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公开(公告)号：US07819361B2
公开(公告)日：2010-10-26
申请号：US11969108
申请日：2008-01-03
IPC分类号： B64D39/00
摘要： A refueling drogue adapted to connect to a refueling hose extending from a refueling aircraft. The drogue may include an active stabilization system adapted to effectively stabilize the refueling drogue via control surfaces on the refueling drogue when the refueling drogue is placed in an airstream.
摘要翻译： 一个加油水龙头适合连接到从加油飞机延伸的加油软管。 锥套可以包括主动稳定系统，其适于当加油锥套放置在气流中时通过加油锥套上的控制表面有效地稳定加油锥套。
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公开(公告)号：US20100237196A1
公开(公告)日：2010-09-23
申请号：US11969108
申请日：2008-01-03
IPC分类号： B64D39/00
摘要： A refueling drogue adapted to connect to a refueling hose extending from a refueling aircraft. The drogue may include an active stabilization system adapted to effectively stabilize the refueling drogue via control surfaces on the refueling drogue when the refueling drogue is placed in an airstream.
摘要翻译： 一个加油水龙头适合连接到从加油飞机延伸的加油软管。 锥套可以包括主动稳定系统，其适于当加油锥套放置在气流中时通过加油锥套上的控制表面有效地稳定加油锥套。
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公开(公告)号：US07404530B2
公开(公告)日：2008-07-29
申请号：US11905479
申请日：2007-10-01
IPC分类号： B64D37/00
摘要： A refueling drogue adapted to connect to a refueling hose extending from a refueling aircraft. The refueling drogue may include an active control system, wherein, in an exemplary embodiment, the active control system is adapted to regulate the position of the drogue to maintain a substantially fixed orientation relative to a refueling aircraft.
摘要翻译： 一个加油水龙头适合连接到从加油飞机延伸的加油软管。 加油锥套可以包括主动控制系统，其中在示例性实施例中，主动控制系统适于调节锥套的位置以相对于加油飞机保持基本上固定的方位。
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公开(公告)号：US07377468B2
公开(公告)日：2008-05-27
申请号：US10849927
申请日：2004-05-21
IPC分类号： B64D39/00
摘要： A refueling drogue adapted to connect to a refueling hose extending from a refueling aircraft. The drogue may include an active stabilization system adapted to effectively stabilize the refueling drogue via control surfaces on the refueling drogue when the refueling drogue is placed in an airstream.
摘要翻译： 一个加油水龙头适合连接到从加油飞机延伸的加油软管。 锥套可以包括主动稳定系统，其适于当加油锥套放置在气流中时通过加油锥套上的控制表面有效地稳定加油锥套。
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公开(公告)号：US07275718B2
公开(公告)日：2007-10-02
申请号：US10891510
申请日：2004-07-15
IPC分类号： B64D39/00
摘要： A refueling drogue adapted to connect to a refueling hose extending from a refueling aircraft. The refueling drogue may include an active control system, wherein, in an exemplary embodiment, the active control system is adapted to regulate the position of the drogue to maintain a substantially fixed orientation relative to a refueling aircraft.
摘要翻译： 一个加油水龙头适合连接到从加油飞机延伸的加油软管。 加油锥套可以包括主动控制系统，其中在示例性实施例中，主动控制系统适于调节锥套的位置以相对于加油飞机保持基本上固定的方位。
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公开(公告)号：US06994294B2
公开(公告)日：2006-02-07
申请号：US10697564
申请日：2003-10-31
IPC分类号： B64D39/00
摘要： A refueling drogue adapted to connect to a refueling hose extending from a refueling aircraft. The drogue may include a rotatable mass adapted to effectively stabilize the refueling drogue via a gyroscopic effect of the rotating mass on the refueling drogue when the refueling drogue is placed in an airstream.
摘要翻译： 一个加油水龙头适合连接到从加油飞机延伸的加油软管。 锥体可以包括可旋转的质量块，其适于在加油锥套放置在气流中时通过旋转体在加油锥套上的陀螺效应来有效地稳定加油锥套。
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公开(公告)号：US5491371A
公开(公告)日：1996-02-13
申请号：US165321
申请日：1993-12-13
申请人： Kean K. Ooi
发明人： Kean K. Ooi
摘要： A lamination for the stator or rotor of an electrical machine, the improvement comprising the lamination having a first periphery extending about a central axis defined by the lamination; the lamination also having a series of circularly spaced protrusions projecting away from the periphery and from the main extent of the lamination; whereby a stack of laminations, at least some of which incorporate the protrusions, define fluid coolant passages adjacent the protrusions.
摘要翻译： 一种用于电机的定子或转子的叠片，其改进包括层压，其具有围绕由层压限定的中心轴线延伸的第一周边; 所述层压体还具有一系列圆周间隔开的突出部，所述突出部远离所述周边和所述叠片的主要范围突出; 其中至少其中一些结合了突起的一叠叠片限定了与突起相邻的流体冷却剂通道。
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