Composite optical window for photogrammetric camera under vacuum low-temperature environment

A kind of optical window and window technology, applied in the field of optical window, can solve the problems that affect the camera shooting effect, digital photo exposure, affect the success of the test, etc., and achieve the effect of eliminating the overexposure phenomenon

Active Publication Date: 2019-05-10
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, in the vacuum and low temperature environment in China, the protection cabins used for photogrammetry use traditional optical windows. During the work process, the strong flashes emitted by the flash will be reflected into the lens of the photogrammetry camera through the window

Method used

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  • Composite optical window for photogrammetric camera under vacuum low-temperature environment
  • Composite optical window for photogrammetric camera under vacuum low-temperature environment
  • Composite optical window for photogrammetric camera under vacuum low-temperature environment

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Embodiment Construction

[0019] The Mars surface thermal environment simulation system of the present invention will be described in detail below with reference to the accompanying drawings, but the description is only exemplary and not intended to limit the protection scope of the present invention.

[0020] see figure 2 , figure 2 It is a structural schematic diagram of a compound optical window used in a photogrammetry camera in a specific embodiment of the present invention. The composite optical window for the photographic camera installed in the protective cabin during the deformation measurement of the spacecraft is a circular optical window with a diameter of Φ170mm and a ratio of diameter to thickness of 10:1. Among them, the diameter of the outer surface of the inner ring window is Φ64mm, and the diameter of the inner surface is Φ70mm. The inner ring window is made of A1 grade fused silica glass, which is processed through optical precision polishing, so that the parallelism of both side...

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Abstract

The invention discloses a composite optical window for a photographic camera arranged in a protection cabin during deformation measurement of a spacecraft. The composite optical window is formed by two portions, that is, an inner ring window and an outer ring window, which are integrated through gluing. The inner ring window is made of A1-level or higher-level fused silica glass; the outer ring window is made of common silica glass; and an interface between the inner ring window and the outer ring window forms an inclination angle of 10 degrees with the window surface normal line. The composite optical window mainly plays a role of realizing total reflection of the light incident into the protection cabin to prevent stray flash from entering a camera lens. The composite optical window canobviously overcome influence of a window of the protection cabin on work of the photographic camera, eliminate the over-exposure phenomenon of the shooting image due to reflection of the window for aflash lamp in the photogrammetry process, and meet photogrammetry application requirements under a special environment of needing a closed optical window.

Description

technical field [0001] The invention belongs to the technical field of optical testing, and in particular relates to a component in a measuring camera, especially an optical window. Background technique [0002] In the vacuum and low temperature environment, when the photogrammetry method is used to measure the deformation of the spacecraft, the photogrammetry camera needs to be photographed at different positions in the container, and then the measurement is carried out. This step is the photogrammetry in the vacuum and low temperature environment. Important guarantee. Since the photogrammetry camera cannot be used directly in a vacuum and low temperature environment, it is necessary to design a special protection cabin. See for example figure 1 , figure 1 The structural diagram of the protective cabin of the photogrammetry camera is shown, wherein the optical projection window 1 is installed on the protective cabin 4, which mainly plays the role of providing an undistor...

Claims

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Application Information

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IPC IPC(8): G01B11/16G01C11/02
Inventor 蒋山平杨林华张鹏嵩张博伦王丹艺王劭溥向艳红李竑松
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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