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
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.
✦ Generated by Eureka AI based on patent content.
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.
Need to check novelty before this filing date? Find Prior Art