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Battery pack packaging device and solar UAV having same

A solar unmanned aerial vehicle and packaging device technology, which is applied to secondary batteries, battery temperature control, circuits, etc., can solve problems such as reduced work performance and poor temperature control effect, so as to improve work performance, meet flight requirements, and meet thermal insulation requirements. desired effect

Active Publication Date: 2019-03-29
航天科工惯性技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The present invention provides a battery pack packaging device and a solar unmanned aerial vehicle equipped with it, which can solve the technical problem of reduced working performance caused by the poor temperature control effect of the energy storage battery system in the prior art

Method used

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  • Battery pack packaging device and solar UAV having same
  • Battery pack packaging device and solar UAV having same
  • Battery pack packaging device and solar UAV having same

Examples

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Embodiment Construction

[0025] Specific embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. In the following description, for purposes of explanation and not limitation, specific details are set forth in order to provide a thorough understanding of the invention. It will be apparent, however, to one skilled in the art that the present invention may be practiced in other embodiments that depart from these specific details.

[0026] It should be noted here that, in order to avoid obscuring the present invention due to unnecessary details, only the device structure and / or processing steps closely related to the solution according to the present invention are shown in the drawings, and the steps related to the present invention are omitted. Invent other details that don't really matter.

[0027] Such as Figure 1 to Figure 4 As shown, a battery pack packaging device is provided according to a specific embodiment of the present invention,...

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Abstract

The invention provides a battery pack packaging device and a solar UAV having the same. The battery pack packaging device comprises a shell body and a temperature control assembly, wherein the shell body has an inner cavity, and a battery pack is arranged in the inner cavity; the temperature control assembly is arranged in the shell body, the temperature control assembly comprises a heat dissipation conduit and a temperature control valve, and the temperature control valve is arranged in the heat dissipation conduit; when the temperature in the shell body is higher than or equal to a set threshold, the temperature control valve is opened, and the heat dissipation conduit is communicated to the outside for deriving heat generated by the battery pack in the inner cavity; and when the temperature in the shell body is lower than the set threshold, the temperature control valve is closed, and the heat dissipation conduit is not communicated with the outside. By applying the battery pack packaging device and the solar UAV having the same provided by the invention, the technical problem of operating performance degradation caused by poor temperature control effect of an energy storage battery system in the prior art.

Description

technical field [0001] The invention relates to the technical field of solar unmanned aerial vehicles, in particular to a battery pack packaging device and a solar unmanned aerial vehicle equipped with the same. Background technique [0002] High-altitude, low-speed and long-endurance UAVs represented by solar-powered UAVs have the characteristics of high flight altitude and strong endurance, and are suitable for military tasks such as wide-area and long-lasting reconnaissance and surveillance or communication support. Compared with other types of near-space equipment such as floating platforms and high-speed aircraft, solar-powered UAVs are faster than floating platforms, can be maneuvered forward and deployed, have a wider range of mission areas, and are easy to adapt to mission changes and emergency support It has longer flight time and wider observation coverage than high-speed aircraft, and is suitable for performing normal high-precision observation and reconnaissance ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01M10/613H01M10/615H01M10/62H01M10/635H01M10/6557H01M10/6562H01M10/6571H01M10/658
CPCH01M10/613H01M10/615H01M10/62H01M10/635H01M10/6557H01M10/6562H01M10/6571H01M10/658Y02E60/10
Inventor 王浩赵洪利庞葳王玉泽李敬
Owner 航天科工惯性技术有限公司
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