In-situ self-assembled slapper ignition component and preparation method thereof

A shock sheet and self-assembly technology, applied in the direction of offensive equipment, detonators, etc., can solve the problems of high cost, difficult weapon system, low processing efficiency of shock sheet detonators, etc., to achieve enhanced mechanical properties, simplified process, simplified preparation and The effect of the assembly process

Inactive Publication Date: 2015-03-04
INST OF CHEM MATERIAL CHINA ACADEMY OF ENG PHYSICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These reasons make the processing efficiency of the shock plate detonator low,

Method used

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  • In-situ self-assembled slapper ignition component and preparation method thereof
  • In-situ self-assembled slapper ignition component and preparation method thereof
  • In-situ self-assembled slapper ignition component and preparation method thereof

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Experimental program
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Embodiment Construction

[0030] The present invention will be further elaborated below in conjunction with the accompanying drawings.

[0031] like Figure 1 to Figure 5 As shown, an in-situ self-assembled impact plate ignition assembly according to an embodiment of the present invention includes an alumina ceramic substrate 1 provided with pins 2, a metal copper explosion foil 3, a polychlorinated p-xylylene fly sheet layer 4, and a photolithography The glue structure layer 5 and the acceleration chamber 6; preferably, the pin 2 is a Kovar pin electrode. The metal copper explosion foil 3 is arranged on the alumina ceramic substrate 1; the polychlorinated p-xylene flying sheet layer 4 is arranged on the metal copper explosion foil 3; the photoresist structure layer 5 is arranged on the The polychlorinated p-xylene flying sheet layer 4; the acceleration chamber 6 is set in the photoresist structure layer 5. The integration of the entire impact plate ignition component is based on alumina ceramics wit...

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PUM

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Abstract

The invention discloses an in-situ self-assembled slapper ignition component and a preparation method thereof. Specifically, the in-situ self-assembled slapper ignition component comprises a pin equipped alumina ceramic substrate, a metal copper exploding foil, a Parylene C slapper layer, a photoresist structural layer and an acceleration chamber. The metal copper exploding foil is disposed on the alumina ceramic substrate, the Parylene C slapper layer is arranged on the metal copper exploding foil, the photoresist structural layer is disposed on the Parylene C slapper layer, and the acceleration chamber is disposed in the photoresist structural layer. The component provided by the invention has the characteristics of self-assembly and flexibility, and can meet the production needs of various slapper ignition components with different specifications. According to the invention, photoresist is applied to preparation of the acceleration chamber and tempering modification treatment thereon so as to further strengthen the mechanical properties. Thus, the acceleration chamber can effectively shear slappers.

Description

technical field [0001] The invention relates to the technical field of pyrotechnics, in particular to a flexible preparation method of an in-situ self-assembled integrated shock plate ignition component. Background technique [0002] Shock disc detonators are highly safe and reliable and are used in in-line detonation systems. A shock detonator is usually composed of a substrate, an explosive bridge foil, a flyer, an accelerating chamber, and a priming charge. Explosive foils are made by copper plating and etching on insulating ceramic substrates. Polyimide or polyester films bonded to the explosive foils are used as flyers. Between the flyers and the priming charge is an aperture of about Acceleration chamber with 1.5 times the width of the bridge area. When the shock detonator acts, the explosive foil undergoes an electric explosion under the action of a high-energy pulse, and generates plasma to drive the flyer to move. The flyer passes through the shearing of the accel...

Claims

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Application Information

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IPC IPC(8): C06C7/00C06C7/02
Inventor 房旷陈清畴蒋小华杜自卫郭菲李茂果
Owner INST OF CHEM MATERIAL CHINA ACADEMY OF ENG PHYSICS
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