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A deployable light shield

A hood and fluid circuit technology, applied in the field of aerospace optical remote sensing, can solve problems such as the influence of optical lenses, the formation of local hot spots, large temperature non-uniformity, etc., to ensure uniformity and stability, and improve the effect of imaging quality.

Active Publication Date: 2014-03-19
BEIJING AEROSPACE HEZHONG TECH DEV
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AI Technical Summary

Problems solved by technology

However, for the expandable sunshade, the size in the length direction is larger, and the closer to the optical lens along the length direction, the smaller the visible view factor of the cool black space. Because the absorbed external heat flow energy cannot be dissipated in time, it will cause local high temperature and even form local hot spots
For large-aperture optical systems, the temperature of the hood has a significant impact on the optical lens. In this case, the local high temperature and hot spots in some areas of the hood will inevitably have a bad impact on the temperature of the optical lens.
In addition, due to the complex wiring of the movable mechanism of the deployable structure, it is impossible to arrange an active temperature control heating circuit on its surface to suppress the temperature fluctuation between different areas on the track and at different times in the same area.
Its large temperature non-uniformity is bound to adversely affect the optical lens

Method used

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Embodiment Construction

[0015] The technical solution of the present invention will be further described below in combination with specific embodiments.

[0016] The purpose of the present invention is to design an expandable shading cover with a fluid temperature control function, and solve the temperature control problem of the expandable shading cover of a large-diameter remote sensor by controlling the flow rate of the working medium in the fluid circuit.

[0017] The expandable shading cover in the present invention includes a fluid circuit pipeline, fins, heat insulation components, and a temperature control system;

[0018] The fluid circuit pipeline forms a spiral skeleton with a taper, one end of the pipeline is the liquid inlet, and the other end is the liquid outlet; several fins are welded sequentially along the fluid circuit pipeline, and the upper end of each fin is welded On the outer wall of the fluid circuit, the other sides are in a free state; the thermal insulation component is wr...

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Abstract

The invention discloses a deployable light shield comprising fluid loop pipelines, fins, a heat insulation assembly and a temperature control system. The deployable light shield designed by the invention has a fluid temperature control function, and solves temperature control problems of existing large aperture optical remote sensor deployable light shields. When sunshine directly shines on the fins or fluid loop pipelines inside the light shield, heat is rapidly taken away through the fluid loops, so that a rapid temperature equalizing effect is realized, and the uniformity and stability of optical lens are ensured, and the quality of imaging is raised. In addition, the fluid loops can provide an auxiliary adjusting effect for a heat control system of a whole machine of a remote sensor.

Description

technical field [0001] The invention relates to an expandable shading cover, in particular to an expandable shading cover with a fluid temperature control function applied to a space remote sensor, and belongs to the technical field of aerospace optical remote sensing. Background technique [0002] In order to suppress the influence of stray light, the front end of the optical lens of the space optical remote sensor needs to be provided with a hood. With the development of space remote sensing technology, the aperture of the optical system of the space optical remote sensor is constantly increasing. In order to effectively suppress the influence of stray light, it is necessary to equip a longer size hood. The length of the hood even exceeds the envelope of the rocket fairing. In this case, the expandable sunshade technology can optimize the space interface relationship between the sunshade and the satellite through the design of retractable launch and in-orbit ejection, so a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D23/20
Inventor 颜吟雪赵宇申春梅于波杨涛于峰王兵张新画
Owner BEIJING AEROSPACE HEZHONG TECH DEV
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