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Mounting of optical elements for imaging in air vehicles

机译:航空飞行器成像光学元件的安装

摘要

An optical assembly comprises a mounting structure, a plurality of optical elements, and a conformal filler material. The mounting structure has a plurality of axially spaced circumferentially recessed undercuts formed into an inner surface of the mounting structure. The optical elements are axially spaced in the mounting structure. At least one of the optical elements includes an undercut in a perimeter edge surface. The undercut is aligned with one of the plurality of undercuts in the mounting structure, such that the aligned circumferential undercuts define a void. The conformal filler material is cast in place in the void to create a mechanical lock between the optical element and mounting structure.
机译:光学组件包括安装结构,多个光学元件和保形填充材料。安装结构具有形成在安装结构的内表面中的多个轴向间隔开的周向凹入的底切。光学元件在安装结构中轴向间隔。光学元件中的至少一个在周边边缘表面中包括底切。底切与安装结构中的多个底切之一对准,使得对准的周向底切限定空隙。共形填充材料被浇铸在空隙中,以在光学元件和安装结构之间建立机械锁定。

著录项

  • 公开/公告号US10330884B2

    专利类型

  • 公开/公告日2019-06-25

    原文格式PDF

  • 申请/专利权人 ROSEMOUNT AEROSPACE INC.;

    申请/专利号US201715437321

  • 发明设计人 TIMOTHY DEANGELO;

    申请日2017-02-20

  • 分类号B64D47/08;G02B7/02;H04N5/225;H04N7/18;

  • 国家 US

  • 入库时间 2022-08-21 12:15:40

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