Air and water stamping combined cross-medium anti-ship and anti-submarine missile

A water stamping and cross-media technology, applied in self-propelled bombs, jet propulsion devices, mechanical equipment, etc., can solve the problems of obvious wake, loud noise, and low speed

Active Publication Date: 2021-07-13
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, traditional torpedo weapons have low speed, loud noise, a...

Method used

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  • Air and water stamping combined cross-medium anti-ship and anti-submarine missile
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  • Air and water stamping combined cross-medium anti-ship and anti-submarine missile

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Embodiment Construction

[0034] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.

[0035] refer to figure 1 -6. The present invention provides an air and water ram combined cross-media anti-ship and anti-submarine missile, which includes an air inlet 1 , a water inlet 2 , a control system 3 , a combat unit 4 , a propulsion system 5 , and an airframe unit 6 .

[0036] Specifically, the front end of the air-water ram combined trans-media anti-ship and anti-submarine missile is provided with an air inlet 1 and a water inlet 2 .

[0037] The airframe unit 6 includes a first rudder 61 , a second rudder 62 , wings 63 , a control device 64 , a shock cone 65 , an outer shell 66 and an inner shell 67 .

[0038] Specifically, the missile inner casing 67 is arranged in the missile body outer casing 66 and the missile inner casing 67 is arranged at the front end of the nozzle 55 positioned at the tail, and the missile inner casi...

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Abstract

The invention discloses an air and water stamping combined cross-medium anti-ship and anti-submarine missile. An liquid oxidizing agent carried by the missile enters a combustion chamber to be subjected to primary combustion with solid metal fuel, gas enters an afterburning chamber through a spraying pipe to be converged with air sucked from the head of a missile body, oxygen in the air and a large amount of fuel-rich gas in the fuel gas are subjected to secondary afterburning and then are ejected out from a tail large spray pipe in an accelerated expansion manner; and the missile close to an enemy throws away from missile wings, opens a fuel gas outlet cover plate at the head and enters water, meanwhile, the fuel gas guided to the head from a combustion chamber is sprayed out from an outlet to the periphery, the fuel gas and the opened cover plate together assist the missile sailing at a high speed to form a stable supercavitation on the periphery of the missile body, water flows in from a tip in front of a fuel gas outlet and located outside a supercavitation area and is led to the combustion chamber for reacting with metal fuel, and at the moment, an engine is in a water stamping working mode until a target is hit, a combat unit fuze is triggered, and damage strike is formed on the enemy.

Description

technical field [0001] The invention relates to the field of cross-medium aircraft, in particular to an air-water ram jet combined cross-medium anti-ship and anti-submarine missile. Background technique [0002] Modern shipboard air defense systems and anti-submarine systems are becoming more and more perfect, especially the main naval battleships represented by guided missile cruisers (CG), guided missile destroyers (DDG) and large guided missile frigates (FFG) are equipped with long-range, medium and short-range air defense systems. Missiles and near-anti-gun systems, thus constructing a multi-level air defense system of medium and long-range short-range plus terminal stage. Among them, many main battle ships and new ships are also equipped with active / passive phased array radars and missile vertical launch systems (VLS), which have strong anti-saturation attack capabilities. Therefore, in this context, traditional subsonic anti-ship missiles, cruise missiles and other st...

Claims

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Application Information

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IPC IPC(8): F42B15/00F02K9/08
CPCF02K9/08F42B15/00
Inventor 石磊杨一言金秉宁肖波何国强
Owner NORTHWESTERN POLYTECHNICAL UNIV
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