发明名称 航空機用静止型電源装置ユニット
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a stationary power supply device unit for aircrafts, capable of performing protection action by securely detecting an earth fault if the earth fault occurs, while maintaining a power supply state without performing earth fault detection if a loop circuit occurs, when power is supplied by a plurality of constant voltage constant frequency devices (CVCF) to one aircraft. <P>SOLUTION: At least one set of a zero-phase-sequence current transformer 4, and an earth fault over-current relay 5 connected to the zero-phase-sequence current transformer 4, is prepared as a stationary power supply device unit X for aircrafts, which includes a plurality of three-phase four-line stationary power supply devices 1A and 1B for supplying power to an aircraft P under parking. When power is supplied to one aircraft P, all three-phase and neutral phase electric lines 2a, 2b, 2c and 3 of the stationary power supply devices 1A and 1B are connected to a load of the aircraft P, while the electric line 3 of the neutral phase is grounded to a body of the aircraft P, and a ground line 32 of each of the stationary power supply devices 1A and 1B is connected to the same ground electrode G through the common zero-phase-sequence current transformer 4. <P>COPYRIGHT: (C)2012,JPO&INPIT</p>
申请公布号 JP5678537(B2) 申请公布日期 2015.03.04
申请号 JP20100208029 申请日期 2010.09.16
申请人 发明人
分类号 B64F3/02;H02H3/347 主分类号 B64F3/02
代理机构 代理人
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