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A modular parachute bay system for an unmanned aerial vehicle

A parachute and modular technology, applied in the field of unmanned aerial vehicles, can solve the problems of complex preparation and assembly process, high integration of the body, poor operation convenience, etc., and achieve the effect of simple structure, low complexity and high reliability.

Pending Publication Date: 2019-01-22
CHANGGUANG SATELLITE TECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Based on this, it is necessary to provide a modular UAV parachute cabin system for the problems of high integration with the body, poor operation convenience and complicated maintenance and assembly process in the current UAV parachute cabin system

Method used

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  • A modular parachute bay system for an unmanned aerial vehicle
  • A modular parachute bay system for an unmanned aerial vehicle

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Embodiment Construction

[0019] The technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings and preferred embodiments.

[0020] In one of the embodiments, the present invention discloses a modular UAV parachute cabin system, which forms an independent module, and the UAV body only has a fixing effect on the parachute system, without any positioning and positioning effect. Specifically, such as Figure 1-2 As shown, the umbrella cabin system in this embodiment includes an umbrella cabin 1, a hatch cover 2, a steering gear 3, a steering gear adapter seat 4, a rocker arm 5, a front lock 6 and a rear hook 7, wherein the rocker arm 5 is installed on On the steering gear 3, the steering gear 3 is fixedly connected to the front side wall of the umbrella cabin 1 through the steering gear adapter 4, the steering gear 3, the steering gear adapter 4 and the rocker arm 5 form a steering gear system, and the steering gear system is directly fixe...

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Abstract

The invention relates to a modular parachute bay system for an unmanned aerial vehicle, solving the problem that the unmanned aerial vehicle parachute bay system is not convenient to use, and the preparation and assembly process is complicated. The parachute bay system comprises a parachute bay, a hatch cover, a steering gear, a steering gear adapter, a rocker arm, a front latch and a rear hook, wherein the steering gear, the rocker arm and the steering gear adapter are assembled(the above three constitute the steering gear system) and fixed on the front side wall of the parachute bay, the front locking fastener and the rear hook are fixed on the hatch cover, the interaction between the steering gear system and the front locking fastener ensures the front locking of the hatch cover, and the interaction between the rear hook and the hook hole of the parachute bay ensures the rear locking of the hatch cover. The invention has the advantages of simple structure, good operation convenience, low complexity, high locking and releasing reliability, realizes that the parachute bay system designed by the modularization can complete the preparation work independently of the unmanned aerial vehicle body system, and the modularization design can realize the modularization production of the parachute bay system, and is no longer influenced by the machining precision of the body and the like.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a modular unmanned aerial vehicle parachute cabin system. Background technique [0002] With the advancement of aviation technology, the UAV market has gradually become hot, especially the civilian UAV market has shown rapid growth. On the one hand, it is usually difficult to ensure a suitable runway for fixed-wing UAVs in practical applications. Therefore, in the civilian market, fixed-wing UAVs usually adopt the method of parachute recovery; With the improvement of the degree of attention, many types of drones are also equipped with emergency parachutes. Therefore, the high reliability and high convenience of use of the parachute parachute system are more and more favored by people. [0003] The current UAV parachute cabin system has the following disadvantages: [0004] (1) The umbrella cabin system is highly integrated with the airframe, and the umbrella c...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64D17/80
CPCB64C39/02B64D17/80B64U70/83
Inventor 臧国岩樊士冉杨云飞宋非非厉明张利波
Owner CHANGGUANG SATELLITE TECH CO LTD
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