Task equipment connecting mechanism

A device connection and task technology, applied in the field of aircraft, can solve problems such as poor flexibility and applicability, low maintenance and replacement efficiency, inconvenient assembly and disassembly, etc., and achieves the effects of high locking reliability, avoiding poor contact, and convenient implementation.

Pending Publication Date: 2020-07-14
成都纵横大鹏无人机科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved and the technical task proposed by the present invention are to improve the existing technology and provide a connection mechanism for mission equipment to solve the problem of poor flexibility and applicability of the connection mode of mission equipment in the current technology, inconvenient assembly and disassembly, maintenance and replacement inefficiency

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Embodiment Construction

[0022] 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 making creative efforts belong to the protection scope of the present invention.

[0023] The task equipment connection mechanism disclosed in the embodiment of the present invention has a simple and compact structure, integrates mechanical connection and electrical connection, is convenient to assemble, disassemble and maintain, and has high efficiency. It can flexibly replace task equipment used in different scenarios, increasing the Scope of application of drones.

[0024] Such as Figure 1 to Figure 5 As shown, the mission equipment con...

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Abstract

The invention discloses a task equipment connecting mechanism. The mechanism comprises an airborne end installed on an aircraft and an equipment end installed on task equipment, wherein the airborne end is provided with an electric connection port, the equipment end is provided with an electric connection head matched with the electric connection port, the airborne end is provided with a sliding groove for the equipment end to be inserted in, and an anti-falling locking mechanism for preventing the equipment end from exiting from the sliding groove is further arranged between the airborne endand the equipment end. The task equipment connecting mechanism is advantaged in that the task equipment can be quickly mounted and dismounted, different task devices can be conveniently replaced to achieve different functions, the application range is enlarged, mechanical connection and electrical connection are integrally achieved, operation is easy and rapid, connection reliability is high, safety is high, the automatic locking function is achieved, and the situation that the task devices are accidentally disengaged and fall off can be effectively avoided.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a mission equipment connection mechanism. Background technique [0002] UAV is an unmanned aircraft controlled by radio remote control equipment or self-contained program control device. At present, the connection mechanism of mission equipment is widely used in aerial photography, agriculture, plant protection, micro selfie, express transportation, disaster relief, observing wild animals, It is well used in monitoring infectious diseases, surveying and mapping, news reports, power inspections, disaster relief, film and television shooting, creating romance, etc. UAVs are usually equipped with mission equipment to carry out a certain practical application task. Existing UAVs usually adopt the method of directly fixing the mission equipment on the fuselage, which cannot be replaced, and the flexibility and applicability are poor. In different scenarios, and when the traditional ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00
CPCB64D47/00
Inventor 李季王利光
Owner 成都纵横大鹏无人机科技有限公司
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