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公开(公告)号:US20090091198A1
公开(公告)日:2009-04-09
申请号:US12241677
申请日:2008-09-30
CPC分类号: H02K21/44
摘要: A flux-switching machine stator comprising two or more C-cores, each C-core having two legs and a back portion joining the legs, and a permanent magnet arranged between legs of adjacent C-cores. Each leg has a main portion and a tip portion further from the back portion characterized in that the tip portion of each leg is angled relative to the main portion of the respective leg.
摘要翻译: 一种磁通切换机定子,包括两个或更多个C芯,每个C芯具有两个支腿和一个连接支腿的后部,以及布置在相邻C芯的支腿之间的永磁体。 每个腿部具有主要部分和远离后部部分的尖端部分,其特征在于,每个腿部的尖端部分相对于相应腿部的主要部分成角度。
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公开(公告)号:US08508095B2
公开(公告)日:2013-08-13
申请号:US12241677
申请日:2008-09-30
CPC分类号: H02K21/44
摘要: A flux-switching machine stator comprising two or more C-cores, each C-core having two legs and a back portion joining the legs, and a permanent magnet arranged between legs of adjacent C-cores. Each leg has a main portion and a tip portion further from the back portion characterized in that the tip portion of each leg is angled relative to the main portion of the respective leg.
摘要翻译: 一种磁通切换机定子,包括两个或更多个C芯,每个C芯具有两个支腿和一个连接支腿的后部,以及布置在相邻C芯的支腿之间的永磁体。 每个腿部具有主要部分和远离后部部分的尖端部分,其特征在于,每个腿部的尖端部分相对于相应腿部的主要部分成角度。
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公开(公告)号:US08561939B2
公开(公告)日:2013-10-22
申请号:US12730586
申请日:2010-03-24
申请人: Peter Malkin , Geraint Wyn Jewell
发明人: Peter Malkin , Geraint Wyn Jewell
IPC分类号: B64D41/00
CPC分类号: B64C25/405 , B64D13/02 , B64D2013/0644 , Y02T50/44 , Y02T50/56 , Y02T50/823
摘要: Apparatus indicated generally at 26 is incorporated within an aircraft. The apparatus 26 includes an electric motor 28, a first drive train 30 and a second drive train 32. The first drive train 30 provides drive from the electric motor 28 for one or more of the wheels 20, allowing the electric motor 28 to propel the aircraft when taxiing. The second drive train 32 provides drive from the electric motor 28 for an aircraft system which is operational at least when the aircraft is in flight. In this example, the electric motor 28 is illustrated using the second drive train 32 for driving a compressor 34 of the ECS 24, the compressor 34 being responsible for cabin pressurization during flight. A clutch 36 allows the drive train 30 to be connected or disconnected from the electric motor 28, thereby connecting or disconnecting the drive from the electric motor 28 to the wheels 20. The clutch 36 is controlled to disconnect the first drive train 30 when the aircraft is in flight. Thus, when the aircraft is in flight, the full output of the motor 28 is available for driving the compressor 34; when the aircraft is on the ground, the compressor 34 is not required or is less demanding, and surplus output of the motor 28 can be used for driving the wheels 20.
摘要翻译: 通常以26表示的装置并入飞机内。 装置26包括电动机28,第一传动系30和第二传动系32.第一传动系30提供用于一个或多个车轮20的电动机28的驱动,允许电动机28推动 飞机时滑行。 第二传动系32提供用于飞机系统的电动马达28的驱动,该飞机系统至少在飞行器飞行时可操作。 在该示例中,使用用于驱动ECS 24的压缩机34的第二传动系32来示出电动机28,压缩机34负责飞行中的客舱加压。 离合器36允许传动系30与电动机28连接或断开,从而将驱动与电动机28连接或断开到车轮20.当飞行器 在飞行中 因此,当飞行器飞行时,马达28的全输出可用于驱动压缩机34; 当飞机在地面上时,压缩机34不需要或要求不高,马达28的剩余输出可以用于驱动车轮20。
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