Explosive initiation shock wave effect optimal mass ratio solving method, system, equipment and medium

By segmenting the total equivalent of explosives and determining the optimal mass ratio, the problem of limited explosive effect of single-shot explosives is solved, and the superposition effect of multiple explosives is maximized, and the effect of blasting and demolition is improved.

CN119940027APending Publication Date: 2025-05-06ZHONGBEI UNIV
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Patent Information

Application Number
CN202510104479.1
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-01-22
Publication Date
2025-05-06

AI Technical Summary

Technical Problem

In the demolition of engineering structures, the explosion effect of a single-engine explosive is limited, resulting in the peak of shock wave overpressure fixed, and the damage effect of multiple-engine explosives is not effectively improved.

Method used

By obtaining the total equivalent of explosives and the shockwave overpressure formula for the explosion of a single explosive, the total equivalent of explosives is divided into multiple parts, and the distance from each part of explosives to the target is the same, the shockwave overpressure formula for each part of explosives is constructed, and the shockwave overpressure superimposed coupling formula after multiple parts of explosives are detonated at the same time is determined, and the optimal mass ratio of each part of explosives is used to solve the impactwave superimposition effect is maximized.

Benefits of technology

By determining the optimal mass ratio when the shock wave superposition effect is maximum after multiple explosives are detonated at the same distance, the blasting and demolition effect is improved and the destructive power of the explosives is improved.

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Abstract

The invention discloses an explosive initiation shock wave effect optimal mass ratio solving method, system and device and a medium, and relates to the field of engineering structure blasting demolition, and the method comprises the steps: obtaining the total equivalent of an explosive and a shock wave overpressure formula of single explosive explosion; dividing the total equivalent of the explosive into a plurality of parts; wherein the distance from the center of each explosive to the target is the same; based on the distance from the center of each explosive to the target, the mass of each explosive and the shock wave overpressure formula of single explosive explosion, the shock wave overpressure formula of each explosive explosion is constructed, and a shock wave overpressure superposition coupling formula after the multiple explosives are detonated at the same time is further determined; and solving the optimal mass ratio of each explosive by adopting a Lagrange multiplier method by taking the maximum shock wave overpressure superposition coupling value after simultaneous initiation of multiple explosives as a target. According to the method, the optimal mass ratio when the shock wave superposition effect is maximum after multiple explosives are detonated at the same distance at the same time is determined, and then the blasting demolition effect is improved.
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Description

Technical Field

[0001] The present application relates to the field of blasting demolition of engineering structures, and in particular to a method, system, equipment and medium for solving the optimal mass ratio of the shock wave effect of explosive detonation. Background Art

[0002] Under the premise of a certain fixed mass of explosive equivalent, the explosion effect of a single explosive is limited, and the peak value of the shock wave overpressure concerned in the blasting demolition of engineering structures is also a fixed value. The explosion effect can be improved after the reasonable arrangement of multiple explosives. At present, the destructive effect of multiple equal portions of explosives is mostly reflected in the software simulation analysis, field tests and other stages, and the principle of superposition of effects and the equivalent ratio of multiple explosives have not received attention. Therefore, the effect of blasting demolition is poor. Summary of the invention

[0003] The purpose of the present application is to provide a method, system, device and medium for solving the optimal mass ratio of the shock wave effect of explosive detonation, which can determine the optimal mass ratio when the shock wave superposition effect is maximum after multiple explosives are detonated simultaneously at the same distance, thereby improving the effect of blasting demolition.

[0004] To achieve the above objectives, this application provides the following solutions:

[0005] In a first aspect, the present application provides a method for solving the optimal mass ratio of the shock wave effect of explosive detonation, comprising:

[0006] Obtaining the total explosive equivalent and the shock wave overpressure formula of a single explosive explosion; the shock wave overpressure formula is a formula for calculating the shock wave overpressure based on the distance from the center of the explosive to the target and the explosive equivalent;

[0007] The total equivalent of the explosive is arbitrarily divided into a plurality of portions, wherein the distance from the center of each portion of the explosive to the target is the same;

[0008] Based on the distance from the center of each explosive to the target, the mass of each explosive and the shock wave overpressure formula of a single explosive explosion, a shock wave overpressure formula for each explosive explosion is constructed;

[0009] Based on the shock wave overpressure formula of each explosive explosion, the shock wave overpressure superposition coupling formula after multiple explosives are detonated simultaneously is determined;

[0010] Based on the shock wave overpressure superposition coupling formula, with the goal of maximizing the shock wave overpressure superposition coupling value after simultaneous detonation of multiple explosives, the Lagrange multiplier method is used to solve the optimal mass ratio of each explosive.

[0011] In a second aspect, the present application provides a system for solving the optimal mass ratio of the explosive detonation shock wave effect, comprising:

[0012] An overpressure formula acquisition module is used to obtain the total explosive equivalent and the shock wave overpressure formula of a single explosive explosion; the shock wave overpressure formula is a formula for calculating the shock wave overpressure based on the distance from the center of the explosive to the target and the explosive equivalent;

[0013] An explosive equivalent division module, used to arbitrarily divide the total explosive equivalent into multiple portions; wherein the distance from the center of each portion of explosive to the target is the same;

[0014] An overpressure formula building module is used to build a shock wave overpressure formula for each explosive explosion based on the distance from the center of each explosive to the target, the mass of each explosive and the shock wave overpressure formula for a single explosive explosion;

[0015] A coupling formula determination module is used to determine the shock wave overpressure superposition coupling formula after multiple explosives are detonated simultaneously based on the shock wave overpressure formula of each explosive explosion;

[0016] The mass ratio solving module is used to solve the optimal mass ratio of each explosive by using the Lagrange multiplier method based on the shock wave overpressure superposition coupling formula and with the goal of maximizing the shock wave overpressure superposition coupling value after multiple explosives are simultaneously detonated.

[0017] In a third aspect, the present application provides a computer device, comprising: a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein the processor executes the computer program to implement the above-mentioned method for solving the optimal mass ratio of the shock wave effect of explosive detonation.

[0018] In a fourth aspect, the present application provides a computer-readable storage medium having a computer program stored thereon, which, when executed by a processor, implements the above-mentioned method for solving the optimal mass ratio of the shock wave effect of explosive detonation.

[0019] According to the specific embodiments provided in this application, this application has the following technical effects:

[0020] The present application provides a method, system, device and medium for solving the optimal mass ratio of the shock wave effect of explosive detonation. On the basis of the shock wave overpressure formula of a single explosive explosion, based on the distance from the center of each explosive to the target and the mass of each explosive, a shock wave overpressure formula for the explosion of each explosive is constructed, and the shock wave overpressure superposition coupling formula after multiple explosives are simultaneously detonated is further determined. With the maximum shock wave overpressure superposition coupling value after multiple explosives are simultaneously detonated as the goal, the Lagrange multiplier method is used to solve the optimal mass ratio of each explosive, and the optimal mass ratio when the shock wave superposition effect is maximized after multiple explosives are simultaneously detonated at the same distance is determined, thereby improving the effect of blasting demolition. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0022] Figure 1 This is an application environment diagram of a method for solving the optimal mass ratio of the shock wave effect of explosive detonation in one embodiment of the present application;

[0023] Figure 2 A schematic flow chart of a method for solving the optimal mass ratio of the shock wave effect of explosive detonation provided in one embodiment of the present application;

[0024] Figure 3 This is a spatial arrangement diagram of an explosive mass ratio of 0.5:0.5 in an embodiment of the present application;

[0025] Figure 4 This is a spatial arrangement diagram of an explosive mass ratio of 0.3:0.7 in an embodiment of the present application;

[0026] Figure 5 This is a comparison diagram of the deflection time history curves of square steel pipes with explosive mass ratios of 0.5:0.5 and 0.3:0.7 in one embodiment of the present application;

[0027] Figure 6 A schematic diagram of functional modules of a system for solving the optimal mass ratio of the shock wave effect of explosive detonation provided in one embodiment of the present application;

[0028] Figure 7 A schematic diagram of the structure of a computer device provided in one embodiment of the present application. DETAILED DESCRIPTION

[0029] The following will be combined with the drawings in the embodiments of the present application to clearly and completely describe the technical solutions in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of this application.

[0030] In order to make the above-mentioned objects, features and advantages of the present application more obvious and easy to understand, the present application is further described in detail below in conjunction with the accompanying drawings and specific implementation methods.

[0031] The method for solving the optimal mass ratio of the explosive detonation shock wave effect provided in the embodiment of the present application can be applied to Figure 1In the application environment shown. Among them, the terminal 102 communicates with the server 104 through the network. The data storage system can store the data that the server 104 needs to process. The data storage system can be set up separately, integrated on the server 104, or placed on the cloud or other servers. The terminal 102 can send the total equivalent of explosives and the shock wave overpressure formula of a single explosive explosion to the server 104. After receiving the total equivalent of explosives and the shock wave overpressure formula of a single explosive explosion, the server 104 divides the total equivalent of explosives into multiple parts, and the shock wave overpressure superposition coupling formula is used. Based on the shock wave overpressure superposition coupling formula, the shock wave overpressure superposition coupling value after multiple explosives are simultaneously detonated is maximized, and the Lagrange multiplier method is used to solve the optimal mass ratio of each explosive. The server 104 can feedback the optimal mass ratio to the terminal 102. In addition, in some embodiments, the method for solving the optimal mass ratio of the shock wave effect of explosive detonation can also be implemented by the server 104 or the terminal 102 alone.

[0032] The terminal 102 may be, but is not limited to, various desktop computers, laptop computers, smart phones, tablet computers, IoT devices, and portable wearable devices. The IoT devices may be smart speakers, smart TVs, smart air conditioners, smart vehicle-mounted devices, etc. The portable wearable devices may be smart watches, smart bracelets, head-mounted devices, etc. The server 104 may be implemented as an independent server or a server cluster consisting of multiple servers, or may be a cloud server.

[0033] In an exemplary embodiment, Figure 2 As shown, a shock wave overpressure superposition coupling formula is provided. The method is executed by a computer device, and can be executed by a computer device such as a terminal or a server alone, or can be executed by a terminal and a server together. In the embodiment of the present application, the method is applied to Figure 1 The server 104 in the example is used for explanation, and the steps include the following steps 201 to 205.

[0034] Step 201, obtaining the total explosive equivalent and the shock wave overpressure formula of a single explosive explosion. The shock wave overpressure formula is a formula for calculating the shock wave overpressure based on the distance from the center of the explosive to the target and the explosive equivalent.

[0035] In an exemplary embodiment, the shock wave overpressure formula for a single explosive explosion is:

[0036]

[0037] Among them, ΔP mis the shock wave overpressure, W is the explosive equivalent (in kg), R is the distance from the center of the explosive to the target (in meters), a1, a2, a3 are combination coefficients, which can be 0.084, 0.27, 0.7 in the engineering design specifications, or 0.067, 0.301, 0.431 based on the test summary.

[0038] Step 202, the total explosive equivalent is arbitrarily divided into a plurality of portions, wherein the distance from the center of each portion of explosive to the target is the same. Specifically, the total explosive equivalent is arbitrarily divided into n portions, where n is a positive integer.

[0039] Step 203, constructing a shock wave overpressure formula for the explosion of each explosive based on the distance from the center of each explosive to the target, the mass of each explosive and the shock wave overpressure formula for the explosion of a single explosive.

[0040] In an exemplary embodiment, the shock wave overpressure formula of the explosion of the i-th explosive is:

[0041]

[0042] Among them, ΔP mi is the shock wave overpressure of the explosion of the i-th explosive, i = 1, 2...n, n is the number of explosives, b i W is the mass of the i-th explosive, b i is the mass ratio of the i-th explosive, 0≤b i ≤1, b1+b2+…+b n =1, let b1≤b2≤…≤b n , then W=(b1+b2+…+b n )W.

[0043] Step 204, based on the shock wave overpressure formula of each explosive explosion, determine the shock wave overpressure superposition coupling formula after multiple explosives are simultaneously detonated:

[0044]

[0045] Among them, ΔP m' is the superposition coupling value of the shock wave overpressure after multiple explosives are detonated simultaneously, is the first mass ratio parameter, is the second mass ratio parameter.

[0046] Step 205, based on the shock wave overpressure superposition coupling formula, with the goal of maximizing the shock wave overpressure superposition coupling value after the simultaneous detonation of multiple explosives, the Lagrange multiplier method is used to solve the optimal mass ratio of each explosive.

[0047] In an exemplary embodiment, find i≤1, i=1, 2…n, b1+b2+…+b n =1, satisfying and The maximum value solution. Step 205 includes the following steps (1) to (5):

[0048] (1) Based on the first mass ratio parameter term and the Lagrangian multiplier factor, the first Lagrangian multiplier function is constructed: Among them, F1(b1,b2,...,b n ,λ) is the first Lagrange multiplier function, and λ is the Lagrange multiplier factor.

[0049] (2) Based on the second mass ratio parameter term and the Lagrangian multiplier factor, the second Lagrangian multiplier function is constructed: Among them, F2(b1,b2,...,b n ,λ) is the second Lagrange multiplier function.

[0050] (3) According to the first Lagrangian multiplier function, each mass ratio in the first mass ratio parameter item and the Lagrangian multiplier factor are differentiated to obtain a first set of equations: in, is the equation about b1 in the first system of equations, is the first set of equations about b n The equation, F' 1,λ is the equation about λ in the first system of equations.

[0051] (4) According to the second Lagrangian multiplier function, each mass ratio in the second mass ratio parameter term and the Lagrangian multiplier factor are differentiated to obtain a second set of equations: in, is the equation about b1 in the second system of equations, is the second set of equations about b n The equation, F' 2,λ is the equation about λ in the second set of equations.

[0052] (5) Solving the first set of equations and the second set of equations respectively to obtain the optimal mass ratio of each portion of explosive.

[0053] In this embodiment, after solving the first and second equations, The maximum value solution is satisfy The maximum solution of

[0054] It can be seen from this that after the explosive with explosive equivalent W is divided into n parts, in order to maximize the overpressure value after the shock wave superposition coupling of each part of explosive, the optimal mass ratio is That is, n portions of explosives are divided into equal parts.

[0055] The present application provides a method for calculating the explosive mass ratio for the best shock wave overpressure superposition effect when multiple explosives are detonated simultaneously when the mass of explosives is fixed. Based on the classical calculation formula for explosion shock wave overpressure, a shock wave superposition coupling formula after multiple explosives are detonated simultaneously at the same distance is obtained, and the Lagrange multiplier method is used to theoretically give the optimal mass ratio when the superposition effect is maximum. This can provide a certain reference for blasting demolition design and has certain economic benefits in the engineering field.

[0056] In order to verify the effectiveness of this application, two implementation cases are provided below.

[0057] Implementation case 1: shock wave overpressure superposition coupling calculation with explosive mass ratio of 0.3:0.7.

[0058] 1) Determine the shock wave overpressure formula for a single explosive explosion with explosive equivalent W and distance from the center of the explosive to the target R. The combination coefficients a1, a2, and a3 are 0.084, 0.27, and 0.7, respectively.

[0059]

[0060] 2) After determining that the explosive with explosive equivalent W is divided into two parts, 0.3W and 0.7W, the shock wave overpressure formula of each part of explosive explosion is:

[0061]

[0062] 3) Determine the shock wave overpressure superposition coupling formula after two explosives of mass 0.3W and 0.7W are detonated simultaneously:

[0063]

[0064] Implementation case 2: shock wave overpressure superposition coupling calculation with explosive mass ratio of 0.5:0.5.

[0065] 1) Determine the shock wave overpressure formula for a single explosion with explosive equivalent W and distance from the center of the explosive to the target R. The combination coefficients a1, a2, and a3 are 0.084, 0.27, and 0.7, respectively.

[0066]

[0067] 2) After determining that the explosive with explosive equivalent W is divided into two parts of 0.5W and 0.5W, the shock wave overpressure formula of each part of explosive explosion is:

[0068]

[0069] 3) Determine the shock wave overpressure superposition coupling formula after two explosives of mass 0.5W and 0.5W are detonated simultaneously:

[0070]

[0071] From the shock wave overpressure superposition coupling formula of the above two cases, it can be seen that the explosion shock wave overpressure after the explosive is divided into two equal parts is greater than the overpressure value with a mass ratio of 0.3:0.7, which means that the explosion shock wave effect of equally divided explosives is better than that of unequally divided explosives.

[0072] In order to make the above theoretical case clearer, the following simulation scheme is made according to the above best implementation case: Q235B steel is used to make square steel tubes, the size of the square steel tubes is 70mm×70mm×70mm, and the wall thickness of the steel tubes is 3.75mm. Take a total charge of 0.9kg, two equal explosives (0.45kg each), and two unequal explosives (0.27kg and 0.63kg). Each explosive is made into a cube, arranged horizontally along the axis of the square steel tube and located directly above it. The net distance between each explosive is 5mm, and the distance from the center of the explosive to the explosion surface of the square steel tube is 500mm. The spatial layout diagram is as follows Figure 3 and Figure 4 The numerical simulation calculations were carried out by using LS-DYNA finite element software and the simultaneous detonation method, and the vertical deflection time history curves at the maximum deformation of the back explosion surface of the steel pipe under each working condition were extracted. The time history curves of two equal explosives and two unequal explosives are shown in Figure 5 As shown, it can be seen that the deflection of the steel pipe under the two equally divided explosives is larger than that under the two unequally divided explosives. This shows that the equally divided explosives have better explosion effects than the unequally divided explosives, and have more significant effects on the target, which can achieve better economic results in the engineering field.

[0073] The present application also provides an application scenario, which applies the above-mentioned method for solving the optimal mass ratio of the shock wave effect of explosive detonation. Specifically: The method for solving the optimal mass ratio of the shock wave effect of explosive detonation provided in this embodiment can be applied in the blasting demolition scenario. During blasting demolition, the total equivalent of the explosives is first obtained, and the optimal mass ratio of each portion of explosives is determined by using the method for solving the optimal mass ratio of the shock wave effect of explosive detonation provided in this application. The explosives are divided into multiple portions based on the optimal mass, and are placed around the blasting target respectively, and the distance between each portion of explosives and the blasting target is the same, and the blasting target is demolished by blasting, thereby improving the effect of blasting demolition.

[0074] Based on the same inventive concept, the embodiment of the present application also provides a system for solving the optimal mass ratio of the explosive detonation shock wave effect for realizing the method for solving the optimal mass ratio of the explosive detonation shock wave effect involved above. The implementation scheme for solving the problem provided by the system is similar to the implementation scheme recorded in the above method, so the specific limitations in one or more embodiments of the system for solving the optimal mass ratio of the explosive detonation shock wave effect provided below can refer to the limitations of the method for solving the optimal mass ratio of the explosive detonation shock wave effect above, and will not be repeated here.

[0075] In an exemplary embodiment, Figure 6 As shown, a system for solving the optimal mass ratio of the explosive detonation shock wave effect is provided, which includes: an overpressure formula acquisition module 601, an explosive equivalent division module 602, an overpressure formula construction module 603, a coupling formula determination module 604 and a mass ratio solving module 605.

[0076] The overpressure formula acquisition module 601 is used to obtain the total explosive equivalent and the shock wave overpressure formula of a single explosive explosion. The shock wave overpressure formula is a formula for calculating the shock wave overpressure based on the distance from the center of the explosive to the target and the explosive equivalent.

[0077] The explosive equivalent division module 602 is used to arbitrarily divide the total explosive equivalent into multiple portions, wherein the distance from the center of each portion of explosive to the target is the same.

[0078] The overpressure formula building module 603 is used to build the shock wave overpressure formula of each explosive explosion based on the distance from the center of each explosive to the target, the mass of each explosive and the shock wave overpressure formula of a single explosive explosion.

[0079] The coupling formula determination module 604 is used to determine the shock wave overpressure superposition coupling formula after multiple explosives are detonated simultaneously based on the shock wave overpressure formula of each explosive explosion.

[0080] The mass ratio solving module 605 is used to solve the optimal mass ratio of each explosive by using the Lagrange multiplier method based on the shock wave overpressure superposition coupling formula and with the goal of maximizing the shock wave overpressure superposition coupling value after multiple explosives are simultaneously detonated.

[0081] In an exemplary embodiment, a computer device is provided. The computer device may be a server or a terminal. The internal structure diagram thereof may be as follows: Figure 7As shown. The computer device includes a processor, a memory, an input / output interface (Input / Output, I / O) and a communication interface. The processor, the memory and the input / output interface are connected through a system bus, and the communication interface is connected to the system bus through the input / output interface. The processor of the computer device is used to provide computing and control capabilities. The memory of the computer device includes a non-volatile storage medium and an internal memory. The non-volatile storage medium stores an operating system, a computer program and a database. The internal memory provides an environment for the operation of the operating system and the computer program in the non-volatile storage medium. The database of the computer device is used to store the total equivalent of explosives and the shock wave overpressure formula of a single explosive explosion. The input / output interface of the computer device is used to exchange information between the processor and an external device. The communication interface of the computer device is used to communicate with an external terminal through a network connection. When the computer program is executed by the processor, a method for solving the optimal mass ratio of the shock wave effect of explosive detonation is implemented.

[0082] Those skilled in the art will understand that Figure 7 The structure shown in the figure is only a block diagram of a part of the structure related to the solution of the present application, and does not constitute a limitation on the computer device to which the solution of the present application is applied. The specific computer device may include more or fewer components than those shown in the figure, or combine certain components, or have a different arrangement of components.

[0083] In an exemplary embodiment, a computer-readable storage medium is provided, storing a computer program, and when the computer program is executed by a processor, the steps in the above method embodiments are implemented.

[0084] In an exemplary embodiment, a computer program product is provided, including a computer program, and when the computer program is executed by a processor, the steps in the above method embodiments are implemented.

[0085] It should be noted that the user information (including but not limited to user device information, user personal information, etc.) and data (including but not limited to data used for analysis, stored data, displayed data, etc.) involved in this application are all information and data authorized by the user or fully authorized by all parties, and the collection, use and processing of relevant data must comply with relevant regulations.

[0086] In this application, all actions to obtain signals, information or data are carried out in compliance with the relevant data protection laws and policies of the country where they are located and with the authorization given by the owner of the corresponding device.

[0087] Those of ordinary skill in the art can understand that all or part of the processes in the above-mentioned embodiment methods can be completed by instructing the relevant hardware through a computer program, and the computer program can be stored in a non-volatile computer-readable storage medium. When the computer program is executed, it can include the processes of the embodiments of the above-mentioned methods. Among them, any reference to the memory, database or other medium used in the embodiments provided in the present application can include at least one of non-volatile and volatile memory. Non-volatile memory can include read-only memory (ROM), magnetic tape, floppy disk, flash memory, optical memory, high-density embedded non-volatile memory, resistive random access memory (ReRAM), magnetic random access memory (MRAM), ferroelectric random access memory (FRAM), phase change memory (PCM), graphene memory, etc. Volatile memory can include random access memory (RAM) or external cache memory, etc. By way of illustration and not limitation, RAM may be in various forms, such as static random access memory (SRAM) or dynamic random access memory (DRAM).

[0088] The database involved in each embodiment provided in this application may include at least one of a relational database and a non-relational database. The non-relational database may include a distributed database based on blockchain, etc., but is not limited thereto. The processor involved in each embodiment provided in this application may be a general-purpose processor, a central processing unit, a graphics processor, a digital signal processor, a programmable logic device, a data processing logic device based on quantum computing, etc., but is not limited thereto.

[0089] The technical features of the above embodiments may be combined arbitrarily. To make the description concise, not all possible combinations of the technical features in the above embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

[0090] This article uses specific examples to illustrate the principles and implementation methods of this application. The description of the above embodiments is only used to help understand the method and core ideas of this application. At the same time, for those skilled in the art, according to the ideas of this application, there will be changes in the specific implementation methods and application scope. In summary, the content of this specification should not be understood as limiting this application.

Claims

1. A method for solving the optimal mass ratio of the shock wave effect of explosive detonation, characterized in that: The method for solving the optimal mass ratio of the explosive detonation shock wave effect comprises: Obtaining the total explosive equivalent and the shock wave overpressure formula of a single explosive explosion; the shock wave overpressure formula is a formula for calculating the shock wave overpressure based on the distance from the center of the explosive to the target and the explosive equivalent; The total equivalent of the explosive is arbitrarily divided into a plurality of portions, wherein the distance from the center of each portion of the explosive to the target is the same; Based on the distance from the center of each explosive to the target, the mass of each explosive and the shock wave overpressure formula of a single explosive explosion, a shock wave overpressure formula for each explosive explosion is constructed; Based on the shock wave overpressure formula of each explosive explosion, the shock wave overpressure superposition coupling formula after multiple explosives are detonated simultaneously is determined; Based on the shock wave overpressure superposition coupling formula, with the goal of maximizing the shock wave overpressure superposition coupling value after simultaneous detonation of multiple explosives, the Lagrange multiplier method is used to solve the optimal mass ratio of each explosive.

2. The method for solving the optimal mass ratio of explosive detonation shock wave effect according to claim 1 is characterized in that: The shock wave overpressure formula for a single explosive explosion is: Among them, ΔP m is the shock wave overpressure, W is the explosive equivalent, R is the distance from the center of the explosive to the target, and a1, a2, and a3 are combination coefficients.

3. The method for solving the optimal mass ratio of explosive detonation shock wave effect according to claim 1, characterized in that: The shock wave overpressure formula for the explosion of the i-th explosive is: Among them, ΔP mi is the shock wave overpressure of the explosion of the i-th explosive, i = 1, 2...n, n is the number of explosives, b i W is the mass of the i-th explosive, b i is the mass ratio of the i-th explosive, 0≤b i ≤1, b1+b2+…+b n =1, W is the explosive equivalent, R is the distance from the center of the explosive to the target, a1, a2, a3 are combination coefficients.

4. The method for solving the optimal mass ratio of explosive detonation shock wave effect according to claim 3 is characterized in that: The shock wave overpressure superposition coupling formula is: Among them, ΔP m ' is the shock wave overpressure superposition coupling value after multiple explosives are detonated simultaneously, is the first mass ratio parameter, is the second mass ratio parameter.

5. The method for solving the optimal mass ratio of explosive detonation shock wave effect according to claim 4 is characterized in that: Based on the shock wave overpressure superposition coupling formula, the Lagrange multiplier method is used to solve the optimal mass ratio of each explosive, with the goal of maximizing the shock wave overpressure superposition coupling value after multiple explosives are simultaneously detonated. Specifically, it includes: Constructing a first Lagrangian multiplier function based on the first mass ratio parameter term and the Lagrangian multiplier factor; constructing a second Lagrangian multiplier function based on the second mass ratio parameter term and the Lagrangian multiplier factor; According to the first Lagrangian multiplier function, differentiating each mass ratio in the first mass ratio parameter item and the Lagrangian multiplier factor to obtain a first set of equations; According to the second Lagrangian multiplier function, differentiating each mass ratio and the Lagrangian multiplier factor in the second mass ratio parameter item to obtain a second set of equations; The first set of equations and the second set of equations are solved respectively to obtain the optimal mass ratio of each portion of explosive.

6. The method for solving the optimal mass ratio of explosive detonation shock wave effect according to claim 5, characterized in that: The first Lagrange multiplier function is: The second Lagrange multiplier function is: The first set of equations is: The second set of equations is: Among them, F1(b1,b2,...,b n ,λ) is the first Lagrange multiplier function, F2(b1,b2,...,b n ,λ) is the second Lagrange multiplier function, λ is the Lagrange multiplier factor, is the equation about b1 in the first system of equations, is the first set of equations about b n The equation, F' 1,λ is the equation about λ in the first system of equations, is the equation about b1 in the second system of equations, is the second set of equations about b n The equation, F' 2,λ is the equation about λ in the second set of equations.

7. The method for solving the optimal mass ratio of explosive detonation shock wave effect according to claim 1, characterized in that: The best mass ratio of each explosive is Where n is the number of explosives.

8. A system for solving the optimal mass ratio of the shock wave effect of explosive detonation, applied to the method for solving the optimal mass ratio of the shock wave effect of explosive detonation as claimed in any one of claims 1 to 7, characterized in that: The optimal mass ratio solution system for explosive detonation shock wave effect comprises: An overpressure formula acquisition module is used to obtain the total explosive equivalent and the shock wave overpressure formula of a single explosive explosion; the shock wave overpressure formula is a formula for calculating the shock wave overpressure based on the distance from the center of the explosive to the target and the explosive equivalent; An explosive equivalent division module, used to arbitrarily divide the total explosive equivalent into multiple portions; wherein the distance from the center of each portion of explosive to the target is the same; An overpressure formula building module is used to build a shock wave overpressure formula for each explosive explosion based on the distance from the center of each explosive to the target, the mass of each explosive and the shock wave overpressure formula for a single explosive explosion; A coupling formula determination module is used to determine the shock wave overpressure superposition coupling formula after multiple explosives are detonated simultaneously based on the shock wave overpressure formula of each explosive explosion; The mass ratio solving module is used to solve the optimal mass ratio of each explosive by using the Lagrange multiplier method based on the shock wave overpressure superposition coupling formula and with the goal of maximizing the shock wave overpressure superposition coupling value after multiple explosives are simultaneously detonated.

9. A computer device comprising: A memory, a processor, and a computer program stored in the memory and executable on the processor, wherein the processor executes the computer program to implement the method for solving the optimal mass ratio of the explosive detonation shock wave effect according to any one of claims 1 to 7.

10. A computer-readable storage medium having a computer program stored thereon, characterized in that: When the computer program is executed by a processor, the method for solving the optimal mass ratio of the explosive detonation shock wave effect described in any one of claims 1 to 7 is implemented.