Battery tank structure of unmanned aerial vehicle

By designing a combination of rectangular parallelepiped structure and positioning holes in the battery compartment of the drone, the problem of the battery compartment occupying a large space is solved, the battery position and center of gravity can be adjusted flexibly, and the overall compactness and space utilization of the drone are improved. efficiency.

CN109941445AInactive Publication Date: 2019-06-28HIWING AVIATION GENERAL EQUIP
6 Cites 2 Cited by

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
HIWING AVIATION GENERAL EQUIP
Filing Date
2017-12-21
Publication Date
2019-06-28
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

Existing UAV battery compartments occupy a large space, making it difficult to rationally allocate the limited space and design a reasonable cabin structure.

Method used

Design a UAV battery cabin with a rectangular parallelepiped structure. Multiple positioning holes are provided on the side wall of the cabin. The battery locking mechanism fixes the battery through these holes, and the battery position can be adjusted to adjust the center of gravity of the UAV.

Benefits of technology

It achieves rational use of space, adjusts the center of gravity of the drone by adjusting the battery position, and improves the overall compactness of the drone.

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Abstract

The invention discloses a battery tank structure of an unmanned aerial vehicle (UAV) and relates to the technologies of battery tank structures of UAVs. The battery tank structure can solve the problem of large space occupation of a battery tank of an existing UAV. A main battery tank body is of a rectangular structure, is placed in the middle of a UAV body, the side wall of the tank body is provided with a plurality of positioning holes, and a battery locking mechanism is fixed by the positioning holes and fixedly connected to a battery after the battery is inserted into the battery tank; byfixing the battery locking mechanism to the positioning holes in different positions, the position of the battery in the whole UAV body is adjusted, and correspondingly the position of the gravity center of the UAV body is adjusted. The structure is mainly used for UAVs.
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Citation Information

Patent Citations

  • Displacement adjustment device, cell holder for UAV (unmanned aerial vehicle) and UAV

    CN105197249A

  • Robot battery gravity center adjusting structure

    CN107284547A

  • Multi-rotor type aircraft battery fixing structure

    CN204473148U

  • Full load bearing structure unmanned aerial vehicle

    CN205396511U

  • Aircraft power mount

    CN206417204U

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