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1. 发明申请

US20070176051A1 ACTUATION DEVICE POSITIONING SYSTEMS AND ASSOCIATED METHODS, INCLUDING AIRCRAFT SPOILER DROOP SYSTEMS 有权
标题翻译：执行装置定位系统及相关方法，包括飞机起落架系统
公开(公告)号：US20070176051A1
公开(公告)日：2007-08-02
申请号：US11116905
申请日：2005-04-27
申请人： Mark Good , Neal Huynh , Kelly Jones , Selya Sakurai
发明人： Mark Good , Neal Huynh , Kelly Jones , Selya Sakurai
IPC分类号： B64C3/50
CPC分类号： B64C9/16 , B64C9/32 , B64C9/323 , B64C2009/143 , Y02T50/32
摘要： Actuation device positioning systems and associated methods, including aircraft spoiler droop systems are generally disclosed herein. One aspect of the invention is directed toward a positioning system that includes an eccentric cam and a drive mechanism coupled to the eccentric cam to rotate the eccentric cam between a first cam position and a second cam position. The system can further include an actuation device having an anchor portion and a movable portion that is movable relative to the anchor portion, the anchor portion operatively coupled to the eccentric cam. The eccentric cam can be positioned to move the anchor portion to a first anchor position when the eccentric cam is rotated to the first cam position and to move the anchor portion to a second anchor position when the eccentric cam is rotated to the second cam position.
摘要翻译：本文通常公开了致动装置定位系统和相关方法，包括飞机扰流器下垂系统。本发明的一个方面涉及一种定位系统，其包括偏心凸轮和联接到偏心凸轮的驱动机构，以在第一凸轮位置和第二凸轮位置之间旋转偏心凸轮。该系统还可以包括具有锚定部分和可相对于锚固部分可移动的可移动部分的致动装置，该锚固部分可操作地联接到偏心凸轮。当偏心凸轮旋转到第一凸轮位置时，偏心凸轮可以定位成将锚固部分移动到第一锚固位置，并且当偏心凸轮旋转到第二凸轮位置时，偏心凸轮可以定位成将锚定部分移动到第一锚定位置。

2. 发明授权

US07309043B2 Actuation device positioning systems and associated methods, including aircraft spoiler droop systems 有权
标题翻译：致动装置定位系统及相关方法，包括飞机扰流器下垂系统
公开(公告)号：US07309043B2
公开(公告)日：2007-12-18
申请号：US11116905
申请日：2005-04-27
申请人： Mark S. Good , Neal V. Huynh , Kelly T. Jones , Selya Sakurai
发明人： Mark S. Good , Neal V. Huynh , Kelly T. Jones , Selya Sakurai
IPC分类号： B64C9/00
CPC分类号： B64C9/16 , B64C9/32 , B64C9/323 , B64C2009/143 , Y02T50/32
摘要： Actuation device positioning systems and associated methods, including aircraft spoiler droop systems are generally disclosed herein. One aspect of the invention is directed toward a positioning system that includes an eccentric cam and a drive mechanism coupled to the eccentric cam to rotate the eccentric cam between a first cam position and a second cam position. The system can further include an actuation device having an anchor portion and a movable portion that is movable relative to the anchor portion, the anchor portion operatively coupled to the eccentric cam. The eccentric cam can be positioned to move the anchor portion to a first anchor position when the eccentric cam is rotated to the first cam position and to move the anchor portion to a second anchor position when the eccentric cam is rotated to the second cam position.
摘要翻译：本文通常公开了致动装置定位系统和相关方法，包括飞机扰流器下垂系统。本发明的一个方面涉及一种定位系统，其包括偏心凸轮和联接到偏心凸轮的驱动机构，以在第一凸轮位置和第二凸轮位置之间旋转偏心凸轮。该系统还可以包括具有锚定部分和可相对于锚固部分可移动的可移动部分的致动装置，该锚固部分可操作地联接到偏心凸轮。当偏心凸轮旋转到第一凸轮位置时，偏心凸轮可以定位成将锚固部分移动到第一锚固位置，并且当偏心凸轮旋转到第二凸轮位置时，偏心凸轮可以定位成将锚定部分移动到第一锚定位置。

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