公开(公告)号：US07677868B2

公开(公告)日：2010-03-16

申请号：US11567773

申请日：2006-12-07

申请人： Zaffir Chaudhry ,  Andrew John Collins ,  Ulf J Jonsson ,  Fanping Sun ,  Brian E Wake ,  Michael G O'Callaghan ,  Jimmy Lin-Min Yeh

发明人： Zaffir Chaudhry ,  Andrew John Collins ,  Ulf J Jonsson ,  Fanping Sun ,  Brian E Wake ,  Michael G O'Callaghan ,  Jimmy Lin-Min Yeh

IPC分类号： F03B3/12

CPC分类号： B64C27/615 ,  B64C2027/7266 ,  Y02T50/34

摘要： A self-lubricated actuator for a rotor blade flap of a helicopter having a housing; a motor having a shaft disposed in a bearing is provided. The actuator further has an output rod and a mechanism operatively associated with the motor and the output rod to transmit movement from the motor to the output rod. The housing includes a lubrication medium capable of substantially immersing the bearing, the motor shaft and the mechanism during operation.

摘要翻译： 一种用于具有壳体的直升机的转子叶片翼片的自润滑致动器; 提供具有设置在轴承中的轴的马达。 致动器还具有输出杆和与马达和输出杆可操作地相关联的机构，以将运动从马达传递到输出杆。 壳体包括能够在运行期间基本上浸入轴承，马达轴和机构的润滑介质。

公开(公告)号：US20080138203A1

公开(公告)日：2008-06-12

申请号：US11567773

申请日：2006-12-07

申请人： Andrew John Collins ,  Zaffir Chaudhry ,  Ulf J Jonsson ,  Fanping Sun ,  Brian E. Wake ,  Michael G. O'Callaghan ,  Jimmy Lin-Min Yeh

发明人： Andrew John Collins ,  Zaffir Chaudhry ,  Ulf J Jonsson ,  Fanping Sun ,  Brian E. Wake ,  Michael G. O'Callaghan ,  Jimmy Lin-Min Yeh

IPC分类号： B64C27/615 ,  F01D25/18

CPC分类号： B64C27/615 ,  B64C2027/7266 ,  Y02T50/34

摘要： A self-lubricated actuator for a rotor blade flap of a helicopter having a housing; a motor having a shaft disposed in a bearing is provided. The actuator further has an output rod and a mechanism operatively associated with the motor and the output rod to transmit movement from the motor to the output rod. The housing includes a lubrication medium capable of substantially immersing the bearing, the motor shaft and the mechanism during operation.

摘要翻译： 一种用于具有壳体的直升机的转子叶片翼片的自润滑致动器; 提供具有设置在轴承中的轴的马达。 致动器还具有输出杆和与马达和输出杆可操作地相关联的机构，以将运动从马达传递到输出杆。 壳体包括能够在运行期间基本上浸入轴承，马达轴和机构的润滑介质。

公开(公告)号：US08915710B2

公开(公告)日：2014-12-23

申请号：US11299159

申请日：2005-12-09

申请人： Zaffir Chaudhry ,  Brian E. Wake ,  Fanping Sun ,  Richard Jeremy Bedwell ,  Jimmy Lin-Min Yeh ,  Lee A. Hoffman

发明人： Zaffir Chaudhry ,  Brian E. Wake ,  Fanping Sun ,  Richard Jeremy Bedwell ,  Jimmy Lin-Min Yeh ,  Lee A. Hoffman

IPC分类号： B64C27/615

CPC分类号： B64C27/615 ,  B64C27/72 ,  B64C2027/7266 ,  Y02T50/34

摘要： A device for controlling the pitch of a helicopter's rotor blade, the device having a BLDC motor based actuator; and at least one control surface operatively connected to the BLDC motor based actuator. The actuator and the control surface are preferably fully integrated into the interior profile of the rotor blade and are capable of controlling the PFC of the helicopter and improving HHC during operation by reducing noise and vibration. The motor is preferably a high power density motor incorporating rare earth permanent magnets connected to a roller/ball screw or planetary gear set to provide the right combination of force/torque, stroke and frequency.

摘要翻译： 一种用于控制直升机转子叶片间距的装置，该装置具有基于无刷直流电动机的致动器; 以及可操作地连接到基于无刷直流电动机的致动器的至少一个控制表面。 致动器和控制表面优选完全集成到转子叶片的内部轮廓中，并且能够通过降低噪音和振动来控制直升机的PFC并改善操作中的HHC。 电动机优选地是结合稀土永磁体的高功率密度电动机，其连接到滚子/滚珠丝杠或行星齿轮组，以提供力/转矩，行程和频率的正确组合。

公开(公告)号：US20080101931A1

公开(公告)日：2008-05-01

申请号：US11299159

申请日：2005-12-09

申请人： Zaffir Chaudhry ,  Brian E. Wake ,  Fanping Sun ,  Richard Jeremy Bedwell ,  Jimmy Lin-Min Yeh ,  Lee A. Hoffman

发明人： Zaffir Chaudhry ,  Brian E. Wake ,  Fanping Sun ,  Richard Jeremy Bedwell ,  Jimmy Lin-Min Yeh ,  Lee A. Hoffman

IPC分类号： B64C11/28

CPC分类号： B64C27/615 ,  B64C27/72 ,  B64C2027/7266 ,  Y02T50/34

摘要： A device for controlling the pitch of a helicopter's rotor blade, the device having a BLDC motor based actuator; and at least one control surface operatively connected to the BLDC motor based actuator. The actuator and the control surface are preferably fully integrated into the interior profile of the rotor blade and are capable of controlling the PFC of the helicopter and improving HHC during operation by reducing noise and vibration. The motor is preferably a high power density motor incorporating rare earth permanent magnets connected to a roller/ball screw or planetary gear set to provide the right combination of force/torque, stroke and frequency.

摘要翻译： 一种用于控制直升机转子叶片间距的装置，该装置具有基于无刷直流电动机的致动器; 以及可操作地连接到基于无刷直流电动机的致动器的至少一个控制表面。 致动器和控制表面优选完全集成到转子叶片的内部轮廓中，并且能够通过降低噪音和振动来控制直升机的PFC并改善操作中的HHC。 电动机优选地是结合稀土永磁体的高功率密度电动机，其连接到滚子/滚珠丝杠或行星齿轮组，以提供力/转矩，行程和频率的正确组合。