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    Aircraft landing gear assembly shimmy damper
    6.
    发明授权
    Aircraft landing gear assembly shimmy damper 有权

    公开(公告)号：US08534600B2

    公开(公告)日：2013-09-17

    申请号：US12538241

    申请日：2009-08-10

    申请人： Paul J. Bachmeyer ,  Douglas A. Swanson ,  Bryan J. Pittman ,  Scott K. Thompson ,  Doug A. Hodgson

    发明人： Paul J. Bachmeyer ,  Douglas A. Swanson ,  Bryan J. Pittman ,  Scott K. Thompson ,  Doug A. Hodgson

    IPC分类号： B64C25/00 ,  F16F1/00

    CPC分类号： B64C25/505 ,  F16F7/02 ,  F16F2224/025

    摘要： An aircraft vehicular assembly is provided that includes a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface contiguous smooth inner surface segment, and a nonelastomeric inner member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer member. The assembly includes an elastomer encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomer has an inner bonding surface segment and an outer grooved elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner member outer bonding surface segment. The assembly includes a grease disposed between the outer elastomer surface and the nonelastomeric outer member frictional interface inner surface segment with the greased grooved outer elastomer surface engaging the nonelastomeric outer member frictional interface inner surface segment and inhibiting an oscillating rotation.

    Auger finger with resilient elastomeric retainer retractor
    7.
    发明申请
    Auger finger with resilient elastomeric retainer retractor 审中-公开
    具有弹性弹性保持器牵开器的螺旋形手指

    公开(公告)号：US20100251683A1

    公开(公告)日：2010-10-07

    申请号：US12384775

    申请日：2009-04-08

    申请人： Scott K. Thompson ,  Gary L. Bich ,  Imants Ekis ,  Ryan Figgins ,  James F. Rayfield

    发明人： Scott K. Thompson ,  Gary L. Bich ,  Imants Ekis ,  Ryan Figgins ,  James F. Rayfield

    IPC分类号： A01D34/00 ,  A01D89/00

    CPC分类号： A01D57/02 ,  A01D75/182

    摘要： A finger for a crop gathering auger of a grain header for an agricultural combine, a forage harvester, or the like, the finger including a resilient elastomeric retainer retractor which spans a failure region of the finger and will retain a free end of the finger in connection with a mounting end thereof when the failure region is broken, and which is configured and operable for automatically retracting the broken off free end into an auger drum and retaining it therein during subsequent rotation of the drum for limiting potential damage from the broken end and preventing entry of the broken end into crop handling equipment of the combine or other machine.

    摘要翻译： 用于农业组合物，饲料收割机等的谷物头部的作物收集螺旋的手指，所述手指包括弹性弹性体保持器牵开器，其跨越手指的失效区域并且将手指的自由端保持在 当故障区域被破坏时与其安装端的连接，并且其被构造和可操作以自动地将断开的自由端收回到螺旋滚筒中并在滚筒的后续旋转期间将其保持在其中，以限制来自破碎端的潜在损坏， 防止破碎的末端进入组合式或其他机器的作物处理设备。

    AIRCRAFT AUXILIARY POWER UNIT SUSPENSION SYSTEM FOR ISOLATING AN AIRCRAFT AUXILIARY POWER UNIT
    8.
    发明申请
    AIRCRAFT AUXILIARY POWER UNIT SUSPENSION SYSTEM FOR ISOLATING AN AIRCRAFT AUXILIARY POWER UNIT 有权
    用于分离飞机辅助动力装置的飞机辅助动力装置悬架系统

    公开(公告)号：US20110084192A1

    公开(公告)日：2011-04-14

    申请号：US12971156

    申请日：2010-12-17

    申请人： Kirk W. Olsen ,  Gerald P. Whiteford ,  Pat Sheridan ,  Scott K. Thompson

    发明人： Kirk W. Olsen ,  Gerald P. Whiteford ,  Pat Sheridan ,  Scott K. Thompson

    IPC分类号： B64D27/00 ,  F16M13/00 ,  B23P17/04

    CPC分类号： B64D41/00 ,  B64D2041/002 ,  Y10T29/49826

    摘要： The invention provides an aircraft with an auxiliary power unit isolated from the aircraft. An auxiliary power unit suspension system includes at least one suspension linkage. The suspension linkage terminates with a first low stiffness elastomeric rod end. The low stiffness elastomeric rod end has a low spring rate with the aircraft auxiliary power unit suspension system providing the aircraft auxiliary power unit with a suspended auxiliary power unit natural frequency, the suspended auxiliary power unit natural frequency below the aircraft auxiliary power unit operation frequency.

    摘要翻译： 本发明提供一种具有与飞行器隔离的辅助动力单元的飞行器。 辅助动力单元悬挂系统包括至少一个悬挂联动装置。 悬挂连杆以第一低刚性弹性体杆端终止。 低刚度弹性体杆端具有较低的弹簧刚度，飞机辅助动力单元悬架系统为飞机辅助动力单元提供悬挂的辅助动力装置固有频率，悬挂辅助动力装置的固有频率低于飞机辅助动力装置的运行频率。

    Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit
    9.
    发明授权
    Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit 有权
    用于隔离飞机辅助动力装置的飞机辅助动力装置悬架系统

    公开(公告)号：US07878448B2

    公开(公告)日：2011-02-01

    申请号：US11397208

    申请日：2006-04-04

    申请人： Kirk W. Olsen ,  Gerald P. Whiteford ,  Pat Sheridan ,  Scott K. Thompson

    发明人： Kirk W. Olsen ,  Gerald P. Whiteford ,  Pat Sheridan ,  Scott K. Thompson

    IPC分类号： B64D27/26

    CPC分类号： B64D41/00 ,  B64D2041/002 ,  Y10T29/49826

    摘要： The invention provides an aircraft with an auxiliary power unit isolated from the aircraft. An auxiliary power unit suspension system includes at least one suspension linkage. The suspension linkage terminates with a first low stiffness elastomeric rod end. The low stiffness elastomeric rod end has a low spring rate with the aircraft auxiliary power unit suspension system providing the aircraft auxiliary power unit with a suspended auxiliary power unit natural frequency, the suspended auxiliary power unit natural frequency below the aircraft auxiliary power unit operation frequency.

    摘要翻译： 本发明提供一种具有与飞行器隔离的辅助动力单元的飞行器。 辅助动力单元悬挂系统包括至少一个悬挂联动装置。 悬挂连杆以第一低刚性弹性体杆端终止。 低刚度弹性体杆端具有较低的弹簧刚度，飞机辅助动力单元悬架系统为飞机辅助动力单元提供悬挂的辅助动力装置固有频率，悬挂辅助动力装置的固有频率低于飞机辅助动力装置的运行频率。

    Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit
    10.
    发明授权
    Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit 有权
    用于隔离飞机辅助动力装置的飞机辅助动力装置悬架系统

    公开(公告)号：US08413926B2

    公开(公告)日：2013-04-09

    申请号：US12971156

    申请日：2010-12-17

    申请人： Kirk W. Olsen ,  Gerald P. Whiteford ,  Pat Sheridan ,  Scott K. Thompson

    发明人： Kirk W. Olsen ,  Gerald P. Whiteford ,  Pat Sheridan ,  Scott K. Thompson

    IPC分类号： B64D27/00

    CPC分类号： B64D41/00 ,  B64D2041/002 ,  Y10T29/49826

    摘要： The invention provides an aircraft with an auxiliary power unit isolated from the aircraft. An auxiliary power unit suspension system includes at least one suspension linkage. The suspension linkage terminates with a first low stiffness elastomeric rod end. The low stiffness elastomeric rod end has a low spring rate with the aircraft auxiliary power unit suspension system providing the aircraft auxiliary power unit with a suspended auxiliary power unit natural frequency, the suspended auxiliary power unit natural frequency below the aircraft auxiliary power unit operation frequency.

    摘要翻译： 本发明提供一种具有与飞行器隔离的辅助动力单元的飞行器。 辅助动力单元悬挂系统包括至少一个悬挂联动装置。 悬挂连杆以第一低刚性弹性体杆端终止。 低刚度弹性体杆端具有较低的弹簧刚度，飞机辅助动力单元悬架系统为飞机辅助动力单元提供悬挂的辅助动力装置固有频率，悬挂辅助动力装置的固有频率低于飞机辅助动力装置的运行频率。