Thermal diaphragm suitable for annular solar telescope

A technology for solar telescopes and thermal apertures, applied in the field of thermal apertures, can solve problems such as difficulty in processing deflectors, affecting heat dissipation effects, and difficult flow of coolant, so as to ensure spatial resolution and polarization measurement accuracy, and ensure spatial resolution efficiency and reduce design difficulty

Active Publication Date: 2019-12-20
YUNNAN ASTRONOMICAL OBSERVATORY CHINESE ACAD OF SCI
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  • Application Information

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Problems solved by technology

The other type of aperture is a flat plate type, and the uniformity of the temperature field is not well controlled. The reflective surface is a plane mirror with an inclined angle, and the light outside the field of view is directed to a predetermined direction. If the direction avoids the surrounding truss, it can be ideally processed. out-of-field light
[0004] However, the shape structure of the conical and flat thermal diaphragms leads to sharp corners near the light hole (the conical type is especially obvious), because the sharp corner shape structure will cause the problem of long heat conduction path and small heat conduction cross-sectional area, which is not conducive to Heat conduction at this position affects the heat dissipation effect, resulting in a higher temperature near the light hole
[0005] In addition, the current open large-aperture solar telescopes use two cooling methods for the diaphragm body, jet impact and flow diversion. However, due to the influence of the shape and structure of the flat plate and conical thermal diaphragms, there are sharp edges in the cooling cavity near the aperture. horn
For the jet impingement cooling method, the sharp corner makes it difficult for the jet nozzle to approach the light hole area, and the coolant in the sharp corner area is not easy to flow, and it is easy to form stagnant water areas; for the diversion method, in order to ensure the thermal diaphragm Heat dissipation efficiency, the deflector also acts as a heat dissipation fin, and should be connected with the upper cover structurally, but the space here is small, and it is extremely difficult to process the deflector in the inner cavity of the upper cover
[0006] Therefore, the disadvantages of the current solar telescope thermal diaphragms in terms of temperature control are that the temperature of the existing flat and conical thermal diaphragms is high at the position of the aperture, and the existing cooling methods cannot effectively control this position. temperature, resulting in thermally induced turbulence generated in the vicinity of the aperture has a more serious adverse effect on imaging

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  • Thermal diaphragm suitable for annular solar telescope
  • Thermal diaphragm suitable for annular solar telescope
  • Thermal diaphragm suitable for annular solar telescope

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Embodiment Construction

[0028] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings of the present invention. Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0029] A thermal diaphragm suitable for annular solar telescopes of the present invention, one end of the thermal diaphragm facing light incident is a reflective surface 1, and the other end is a bottom surface 2, the reflective surface 1 of the thermal diaphragm is in the shape of an inverted cone, The bottom surface 2 is in the shape of a regular cone. The reflective surface 1 in the shape of an inverted cone and the bottom surface 2 in the shape of a regular cone are tangent after the fu...

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Abstract

The invention provides a thermal diaphragm suitable for an annular solar telescope. One end of the thermal diaphragm suitable for the annular solar telescope toward the direction of light incidence isa reflective surface, and the other end is a bottom surface; the reflective surface of the thermal diaphragm suitable for the annular solar telescope is an inverted cone shape, and the bottom surfaceis a positive cone shape; the reflective surface with the inverted cone shape and the bottom surface with the positive cone shape are tangent at the vertexes of the two cones to form a light passinghole; and the cone angle of the inverted cone of the reflective surface is 88 to 93 degrees. The thermal diaphragm structure design provided by the invention strengthens the thermal control ability near the light passing hole, optimizes the temperature field near the light passing hole, reduces stray light to the greatest extent, and suppresses a ghost image; and the thermal diaphragm suitable forthe annular solar telescope has good temperature control effect, no ghost image and good stray light suppression effect, which ensures the imaging quality of the telescope.

Description

technical field [0001] The invention relates to the technical field of precision optical instruments, in particular to a thermal aperture suitable for an annular solar telescope. Background technique [0002] The design of solar telescope thermal aperture faces the problem of thermal control of the aperture and the processing of light outside the field of view. Regarding thermal control, the local seeing at the thermal aperture has an important impact on the final imaging effect of the telescope. The turbulence generated by the heat of the thermal aperture will cause image plane jitter, image plane defocus, and image quality degradation. In order to suppress The thermal diaphragm is affected by the thermal turbulence of the light surface on the image quality, so it needs to be thermally controlled to ensure that the thermal diaphragm is not damaged by heat. Regarding the processing of light outside the field of view, it can be divided into two parts: ghost image and stray l...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G02B23/00G02B23/02
CPCG02B23/00G02B23/02
Inventor 许方宇张雨辰黄善杰徐稚王飞翔
Owner YUNNAN ASTRONOMICAL OBSERVATORY CHINESE ACAD OF SCI
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