Launching canister and launching device

A launch tube and tube technology, which is applied in the field of unmanned aerial vehicles, can solve the problems such as the influence of the carrier aircraft and the impact on the launch of the missile, and achieve the effect of low cost, simple structure, and convenient for a large number of equipment

Active Publication Date: 2019-02-22
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in this technical solution, when the missile breaks through the launch cover, the missile will experience a resistance that will affect the missile's ejection, and the small fragments that break through will have an impact on the carrier aircraft.

Method used

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  • Launching canister and launching device
  • Launching canister and launching device
  • Launching canister and launching device

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Embodiment Construction

[0029] In order to make those skilled in the art better understand the solutions of the present invention, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only Embodiments are part of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0030] The terms "first", "second", "third", "fourth", etc. (if present) in the description and claims of the present invention and the above-mentioned drawings are used to distinguish similar objects and are not necessarily used to describe a specific order or sequence. It is to be understood that data so used may be interchanged under appropri...

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Abstract

The invention provides a launching canister and a launching device. The launching canister is sequentially provided with a head part opening cover, a launching canister body, a tail part opening coverand a wire, the launching canister body is of a hollow cylindrical structure, the head end of the launching canister body is connected with the head part opening cover, and the tail end of the launching canister body is connected with the tail part opening cover; and the launching canister body is sequentially provided with a launching canister inner wall base, a heating net layer, a glass fiberinner coating layer, a heat preservation layer and a glass fiber outer coating layer from inside to outside. According to the launching canister and the launching device, a missile can be kept in a normal working state all the time in the high-altitude flying process of an aerial carrier; and the air resistance borne by the launching canister in the flying process can be effectively reduced.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a launch tube and a launch device for dealing with high-altitude, high-speed and low-temperature environments. Background technique [0002] As a new type of aircraft and weapon-carrying platform, UAVs play an increasingly important role in modern warfare. With the gradual development of technology, the flying airspace of UAVs has gradually expanded, and some UAVs can fly at high altitudes. Fly at high speed. As the altitude gradually increases, the ambient temperature gradually decreases. This puts forward higher requirements for the low temperature adaptability of the weapon system. [0003] The existing launch box technology is mainly used for ground-based or ship launch, and its equipment is complicated and heavy, and it is difficult to achieve aircraft mounting. At this stage, most weapons on the UAV platform are carried naked or in the abdomen. It is dif...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F7/00
CPCF41F7/00
Inventor 徐晨阳马伍元马青葛航宇刘晓东
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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