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Folding wing miniature missile platform

A folding wing and miniature technology, applied to self-propelled bombs, weapon types, projectiles, etc., can solve the problems of large space occupied by wing folding, inability to achieve high-precision control, and affect missile control accuracy, etc., to achieve good folding effect , cost-effective, low-cost effect

Inactive Publication Date: 2020-10-30
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, micro-missiles are widely used due to their extremely strong individual combat capabilities, but most of the existing micro-missiles generally use smaller fixed wings and are rarely equipped with folding wings, resulting in poor aerodynamic performance and inconvenient for individual soldiers Portable, unable to achieve high-precision control
Among them, a small number of missiles equipped with folding wings also have problems such as too much space occupied by the folded wings, and self-locking cannot be realized, which causes the wings to easily shake in the high-speed airflow, which greatly affects the control accuracy of the missile.

Method used

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  • Folding wing miniature missile platform
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  • Folding wing miniature missile platform

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Embodiment Construction

[0023] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0024] see Figure 1~4 , in an embodiment of the present invention, a folding-wing miniature missile platform includes a guide cabin 1, a front folding wing module 3, a warhead module 4, a control module 5, a rear folding wing module 7 and a power module 6, and the missile body Folding wing modules are symmetrically arranged around the front part and the rear part, the front end of the projectile body is provided with a guide bin 1, the middle part of the proj...

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Abstract

The invention discloses a folding wing miniature missile platform. The folding wing miniature missile platform includes a guide cabin, a front folding wing module, a warhead module, a control module,a power module and a rear folding wing module; the guide cabin is connected to the front end of the front folding wing module; the rear end of the front folding wing module is connected to the warheadmodule; the rear end of the warhead module is connected to the control module; the rear end of the control module is connected to the power module; the rear folding wing module is sleeved on the outside of the nozzle of the power module; and both the front folding wing module and the rear folding wing module have wings that can be folded and ejected. The folding wing miniature missile platform has a good folding effect; the wings can be self-locked after being ejected; the folding wing miniature missile platform has good aerodynamic performance and high control accuracy, brings great guidanceaccuracy, is easy to carry, and can adapt to various launch environments; and the device has low cost and high cost performance.

Description

Technical field [0001] The invention relates to the technical field of micro missile platforms, specifically a folding wing micro missile platform. Background technique [0002] Through research on existing micro missile platforms, they are often divided into: fixed-wing type, folding-wing type, and wingless type. The fixed-wing platform has the simplest structure. The wings are rigidly connected to the missile body, but it is difficult to carry. The wingless platform does not have fins, but requires precise control by a vector engine or gas rudder, and the control efficiency is relatively poor. The folding-wing platform has relatively poor control efficiency. The film is folded inwards, which saves space and is easy to carry. It is suitable for various launch environments. It also facilitates the configuration of different types of fins, making the design more flexible. [0003] At present, micro missiles are widely used due to their extremely strong individual combat capa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/00F42B15/01F42B10/14
CPCF42B10/14F42B15/00F42B15/01
Inventor 龚春林高戈黄岳刘皓任浩豪李文源
Owner NORTHWESTERN POLYTECHNICAL UNIV
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