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A portable missile with rapidly inflatable wings

A portable and wing-wing technology, which is applied in self-propelled bombs, projectiles, offensive equipment, etc., can solve problems such as difficult to cope with the battlefield environment, unsuitable for carrying or transferring, and increasing the difficulty of system control, so as to improve the flexibility of the battlefield, reduce the The effect of small maximum cross-sectional size and shortened launch time

Active Publication Date: 2017-09-05
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, this cannon-launched small missile has the following defects: it is designed without tails, has short air time, lacks maneuverability, and poor penetration capability; In the battlefield environment, the entire system is bulky and not suitable for carrying or transferring; during the flight, the missile rotates around the central axis at high speed, resulting in a large moment of inertia, which increases the difficulty of system control

Method used

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  • A portable missile with rapidly inflatable wings
  • A portable missile with rapidly inflatable wings
  • A portable missile with rapidly inflatable wings

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Embodiment Construction

[0029] In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0030] refer to Figure 1 to Figure 3 , the present invention provides a portable missile adopting fast inflatable wings, comprising projectile body 10, inflatable wings 1, tail rudder 5, engine 6, wing protective cover 2, and inflation device. The inflatable wings 1 in the present invention are flexible inflatable wings, and a pair of inflated wings 1 symmetrically arranged on the left and right are installed on the left and right sides of the middle position of the projectile body 10 respectively. Connected inflatable device, the inflatable wing 1 is folded and stored...

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Abstract

Disclosed is a portable missile adopting fast inflatable missile wings. The portable missile comprises a missile body and the pair of inflatable missile wings arranged on the left side and the right side of the middle of the missile body symmetrically. An air inflating device connected with the inflatable missile wings is arranged in the missile body. The inflatable missile wings are flexible inflatable missile wings, are stored on the left side and the right side of the middle of the missile body in a folded mode before the missile is launched, and are unfolded through air inflation of the air inflating device after the missile is launched. Before launching, the inflatable missile wings are stored in a folded mode, and missile wing protective covers are arranged, so that the maximum sectional size of the missile before launching is reduced, the requirements for the calibre size of a launching platform are reduced, the launching process is simplified, the launching time is shortened, the design cost is reduced, and carrying and transferring are convenient. The flexible inflatable missile wings are adopted for the portable missile and are stored in a folded mode before launching, so that fast launching is facilitated. The flexible inflatable missile wings are unfolded after launching, so that a large lift-drag ratio is provided. Explosion throwing is conducted during target attacking, and thus battlefield flexibility is improved.

Description

technical field [0001] The invention belongs to the technical field of portable missiles, in particular to a portable missile with inflatable wings. Background technique [0002] Missile, as a precision strike weapon, is playing an increasingly important role in modern warfare. However, traditional missiles are bulky, complex in structure, long in launch preparation time, short in air time, and relatively expensive to use. On the other hand, most of the smaller guided shells are designed without tail fins, which lack maneuverability and poor penetration capabilities, making it difficult to perform diverse military tasks. Therefore, miniaturized portable missiles that can be quickly launched into the combat area, have strong defense penetration capabilities, and have a long time in the air have become the development trend of the future missile field. [0003] Publication No. 103808212A discloses a cannon-launched small missile that can rapidly utilize a cannon to continuou...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B10/20F42B15/36F42B15/00
CPCF42B10/20F42B15/00F42B15/36
Inventor 向敏刘轩岑杨晓骞刘龙斌江振宇
Owner NAT UNIV OF DEFENSE TECH