Pod for near space aircraft

A near space, aircraft technology, applied in the field of aircraft

Pending Publication Date: 2018-04-17
海口未来技术研究院
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, at this stage, the thermal insulation and heat dissipation requirements for the pods of near-space vehicles are highly challenging.

Method used

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  • Pod for near space aircraft
  • Pod for near space aircraft
  • Pod for near space aircraft

Examples

Experimental program
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Embodiment Construction

[0025] Various embodiments of the invention will be described in more detail below with reference to the accompanying drawings. In the various drawings, the same elements are denoted by the same or similar reference numerals. For the sake of clarity, various parts in the drawings have not been drawn to scale.

[0026] Figure 1-2 A pod for a near-space vehicle according to an embodiment of the present invention is shown. Such as Figure 1-2 As shown, the pod for a near-space vehicle includes a pod body 1 and a cover 2, the interior of the pod body 1 forms an accommodating space such as electronic equipment, and a heat dissipation part 11 is arranged on the pod body 1 , for dissipating the heat inside the pod body 1 , the cover 2 is movably connected to the outside of the pod body 1 , and is used to cover the heat dissipation portion 11 or be spaced from the heat dissipation portion 11 at a certain distance.

[0027] The pod for a near-space vehicle includes a cover driving...

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PUM

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Abstract

The invention relates to a pod for a near space aircraft. The pod comprises a pod body (1) and a covering piece (2), a heat dissipation part (11) is arranged on the pod body and used for dissipating heat inside the pod body, the covering piece (2) is movably connected to the exterior of the pod body (1) and used for covering the heat dissipation part (11) or keeping a certain distance from the heat dissipation part (11). According to the pod for the near space aircraft, since the covering piece can adjust the distance between the covering piece and the heat dissipation part in time according to temperature change or cover the heat dissipation part, the heat dissipation speed of the pod can be effectively controlled, the temperature in the pod is kept within a reasonable range, and it is ensured that electronic equipment and the like in the pod run under a good temperature environment.

Description

technical field [0001] The invention relates to the technical field of aircraft, and more particularly, to a pod for an aircraft near space. Background technique [0002] Near space generally refers to the airspace 20-100 kilometers above the ground, which has attracted widespread attention in the world due to its important development and application value. Near-space vehicles refer to aircraft or sub-orbital vehicles that can only fly in or are capable of long-term and continuous flight in near space, or hypersonic cruise vehicles that fly in near space. They have advantages that aviation and aerospace vehicles do not have, especially in communication support. , intelligence collection, electronic suppression, early warning, civilian use and other aspects have great potential for development. [0003] Many electronic devices of the adjacent space vehicle are concentrated in the pod, resulting in a very large heating power in the pod. The basic condition for the electroni...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00B64D33/08
CPCB64D33/08B64D47/00B64G1/50B64G1/503B64G1/10B64G1/226
Inventor 不公告发明人
Owner 海口未来技术研究院
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