发明名称 Aircraft electrical power system including air conditioning system generator
摘要 An electrical power system for an aircraft includes an ac generator bus, an air conditioning system ("ACS") generator and a main engine generator. The ACS generator supplies primary ac power to the bus while the frequency of the ac power is within a frequency range. If the frequency of the ac power goes outside the frequency range, the main engine generator supplies backup ac power to the bus. The frequency of the ac power generated the ACS generator is maintained between upper and lower limits. Such ac power can be used directly by certain ac loads onboard the aircraft. Other ac loads onboard the aircraft are supplied with fixed frequency ac power by reduced-size inverters.
申请公布号 US5939800(A) 申请公布日期 1999.08.17
申请号 US19980022198 申请日期 1998.02.11
申请人 ALLIEDSIGNAL INC. 发明人 ARTINIAN, VATCHE;BRIM, TERRY;MATULICH, DAN;MURRY, ROGER
分类号 B64D13/06;B64D13/08;B64D41/00;(IPC1-7):H02J9/06 主分类号 B64D13/06
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