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Experimental device and experimental method for influence of convective combustion on deflagration to detonation transition

A combustion-to-detonation and experimental device technology, which is applied in the direction of chemical analysis using combustion, and can solve the problems of incombustible-to-detonation mechanism and process research, inability to simulate experiments and quantitative evaluation, quantitative evaluation of effects and effects, etc.

Active Publication Date: 2018-05-29
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] Although the above-mentioned devices have their own strengths in the study of combustion-to-detonation mechanism and influencing factors, they cannot carry out simulation experiments and quantitative evaluations of the influence of convective combustion on combustion-to-detonation mechanism.
With the in-depth understanding of the combustion-to-detonation mechanism of energetic materials, the original device cannot be used to quantitatively evaluate the influence and effect of convective combustion on the combustion-to-detonation process, and it is impossible to conduct more in-depth research on the combustion-to-detonation mechanism and process

Method used

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  • Experimental device and experimental method for influence of convective combustion on deflagration to detonation transition
  • Experimental device and experimental method for influence of convective combustion on deflagration to detonation transition
  • Experimental device and experimental method for influence of convective combustion on deflagration to detonation transition

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Embodiment 1

[0033] Such as Figure 1a , Figure 1b , figure 2 , Figure 3a , Figure 3b , Figure 4a , Figure 4b and Figure 5 As shown, this embodiment of the present invention is an experimental device for measuring the influence of convective combustion on combustion-to-detonation, including ignition head 1, ignition powder 2, start end cap 3, combustion-to-detonation tube 4, phenolic resin sleeve Pipe 5, experimental sample 6, punching network pipe 7, speed measuring probe 8, pressure sensor 9, strain gauge 10 and end cap 11; punching network pipe 7 passes through the stepped hole 11-2 on the end cap 11 and the end cap 11 connection; the threaded hole 11-1 on the end cover 11 has an internal thread, which is connected to the end of the combustion-to-detonation tube 4 through the internal thread; the belt formed by pressing in the phenolic resin casing 5 is connected with the punching network pipe 7 The experimental sample 6 with the same outer diameter hole is loaded into the ...

Embodiment 2

[0048] The end cover 11 is connected to the end of the combustion-to-detonation tube 4 through the threaded hole 11-1; there is a step hole 11-2 on the central axis of the end cover 11, and the punching network pipe 7 passes through the step on the end cover 11 The hole 11-2 is installed on the end cover 11; the phenolic resin sleeve 5 is installed in the combustion-detonation tube 4, and the experimental sample 6 of bulk particles is freely loaded into the phenolic resin sleeve 5; the combustion-detonation tube 4 Reserve a 20mm high space at the beginning to place the ignition head 1 and the ignition powder 2, the ignition head 1 is located in the center of the ignition powder 2, the ignition powder 2 is in contact with the end surface of the experimental sample 6, and the lead wire of the ignition head 1 passes through the center of the end cover 3 at the beginning The step through hole 3-1 leads out, and the beginning end cover 3 is connected to the beginning end of the comb...

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Abstract

The invention relates to an experimental device and an experimental method for influence of convective combustion on deflagration to detonation transition. The experimental device comprises an ignition head, ignition powder, an initial end cover, a deflagration to detonation transition tube, a phenolic resin casing pipe, an experimental sample of an energetic material, a punching net pipe, a speedmeasurement probe, a pressure sensor, a strain gauge and a tail end cover, wherein the initial end and the tail end of the deflagration to detonation transition tube are respectively connected with the initial end cover and the tail end cover; the phenolic resin casing pipe is positioned in the deflagration to detonation transition tube and is in clearance fit with the deflagration to detonationtransition tube; the punching net pipe is arranged on the tail end cover by a stepped hole in the tail end cover and is used for forming convective combustion and controlling the intensity of the convective combustion; an experimental sample is putted into the phenolic resin casing pipe and the punching net pipe can be putted into the experimental sample; the pressure sensor and the speed measurement probe are inserted into the experimental sample through pressure measurement holes in the deflagration to detonation transition tube and speed measurement holes in the phenolic resin casing pipe;the strain gauge is arranged between two adjacent pressure measurement holes of the deflagration to detonation transition tube.

Description

technical field [0001] The invention relates to a combustion-to-detonation experimental device and method, which are used for experiments on the influence of convective combustion on combustion-to-detonation, and belong to the technical field of evaluating the safety of energetic materials. Background technique [0002] The degree of difficulty in transitioning from combustion to detonation of energetic materials is an important indicator for evaluating the safety of energetic materials, and is particularly important for the production, use, storage, safety analysis, and setting of corresponding safety measures of energetic materials. For energetic materials with a certain porosity, the combustion-to-detonation process includes ignition surface combustion, conduction combustion, convective combustion, compression combustion, shock wave formation, compression combustion under the action of shock waves, and detonation formation. The literature "Burning to Detonation Transition...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N31/12
CPCG01N31/12
Inventor 王丽琼甄菲王卓群文玉史王永强
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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