发明名称 WHEEL DRIVE SYSTEM FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide a wheel drive system for an aircraft, which can properly achieve both taxing and prerotation by rotating wheels with use of a common motor.SOLUTION: A wheel drive system for an aircraft comprises: a motor 2 which is connected to wheels 12 and has two voltage supply lines L1, L2 for supplying voltages Vta, Vpr while differentiating the lengths of windings to be energized; an inverter 3 for taxing and an inverter 4 for prerotation, which supply the voltages Vta, Vpr to the two voltage supply lines L1, L2; and a control part 8 for controlling the inverter 3 for taxing and the inverter 4 for prerotation. The control part 8 is configured to select either one of the two voltage supply lines L1, L2 and supply the voltage Vta or Vpr by controlling the inverter 3 for taxing and the inverter 4 for prerotation.
申请公布号 JP2015196466(A) 申请公布日期 2015.11.09
申请号 JP20140075751 申请日期 2014.04.01
申请人 SINFONIA TECHNOLOGY CO LTD;IHI AEROSPACE CO LTD;SUMITOMO PRECISION PROD CO LTD 发明人 SAITO HIROSHI;NAKANISHI NOBUYUKI;OYORI HITOSHI;TAKADA MASAYUKI
分类号 B64C25/40;H02P27/06 主分类号 B64C25/40
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