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aerial grenade launcher

A technology for aircraft and launchers, which is applied to launch devices, weapon accessories, aircraft parts, etc., can solve the problems of low take-off and landing requirements for rotorcraft, achieve great application value, reduce own costs, and ensure the effect of shooting accuracy

Active Publication Date: 2018-07-27
SHENZHEN QZU TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, in the current prior art, few people combine the grenade launcher with the rotorcraft, and give full play to the low requirements for the takeoff and landing of the rotorcraft, which greatly improves the individual firepower of soldiers and provides fire support in the air.

Method used

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Examples

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Embodiment 1

[0030] Example 1 as figure 1 , 2 , 3, the present embodiment discloses a six-axis aerial grenade launching aircraft; it comprises a grenade launcher, a body, a shock absorbing buffer device, and a percussion device and consists of four parts, wherein the grenade launcher includes a gun body 15, a barrel 22. Drum 23;

[0031] The body includes power battery 1, support arm 2, support arm turning part 3, body lower plate 4, bracket 5, body support structure 6, body upper plate 7, and rain shield 8;

[0032] The shock absorbing buffer device includes a guide rod fixing seat 9, a recoil spring 10, a front clamp upper valve 11, a front clamp lower valve 12, a guide rod 13, a rear clamp upper valve 14, and a rear clamp lower valve 21;

[0033] The firing device includes a driving steering gear 16, a firing rod 17, a connecting rod 18, a steering gear disc 19, and a firing fixing seat 20.

[0034] A body upper plate 7 is arranged above the body, and a body lower plate 4 is arranged...

Embodiment 2

[0044] Example 2 as Figure 8 , 2, 3, the present invention discloses a four-axis aerial grenade launching aircraft, which comprises a grenade launcher, a multi-rotor aircraft body, a shock-absorbing buffer system, and a percussion system. Gun barrel 22, magazine drum 23, multi-rotor aircraft body includes power battery 1, support arm 2, support arm turning piece 3, body lower plate 4, bracket 5, body support structure 6, body upper plate 7, rain shield 8 , the shock-absorbing buffer system includes a guide rod fixing seat 9, a recoil spring 10, a front clamp upper valve 11, a front clamp lower valve 12, a guide rod 13, a rear clamp upper valve 14, and a rear clamp lower valve 21. The system includes a driving steering gear 16, a firing rod 17, a connecting rod 18, a steering gear disc 19, and a firing fixing seat 20.

[0045] Such as Figure 4 As shown, after the soldier confirms the target, he gives the grenade launcher a firing signal to drive the steering gear 16 to wor...

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PUM

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Abstract

The invention belongs to the field of aircraft processing, and particularly relates to an aerial grenade launch aircraft. With organic synthesis of a folding aircraft and a grenade launcher, the aerial grenade launch aircraft is convenient to fold and easy to disassembly and assembly, and an aerial fire support device convenient to carry and transport is provided for soldiers. By designing an effective damping buffer device, shooting precision can be well guaranteed. The aerial grenade launch aircraft is simple in structure, and by the selection of molding materials, self cost of the weapon device can be effectively reduced. The aerial grenade launch aircraft has great application value.

Description

technical field [0001] The invention belongs to the field of aircraft processing, and in particular relates to an aerial grenade launching aircraft. Background technique [0002] Rotorcraft is a new type of aircraft with novel structure, simple control and high stability. It has unique flight functions such as vertical take-off and landing, hovering and maneuvering obstacle avoidance, and can ideally complete flight tasks in a small space. [0003] However, in the current prior art, few people combine the grenade launcher and the rotorcraft to fully utilize the low requirements for the takeoff and landing of the rotorcraft, greatly improve the individual firepower of soldiers, and provide fire support in the air. Contents of the invention [0004] For this reason, the technical problem to be solved by the present invention is to overcome the bottleneck of the prior art, thereby proposing an aerial grenade launching aircraft. [0005] In order to solve the above-mentioned ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D1/06B64C1/06F41A25/12
CPCB64C1/063B64D1/06F41A25/12
Inventor 薛堃
Owner SHENZHEN QZU TECH CO LTD
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