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Novel Cassegrain system primary mirror and secondary mirror supporting structure

A technology supported by Cassegrain and secondary mirrors, applied in the field of aerospace optical remote sensors, can solve the problems of poor stability, poor stability, and optical system influence in the adjustment link of the lens, and achieve the effect of achieving stability and improving the ability to maintain accuracy.

Active Publication Date: 2021-03-19
HUAZHONG PHOTOELECTRIC TECH INST (CHINA SHIPBUILDING IND CORP THE NO 717 INST)
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  • Application Information

AI Technical Summary

Problems solved by technology

There are mainly three problems in the current support design of the primary and secondary mirror structures: the lens is mainly fixed by various types of curing glue, which is not easy to generate stress, and then has poor stability for a long time; the assembly and adjustment of the secondary mirror part, the secondary mirror is more prone to pose Changes, and the impact on the optical system is more serious; the adjustment link of the lens is often poor in stability or complex in structure

Method used

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  • Novel Cassegrain system primary mirror and secondary mirror supporting structure
  • Novel Cassegrain system primary mirror and secondary mirror supporting structure
  • Novel Cassegrain system primary mirror and secondary mirror supporting structure

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Embodiment Construction

[0020] Embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0021] Such as figure 1 As shown, the overall structure of this embodiment includes a mirror frame mechanism, a primary mirror holder 4 and a secondary mirror holder 5, and the mirror frame mechanism includes a primary mirror frame 1, a secondary mirror frame 3 and a connecting rod 2, and the primary mirror The frame 1 and the secondary mirror frame 3 are ring-shaped structures, coaxially arranged, and connected by a plurality of connecting rods 2. The primary mirror 6 and the secondary mirror 7 are respectively arranged in the inner holes of the primary mirror frame 1 and the secondary mirror frame 3. The primary mirror 6 is fixed by the primary mirror hold-down ring 4, and the secondary mirror 7 is fixed by the secondary mirror hold-down ring 5. The primary mirror frame 1 is provided with a plurality of primary mirror pose adjustment devices 8, which...

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Abstract

The invention provides a novel Cassegrain system primary mirror and secondary mirror supporting structure, which is mainly characterized in that an assembly adjustment structure of a lens is designedon a primary mirror bracket, and flexible support is adopted to position and support the lens, so that the problem of relative position change of a primary mirror and a secondary mirror caused by temperature change, vibration and the like is solved, and the long-time relative stability of the primary mirror and the secondary mirror is effectively maintained. According to the technical scheme, thenovel Cassegrain system primary mirror and secondary mirror supporting structure comprises a lens frame mechanism, a primary lens pressing ring and a secondary lens pressing ring, the lens frame mechanism comprises a primary lens frame, a secondary lens frame and connecting rods, the primary lens frame and the secondary lens frame are both of an annular structure, are coaxially arranged and are connected through the multiple connecting rods, a primary lens and a secondary lens are correspondingly arranged in the inner holes of the primary lens frame and the secondary lens frame respectively, the primary lens is fixed through the primary lens pressing ring, the secondary lens is fixed through the secondary lens pressing ring, and a plurality of primary lens pose adjusting devices are arranged on the primary lens frame and can adjust the pose of the primary lens relative to the secondary lens.

Description

technical field [0001] The invention relates to the technical field of aerospace optical remote sensors, in particular to a novel Cassegrain system primary and secondary mirror support structure. Background technique [0002] In the field of astronomical star measurement, star measuring devices based on the principle of the Cassegrain optical system are widely used. This type of Cassegrain optical system requires extremely high precision, but the operating environment is often very harsh, and it must withstand large temperature changes and Strong vibration will cause changes in the relative pose of the primary and secondary mirrors, reducing the accuracy of the optical system. There are mainly three problems in the current support design of the primary and secondary mirror structures: the lens is mainly fixed by various types of curing glue, which is not easy to generate stress, and then has poor stability for a long time; the assembly and adjustment of the secondary mirror ...

Claims

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Application Information

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IPC IPC(8): G02B7/183
CPCG02B7/183Y02E10/47
Inventor 刘元锋陈冲马晓熊海宏
Owner HUAZHONG PHOTOELECTRIC TECH INST (CHINA SHIPBUILDING IND CORP THE NO 717 INST)
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