Cylinder type launching rotorcraft

Abstract

The invention discloses a rotorcraft which has the advantages of hovering, flying in a closed space, obstacle avoidance in a dense obstacle area and the like. The cylinder type form has the advantages of convenience in storage, transportation and maintenance, placement on a high-speed mobile platform, post-disaster and post-war complex terrain and cluster deployment and quick release. The invention provides a rotorcraft suitable for being put on a single and dense medium-large-caliber barrel and launch canister platform in allusion to the industrial pain points that an existing rotorcraft is inconvenient to store, transport and maintain, difficult to put on a high-speed mobile platform, and difficult in post-disaster and post-war complex terrain and cluster deployment. The method disclosed by the invention has convenience in storage, transportation and launch, is widely applicable to various medium and large-caliber individual soldier, airborne and vehicle-mounted platforms and complex terrain environments, and can be quickly clustered and deployed.

Description

[0001]The present invention belongs to the field of aircraft, and involves a cylindrical emission rotor aircraft.Background technique[0002]The rotor aircraft has the advantages of hovering, closed space flight, and intensive obstacle area avoidance. Common rotor aircraft, such as coaxial helicopters, quadrevers, and multi-rotating aircraft. The rotorfire is usually placed on a horizontal table, and the system is powered on, the system is powered on, the propeller rotation, the body is gradually rising to a specific height.[0003]Therefore, in special circumstances, the rotor aircraft is difficult to be released or difficult to use. These conditions include:[0004]1) High-speed mobile platform deployment problem[0005]As at high-speed moving vehicles and aircraft, since the mobile platform has a relatively high moving speed, a strong lateral aerodynamic force is generated. The rotorfire zero start speed takes off, which will cause posture disturbance from the lateral aerodynamic force o...

AI Technical Summary

Problems solved by technology

[0006] 2) Post-disaster and post-war complex terrain deployment issues

[0007] In post-disaster and post-war complex terrain areas, because the ground is full of construction debris, etc., it does not have basic flatness and levelness, and it is difficult to find a suitable area for rotorcraft deployment

[0008] 3) Cluster deployment issues

As the size of the rotorcraft and the size of the cluster continue to increase, the size of the field will also increase, so it is difficult to ensure the flatness and levelness of different areas

Excessive differences in flatness and levelness will limit the number of swarms and the size of the rotorcraft

[0010] 4) Deployment issues in bad weather conditions

The problem is that the box storage occupies a large horizontal space, and the use process is time-consuming

Especially when used on a large scale, it is time-consuming and labor-intensive, which is very inconvenient

[0014] Based on the above situation, under severe weather conditions, in the field, on high-speed mobile or high-speed moving aircraft, there are difficulties in single and cluster deployment of traditional rotorcraft

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