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Combined type aircraft based on barreled type launching

A combined and aircraft technology, applied in the field of aviation systems, can solve the problems of short flight range and low flight speed of multi-rotor aircraft

Active Publication Date: 2019-03-26
BEIJING INST OF SPECIALIZED MACHINERY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved in the present invention is: how to design a combined aircraft based on barrel launch that is convenient for individual soldiers to carry in combat against the problems of low flight speed and short flight range of multi-rotor aircraft

Method used

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  • Combined type aircraft based on barreled type launching
  • Combined type aircraft based on barreled type launching
  • Combined type aircraft based on barreled type launching

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Embodiment Construction

[0023] In order to make the purpose, content, and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0024] Such as figure 1 As shown, a combined aircraft based on a tube launch proposed by the present invention includes: a launch tube 1, an aircraft carrier aircraft 2, and an unmanned drone 3 with a spherical structure imitating a ladybug.

[0025] The flight-type mother machine 2 and the unmanned drone 3 with a ladybug-like spherical structure form a combined aircraft body, that is, the master aircraft. The combined aircraft body is launched through the launch tube 1, and then the combined aircraft body enters the combined aircraft flight stage. During the flight phase of the combined aircraft, the flying carrier aircraft 2 is used to transport the imitation ladybug spherical unmanned drone 3 to the mission area, an...

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Abstract

The invention relates to a combined type aircraft based on barreled type launching and belongs to the technical field of aviation systems. The combined type aircraft is composed of an air traffic typemaster and a ladybird-imitated spherical-structure unmanned parasite aircraft, the ladybird-imitated spherical-structure unmanned parasite aircraft is launched out through a launching barrel, the characteristic of the high flight speed of the air traffic type master is used, the ladybird-imitated spherical-structure unmanned parasite aircraft is quickly transported to a task area, then the ladybird-imitated spherical-structure unmanned parasite aircraft is separated from the air traffic type master, and finally, the ladybird-imitated spherical-structure unmanned parasite aircraft is convertedinto a flight state from a folded state and starts to execute reconnaissance and monitoring tasks. The launching barrel adopts foldable design, and individual combat portability is greatly improved;and the ladybird-imitated spherical-structure unmanned parasite aircraft is designed through imitation of the appearance structure of coccinella septempunctata and has the folded state and the flightstate, in the folded state, the whole unmanned parasite aircraft is spherical and is convenient to store and carry, and in the flight state, the unmanned parasite aircraft is in a multi-rotor state and has good flight stability.

Description

technical field [0001] The invention belongs to the technical field of aviation systems, and in particular relates to a combined aircraft based on barrel launch. Background technique [0002] The prospect of bionic technology application is very broad, and the reasonable application of bionic technology in the product design process can greatly improve the performance of the product. Multi-rotor aircraft has the advantages of vertical take-off and landing, stable hovering, and easy maneuverability, and is widely used in aerial surveying and mapping, precision agriculture, enemy detection and other fields. In addition, the miniature multi-rotor aircraft is convenient for mass deployment, and realizes cluster formation flight between aircraft, which has extremely high military application value. However, the range and flight speed of multi-rotor aircraft are not as good as those of fixed-wing aircraft, and the portability of multi-rotor aircraft still needs to be improved. It...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04B64C39/02
CPCB64C39/02B64F1/04
Inventor 贾华宇李兆博唐文武苏红任礽白璐瑶
Owner BEIJING INST OF SPECIALIZED MACHINERY
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