Jet field evaluation method and device for aircraft tire explosion

Abstract

The invention discloses a jet flow field evaluation method and device for aircraft tire explosion. The method comprises the steps that tire position information and a jet flow field measurement data set are obtained; the jet field measurement data set comprises a plurality of measurement data sequences and corresponding test site position information; the measurement data sequence comprises measurement data measured at a plurality of moments; preprocessing the jet field measurement data set to obtain a preprocessed data set; and performing evaluation processing on the preprocessed data set to obtain an evaluation result value.

Description

Technical Field

[0001] The invention relates to the fields of aircraft tire testing and industrial data processing, and in particular to a jet field evaluation method and device for aircraft tire explosion. Background Art

[0002] Aircraft tires are generally filled with nitrogen. Long-term excessively high tire pressure will lead to the risk of tire blowout. At the same time, the jet field generated during the tire blowout lasts for a short time, the process is violent, and the impact area is large. How to evaluate the adverse effects of the jet field is a problem that needs to be solved at present.

[0003] Existing aircraft tire burst measurements mainly use recorders to measure tire pressure. The measurement method is relatively simple and can only detect tire pressure changes, but cannot achieve rapid and accurate evaluation of the jet field. Summary of the invention

[0004] The invention mainly solves the problem of how to realize rapid and accurate evaluation of the jet field influence of aircraft tire bursting, and discloses a jet field evaluation method and device for aircraft tire bursting.

[0005] In a first aspect of an embodiment of the present invention, a jet flow field evaluation method for aircraft tire explosion is disclosed, comprising:

[0006] S1, obtaining tire position information and a jet field measurement data set; the jet field measurement data set includes a plurality of measurement data sequences and corresponding test site position information; the measurement data sequence includes measurement data measured at a plurality of moments;

[0007] S2, preprocessing the jet field measurement data set to obtain a preprocessed data set;

[0008] S3, performing evaluation processing on the preprocessed data set to obtain an evaluation result value.

[0009] The preprocessing of the jet field measurement data set to obtain a preprocessed data set includes:

[0010] S21, performing time alignment processing on the jet field measurement data set to obtain a first data set;

[0011] S22, performing category checking processing on the first data set to obtain a second data set;

[0012] S23, performing pattern checking processing on the second data set to obtain a preprocessed data set.

[0013] The performing pattern checking processing on the second data set to obtain a preprocessed data set includes:

[0014] S231, using all data collection information of the second data set as independent variables and all measurement data of the second data set as dependent variables, performing autoregression-moving average modeling to obtain a regression model;

[0015] S232, using the regression model, calculating and processing the independent variable to obtain regression data values;

[0016] S233, determining whether the absolute value of the difference between the regression data value and the corresponding dependent variable value is greater than a set first regression discrimination threshold; if it is greater than the first regression discrimination threshold, deleting the measurement data from the second data set; if it is not greater than the first regression discrimination threshold, not processing the measurement data;

[0017] S234, executing S231 to S233 for each measurement data of the second data set, to obtain a preprocessed data set.

[0018] The jet field measurement data set is measured by the jet field test device for aircraft tire explosion; the jet field test device for aircraft tire explosion comprises: a jet port sealing component, a reinforcement component, a deflagration power component, an open-hole tire and a piezoelectric sensor array;

[0019] The perforated tire is used to provide a burst tire that generates a jet field;

[0020] The jet port sealing assembly is used to construct the jet port and the jet channel to form the jet field required for the test;

[0021] The reinforcing component is connected to the jet port sealing component and the perforated tire, and is used to provide a channel for the gas inside the tire body to flow to the jet port of the tire body;

[0022] The deflagration power assembly is connected to the jet port sealing assembly and is used to provide the deflagration power required to generate the jet field for bursting the aircraft tire;

[0023] The piezoelectric sensor array is arranged within the distribution range of the jet field and is used to measure the pressure distribution of the jet field when the aircraft tire explodes.

[0024] The step of performing evaluation processing on the preprocessed data set to obtain an evaluation result value includes:

[0025] S31, obtaining a standard measurement data set; the standard measurement data set includes a pressure standard value and corresponding standard position information;

[0026] S32, determining the nearest standard position information and the corresponding pressure standard value in the standard measurement data set according to the test location position information corresponding to each measurement data sequence in the preprocessing data set;

[0027] S33, performing a difference calculation process on each measurement data sequence and the pressure standard value corresponding to the determined most recent standard position information to obtain a difference value of the measurement data sequence;

[0028] S34, performing weight calculation processing on the test location location information corresponding to each measurement data sequence and the determined nearest standard location information to obtain a weight value of the measurement data sequence;

[0029] S35, performing weighted summation processing on the difference values ​​and weight values ​​of all measurement data sequences to obtain an evaluation result value.

[0030] The difference calculation process includes:

[0031] Subtracting the pressure standard value corresponding to the measured data sequence and the nearest standard position information determined by the measured data sequence to obtain a difference sequence;

[0032] Taking the data collection information of the difference sequence as a known independent variable, taking the data value of the difference sequence as a known dependent variable, and constructing a curve to be approximated by using the known independent variable and the known dependent variable;

[0033] Performing curve fitting on the curve to be approximated to obtain a characteristic polynomial;

[0034] Using characteristic polynomials to calculate and process the data collection information of the difference sequence to obtain a corresponding output value sequence;

[0035] The maximum value in the output value sequence is determined as the difference value of the measurement data sequence.

[0036] The weight calculation process includes:

[0037] Taking the tire position information as a starting point, taking the test location position information corresponding to the measurement data sequence as an end point and taking the determined nearest standard position information as an end point, a first vector and a second vector are constructed;

[0038] Calculate the angle between the first vector and the second vector;

[0039] Performing fusion calculation processing on the first vector, the second vector and the angle value to obtain a weight value of the measurement data sequence;

[0040] The expression of the fusion calculation process is:

[0041] w=L2(sin(α))[sin(|x2-x1| / |z1+z2|+)+tan|1-y1 / y2|],

[0042] Wherein, w is the weight value of the measurement data sequence, L2() is the second-order Legendre function, α is the angle between the first vector and the second vector, (x1, y1, z1) and (x2, y2, z2) are the expressions of the first vector and the second vector respectively.

[0043] The beneficial effects of the present invention are:

[0044] The invention discloses a jet field evaluation method and device for aircraft tire explosion, which mainly solve the problem of how to realize rapid and accurate evaluation of the jet field influence of aircraft tire explosion.

[0045] When processing the measured piezoelectric data sequence, the present invention utilizes all piezoelectric data sequences and piezoelectric sensor positions to construct a measurement data set; a pattern matching model is constructed for the measurement data set, and the field distribution of the measurement data is extracted through the model, thereby achieving rapid and accurate modeling of the jet field. BRIEF DESCRIPTION OF THE DRAWINGS

[0046] Figure 1 1 is a flow chart for implementing the method of the present invention;

[0047] Figure 2 The jet flow field testing device for aircraft tire explosion of the present invention;

[0048] Figure 3 is a schematic diagram of an inner reinforcement plate of the present invention;

[0049] Figure 4 is a schematic diagram of an outer reinforcement plate of the present invention;

[0050] Figure 5 It is a schematic diagram of the jet port sealing assembly of the present invention;

[0051] Figure 6 It is a schematic diagram of the composition of the deflagration power assembly of the present invention. DETAILED DESCRIPTION

[0052] In order to better understand the content of the present invention, an embodiment is given here.

[0053] Figure 1 1 is a flow chart for implementing the method of the present invention; Figure 2 The jet flow field testing device for aircraft tire explosion of the present invention; Figure 3 is a schematic diagram of an inner reinforcement plate of the present invention; Figure 4 is a schematic diagram of an outer reinforcement plate of the present invention; Figure 5 It is a schematic diagram of the jet port sealing assembly of the present invention; Figure 6 It is a schematic diagram of the composition of the deflagration power assembly of the present invention.

[0054] In a first aspect of an embodiment of the present invention, a jet flow field evaluation method for aircraft tire explosion is disclosed, comprising:

[0055] S1, obtaining tire position information and a jet field measurement data set; the jet field measurement data set includes a plurality of measurement data sequences and corresponding test site position information; the measurement data sequence includes measurement data measured at a plurality of moments;

[0056] S2, preprocessing the jet field measurement data set to obtain a preprocessed data set;

[0057] S3, performing evaluation processing on the preprocessed data set to obtain an evaluation result value;

[0058] The preprocessing of the jet field measurement data set to obtain a preprocessed data set includes:

[0059] S21, performing time alignment processing on the jet field measurement data set to obtain a first data set;

[0060] S22, performing category checking processing on the first data set to obtain a second data set;

[0061] S23, performing pattern checking processing on the second data set to obtain a preprocessed data set.

[0062] The performing pattern checking processing on the second data set to obtain a preprocessed data set includes:

[0063] S231, using all data collection information of the second data set as independent variables and all measurement data of the second data set as dependent variables, performing autoregression-moving average modeling to obtain a regression model;

[0064] S232, using the regression model, calculating and processing the independent variable to obtain regression data values;

[0065] S233, determining whether the absolute value of the difference between the regression data value and the corresponding dependent variable value is greater than a set first regression discrimination threshold; if it is greater than the first regression discrimination threshold, deleting the measurement data from the second data set; if it is not greater than the first regression discrimination threshold, not processing the measurement data;

[0066] S234, executing S232 to S233 for each measurement data of the second data set, to obtain a preprocessed data set;

[0067] The jet field measurement data set is measured by the jet field test device for aircraft tire explosion; the jet field test device for aircraft tire explosion, such as Figure 2As shown, it includes: a jet port sealing component 1, a reinforcement component 2, a deflagration power component 3, a perforated tire 4 and a piezoelectric sensor array.

[0068] The perforated tire is used to provide a burst tire that generates a jet field;

[0069] The jet port sealing assembly is used to construct the jet port and the jet channel to form the jet field required for the test;

[0070] The reinforcing component is connected with the jet port sealing component and the perforated tire, and is used to provide a channel for the gas inside the tire body to flow to the jet port of the tire body;

[0071] The deflagration power assembly is connected to the jet port sealing assembly and is used to provide the deflagration power required to generate the jet field for bursting the aircraft tire;

[0072] The piezoelectric sensor array is used to measure the pressure distribution of the jet field when the aircraft tire explodes, and is arranged within the distribution range of the jet field.

[0073] The step of performing evaluation processing on the preprocessed data set to obtain an evaluation result value includes:

[0074] S31, obtaining a standard measurement data set; the standard measurement data set includes a pressure standard value and corresponding standard position information;

[0075] S32, determining the nearest standard position information and the corresponding pressure standard value in the standard measurement data set according to the test location position information corresponding to each measurement data sequence in the preprocessing data set;

[0076] S33, performing a difference calculation process on each measurement data sequence and the pressure standard value corresponding to the determined nearest standard position information to obtain a difference value of the measurement data sequence;

[0077] S34, performing weight calculation processing on the test location location information corresponding to each measurement data sequence and the determined nearest standard location information to obtain a weight value of the measurement data sequence;

[0078] S35, performing weighted summation processing on the difference values ​​and weight values ​​of all measurement data sequences to obtain an evaluation result value.

[0079] The difference calculation process includes:

[0080] Subtracting the pressure standard value corresponding to the measured data sequence and the nearest standard position information determined by the measured data sequence to obtain a difference sequence;

[0081] Taking the data collection information of the difference sequence as a known independent variable, taking the data value of the difference sequence as a known dependent variable, and constructing a curve to be approximated by using the known independent variable and the known dependent variable;

[0082] Performing curve fitting on the curve to be approximated to obtain a characteristic polynomial;

[0083] Using characteristic polynomials to calculate and process the data collection information of the difference sequence to obtain a corresponding output value sequence;

[0084] The maximum value in the output value sequence is determined as the difference value of the measurement data sequence.

[0085] The weight calculation process includes:

[0086] Taking the tire position information as a starting point, taking the test location position information corresponding to the measurement data sequence as an end point and taking the determined nearest standard position information as an end point, a first vector and a second vector are constructed;

[0087] Calculate the angle between the first vector and the second vector;

[0088] Performing fusion calculation processing on the first vector, the second vector and the angle value to obtain a weight value of the measurement data sequence;

[0089] The expression of the fusion calculation process is:

[0090] w=L2(sin(α))[sin(|x2-x1| / |z1+z2|+)+tan|1-y1 / y2|], wherein w is the weight value of the measurement data sequence, L2() is the second-order Legendre function, α is the angle between the first vector and the second vector, and (x1, y1, z1) and (x2, y2, z2) are the expressions of the first vector and the second vector respectively.

[0091] The weighted summation of the difference values ​​and weight values ​​of all measurement data sequences is performed to obtain the evaluation result value, which is obtained by multiplying the difference value and the weight value of each measurement data sequence to obtain the result value, and adding all the result values ​​to obtain the evaluation result value.

[0092] The curve fitting may adopt a polynomial fitting method;

[0093] The data collection information may be data collection time or sequence number value;

[0094] The larger the evaluation result value is, the more serious the impact of the jet field on the environment is.

[0095] The standard measurement data set may be obtained through historical measurement data or derived through a theoretical formula of air pressure.

[0096] The autoregressive-moving average modeling may adopt an ARMA model;

[0097] The category checking process is to determine whether each type of data in the jet field measurement data set is consistent with a preset data type, and to delete the inconsistent data from the jet field measurement data set.

[0098] The time alignment process is to unify different measurement data sequences to the same time reference; the time alignment process may adopt an interpolation / extrapolation method, a Lagrange three-point interpolation method, etc.;

[0099] The measurement data is pressure measurement data;

[0100] The piezoelectric sensor array includes a plurality of piezoelectric sensors and a data processing module; the piezoelectric sensor is used to measure and obtain a measurement data sequence;

[0101] The data processing module is connected to each piezoelectric sensor and is used to perform filtering and fusion processing on the pressure measurement data sequences and piezoelectric sensor positions measured by all piezoelectric sensors to obtain jet field information;

[0102] The piezoelectric data sequences and piezoelectric sensor positions measured by all piezoelectric sensors are filtered and fused to obtain jet field information, including

[0103] S201, constructing a measurement data set using all piezoelectric data sequences and piezoelectric sensor positions;

[0104] S202, for each type of data set in the measurement data set, using the data sequence of each type of data set in the data set as a row vector, constructing an approximation matrix; using the data acquisition information of each type of data sequence in the data set, constructing an acquisition matrix; the row vector of the acquisition matrix is ​​the data acquisition information of a type of data sequence; using the approximation matrix as a dependent variable and the acquisition matrix as an independent variable, constructing a pattern matching model;

[0105] S203, solving the pattern matching model to obtain a matching model for each type of data set; the expression of the matching model is f(x)=xA, x is the acquisition matrix of the input of the matching model, and the matrix A is obtained by solving the pattern matching model;

[0106] S204, using the matching model of each type of data set, calculating and processing the data collection information of the data sequence of the corresponding type of data set to obtain a solution matrix;

[0107] S205, subtracting each data in the solution matrix from the data in the approximation matrix corresponding to the same row and column as the data in the solution matrix, and calculating the absolute value to obtain a difference value of the data;

[0108] S206, deleting the data whose difference value is greater than a set difference threshold from the measurement data set;

[0109] S207, executing S202 to S206 for all types of data sets in the measurement data set to obtain jet field information.

[0110] For the deployment of the piezoelectric sensor array, based on the geometric shape of the tire blasting jet field and the axial symmetry of the pressure distribution, following the principle that "at any distance from the top of the cone, any busbar forms an 'isobaric circle' on the cross section perpendicular to the axis of the conical jet field", the sensors at different front and rear positions on the cone surface formed by the same busbar are cross-arranged on the truncated circles at different distances. This can avoid mutual interference between the front and rear sensors, reduce the interference of the sensor array on the jet free field, and perform a three-dimensional test on the pressure distribution characteristics of the jet free field, overcoming the disadvantage of arranging sensors on only one plane.

[0111] The perforated tire comprises: a tire body, jet holes and bolt holes; the bolt holes and jet holes are hole-shaped structures evenly distributed on the circumference of the tire body; the tire body is a circumferential structure composed of hollow rubber;

[0112] The axis of the jet hole is parallel to the axis of the bolt hole;

[0113] The number n of the bolt holes satisfies the first constraint condition; the expression of the first constraint condition is:

[0114] Fz=73.2+n×7.32,

[0115] Among them, Fz is the preset total reinforcement force value, and its value can be 102.48.

[0116] The reinforcement assembly includes: an inner reinforcement plate, an outer reinforcement plate with a jet hole sealing ring, a bolt group, and a bowl-shaped pressure ring.

[0117] The inner reinforcing plate is a metal curved plate that fits the inner tread of the tire body. The curved plate is provided with a plurality of bolt holes, such as Figure 3 As shown, the inner reinforcing plate is used to bear the tightening force of the bolt group; prevent the inner tread of the tire body from directly contacting the bolt group; provide a channel for the gas inside the tire body to flow to the jet holes of the tire body; and hinder the flow of the gas inside the tire body to the lower edges of each bolt hole.

[0118] The outer reinforcing plate is a metal curved plate that fits the outer surface of the tire body and has a plurality of bolt holes. Figure 4 As shown, the outer reinforcing plate cooperates with the inner reinforcing plate and the tire body to form a position for fixing the bolt group; bears the tightening force of the bolt group; provides an installation position for the bowl-shaped pressure ring and applies a clamping force to the bowl bottom of the bowl-shaped pressure ring; provides an installation position for the jet hole sealing ring and applies a clamping force to the jet hole sealing ring; cooperates with the jet hole of the tire body to provide a channel for the jet; and provides an assembly position for the base of the jet port sealing component.

[0119] The jet port sealing assembly base and the jet hole sealing ring are respectively installed on the upper surface and the lower surface of the outer reinforcing plate.

[0120] The bolt assembly comprises bolts and nuts;

[0121] The jet port sealing component, such as Figure 5 As shown, including the lower cover (such as Figure 5 Gray parts shown in Figure 5 The light green parts shown in the figure), the base, the upper cover (as shown in the figure Figure 5 The light yellow parts shown in Figure ), seals and fasteners ( Figure 5 Only the holes for fastener installation are shown in the figure). The sealing member is arranged between the upper cover plate and the lower cover plate, and is used to seal the jet channel between the upper cover plate and the lower cover plate. The fastener is used to fasten and connect the lower cover plate, the upper cover plate and the plate valve. The base is used to connect the jet port sealing component with the reinforcement component;

[0122] The upper cover plate and the lower cover plate are annular structures; the middle channel of the annular structure of the upper cover plate is a jet channel; the middle channel of the annular structure of the lower cover plate is a jet channel;

[0123] The function of the jet port sealing assembly is: by arranging a plate valve between the jet channels of the upper cover plate and the lower cover plate, when the tire body is inflated, the plate valve seals the jet channel thereunder to meet the pressure requirement; when a jet needs to be generated, the deflagration power assembly (such as Figure 5 The dark green and orange components connected to both ends of this component are shown), and the plate valve is quickly pulled open to open the jet port. The high-pressure gas under the plate valve is ejected through the channel on the upper cover plate to form the jet field required for the test.

[0124] The fastener may be a bolt structure; the sealing member may be made of rubber.

[0125] The length of the plate valve is obtained according to a first length calculation model; the expression of the first length calculation model is:

[0126] L1=0.5D2+(4~5)mm,

[0127] Wherein, D2 is the outer diameter of the O-type sealing ring around the jet port, and the increased 4 to 5 mm is for the edge of the plate valve to reliably compress the sealing ring; the sealing member is an O-type sealing ring;

[0128] The diameter D1 of the jet channel of the lower cover plate is obtained according to the second length calculation model; the expression of the second length calculation model is:

[0129] D1=d+(H+h1-h)tan19°,

[0130] Among them, d is the diameter of the jet hole on the outer reinforcing plate, H is the thickness of the disc of the lower cover plate, h1 is the distance between the lower bottom surface of the disc of the lower cover plate and the upper surface of the outer reinforcing plate, and h is the depth of the plate valve slide groove.

[0131] The outer diameter D2 of the outer circle of the O-type sealing ring around the jet port is obtained according to the third length calculation model; the expression of the third length calculation model is:

[0132] D2=D1+2(b1+b2),

[0133] Among them, b1 is the difference between the radius of the jet port and the inner radius of the O-ring around it, which is generally taken as 1.2mm~2mm; b2 is the radial width of the O-ring around the jet port, which is selected according to the size of the sealing ring and referenced to relevant standards.

[0134] The jet channel of the upper cover plate is a tapered hole with a gradually increasing cross-sectional area from bottom to top. The tapered hole and the jet channel of the lower cover plate are on the same axis, and the diameter D3 of the smallest cross-sectional circle of the tapered hole is obtained according to the fourth length calculation model; the expression of the fourth length calculation model is:

[0135] D3=D1+2h×tan19°,

[0136] Wherein, D3 is the diameter of the smallest cross-sectional circle of the tapered hole.

[0137] The diameter D4 of the largest cross-sectional circle of the tapered hole is obtained according to the fourth length calculation model; the expression of the fourth length calculation model is:

[0138] D4=D3+2H×tan19°,

[0139] Wherein, D4 is the diameter of the largest cross-sectional circle of the tapered hole.

[0140] The deflagration power assembly comprises: a power cylinder, a piston rod, a fireproof sealing ring, a sealing ring, a baffle, gunpowder, a wire, a piston and a leakage hole;

[0141] The power cylinder is the outer shell of the deflagration power assembly, and a piston rod is arranged in the circular hole-shaped structure at the front end thereof; the first end of the piston rod is in contact with the plate valve, and the second end of the piston rod is inserted into the piston; the piston is arranged at the end of the internal space of the power cylinder; a baffle is arranged at a position adjacent to the part of the second end of the piston rod inserted into the piston, and gunpowder is arranged in the closed space formed by the baffle and the piston, the first end of the wire passes through the piston and extends into the gunpowder, and the second end of the wire extends to the outside of the power cylinder; a fire-proof sealing ring is arranged on the part of the baffle in contact with the inner wall of the power cylinder; a closed sealing ring is arranged on the part of the piston in contact with the inner wall of the power cylinder; a leakage hole is provided on the cylinder wall at the rear of the power cylinder for gas leakage at the end stage of the piston stroke to reduce the movement speed of the piston.

[0142] The piezoelectric sensor array includes a plurality of piezoelectric sensors and a data processing module;

[0143] According to a second aspect of the present invention, a jet flow field evaluation device for aircraft tire explosion is disclosed, the device comprising:

[0144] A memory storing executable program code;

[0145] a processor coupled to the memory;

[0146] The processor calls the executable program code stored in the memory to execute the jet field evaluation method for aircraft tire explosion.

[0147] According to a third aspect of the present invention, a computer storable medium is disclosed, wherein the computer storable medium stores computer instructions, and when the computer instructions are called by a computer, they are used to execute the jet field evaluation method for aircraft tire explosion.

[0148] According to a fourth aspect of the present invention, an information data processing terminal is disclosed. The information data processing terminal is used to implement the jet field evaluation method for aircraft tire explosion.

[0149] The above description is only an embodiment of the present invention and is not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and variations. Any modification, equivalent substitution, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.

Claims

1. A jet flow field evaluation method for aircraft tire explosion, characterized in that: include: S1, obtaining tire position information and a jet field measurement data set; the jet field measurement data set includes a plurality of measurement data sequences and corresponding test site position information; the measurement data sequence includes measurement data measured at a plurality of moments; S2, preprocessing the jet field measurement data set to obtain a preprocessed data set; S3, performing evaluation processing on the preprocessed data set to obtain an evaluation result value.

2. The jet flow field evaluation method for aircraft tire explosion according to claim 1, characterized in that: The preprocessing of the jet field measurement data set to obtain a preprocessed data set includes: S21, performing time alignment processing on the jet field measurement data set to obtain a first data set; S22, performing category checking processing on the first data set to obtain a second data set; S23, performing pattern checking processing on the second data set to obtain a preprocessed data set.

3. The jet flow field evaluation method for aircraft tire explosion according to claim 2, characterized in that: The performing pattern checking processing on the second data set to obtain a preprocessed data set includes: S231, using all data collection information of the second data set as independent variables and all measurement data of the second data set as dependent variables, performing autoregression-moving average modeling to obtain a regression model; S232, using the regression model, calculating and processing the independent variable to obtain regression data values; S233, determining whether the absolute value of the difference between the regression data value and the corresponding dependent variable value is greater than a set first regression discrimination threshold; if it is greater than the first regression discrimination threshold, deleting the measurement data from the second data set; if it is not greater than the first regression discrimination threshold, not processing the measurement data; S234, executing S231 to S233 for each measurement data of the second data set, to obtain a preprocessed data set.

4. The jet flow field evaluation method for aircraft tire explosion according to claim 2, characterized in that: The jet field measurement data set is measured by the jet field test device for aircraft tire explosion; The jet field testing device for aircraft tire explosion comprises: a jet port sealing component, a reinforcement component, an explosion power component, an open-hole tire and a piezoelectric sensor array; The perforated tire is used to provide a burst tire that generates a jet field; The jet port sealing assembly is used to construct the jet port and the jet channel to form the jet field required for the test; The reinforcing component is connected to the jet port sealing component and the perforated tire, and is used to provide a channel for the gas inside the tire body to flow to the jet port of the tire body; The deflagration power assembly is connected to the jet port sealing assembly and is used to provide the deflagration power required to generate the jet field for bursting the aircraft tire; The piezoelectric sensor array is arranged within the distribution range of the jet field and is used to measure the pressure distribution of the jet field when the aircraft tire explodes.

5. The jet flow field evaluation method for aircraft tire explosion according to claim 1, characterized in that: The step of performing evaluation processing on the preprocessed data set to obtain an evaluation result value includes: S31, obtaining a standard measurement data set; the standard measurement data set includes a pressure standard value and corresponding standard position information; S32, determining the nearest standard position information and the corresponding pressure standard value in the standard measurement data set according to the test location position information corresponding to each measurement data sequence in the preprocessing data set; S33, performing a difference calculation process on each measurement data sequence and the pressure standard value corresponding to the determined most recent standard position information to obtain a difference value of the measurement data sequence; S34, performing weight calculation processing on the test location location information corresponding to each measurement data sequence and the determined nearest standard location information to obtain a weight value of the measurement data sequence; S35, performing weighted summation processing on the difference values ​​and weight values ​​of all measurement data sequences to obtain an evaluation result value.

6. The jet flow field evaluation method for aircraft tire explosion according to claim 5, characterized in that: The difference calculation process includes: Subtracting the pressure standard value corresponding to the measured data sequence and the nearest standard position information determined by the measured data sequence to obtain a difference sequence; Taking the data collection information of the difference sequence as a known independent variable, taking the data value of the difference sequence as a known dependent variable, and constructing a curve to be approximated by using the known independent variable and the known dependent variable; Performing curve fitting on the curve to be approximated to obtain a characteristic polynomial; Using characteristic polynomials to calculate and process the data collection information of the difference sequence to obtain a corresponding output value sequence; The maximum value in the output value sequence is determined as the difference value of the measurement data sequence.

7. The jet flow field evaluation method for aircraft tire explosion according to claim 5, characterized in that: The weight calculation process includes: Taking the tire position information as a starting point, taking the test location position information corresponding to the measurement data sequence as an end point and taking the determined nearest standard position information as an end point, a first vector and a second vector are constructed; Calculate the angle between the first vector and the second vector; Performing fusion calculation processing on the first vector, the second vector and the angle value to obtain a weight value of the measurement data sequence; The expression of the fusion calculation process is: w=L2(sin(α))[sin(|x2-x1| / |z1+z2|+)+tan|1-y1 / y2|], Wherein, w is the weight value of the measurement data sequence, L2() is the second-order Legendre function, α is the angle between the first vector and the second vector, (x1, y1, z1) and (x2, y2, z2) are the expressions of the first vector and the second vector respectively.

8. A jet field evaluation device for aircraft tire explosion, characterized in that: The device comprises: A memory storing executable program code; a processor coupled to the memory; The processor calls the executable program code stored in the memory to execute the jet field evaluation method for aircraft tire bursting according to any one of claims 1 to 7.

9. A computer storable medium, characterized in that: The computer storable medium stores computer instructions, and when the computer instructions are called by a computer, they are used to execute the jet flow field evaluation method for aircraft tire explosion according to any one of claims 1 to 7.

10. An information data processing terminal, characterized in that: The information data processing terminal is used to implement the jet field evaluation method for aircraft tire explosion according to any one of claims 1 to 7.

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