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Pod system capable of hoisting two unmanned aerial vehicles simultaneously

A technology of unmanned aerial vehicles and pods, which is applied in the field of pod systems for hoisting two unmanned aerial vehicles at the same time, achieving the effects of reasonable structure and space layout, reliable fixation, and convenient maintenance

Pending Publication Date: 2018-09-04
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There is no relevant existing technology in the country and the company for reference

Method used

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  • Pod system capable of hoisting two unmanned aerial vehicles simultaneously
  • Pod system capable of hoisting two unmanned aerial vehicles simultaneously
  • Pod system capable of hoisting two unmanned aerial vehicles simultaneously

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0059] A pod system for hoisting two drones at the same time, characterized in that it includes: slide rail 1, fixed stopper 2, adjustment screw 3, pre-jack spring 4, sliding stopper 5, sliding bushing 6, front Block pin 7, nut 8, lug 9, guide rod 10, spring 11, L profile 12, T profile 13, pull-off support arm 14, large spring coil 15, micro-movement pin 16, small spring coil 17, pull pin support Arm 18, limit screw 19, pin puller mounting lug 20, pin puller 21, screw 22, pin puller mounting part 23, UAV rear roller 24, UAV anti-sway roller 25, none Man-machine front roller 26, pull-off steel wire rope 27, pull-off plug 28, UAV startup and power-on micro switch 29, sliding block and adjustment screw conflicting surface 30, front stop latch and front roller locking action slope 31, adjustment Screw hexagon head 32, pin puller manual pin puller hexagonal nut 33, slide rail side limit groove 34, sliding block and rear roller conflict limit surface 35, locking pin relief groove 36...

Embodiment 2

[0061] A pod system for hoisting two drones at the same time, characterized in that it includes: slide rail 1, fixed stopper 2, adjustment screw 3, pre-jack spring 4, sliding stopper 5, sliding bushing 6, front Block pin 7, nut 8, lug 9, guide rod 10, spring 11, L profile 12, T profile 13, pull-off support arm 14, large spring coil 15, micro-movement pin 16, small spring coil 17, pull pin support Arm 18, limit screw 19, pin puller mounting lug 20, pin puller 21, screw 22, pin puller mounting part 23, UAV rear roller 24, UAV anti-sway roller 25, none Man-machine front roller 26, pull-off steel wire rope 27, pull-off plug 28, UAV startup and power-on micro switch 29, sliding block and adjustment screw conflicting surface 30, front stop latch and front roller locking action slope 31, adjustment Screw hexagon head 32, pin puller manual pin puller hexagonal nut 33, slide rail side limit groove 34, sliding block and rear roller conflict limit surface 35, locking pin relief groove 36...

Embodiment 3

[0069]A pod system for hoisting two drones at the same time, characterized in that it includes: slide rail 1, fixed stopper 2, adjustment screw 3, pre-jack spring 4, sliding stopper 5, sliding bushing 6, front Block pin 7, nut 8, lug 9, guide rod 10, spring 11, L profile 12, T profile 13, pull-off support arm 14, large spring coil 15, micro-movement pin 16, small spring coil 17, pull pin support Arm 18, limit screw 19, pin puller mounting lug 20, pin puller 21, screw 22, pin puller mounting part 23, UAV rear roller 24, UAV anti-sway roller 25, none Man-machine front roller 26, pull-off steel wire rope 27, pull-off plug 28, UAV startup and power-on micro switch 29, sliding block and adjustment screw conflicting surface 30, front stop latch and front roller locking action slope 31, adjustment Screw hexagon head 32, pin puller manual pin puller hexagonal nut 33, slide rail side limit groove 34, sliding block and rear roller conflict limit surface 35, locking pin relief groove 36,...

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Abstract

The invention belongs to the technical field of aerospace application and relates to a mechanism capable of carrying, locking, automatically unlocking and releasing two small unmanned aerial vehiclesin a pod, in particular to a pod system capable of hoisting the two unmanned aerial vehicles simultaneously. The pod system is characterized by comprising an unmanned aerial vehicle carrying, locking,automatic unlocking and releasing sliding rail mechanism. By applying the unmanned aerial vehicle carrying, locking, automatic unlocking and releasing sliding rail mechanism, pin pullers do not needto be demounted in the maintenance process of the unmanned aerial vehicles during mounting and demounting, and maintenance is convenient and rapid through the manual pin pulling function and front blocking compression springs; the individual difference of the interval of front and rear roller shafts of each unmanned aerial vehicle can be eliminated through an adjustable rear blocking assembly, andreliable fixing can be achieved; front blocking plug pins adopts bevel locking through the weight component, and electric initiation pin pullers are applied, so that the mechanism achieves the function of reliably locking, automatically unlocking and releasing the unmanned aerial vehicles; and the unmanned aerial vehicles are limited, supported and carried by sliding rail assemblies, strength issufficient, and the structure and space arrangement is reasonable.

Description

technical field [0001] The invention belongs to the technical field of aerospace applications, and relates to a mechanism for carrying, locking, automatically unlocking and releasing two small unmanned aerial vehicles in a pod, specifically a pod system for hoisting two unmanned aerial vehicles at the same time. Background technique [0002] Due to the limitations of its aerodynamic shape and structure, materials, power, energy, etc., the existing light and small UAVs with folding wings are not suitable for achieving long-range flight to frontier positions to perform tasks alone, nor can they be directly hung by the parent aircraft like weapons and ammunition Do high-speed hang and launch. How to effectively deliver the UAV to the forward position to perform tasks is an urgent problem to be solved. After demonstration, the feasible technical solution is: put the folding UAV into the carrying pod, and one pod can carry two drones. Man-machine, a mother aircraft can mount two...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D5/00B64D9/00
CPCB64D5/00B64D9/00B64U80/82
Inventor 阳治平李长宇钱晓琼丁健陈思圯
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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