-
公开(公告)号：US20130341457A1
公开(公告)日：2013-12-26
申请号：US13531650
申请日：2012-06-25
申请人： Phillip K. Wilson
发明人： Phillip K. Wilson
IPC分类号： B64C25/60
摘要： The landing gear system for an aircraft includes a shock strut assembly that is coupled to the airframe with a universal joint. A tire member is mounted to the shock strut assembly. The landing gear system also includes a drag brace assembly coupled to an airframe of the aircraft with a spindle, the spindle being rotatable about a spindle axis. A radius rod is rotatably coupled to the airframe of the aircraft. The radius rod and the shock strut assembly are retractable about a retraction rotation axis. Further, the spindle axis has a common intersection point with the centerline axis and the retraction rotation axis. The orientation of the spindle axis causes a translation of the tire member to have a longitudinal component during a compression of the shock strut assembly.
摘要翻译： 用于飞机的起落架系统包括用万向接头联接到机身的冲击支柱组件。 轮胎构件安装在冲击支柱组件上。 起落架系统还包括与主轴联接到飞行器的机身的牵引支架组件，所述主轴可围绕主轴轴线旋转。 半径杆可旋转地联接到飞行器的机身。 半径杆和冲击支柱组件围绕收回旋转轴线可收缩。 此外，主轴具有与中心线轴和缩回旋转轴线的共同交点。 在冲击支柱组件的压缩过程中，主轴的方位导致轮胎构件的平移，以具有纵向分量。
-
公开(公告)号：US20090321560A1
公开(公告)日：2009-12-31
申请号：US12491021
申请日：2009-06-24
IPC分类号： B64C25/10
CPC分类号： B64C25/14 , B64C2025/008
摘要： A landing gear system includes a shock strut assembly and a linkage member coupled to an aircraft. Preferably, the shock strut assembly and linkage member are oriented or angled relative to one another in a non-parallel relationship. Actuation of the linkage member moves the shock strut from a de-hiked to a hiked configuration or vice-versa. In addition, the orientation of the linkage member relative to the shock strut assembly permits it to automatically move the shock strut assembly to the de-hiked position during retraction of the landing gear system and prevents the shock strut assembly from exceeding a desired length during retraction. The linkage member may take the form of a hydraulic actuator having a lower end portion coupled to an inner cylinder of the shock strut assembly and an upper end portion coupled to the aircraft aft of where the shock strut assembly is coupled to the aircraft.
摘要翻译： 起落架系统包括冲击支柱组件和联接到飞行器的联动构件。 优选地，冲击支柱组件和连接构件以非平行关系相对于彼此定向或成角度。 联动构件的致动将冲击支柱从脱轨装置移动到高架配置，反之亦然。 此外，联动构件相对于冲击支柱组件的取向允许其在起落架系统缩回期间自动地将冲击支柱组件移动到脱离位置，并且在缩回期间防止冲击支柱组件超过所需长度 。 连杆构件可以采取液压致动器的形式，其具有联接到减震支柱组件的内圆筒的下端部分，以及联接到飞行器后部的上端部分，其中冲击支柱组件联接到飞行器。
-
公开(公告)号：US08186620B2
公开(公告)日：2012-05-29
申请号：US12491021
申请日：2009-06-24
IPC分类号： B64C25/10
CPC分类号： B64C25/14 , B64C2025/008
摘要： A landing gear system includes a shock strut assembly and a linkage member coupled to an aircraft. Preferably, the shock strut assembly and linkage member are oriented or angled relative to one another in a non-parallel relationship. Actuation of the linkage member moves the shock strut from a de-hiked to a hiked configuration or vice-versa. In addition, the orientation of the linkage member relative to the shock strut assembly permits it to automatically move the shock strut assembly to the de-hiked position during retraction of the landing gear system and prevents the shock strut assembly from exceeding a desired length during retraction. The linkage member may take the form of a hydraulic actuator having a lower end portion coupled to an inner cylinder of the shock strut assembly and an upper end portion coupled to the aircraft aft of where the shock strut assembly is coupled to the aircraft.
摘要翻译： 起落架系统包括冲击支柱组件和联接到飞行器的联动构件。 优选地，冲击支柱组件和连接构件以非平行关系相对于彼此定向或成角度。 联动构件的致动将冲击支柱从脱轨装置移动到高架配置，反之亦然。 此外，联动构件相对于冲击支柱组件的取向允许其在起落架系统缩回期间自动地将冲击支柱组件移动到脱离位置，并且在缩回期间防止冲击支柱组件超过所需长度 。 连杆构件可以采取液压致动器的形式，其具有联接到减震支柱组件的内圆筒的下端部分，以及联接到飞行器后部的上端部分，其中冲击支柱组件联接到飞行器。
-
公开(公告)号：US08752785B2
公开(公告)日：2014-06-17
申请号：US13531650
申请日：2012-06-25
申请人： Phillip K. Wilson
发明人： Phillip K. Wilson
IPC分类号： B64C25/00
摘要： The landing gear system for an aircraft includes a shock strut assembly that is coupled to the airframe with a universal joint. A tire member is mounted to the shock strut assembly. The landing gear system also includes a drag brace assembly coupled to an airframe of the aircraft with a spindle, the spindle being rotatable about a spindle axis. A radius rod is rotatably coupled to the airframe of the aircraft. The radius rod and the shock strut assembly are retractable about a retraction rotation axis. Further, the spindle axis has a common intersection point with the centerline axis and the retraction rotation axis. The orientation of the spindle axis causes a translation of the tire member to have a longitudinal component during a compression of the shock strut assembly.
摘要翻译： 用于飞机的起落架系统包括用万向接头联接到机身的冲击支柱组件。 轮胎构件安装在冲击支柱组件上。 起落架系统还包括与主轴联接到飞行器的机身的牵引支架组件，所述主轴可围绕主轴轴线旋转。 半径杆可旋转地联接到飞行器的机身。 半径杆和冲击支柱组件围绕收回旋转轴线可收缩。 此外，主轴具有与中心线轴和缩回旋转轴线的共同交点。 在冲击支柱组件的压缩过程中，主轴的方位导致轮胎构件的平移，以具有纵向分量。
-
-
-
搜索结果
4 条记录 (耗时 0.011 秒)
