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Automatic grenade launcher carrying rotor armed unmanned aerial vehicle

A launcher and unmanned aerial vehicle technology, which is applied in the field of automatic grenade launcher mounted on the rotor unmanned aerial vehicle as a platform, which can solve the problems of difficulty in aiming and shooting, large impact of unmanned aerial vehicle, etc., achieve good hovering performance, reduce impact, compact effect

Inactive Publication Date: 2018-01-05
牟正芳
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the rotor UAV platform is equipped with an automatic grenade launcher, and there are still some technical bottlenecks. In particular, it is necessary to solve the problems that the grenade launcher has a greater impact on the UAV and it is difficult to aim and shoot.

Method used

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  • Automatic grenade launcher carrying rotor armed unmanned aerial vehicle
  • Automatic grenade launcher carrying rotor armed unmanned aerial vehicle

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Embodiment Construction

[0013] In order to describe in detail the technical content, structural features, achieved objectives and effects of the present invention, the following is a detailed description in conjunction with the embodiments and accompanying drawings.

[0014] Such as figure 1 , figure 2 As shown, a rotary-wing armed drone equipped with an automatic grenade launcher includes a coaxial oil-electric hybrid drone, a sighting system, a fire control module, and an automatic grenade launcher.

[0015] The coaxial oil-electric hybrid drone is preferably a fuel rotary engine 4. The rotary engine 4 has stable power, low vibration, and good hovering stability with coaxial twin rotors.

[0016] The sighting system includes an electric pan / tilt 11, a camera 13, a rangefinder 12, and a navigation locator 5. The camera 13 and the rangefinder 12 are installed on the electric pan / tilt. The preferred camera 13 has both white light and infrared functions; preferably The rangefinder 12 has the functions of m...

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Abstract

The invention discloses an automatic grenade launcher carrying rotor armed unmanned aerial vehicle and belongs to the field of application of rotor unmanned aerial vehicles and automatic grenade launchers. The automatic grenade launcher carrying rotor armed unmanned aerial vehicle comprises a coaxial gasoline-electric hybrid unmanned aerial vehicle, a sight system, a fire control module, an automatic grenade launcher and a remote control firing device. An unmanned aerial vehicle platform which adopts a rotor engine and coaxial double main rotors is small in noise, compact in structure, good inhovering performance and stronger in cruising capacity and carrying capacity. The carried grenade launcher is small in recoil force, and impact on an unmanned aerial vehicle platform is further reduced through vibration reduction of a guide rod spring. The sight system and the fire control module better meet the aimed firing demand of the grenade launcher on the unmanned aerial vehicle platform.

Description

Technical field [0001] The invention relates to the application field of a rotary wing drone and an automatic grenade launcher, in particular to a rotary wing drone as a platform to carry an automatic grenade launcher. Background technique [0002] Rotor UAV has the characteristics of convenient take-off and landing, flexible maneuverability, and ability to hover in the air. When applied to the field of military equipment, it will have strong defense penetration capabilities. However, electric rotor drones are currently limited by batteries, with short flight time, limited range, and limited load capacity. Fuel-powered rotor drones overcome the short flight time, limited range, and load capacity of electric rotor drones to a certain extent. Weaknesses, but it has shortcomings such as large size and loud noise, which reduces concealment, and is still insufficient as a weapon carrying platform. The development of rotor-armed UAVs is constrained by UAVs on the one hand and weapon s...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F7/00B64C27/08B64C27/10
Inventor 刘涛刘一凡尹中锋
Owner 牟正芳
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