专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20060175468A1 Systems and methods for controlling aircraft flaps and spoilers 有权
标题翻译：用于控制飞机襟翼和扰流板的系统和方法
公开(公告)号：US20060175468A1
公开(公告)日：2006-08-10
申请号：US11051738
申请日：2005-02-04
申请人： Neal Huynh , Robert Bleeg , Ralph Pepper , John Standley , Brian Bocksch
发明人： Neal Huynh , Robert Bleeg , Ralph Pepper , John Standley , Brian Bocksch
IPC分类号： B64C9/22
CPC分类号： B64C9/16 , B64C9/323 , B64D2045/001 , Y02T50/32 , Y02T50/44
摘要： Systems and methods for controlling aircraft flaps and spoilers are disclosed. Systems in accordance with some embodiments include a wing having a trailing edge, and a flap positioned proximate to the wing trailing edge and being deployable relative to the wing between a first flap position and a second flap position by operation of a first actuator. A spoiler can be positioned at least proximate to the trailing edge and can be movable among at least three positions, including a first spoiler position in which the spoiler forms a generally continuous contour with an upper surface of the wing, a second spoiler position deflected downwardly from the first, and a third spoiler position deflected upwardly from the first. A second actuator can be operatively coupled to the spoiler to move the spoiler among the first, second and third spoiler positions in a manner that is mechanically independent of the motion of the flap.
摘要翻译：公开了用于控制飞机襟翼和扰流板的系统和方法。根据一些实施例的系统包括具有后缘的机翼和靠近机翼后缘设置的翼片，并且通过第一致动器的操作可相对于翼片在第一翼片位置和第二翼片位置之间展开。扰流器可以至少靠近后缘定位，并且可以在至少三个位置之间移动，包括第一扰流器位置，其中扰流器与翼的上表面形成大致连续的轮廓，向下偏转的第二扰流器位置从第一和第三扰流器位置向上偏离第一扰流器位置。第二致动器可以可操作地联接到扰流板，以在机械上独立于挡板的运动的方式在第一，第二和第三扰流板位置之间移动扰流板。

IPRDB

热门服务

关于我们

友情链接

联系方式