Battery accommodating device, unmanned aerial vehicle and electronic device

A technology of unmanned aerial vehicle and accommodating device, which is applied in the field of battery assembly, can solve the problems of increasing weight, occupying top and bottom space, and wasting space in the fuselage, so as to strengthen the structural strength, ensure the center of gravity of the fuselage, and reduce the weight of the whole machine. Effect

Active Publication Date: 2016-09-14
SZ DJI TECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Most of the existing aircraft battery installation solutions are to glue the battery on the top or bottom of the aircraft through Velcro, but this bonding method will make the connection between the battery and the aircraft unstable, resulting in the battery being easily removed from the aircraft during the flight. Prolapse
Secondly, in order to prolong the flight time of the aircraft, it is usually necessary to increase the battery capacity, resulting in the battery being too large and inconvenient to install in the fuselage, resulting in a waste of space in the fuselage, and occupying the top and bottom space, resulting in no external expansion parts. installation location
At the same time, in order to enhance the rigidity of the fuselage, it is necessary to add many structural connectors in the fuselage, thus adding extra weight and reducing the endurance of the aircraft
In addition, batteries bonded by bonding cannot guarantee the repeatability of bonding each time, resulting in frequent changes in the center of gravity of the fuselage, which affects the flight performance of the aircraft

Method used

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  • Battery accommodating device, unmanned aerial vehicle and electronic device
  • Battery accommodating device, unmanned aerial vehicle and electronic device
  • Battery accommodating device, unmanned aerial vehicle and electronic device

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Embodiment Construction

[0082] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. 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.

[0083] Please also refer to Figure 1-2 , is a perspective view of a battery containing device 20 according to an embodiment of the present invention. The battery containing device 20 includes a first base plate 21 , a second base plate 22 , and a plurality of battery fixing frames 24 . Wherein, the plurality of battery fixing frames 24 are radially arranged and supported between the first substrate 21 and the second substrate 22 . In this embodiment, each of the...

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Abstract

A battery accommodating device (20) comprises a first substrate (21), a second substrate (22) and a plurality of battery fixing frames (24). The plurality of battery fixing frames (24) are radially arranged and supported between the first substrate (21) and the second substrate (22). An accommodating cavity (241) for allowing a battery (30) to be inserted is formed in each battery fixing frame (24). The present invention also relates to an unmanned aerial vehicle and an electronic device using the battery accommodating device (20).

Description

technical field [0001] The invention relates to the technical field of battery assembly, in particular to a battery containing device, an unmanned aerial vehicle and an electronic device using the battery containing device. Background technique [0002] Most of the existing aircraft battery installation solutions are to glue the battery on the top or bottom of the aircraft through Velcro, but this bonding method will make the connection between the battery and the aircraft unstable, resulting in the battery being easily removed from the aircraft during the flight. out. Secondly, in order to prolong the flight time of the aircraft, it is usually necessary to increase the battery capacity, resulting in the battery being too large and inconvenient to install in the fuselage, resulting in a waste of space in the fuselage, and occupying the top and bottom space, resulting in no external expansion parts. installation location. At the same time, in order to enhance the rigidity o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/26B64D27/24H01M50/209H01M50/244H01M50/249H01M50/264H01M50/271H01M50/50
CPCB64D27/24B64D27/26H01M50/271H01M50/244H01M50/209H01M50/50H01M50/264H01M50/249B64U10/10B64U50/19Y02E60/10
Inventor 张永生陈泽杰段玉琴肖文龙
Owner SZ DJI TECH CO LTD
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