Invention Grant
US07708561B2 Method and apparatus for modifying aircraft simulator wide-angled infinity display equipment mirror to enlarge field of vision and for reskinning aircraft simulator spherical mirror cell to minimize mirror stress and distortion 有权
用于修改飞机模拟器广角无限展示设备镜的方法和装置,以扩大视野并重新激光飞行器模拟器球面镜单元以最小化镜面应力和变形

  • Patent Title: Method and apparatus for modifying aircraft simulator wide-angled infinity display equipment mirror to enlarge field of vision and for reskinning aircraft simulator spherical mirror cell to minimize mirror stress and distortion
  • Patent Title (中): 用于修改飞机模拟器广角无限展示设备镜的方法和装置,以扩大视野并重新激光飞行器模拟器球面镜单元以最小化镜面应力和变形
  • Application No.: US11534176
    Application Date: 2006-09-21
  • Publication No.: US07708561B2
    Publication Date: 2010-05-04
  • Inventor: Michael Luther PonderMartyn John Rolls
  • Applicant: Michael Luther PonderMartyn John Rolls
  • Applicant Address: US FL Winter Park
  • Assignee: Q4 Services LLC
  • Current Assignee: Q4 Services LLC
  • Current Assignee Address: US FL Winter Park
  • Agency: CARR LLP
  • Agent Theodore F. Shiells
  • Main IPC: G09B19/16
  • IPC: G09B19/16
Method and apparatus for modifying aircraft simulator wide-angled infinity display equipment mirror to enlarge field of vision and for reskinning aircraft simulator spherical mirror cell to minimize mirror stress and distortion
Abstract:
A method and apparatus for extending the effective circumferential extent of an original an aircraft simulator mirror cell having a base support structure mounted to a movable platform, the base support structure being in generally the shape of a portion of a sphere of a predetermined radius and having a predetermined circumferential extent defined by original edges of the support structure configured to support a vacuum-shaped reflective film. The improvement includes a pair of extension wing structures having substantially the same spherical radius as the base support structure and a substantial circumferential extent, each of the pair of wing structures being attached to one of the original edges of the base support structure and substantially sealed thereto, the extension wing structures, when attached, extending the effective circumferential extent of the base support structure by a substantial amount, each of the pair of extension wing structures having outer edges for supporting a vacuum-shaped reflective film.
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