发明授权
- 专利标题: RECESSED LIFT SPOILER ASSEMBLY FOR AIRFOILS
- 专利标题(中): 用于AIRFOILS的升降式升降机组件
-
申请号: EP14792283.5申请日: 2014-04-28
-
公开(公告)号: EP2991896B1公开(公告)日: 2017-11-15
- 发明人: EMERICK, Mark F.
- 申请人: Northrop Grumman Systems Corporation
- 申请人地址: 2980 Fairview Park Drive Falls Church, VA 22042 US
- 专利权人: Northrop Grumman Systems Corporation
- 当前专利权人: Northrop Grumman Systems Corporation
- 当前专利权人地址: 2980 Fairview Park Drive Falls Church, VA 22042 US
- 代理机构: CSY St Albans
- 优先权: US201361818395P 20130501; US201414262647 20140425
- 国际公布: WO2014179225 20141106
- 主分类号: B64C21/02
- IPC分类号: B64C21/02 ; B64C7/00 ; B64C39/10 ; B64C21/00
摘要:
A spoiler assembly is provided that is engageable to a UAV that defines a body, an outer surface and an inner surface. The spoiler assembly comprises a spoiler, translatably connected to the UAV inner surface adjacent a first portion of the spoiler aperture. The spoiler defines an upper surface and an outer surface, the upper surface being substantially the same size and shape as the spoiler aperture. A spoiler shroud is connected to the UAV inner surface and extends within the UAV body about at least a portion of the spoiler aperture. A spoiler activating mechanism is secured to the UAV inner surface and connected the spoiler lower surface. The mechanism is operative to translate the spoiler between a first position wherein the spoiler upper surface is substantially flush with the UAV outer surface, and second a position, wherein the spoiler upper surface is disposed substantially within the UAV body.
公开/授权文献
- EP2991896A1 RECESSED LIFT SPOILER ASSEMBLY FOR AIRFOILS 公开/授权日:2016-03-09
信息查询