Anti-submarine missile based on dive buffer device and control method

A buffer device and missile technology, applied in self-propelled projectiles, rocket torpedoes, offensive equipment, etc., can solve the problems of installing high energy consumption, high quality, multi-space buffer equipment, etc.

Pending Publication Date: 2021-05-11
HARBIN ENG UNIV
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Aiming at the deficiencies in the existing anti-submarine missile water entry protection technology, the purpose of the present invention is to solve the disadvantages in the prior art, such as either alleviating the slamming effect at the cost of deceleration, or installing a buffer device with high energy consumption, large mass, an

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  • Anti-submarine missile based on dive buffer device and control method

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Embodiment Construction

[0025]The present invention will be described in detail below with reference to the accompanying drawings.

[0026]The present invention discloses an anti-submarine missile based on an inlet buffer device, in particular to the field of missile structural protection and motion reduction. The anti-submaribilizing missile provided by the present invention includes a matrix 3, a propulsion device, a three-stage TEG thermoelectric conversion module, an exhaust gas integration module, and a small head calendon. The propulsion device includes a vector propeller 1 and a computer guidance system 2; the three-stage TEG thermoelectric conversion module includes a thermoelectric conversion end and a control device 6; the exhaust gas integrated module includes air supply lines 401, 402, gas storage chamber 7, electronic pressure regulating valve 501, 502; head Miniature cavifiers include a rectifier cover 8, a nozzle 9, a gas jet 10, and a pressure sensor 11.

[0027]In order to reuse the plurality of...

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Abstract

The invention discloses an anti-submarine missile based on a dive buffer device and a control method. A generation principle of supercavitation is bidirectionally applied, a propelling device at the tail pushes a missile body to reach a cavitation speed, a cavitator at the head sprays reverse jet flow, and the water surface is cavitated in advance before the missile body arrives, so that it is guaranteed that the missile body is located in a complete and stable supercavity in the whole dive process, direct slamming with water is avoided, and an effective buffering effect is provided for the whole missile body structure; due to the fact that the missile body reaches the cavitation speed before entering water, compared with the reverse jet flow jetted by the head cavitator, the purpose of head cavitation can be achieved without jetting the jet flow at a too high speed, namely, the cavitator does not need large energy; and a thermoelectric conversion module is applied, the problem that a power device is overheated is solved, redundant useless energy of the power device can be stored and reused, and the energy cost is greatly reduced.

Description

Technical field[0001]The present invention belongs to the field of missile structure protection and motion reduction technology, and is specifically involved in an anti-submarine missile and control method based on an inlet buffer device.Background technique[0002]In recent years, with the continuous development of my country's strong military industry, the defense strength is continuously improved, and the weapons and equipment equipped with the army have become more advanced. In particular, my country has raised the strategy of marine strong country, and the naval equipment has been faster, and the demand is more obvious. In many weapon equipment, the important position of anti-submarine missiles has always been self-evident. Since the anti-submarine missile has a large combat advantage on the submarine, the world is competing to develop the weapons based on the results of existing missiles and torpedo research. The traditional anti-submarine missile consists of the body, the fight...

Claims

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Application Information

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IPC IPC(8): F42B15/00F42B15/01F42B15/34F42B17/00F42B10/02F42B10/66
CPCF42B15/00F42B15/01F42B15/34F42B17/00F42B10/02F42B10/668
Inventor 齐辉于家明郭晶
Owner HARBIN ENG UNIV
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