发明名称 acionamento de um rotor de cauda de um helicóptero
摘要 The drive (1) has a disk-shaped armature (5) arranged between two stators (4), where the drive is formed as a permanently excited transverse flow motor arranged in a duplex manner. The armature has permanent magnets (15) at whose external circumference a propeller wing (14) of a tail rotor (12) of a helicopter is arranged, where the magnets are arranged in layers. The stators have a circular winding system (8) that is cooled using oil, and a common radial bearing and a common axial bearing are provided in the drive.
申请公布号 BR112013002109(A2) 申请公布日期 2016.09.20
申请号 BR20131102109 申请日期 2011.07.15
申请人 SIEMENS AKTIENGELLSCHAFT 发明人 DIETMAR STOIBER;HANS-GEORG KÖPKEN;JENS HAMANN
分类号 B64C27/82;H02K5/128;H02K7/09;H02K9/19;H02K21/24 主分类号 B64C27/82
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