CN-224232872-U - Unmanned aerial vehicle electric Chi Cang structure with guide rail positioning function

Abstract

The utility model relates to an unmanned aerial vehicle power Chi Cang structure with a guide rail for positioning, which comprises at least one electric guide rail, wherein guide rail positioning grooves extending along the length direction are arranged on two sides of the electric guide rail, a connection accommodating section is formed between the two guide rail positioning grooves, and a storage battery assembly is in sliding connection with the electric guide rail. The storage battery assembly consists of a storage battery body and sliding connection terminals arranged at two ends of the storage battery body, wherein the sliding connection terminals can slide into the guide rail positioning grooves and are electrically connected with the inner conductive layers of the electric guide rails. In addition, a plurality of clamping grooves penetrating through the clamping grooves are uniformly distributed on the electric guide rail, and transmission lines penetrating through the clamping grooves and electrically connected with the sliding connection terminals are arranged inside the clamping grooves. An elastic abutting assembly is arranged between the sliding connection terminal and the guide rail positioning groove and comprises an elastic abutting piece on the sliding connection terminal and an abutting inclined plane in the guide rail positioning groove.

Inventors

• Kui Shouqi
• LIU YUTONG
• GAO ZIHAN
• DONG JIAHUI

Assignees

• 隗寿齐

Dates

Publication Date

20260512

Application Date

20250519

Claims (6)

1. 1. The unmanned aerial vehicle electric Chi Cang structure with the guide rail positioning function comprises at least one electric guide rail (1) and is characterized in that guide rail positioning grooves (3) extending in the length direction are formed in two sides of the electric guide rail (1), a connection accommodating section (4) is formed between the guide rail positioning grooves (3), the electric guide rail (1) is connected with a storage battery assembly (2) in a sliding mode, the storage battery assembly (2) comprises a storage battery body (21) and sliding connection terminals (22) arranged at two ends of the storage battery body, and the sliding connection terminals (22) can slide into the guide rail positioning grooves (3) and are electrically connected with an inner conductive layer of the electric guide rail (1).
2. 2. The structure of the unmanned aerial vehicle with guide rail positioning function Chi Cang as set forth in claim 1, wherein an elastic abutting component is arranged between the sliding connection terminal (22) and the guide rail positioning groove (3), and comprises an elastic abutting piece on the sliding connection terminal (22) and an abutting inclined plane in the guide rail positioning groove (3).
3. 3. The structure of the unmanned aerial vehicle Chi Cang with guide rail positioning of claim 1, wherein the electric guide rail (1) is provided with a plurality of clamping grooves (11) which are uniformly distributed and penetrate through the electric guide rail, and a transmission line (5) which penetrates through the electric guide rail and is electrically connected with the sliding connection terminal (22) is arranged inside the clamping grooves (11).
4. 4. The unmanned aerial vehicle power Chi Cang with guide rail positioning structure according to claim 1, wherein the sliding connection terminal (22) comprises a plurality of conductive plates (23) which are compact and are connected to the electric guide rail (1) in a sliding manner, and an insulating rubber sleeve (24) is arranged between the plurality of conductive plates (23).
5. 5. The structure of the unmanned aerial vehicle Chi Cang with guide rail positioning according to claim 4, wherein the insulating rubber sleeve (24) is connected to the electric guide rail (1) in a sliding manner.
6. 6. The unmanned aerial vehicle power Chi Cang structure with the guide rail positioning function according to claim 1 is characterized in that an electric storage center (6) electrically connected with the electric guide rail (1) is arranged between the storage battery bodies (21), the electric storage center (6) controls electric quantity distribution, a sliding groove (25) corresponding to the electric guide rail (1) and clamped with one end of the storage battery body (21) close to the electric guide rail (1) is arranged, and fixing lugs (26) fixedly connected with the outer shell of the storage battery body (21) are arranged on two sides of the sliding groove (25).

Description

Unmanned aerial vehicle electric Chi Cang structure with guide rail positioning function Technical Field The utility model provides an unmanned aerial vehicle battery cabin structure, and particularly relates to an unmanned aerial vehicle battery cabin structure with guide rail positioning. Background The unmanned aerial vehicle battery compartment is a core structure of an unmanned aerial vehicle energy system, and has the core functions of providing stable and reliable power supply for an aircraft and ensuring that a battery is safely fixed in the flight process. Conventional battery compartments typically employ a fixed design with a single or small number of battery modules embedded within the housing for electrical connection through a rigid interface. The structure needs to be light in weight, structural strength and electrical stability, but is limited by a fixed mounting mode, and the type, the number and the layout of batteries are difficult to dynamically adjust, so that the unmanned aerial vehicle is difficult to adapt to the requirements of various tasks. The existing unmanned aerial vehicle battery compartment adopts a split type plug interface or a fixed mounting groove structure, and the battery module is required to be connected with an unmanned aerial vehicle circuit through an independent interface. For example, a part of modularized scheme is connected in parallel through a plurality of independent battery bins, but each battery needs to be independently wired, so that line redundancy and weight increase are caused, and a plug interface is easy to be in poor contact in flight vibration. In addition, the battery type and the capacity are fixed, and the battery type and the capacity cannot be flexibly mixed according to task requirements, so that the continuous voyage and the load capacity are wasted. The core defects are as follows: 1. the expansibility and the compatibility are poor, namely the battery configuration is limited by a fixed slot position, and the batteries of different types can not be increased or decreased or replaced as required; 2. The electrical connection reliability is low, the plug interface depends on spring contacts, is easy to wear after long-term use, and is easy to break in a vibration environment; 3. Circuit complexity-multiple battery independent wiring increases system complexity and risk of failure. Disclosure of utility model The application aims to solve the problems, and solves the problems of lower flexibility, poor positioning effect and inconvenient use of a battery compartment of the existing unmanned aerial vehicle by providing the unmanned aerial vehicle motor Chi Cang structure with the guide rail for positioning. In order to solve the technical problems, the utility model provides a technical scheme that an unmanned aerial vehicle power supply Chi Cang structure with guide rail positioning comprises at least one electric guide rail, guide rail positioning grooves extending along the length direction are formed in two sides of the electric guide rail, a connection accommodating section is formed between the guide rail positioning grooves, the electric guide rail is connected with a storage battery assembly in a sliding mode, the storage battery assembly comprises a storage battery body and sliding connection terminals arranged at two ends of the storage battery body, and the sliding connection terminals can slide into the guide rail positioning grooves and are electrically connected with an inner conductive layer of the electric guide rail. Preferably, an elastic abutting assembly is arranged between the sliding connection terminal and the guide rail positioning groove and comprises an elastic abutting piece on the sliding connection terminal and an abutting inclined plane in the guide rail positioning groove. Preferably, the electric guide rail is provided with a plurality of clamping grooves which are uniformly distributed and penetrate through the electric guide rail, and transmission lines which penetrate through the electric guide rail and are electrically connected with the sliding connection terminals are arranged in the clamping grooves. Preferably, the sliding connection terminal comprises a plurality of compact conductive plates which are connected to the electric guide rail in a sliding manner, and an insulating rubber sleeve is arranged between the conductive plates. Preferably, the insulating rubber sleeve is connected to the electric guide rail in a sliding manner. The storage battery is characterized in that a storage center is arranged between the storage battery bodies and is electrically connected with the electric guide rail, the storage center controls electric quantity distribution, a sliding groove which is correspondingly clamped with the electric guide rail is arranged at one end, close to the electric guide rail, of the storage battery body, and fixing lugs which are fixedly connected with the outer shell of the storage bat