Amphibious cruise missile based on throat offset type pneumatic thrust-vectoring nozzle and posture control method of amphibious cruise missile

A technology of vector nozzles and cruise missiles, applied in the direction of projectiles, offensive equipment, weapon types, etc., can solve the problems of increasing the radar reflection area of ​​missiles, increasing the probability of missiles being intercepted, reducing the hit rate of missiles, and achieving low noise , fast speed and responsive effect

Active Publication Date: 2017-11-28
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
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  • Description
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AI Technical Summary

Problems solved by technology

At this stage, cruise missiles usually use rudder surfaces to control the direction, which increases the radar reflection area of ​​the missile and greatly increases the probability of the missile being intercepted during flight, thereby greatly reducing the missile's hit rate. Rate

Method used

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  • Amphibious cruise missile based on throat offset type pneumatic thrust-vectoring nozzle and posture control method of amphibious cruise missile
  • Amphibious cruise missile based on throat offset type pneumatic thrust-vectoring nozzle and posture control method of amphibious cruise missile
  • Amphibious cruise missile based on throat offset type pneumatic thrust-vectoring nozzle and posture control method of amphibious cruise missile

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Embodiment Construction

[0038] Apparently, the described embodiments are only some of the embodiments of the present invention, but not all of them. The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. The relative arrangements, expressions and numerical values ​​of components and steps set forth in these embodiments do not limit the scope of the present invention unless specifically stated otherwise. At the same time, it should be understood that, for the convenience of description, the sizes of the various parts shown in the drawings are not drawn according to the actual proportional relationship. Techniques, methods and devices known to those of ordinary skill in the relevant art m...

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Abstract

The invention discloses an amphibious cruise missile based on a throat offset type pneumatic thrust-vectoring nozzle and a posture control method of the amphibious cruise missile. The amphibious cruise missile comprises a missile body, a switching section and the throat offset type pneumatic thrust-vectoring nozzle. The advancing direction of the missile is changed and jumping out of water is achieved by controlling the tail throat offset type pneumatic thrust-vectoring nozzle. Compared with a traditional missile, the amphibious cruise missile has the beneficial effects that a rudder and other structures are removed, smaller radar reflection area is achieved, and therefore the stealth performance is better. When the throat offset type pneumatic thrust-vectoring nozzle works underwater, water serves as a working medium, and the beneficial effects that no gas is exhausted, no sailing path exists, the noise is small and the stealthiness is good are achieved; and when the throat offset type pneumatic thrust-vectoring nozzle works in the air, high-temperature fuel serves as a working medium of the thrust-vectoring nozzle, and the beneficial effects that reaction is sensitive, the flight speed is high, and the voyage is far are achieved.

Description

technical field [0001] The invention relates to an amphibious cruise missile based on a throat offset aerodynamic vector nozzle, which is mainly used to improve the maneuverability of the missile, improve the concealment of the missile and significantly increase the hit rate of the missile. Background technique [0002] Since the advent of the Second World War, missiles have developed rapidly. Because of their small size, light weight, and easy maneuverability, cruise missiles have brought a huge and far-reaching impact on the strategy and tactics of modern warfare. more and more attention from all countries. At this stage, cruise missiles usually use rudder surfaces to control the direction, which increases the radar reflection area of ​​the missile and greatly increases the probability of the missile being intercepted during flight, thereby greatly reducing the missile's hit rate. Rate. Contents of the invention [0003] The present invention develops an amphibious cru...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B10/66
CPCF42B10/665
Inventor 许保成徐惊雷黄帅陈匡世林泳辰
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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