发明名称 SPEED CONTROL UNIT OF AIRCRAFT GENERATOR
摘要 <p>A generator (13) is driven by an aircraft engine (11) through a continuously variable ratio drive device (20) responsive to error signals from a circuit (24) indicating a difference between desired and actual speeds of an output shaft (21) of the device (20). The circuit (24) includes a switch for preventing the error signal from being applied to the device (20) until the shaft (21) reaches a predetermined speed and a ramp generating circuit for increasing the rise time of the error signal after the predetermined speed has been reached.</p>
申请公布号 JPS62100200(A) 申请公布日期 1987.05.09
申请号 JP19860228500 申请日期 1986.09.29
申请人 LUCAS IND PLC 发明人 SHIDONII BEISHIRU SUMISU
分类号 G05D13/62;B64D33/00;F02N11/04;H02P9/00;H02P9/04;H02P29/00 主分类号 G05D13/62
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