay 6 is also de-energized to turn off the contact 6a which has shortcircuited the resistor 7 thereby the resistor 7 is connected in series with the drive motor 11. Consequently the rotation is maintained in proper range.
申请公布号 JPS5949328(A) 申请公布日期 1984.03.21
申请号 JP19820160705 申请日期 1982.09.11
申请人 YANMAR DIESEL KK 发明人 NAKANO HIROBUMI
分类号 F02C7/22;F02C7/26;F02N11/08 主分类号 F02C7/22
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