A device for quick installation of a drone battery

Abstract

The application provides a device for quick installation of a battery of a UAV, which comprises a bottom mounting beam fixedly connected with a mounting surface of the UAV, a bottom plate arranged on the bottom mounting beam and used for mounting the battery, and an angle bar arranged on the left and right sides of the bottom plate and used for limiting lateral displacement of the battery; a cable tie is connected with the upper and lower edges of the bottom plate and used for limiting longitudinal displacement of the battery. The device for quick installation of a lithium battery of a UAV provided by the application can meet the installation requirements and realize quick installation of a lightweight battery.

Description

Technical Field

[0001] This application belongs to the field of unmanned aerial vehicle (UAV) structural design technology, specifically relating to a device for rapid installation of UAV batteries. Background Technology

[0002] A drone mainly consists of an airframe, a power system, a flight control system, and a transmission system. The power system typically consists of an engine, a generator, and batteries, providing the power required by the aircraft.

[0003] In the design of drone lithium battery installation, it is necessary to ensure the stability and accuracy of battery installation while avoiding a significant increase in weight as much as possible.

[0004] Designing a structure that meets installation requirements while enabling lightweight and rapid battery installation is of paramount importance. Utility Model Content

[0005] Purpose of the utility model: To provide a device for the rapid installation of lithium batteries for drones, which can meet the installation requirements and achieve rapid installation of lightweight batteries.

[0006] This application provides an apparatus for rapid installation of a drone battery, the apparatus comprising: The bottom mounting beam is fixedly connected to the mounting surface of the drone; A base plate, mounted on the bottom mounting beam, is used to mount the battery. Angle members are provided on the left and right sides of the base plate, and the angle members are used to limit the lateral displacement of the battery; Cable ties are connected to the upper and lower edges of the base plate, and the cable ties are used to limit the longitudinal displacement of the battery.

[0007] Preferably, the device further includes: The first adhesive-backed Velcro fastener is attached to the base plate; A second adhesive-backed Velcro strap is installed on the bottom surface of the battery; the first adhesive-backed Velcro strap and the second adhesive-backed Velcro strap are attached to each other to fix the bottom surface of the battery to the base plate.

[0008] Preferably, the shape of the bottom mounting beam matches the shape of the mounting surface of the UAV.

[0009] Preferably, the base plate is a carbon fiber base plate.

[0010] Preferably, the angle material is carbon fiber angle material.

[0011] Preferably, the carbon fiber angle and the bottom mounting beam are installed to the carbon fiber base plate by riveting.

[0012] This application has the following technical advantages: This application provides a device for quick installation of drone batteries, which effectively improves the structural strength and reliability of the product in extreme environments, and reduces the product weight; the Velcro's easy installation and removal feature enhances the product's maintainability. Attached Figure Description

[0013] Figure 1 This is a schematic diagram of a device for rapid installation of drone batteries provided in an embodiment of this application; Figure 2 This is a schematic diagram showing the lithium battery after installation, as provided in the embodiments of this application. Detailed Implementation Please see Figure 1 and Figure 2 This utility model provides a device for the rapid installation of lithium batteries on a certain type of drone.

[0014] The device mainly consists of a mounting bracket assembly, cable ties, and Velcro with adhesive backing. The specific structure is as follows: Figure 1 As shown, carbon fiber angle piece 1, carbon fiber base plate 2, bottom mounting beam 3, Velcro with adhesive backing 4, cable ties 5.

[0015] The overall structure of the mounting device is constructed by riveting together multiple carbon fiber sheets and angle brackets through simple mechanical cutting. Carbon fiber is characterized by its low density and high strength, and is widely used in aerospace, drones, automobiles, and other fields. Carbon fiber also exhibits high reliability when operating in extreme environments.

[0016] Because the overall structure of the installation device has a small spatial dimension, waste materials generated during the processing of other drone components can be used for supplementary processing, saving production and manufacturing costs.

[0017] This design effectively improves the product's structural strength and reliability in extreme environments, while reducing the product's weight; the Velcro's easy installation and removal feature enhances the product's maintainability.

[0018] Assembly of the mounting device: According to the component diagram of the lithium battery mounting bracket, the carbon fiber angle and the bottom mounting beam (for matching the drone mounting surface) are installed to the base plate by riveting.

[0019] Installation of the mounting device: After assembly, fix the base plate mounting beam to the drone mounting surface.

[0020] Lithium battery installation: Attach adhesive Velcro straps to the base plate to secure the lithium battery mounting surface to the base plate, and finally use cable ties to laterally secure the lithium battery.

Claims

1. A device for rapid installation of a drone battery, characterized in that, The device includes: The bottom mounting beam is fixedly connected to the mounting surface of the drone; A base plate, mounted on the bottom mounting beam, is used to mount the battery. Angle members are provided on the left and right sides of the base plate, and the angle members are used to limit the lateral displacement of the battery; Cable ties are connected to the upper and lower edges of the base plate, and the cable ties are used to limit the longitudinal displacement of the battery.

2. The apparatus according to claim 1, characterized in that, The device further includes: The first adhesive-backed Velcro fastener is installed on the base plate; A second adhesive-backed Velcro strap is installed on the bottom surface of the battery; the first adhesive-backed Velcro strap and the second adhesive-backed Velcro strap are attached to each other to fix the bottom surface of the battery to the base plate.

3. The apparatus according to claim 2, characterized in that, The shape of the bottom mounting beam matches the shape of the mounting surface of the UAV.

4. The apparatus according to claim 3, characterized in that, The base plate is a carbon fiber base plate.

5. The apparatus according to claim 4, characterized in that, The angle material is carbon fiber angle material.

6. The apparatus according to claim 5, characterized in that, The carbon fiber angle and the bottom mounting beam are respectively installed to the carbon fiber base plate by riveting.

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