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High-sensitivity impact-triggered supersonic nose fuse

A high-sensitivity, supersonic technology, applied in the field of fuze, can solve the problem that the sensitivity is difficult to meet such requirements, and achieve the effect of improving intrinsic safety, good economy, and increasing sensitivity

Active Publication Date: 2021-07-09
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The sensitivity of most types of trigger mechanisms of traditional fuzes is difficult to meet such requirements

Method used

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  • High-sensitivity impact-triggered supersonic nose fuse

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Embodiment Construction

[0013] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0014] Such as figure 1 As shown, a high-sensitivity impact-triggered supersonic warhead fuze is based on the existing supersonic warhead fuze, and a sliding seat 3 and a spring 5 are added in the head cavity of the fuze body 4, and the existing supersonic warhead fuze The detonating element 2 in the warhead fuze is moved up to the sliding seat 3, and there is a clearance fit between the sliding seat 3 and the head cavity, and the top surface of the sliding seat 3 is close to the cover foil in the existing supersonic warhead fuze 1 bottom surface, so that the detonating explosive element 2 is close to the cover foil 1, the sliding seat 3 is cylindrical, and there are two-stage through holes along its axial direction. From top to bottom, there are first-stage holes and second-stage holes. The diameter of the first-order hole is greater than that of the second...

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PUM

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Abstract

The invention discloses a high-sensitivity impact-triggered supersonic nose fuze. A sliding seat and a spring are additionally arranged in a head cavity body of an existing supersonic nose fuse, a collision explosion element is moved upwards into the sliding seat, the sliding seat is in clearance fit with the head cavity body, the top face of the sliding seat is tightly attached to the bottom face of a cover foil of the existing supersonic nose fuse, and the spring is arranged below the sliding seat. The collision explosion element can sense an aerodynamic thermal environment generated by a bullet flying at a high speed at the head of the nose fuse, the sensitivity of the collision explosion element is obviously increased along with temperature rise, as the collision explosion element is tightly attached to the lower portion of the cover foil, when the fuse collides with a target at a high speed, the sliding seat carries the collision explosion element in the sliding seat to move forwards inertially, and therefore the trigger sensitivity of the fuse is greatly improved, and the high-sensitivity impact-triggered supersonic nose fuze is especially suitable for attacking weak targets such as hot-air balloons and small unmanned aerial vehicles; and when the fuse head falls downwards during service handling, the falling speed is low, the spring below the sliding seat can be pressed to retreat, and therefore the safety of the collision explosion element in the sliding seat is guaranteed.

Description

technical field [0001] The invention belongs to fuze technology, in particular to a high-sensitivity impact-triggered supersonic warhead fuze. Background technique [0002] For most ammunition, in order to achieve the ideal damage effect, it is often required that the fuze has a high trigger sensitivity. Fuze trigger sensitivity refers to the ability of the fuze to ignite easily when the projectile touches the target. The trigger sensitivity of the fuze is related to the target type and mechanical (strength, density, energy, etc.) characteristics, the relative velocity and attitude of the projectile, the size of the trigger area of ​​the fuze, the sensitivity of the detonating element, and the principle and structure of the trigger mechanism. [0003] The high-sensitivity impact trigger mechanism of the classic supersonic warhead fuze is mainly the impact cap (detonator) ignition mechanism. This type of ignition mechanism has high sensitivity and good reliability, and its ...

Claims

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Application Information

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IPC IPC(8): F42C1/10F42C19/02
CPCF42C1/10F42C19/02
Inventor 王雨时蒋鑫闻泉
Owner NANJING UNIV OF SCI & TECH
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