Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Propellant charge ignition comprehensive simultaneity evaluation method

A technology of propellant and simultaneity, which is applied in the direction of chemical analysis by combustion, can solve the problems of high risk, explosion accident and high test cost, and achieve the effect of ensuring complete test, improving service life and increasing test safety.

Active Publication Date: 2018-08-21
XIAN MODERN CHEM RES INST
View PDF6 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This method has the following defects: 1) Indirect inspection of charge ignition design effect through the repeatability and consistency of barrel weapon shooting, does not really grasp whether the actual charge has reached full and simultaneous ignition; 2) For large-caliber barrel weapons, The cost of the full-bomb shooting test is relatively high; 3) The initial ignition performance test is very dangerous, and many bombing accidents have occurred

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Propellant charge ignition comprehensive simultaneity evaluation method
  • Propellant charge ignition comprehensive simultaneity evaluation method
  • Propellant charge ignition comprehensive simultaneity evaluation method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0023] The present invention will be further described in detail below in conjunction with the accompanying drawings and preferred embodiments.

[0024] Such as figure 1 As shown, the preferred embodiment of the present invention is implemented, and the device includes a drug chamber 3, a sensor 4, a propellant charge 5, a sensor bracket 7, a left plug 8, and a right plug 9. Its left plug 8 is equipped with an igniter 1 and an insulating sealing electrode 2 connected to the two-stage wiring of the sensor, and a pressure relief fragment mechanism 6 is installed on the right plug 9 .

[0025] The left plug 8 and the right plug 9 are used to connect the drug chamber 3 to form a simulated barrel weapon drug room environment, and have the sealing and pressure-resistant functions of the drug chamber. The drug chamber 3, the left plug 8 and the right plug 9 are all Made of PCrNiMoV steel, the three are fastened and connected with threaded structure. On the left plug 8, an igniter 1...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

PropertyMeasurementUnit
diameteraaaaaaaaaa
lengthaaaaaaaaaa
densityaaaaaaaaaa
Login to View More

Abstract

The invention discloses a propellant charge ignition comprehensive simultaneity evaluation method. According to the propellant charge ignition comprehensive simultaneity evaluation method, sensor supports of fixed sensors are prepared based on the shape of a propellant chamber and charged propellant structures, the sensors are fixedly arranged on the sensor supports; one terminal of each sensor isarranged on a corresponding sensor support via welding, is introduced into the propellant chamber, is firmly contacted with the propellant chamber, and is taken as one signal line terminal, the otherlead of the sensor is fixedly connected with an insulation sealed electrode on an end cap of the propellant chamber so as to form another signal line terminal; the propellant is introduced into the propellant chamber; a pressure release fragment is selected and installed based on projectile pulling in pressure and propellant charge comprehensive ignition theoretical pressure; igniting and testingare carried out, analysis on test signals is carried out so as to realize evaluation of the ignition comprehensive simultaneity of propellant charge. The propellant charge ignition comprehensive simultaneity evaluation method is capable of solving test problems in propellant charge ignition effects (simultaneous and comprehensive effect), solving a key technical problem that no scientific effective method used for evaluation of propellant charge ignition is available, and providing feasible testing and evaluating means for propellant charge design.

Description

technical field [0001] The invention belongs to the technical field of propellants and explosives, and mainly relates to a propellant charge evaluation method. Background technique [0002] Barrel weapons are still the main equipment on the battlefield. Barrel weapons generally rely on propellant charges to provide firing kinetic energy. The design of propellant charges is used to control the energy release process of the charges, so that they can complete the shooting task under the premise of safe launch. , to meet the propellant charge and ballistic design indicators. [0003] The comprehensive simultaneous ignition of the propellant charge means that after the propellant charge receives the energy generated by the ignition system combustion, the initial burning surface of each propellant charge at each geometric point of the charge structure simultaneously reaches the ignition combustion conditions and burns simultaneously. Simultaneous ignition of the propellant charge...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G01N31/12
CPCG01N31/12
Inventor 赵宝明赵宏立靳建伟张衡何昌辉张邹邹杨丽侠辛凯迪
Owner XIAN MODERN CHEM RES INST
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products