阅读说明：本技术 一种燃烧转爆轰过程参数的测试装置及方法 (Device and method for testing parameters of combustion-to-detonation process ) 是由 王长健 仪建华 秦钊 赵凤起 李海建 郝宁 许毅 孙志华 于 2019-09-03 设计创作，主要内容包括：本发明提出一种燃烧转爆轰过程参数的测试装置及方法,测试装置中DDT管身的管壁均匀分布一列相同尺寸的贯通微孔；挡板内部具有格挡,格挡板数量与贯通微孔数量相同,用于使各贯通微孔上方的空间隔离开。通过拍摄DDT管内主装药点火燃烧后微孔喷焰的全过程,利用贯通微孔处火焰大小及喷射速度与DDT管内部化学反应的剧烈程度及其产生的波速和压强的大小存在正相关联系,通过计算分析各微孔喷焰的特征参数,获得主装药点火-低速燃烧-高速燃烧-燃烧转爆轰-稳定爆轰过程中各自发生的区域及时刻等参数,建立燃烧转爆轰判据。(the invention provides a device and a method for testing parameters of a combustion-to-detonation process, wherein a row of through micropores with the same size are uniformly distributed on the pipe wall of a DDT pipe body in the testing device; the baffle is internally provided with the grid baffles, and the number of the grid baffles is the same as that of the through micropores, so that the space above each through micropore is isolated. By shooting the whole process of micropore jet flames after main explosive in a DDT (dinitrophenol) tube is ignited and combusted, and utilizing the fact that the size and the jet speed of the flame at a through micropore are in direct correlation with the intensity of chemical reaction in the DDT tube and the wave velocity and the pressure intensity generated by the chemical reaction, the characteristic parameters of each micropore jet flame are calculated and analyzed, so that the parameters of the region, the moment and the like of each micropore jet flame in the processes of main explosive ignition, low-speed combustion, high-speed combustion, combustion-detonation transition and stable detonation are obtained, and the criterion of combustion-detonation transition is established.)

1. a device for testing combustion to detonation process parameters, the device comprising: the device comprises a DDT tube, an igniter, a high-speed camera, a baffle, an ignition power supply and a portable computer; the DDT pipe comprises a DDT pipe body, and an ignition end plug and a bottom plug which are positioned at two ends of the pipe body; a row of through micropores with the same size are uniformly distributed on the pipe wall of the DDT pipe body; the ignition end plug is a bolt with a through hole axially formed in the middle, and the side groove is used for mounting a fastening bolt and is fixed at the head of the DDT pipe body; the bottom plug is a disc and is welded at the bottom of the DDT pipe body; the main charge in the DDT pipe is a gunpowder and explosive sample; an electric ignition head is arranged in the igniter and is arranged at the head part of the DDT tube, and an ignition lead penetrates out of an axial through hole of the ignition end plug; the high-speed camera is used for recording the dynamic process of converting the combustion of explosives and powders into detonation in the DDT pipe; the ignition power supply is used for providing a current source for the ignition tool and outputting a synchronous trigger signal for the high-speed camera; the inner part of the baffle is provided with the grid baffles, the number of the grid baffles is the same as that of the through micropores on the DDT pipe wall, and the grid baffles are used for isolating the space above each through micropore; the portable computer is used for controlling the high-speed camera and has the functions of high-speed image acquisition, data processing and terminal display; the DDT tube is placed in the explosion tower after charging, the high-speed camera is arranged outside a window of the explosion tower, is close to the bulletproof glass and keeps a certain distance, and the ignition power supply and the portable computer are arranged in a safe area outside the explosion tower.

2. The test device of claim 1, wherein the DDT tube is made of carbon steel.

3. The testing device of claim 1, wherein the DDT tube body has a length of 1200mm, an inner diameter of 40mm, and a wall thickness of 9 mm.

4. the test device according to claim 1, wherein the through-micro holes each have a pore diameter of 1mm and a number of 10.

5. The test device according to claim 1, wherein the main charge in the DDT tube is a powder, granular, sheet or columnar explosive sample, and is charged by a free-filling or casting mode.

6. The test device of claim 1, wherein the igniter is a black powder igniter charge.

7. The test device of claim 1, wherein the high-speed camera uses visible light band, has a storage time of not less than 0.1s under the conditions of maximum frame frequency and maximum resolution, and has an external trigger function.

8. A method for testing parameters of a combustion to detonation process, using a testing device according to any one of the preceding claims, the method comprising the steps of:

S1, test preparation, including:

a) erecting a high-speed camera and connecting the high-speed camera with a portable computer; starting up and debugging the placing position of the high-speed camera and lens parameters thereof, so that the high-speed camera can shoot the full length of the DDT tube and image the full length of the DDT tube at the bottom of an image; fixing the position of the high-speed camera and lens parameters thereof;

b) Sealing the through micropores of the DDT tube by using an insulating adhesive tape, filling the main charge into the DDT tube, penetrating out a lead of an igniter through an axial through hole of an ignition end plug, and installing the ignition end plug;

c) horizontally placing the DDT pipe on a support table, and ensuring that the through micropores are vertically upward; placing the baffle on the support table so that the space above each through micropore is isolated; connecting a signal wire of a trigger signal output end of the thermal power supply with an external trigger port of the high-speed camera; connecting an output end cable of the thermal power supply with a lead of the ignition tool;

s2, process testing, comprising:

d) Setting a shutter, a frame rate and a resolution of the high-speed camera;

e) The high-speed camera shoots 1 frame of image in a low illumination mode, sequentially marks coordinates of positions of through micropores of the DDT tube in the image, and takes the image as a reference image and stores the reference image after the coordinates are marked;

f) restoring the parameter conditions set by the high-speed camera in the step d), starting an ignition power supply to ignite the main charge in the DDT pipe, and synchronously triggering the high-speed camera to acquire images;

g) after the image acquisition is finished, storing the acquired images on a portable computer in an image sequence form;

s3, data processing, including:

h) Finding the positions of all the through micropores 4 on the reference image, taking a certain through micropore 4 as a central point, taking half of the distance between every two adjacent through micropores 4 as the width of a micropore flame spraying area on the left and right, and taking the height as the maximum height of the frame image;

i) in the test image sequence, finding out the 1 st frame image of flame appearing in the micropore of the wire of the igniter, wherein the shooting time interval between the 1 st frame image of the image sequence and the image is ignition delay time of the ignition charge;

j) In the test image sequence, calculating the flame height above each through micropore 4, and drawing a flame height-time curve of each through micropore 4;

k) Performing second-order derivation on the flame height-time curve of each through micropore 4 to obtain an acceleration-time curve of the flame of each through micropore 4;

l) finding the maximum acceleration a on the flame acceleration-time curve of each through-going micro-hole 4_iand corresponding time t_i(ii) a 1, 2, 3.. k.. N, where N is the number of through-micropores 4;

m) finding a_iMaximum value of (a)_kand its corresponding time point is t_k(ii) a If a_k>>a_k-1And a is_k>>a_k+1That is, the acceleration of the jet flame penetrating through the micro-hole k is different in magnitude from that of the adjacent micro-holes, it can be determined that the region starting detonation in the DDT tube is located in the region having the k-th through micro-hole at the center and the left-right width as half of the adjacent hole distance, and the time when the combustion changes to detonation is t_kTime of day; if the acceleration of the jet flame penetrating through the micropore k has no magnitude difference compared with that of the adjacent penetrating micropore, the detonation can be judged not to occur;

and S4, result expression, including:

The area with the kth through micropore in the center and the left-right width of half of the adjacent hole distance is used as the area for the detonation from the combustion,

taking the distance between the center of the kth through micropore and the ignition end plug 1 as the induction distance for converting combustion into detonation, and taking t_kthe time is taken as the time when the combustion-to-detonation occurs.

9. The test method according to claim 8, wherein in the step b, the through-micro holes of the DDT tube are closed with an insulating tape.

10. The test method of claim 8, wherein in the step d, the shutter time is not more than 0.5 x 10^-5Second, frame rate set to 10⁵Frame/sec, horizontal resolution setting guarantees to beat full DDT tube 2, vertical resolution setting is highest.

Technical Field

the invention belongs to the technical field of testing of the performance of explosives and powders, and particularly relates to a device and a method for testing combustion-to-detonation process parameters, which are suitable for measuring the process parameters of combustion-to-detonation of the explosives and powders and researching related rules.

background

the combustion-to-detonation (DDT) of explosives and powders undergoes a very complex multi-stage chemical-physical reaction, and the combustion speed, the pressure and the temperature of a combustion reaction zone all undergo orders of magnitude changes, and the time varies from tens of microseconds to milliseconds. The study of such a very complex process of change with such a large parameter span is challenging both experimentally and theoretically.

The DDT process for studying energetic materials such as explosives and powders is typically carried out in DDT tubes. According to different experimental conditions, two kinds of DDT tubes are commonly used, one is a thick-wall metal tube with two closed ends (called strong constraint); one is a plexiglas or plastic tube (known as weak constraint). The metal DDT pipe has high strength, the pipe wall is not easy to deform, and the transition from combustion to detonation is easy to realize, so most of tests adopt the metal pipe. The organic glass or plastic tube has good light transmission, so that the propagation rule of flame wave in the whole DDT process can be observed by using a high-speed photography technology, and the propagation rule of compression wave can be analyzed by observing the density distribution of the medicine bed by using X-ray. However, the tube wall of the organic glass tube is easy to deform and is easy to laterally expand to generate rarefaction waves, so that the transformation from combustion to detonation is difficult to realize in the tube with limited length; in addition, gas is generated under the action of high temperature and high pressure, and the inner wall of the pipe has influence on the flow field.

In the early research of the DDT process, no test element is installed, whether the sample is subjected to combustion-to-detonation or not is qualitatively judged by the size of the dent of the evidence plate at the burst part of the metal DDT pipe and the shape of the fragment, and the DDT risk grade of the sample is sequenced by the distance (induction distance) Ld from the ignition starting point to the burst part of the metal pipe. The test method can not obtain many process details in the metal pipe before the metal pipe is smashed, the induction distance Ld can not truly reflect the DDT danger, and correct comparison and classification of the DDT danger of the explosive can be possible only after the details of the ignition-low-speed combustion-high-speed combustion-detonation conversion-stable detonation process and the critical detonation conversion conditions are mastered.

Later, various probes, strain gauges, radiography, and laser fiber optic methods were developed, with test subjects being primarily combustion wave, compression wave propagation, and shock wave formation and implosion events. Because the combustion and detonation are very different in nature, the combustion and detonation are mutually interwoven in the rotary explosion stage, and the positions of various disturbance front surfaces are difficult to accurately measure. In addition, due to the limitations of the related art such as the range of the sensor and the response accuracy, the test result is not ideal.

disclosure of Invention

Technical problem to be solved

The invention provides a device and a method for testing parameters of a process from combustion to detonation, which aim to solve the technical problem of accurately testing the parameters of the process from combustion to detonation.

(II) technical scheme

In order to solve the above technical problem, the present invention provides a testing apparatus for parameters of a process of converting combustion into detonation, the testing apparatus comprising: the device comprises a DDT tube, an igniter, a high-speed camera, a baffle, an ignition power supply and a portable computer; the DDT pipe comprises a DDT pipe body, and an ignition end plug and a bottom plug which are positioned at two ends of the DDT pipe body; a row of through micropores with the same size are uniformly distributed on the pipe wall of the DDT pipe body; the ignition end plug is a bolt with a through hole axially formed in the middle, and the side groove is used for mounting a fastening bolt and is fixed at the head of the DDT pipe body; the bottom plug is a disc and is welded at the bottom of the DDT pipe body; the main charge in the DDT pipe is a gunpowder and explosive sample; an electric ignition head is arranged in the igniter and is arranged at the head part of the DDT tube, and an ignition lead penetrates out of an axial through hole of the ignition end plug; the high-speed camera is used for recording the dynamic process of converting the combustion of explosives and powders into detonation in the DDT pipe; the ignition power supply is used for providing a current source for the ignition tool and outputting a synchronous trigger signal for the high-speed camera; the inner part of the baffle is provided with the grid baffles, the number of the grid baffles is the same as that of the through micropores on the DDT pipe wall, and the grid baffles are used for isolating the space above each through micropore; the portable computer is used for controlling the high-speed camera and has the functions of high-speed image acquisition, data processing and terminal display; the DDT tube is loaded with powder and then placed in the explosion tower, the high-speed camera is arranged outside a window of the explosion tower, is close to the bulletproof glass and keeps a certain distance, and the ignition power supply and the portable computer are arranged in a safe area outside the explosion tower.

Furthermore, the DDT pipe is made of carbon steel.

further, the DDT pipe body has the length of 1200mm, the inner diameter of 40mm and the wall thickness of 9 mm.

furthermore, the aperture of the through micropores is 1mm, and the number of the through micropores is 10.

furthermore, the main charge in the DDT pipe is powder, granular, flaky or columnar explosive samples, and the charge is carried out by adopting a free filling or casting mode.

Furthermore, the igniter is a black powder ignition explosive package.

Furthermore, the high-speed camera adopts a visible light wave band, the storage time is not less than 0.1s under the conditions of the maximum frame frequency and the maximum resolution, and the high-speed camera has an external trigger function.

In addition, the invention also provides a testing method of parameters in the process of converting combustion into detonation, which adopts the testing device and comprises the following steps:

S1, test preparation, including:

a) Erecting a high-speed camera and connecting the high-speed camera with a portable computer; starting up and debugging the placing position of the high-speed camera and lens parameters thereof, so that the high-speed camera can shoot the full length of the DDT tube and image the full length of the DDT tube at the bottom of an image; fixing the position of the high-speed camera and lens parameters thereof;

b) Sealing the through micropores of the DDT tube by using an insulating adhesive tape, filling the main charge into the DDT tube, penetrating out a lead of an igniter through an axial through hole of an ignition end plug, and installing the ignition end plug;

c) Horizontally placing the DDT pipe on a support table, and ensuring that the through micropores are vertically upward; placing the baffle on the support table so that the space above each through micropore is isolated; connecting a signal wire of a trigger signal output end of the thermal power supply with an external trigger port of the high-speed camera; connecting an output end cable of the thermal power supply with a lead of the ignition tool;

S2, process testing, comprising:

d) setting a shutter, a frame rate and a resolution of the high-speed camera;

e) The high-speed camera shoots 1 frame of image in a low illumination mode, sequentially marks coordinates of positions of through micropores of the DDT tube in the image, and takes the image as a reference image and stores the reference image after the coordinates are marked;

f) Restoring the parameter conditions set by the high-speed camera in the step d), starting an ignition power supply to ignite the main charge in the DDT pipe, and synchronously triggering the high-speed camera to acquire images;

g) After the image acquisition is finished, storing the acquired images on a portable computer in an image sequence form;

S3, data processing, including:

h) finding the positions of all the through micropores 4 on the reference image, taking a certain through micropore 4 as a central point, taking half of the distance between every two adjacent through micropores 4 as the width of a micropore flame spraying area on the left and right, and taking the height as the maximum height of the frame image;

i) in the test image sequence, finding out the 1 st frame image of flame appearing in the micropore of the wire of the igniter, wherein the shooting time interval between the 1 st frame image of the image sequence and the image is ignition delay time of the ignition charge;

j) In the test image sequence, calculating the flame height above each through micropore 4, and drawing a flame height-time curve of each through micropore 4;

k) Performing second-order derivation on the flame height-time curve of each through micropore 4 to obtain an acceleration-time curve of the flame of each through micropore 4;

l) finding the maximum acceleration a on the flame acceleration-time curve of each through-going micro-hole 4_iand corresponding time t_i(ii) a 1, 2, 3.. k.. N, where N is the number of through-micropores 4;

m) finding a_iMaximum value of (a)_kand its corresponding time point is t_k(ii) a If a_k>>a_k-1And a is_k>>a_k+1That is, the acceleration of the jet flame penetrating through the micro-hole k is different in magnitude from that of the adjacent micro-holes, it can be determined that the region starting detonation in the DDT tube is located in the region having the k-th through micro-hole at the center and the left-right width as half of the adjacent hole distance, and the time when the combustion changes to detonation is t_kTime of day; if the acceleration of the jet flame penetrating through the micropore k has no magnitude difference compared with that of the adjacent penetrating micropore, the detonation can be judged not to occur;

and S4, result expression, including:

The area with the kth through micropore in the center and the left-right width of half of the adjacent hole distance is used as the area for the detonation from the combustion,

Taking the distance between the center of the kth through micropore and the ignition end plug 1 as the induction distance for converting combustion into detonation, and taking t_kthe time is taken as the time when the combustion-to-detonation occurs.

Further, in step b, the through-holes of the DDT tube are closed with an insulating tape.

further, in step d, the shutter time is not more than 0.5 × 10^-5Second, frame rate set to 10⁵frame/sec, horizontal resolution setting guarantees to beat full DDT tube 2, vertical resolution setting is highest.

(III) advantageous effects

the invention provides a device and a method for testing parameters of a process of converting combustion into detonation, wherein the testing device comprises a DDT (double-diffused T) tube, an igniter, a high-speed camera, a baffle, an ignition power supply and a portable computer; wherein, a row of through micropores with the same size are uniformly distributed on the pipe wall of the DDT pipe body; the baffle is internally provided with grid baffles, the number of the grid baffles is the same as that of the through micropores of the DDT pipe wall, and the grid baffles are used for isolating the space above each through micropore.

By shooting the whole process of micropore jet flames after main explosive in a DDT (dinitrophenol) tube is ignited and combusted, and utilizing the fact that the size and the jet speed of the flame at a through micropore are in direct correlation with the intensity of chemical reaction in the DDT tube and the wave velocity and the pressure intensity generated by the chemical reaction, the characteristic parameters of each micropore jet flame are calculated and analyzed, so that the parameters of the region, the moment and the like of each micropore jet flame in the processes of main explosive ignition, low-speed combustion, high-speed combustion, combustion-detonation transition and stable detonation are obtained, and the criterion of combustion-detonation transition is established. The device and the method are suitable for parameter testing of a process of converting combustion of explosives and powders into detonation and research of related rules, and are high in visualization degree and low in cost.

The beneficial effects of the invention specifically comprise:

1. The length and the jet speed of the microporous jet flame of the DDT pipe are directly determined by the intensity of the chemical reaction in the DDT pipe and the wave speed and the pressure intensity generated by the chemical reaction, and the influence on the intensity and the pressure intensity is small;

2. By utilizing the positive correlation of the micropore jet flame state and the pressure field of the space near the interior of the micropore, the combustion and detonation conditions of the whole DDT tube can be obtained through micropore arrays and data analysis, and the region and time of combustion-detonation transition can be judged.

Drawings

FIG. 1 is a schematic diagram of a DDT tube and charge structure in an embodiment of the invention;

fig. 2 is a schematic diagram of a test site layout in an embodiment of the invention.

Detailed Description

in order to make the objects, contents and advantages of the present invention clearer, the following detailed description of the embodiments of the present invention will be made in conjunction with the accompanying drawings and examples.

The present embodiment provides a device for testing parameters of a process of converting combustion into detonation, as shown in fig. 1, the device includes a DDT tube 2, an igniter 6, a high-speed camera 8, a baffle 11, an ignition power supply 9, and a portable computer 10. Wherein the content of the first and second substances,

The DDT pipe 2 comprises a DDT pipe body, an ignition end plug 1 and a bottom plug 5, wherein the ignition end plug 1 and the bottom plug 5 are positioned at two ends of the pipe body, the DDT pipe body is made of high-quality carbon steel, the length of the DDT pipe body is 1200mm, the inner diameter of the DDT pipe body is 40mm, and the wall thickness of the DDT pipe body is 9 mm. A row of through micropores 4 with the aperture of 1mm are uniformly distributed on the pipe wall of the DDT pipe body, and the number of the micropores 4 is 10; the ignition end plug 1 is a bolt with a through hole axially formed in the middle, and the side groove is used for mounting 4 fastening bolts and is fixed at the head of the DDT pipe body; the bottom plug 5 is a disc with the diameter of 74mm and is welded at the bottom of the DDT pipe body; the main charge in the DDT pipe 2 is a granular propellant sample and is charged in a free filling mode.

the igniter 6 is a black powder ignition explosive bag, an electric ignition head is arranged in the igniter, and is placed at the head part of the DDT tube 2, and an ignition lead penetrates out of an axial through hole of an ignition end plug. The black powder conforms to GJB1056A, ignition current 5A.

The high-speed camera 8 is used for recording the dynamic process of explosive combustion to detonation in the DDT pipe 2, adopts a visible light wave band, has a maximum frame frequency of 105 frames/second and a storage time of 0.1s, and has an external trigger function.

the ignition power supply 9 is used for providing a current source for the ignition tool 6 and outputting a current 5A; and outputs a synchronization trigger signal 8 for the high-speed camera.

the baffle plate 11 is used for separating the space above each through micropore 4, is made of stainless steel, has a height of 1m and a length of 1200mm, and is provided with 10 grids for blocking, and the surface is blackened.

the portable computer 10 is used for controlling the high-speed camera 8 and has the functions of high-speed image acquisition, data processing and terminal display.

A test site arrangement comprising: the DDT pipe 2 is loaded and then placed in an explosion tower; the high-speed camera 8 is arranged outside the window of the explosion tower, is close to the bulletproof glass and keeps a distance of 10 mm; the ignition power supply 9 and the portable computer 10 are arranged in a safety area outside the explosion tower.

the method for testing parameters of the process of converting combustion into detonation by adopting the testing device comprises four main steps of testing preparation, process testing, data processing and result expression, wherein the four main steps comprise:

s1, test preparation, including:

a) Erecting a high-speed camera 8 and connecting a portable computer 10; starting up and debugging the placing position of the high-speed camera 8 and lens parameters thereof, so that the high-speed camera 8 can shoot the total length of the DDT tube 2 and form an image at the bottom of the image; fixing the position of the high-speed camera 8 and lens parameters thereof;

b) Sealing the through micropores 4 of the DDT pipe 2 by using an insulating tape, then filling the main charge into the DDT pipe 2, penetrating out a lead of an igniter 6 through an axial through hole of the ignition end plug 1, and then installing the ignition end plug 1;

c) horizontally placing the DDT pipe 2 on a support table 7 and ensuring that the through micropores 4 are vertically upward; placing the baffle plate 11 on the support table 7 so that the space above each through micro hole 4 is isolated; connecting a signal wire of a trigger signal output end of the thermal power supply 9 with an external trigger port of the high-speed camera 8; connecting an output end cable of the thermal power supply 9 with a lead of the ignition device 6;

S2, process testing, comprising:

d) setting parameters of shutter, frame rate, resolution, etc. of the high-speed camera 8, wherein the shutter time is not more than 0.5 x 10^-5second, frame rate set to 10⁵Frame/second, the transverse resolution is set to ensure that the full DDT tube 2 is shot, and the longitudinal resolution is set to be the highest;

e) the high-speed camera 8 shoots 1 frame of image in a low illumination mode, sequentially marks coordinates of positions of through micropores 4 of the DDT tube 2 in the image, and takes the image as a reference image and stores the reference image after the coordinates are marked;

f) Restoring the parameter conditions set by the high-speed camera 8 in the step d), starting an ignition power supply 9 to ignite the main charge in the DDT pipe 2, and synchronously triggering the high-speed camera 8 to acquire images;

g) after the image acquisition is finished, the acquired images are stored on the portable computer 10 in the form of an image sequence.

s3, data processing, including:

h) Finding the positions of all the through micropores 4 on the reference image, taking a certain through micropore 4 as a central point, taking half of the distance between every two adjacent through micropores 4 as the width of a micropore flame spraying area on the left and right, and taking the height as the maximum height of the frame image;

i) in the test image sequence, finding out the 1 st frame image of flame appearing in the micropore of the wire of the igniter, wherein the shooting time interval between the 1 st frame image of the image sequence and the image is ignition delay time of the ignition charge;

j) in the test image sequence, calculating the flame height above each through micropore 4, and drawing a flame height-time curve of each through micropore 4;

k) Performing second-order derivation on the flame height-time curve of each through micropore 4 to obtain an acceleration-time curve of the flame of each through micropore 4;

l) finding the maximum acceleration a on the flame acceleration-time curve of each through-going micro-hole 4_iAnd corresponding time t_i(ii) a 1, 2, 3.. k.. N, where N is the number of through-micropores 4;

m) finding a_iMaximum value of (a)_kAnd its corresponding time point is t_k(ii) a If a_k>>a_k-1And a is_k>>a_k+1That is, the acceleration of the jet flame penetrating through the micro-hole k is different in magnitude from that of the adjacent micro-holes, it can be determined that the region starting detonation in the DDT tube is located in the region having the k-th through micro-hole at the center and the left-right width as half of the adjacent hole distance, and the time when the combustion changes to detonation is t_ktime of day; if the acceleration of the jet flame penetrating through the micropore k has no magnitude difference compared with that of the adjacent penetrating micropore, the detonation can be judged not to occur;

and S4, result expression, including:

the area with the kth through micropore in the center and the left-right width of half of the adjacent hole distance is used as the area for the detonation from the combustion,

taking the distance between the center of the kth through micropore and the ignition end plug 1 as the induction distance for converting combustion into detonation, and taking t_kThe time is taken as the time when the combustion-to-detonation occurs.

The above description is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, several modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.