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1. 发明申请

US20080203222A1 Yaw Control System and Method 失效
标题翻译：偏航控制系统和方法
公开(公告)号：US20080203222A1
公开(公告)日：2008-08-28
申请号：US11678044
申请日：2007-02-22
申请人： Edward D. Johnson , Howard C. Kress
发明人： Edward D. Johnson , Howard C. Kress
IPC分类号： B64C3/38 , B64C13/00
CPC分类号： B64C27/10 , B64C27/72 , B64C2027/7266 , Y02T50/34
摘要： A yaw control system and a method of controlling yaw for an aircraft are provided. The yaw control system includes a first wing set and a second wing set which are rotatable in opposite directions. Each of the wing sets includes at least two wings each including a pivotable flap forming a trailing edge of its respective wing. A flap control assembly controls the pivotable flaps of the first wing set and of the second wing set such that when the pivotable flaps of the first wing set are pivoted in a first direction by a first set angle, the pivotable flaps of the second wing set are simultaneously pivoted by a second set angle in an opposite direction, thereby providing yaw control for the aircraft.
摘要翻译：提供了一种用于飞行器的偏航控制系统和控制偏航的方法。偏航控制系统包括可沿相反方向旋转的第一机翼组和第二机翼组。每个翼组包括至少两个翼，每个翼包括形成其相应翼的后缘的可枢转翼。翼片控制组件控制第一翼组和第二翼组的可枢转翼片，使得当第一翼组的可枢转翼片沿第一方向枢转第一设定角时，第二翼组的可枢转翼片同时以相反方向枢转第二设定角度，从而为飞行器提供偏航控制。

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