Blade maintenance scheme generation method, equipment, equipment and storage medium

Abstract

The embodiment of the invention relates to the technical field of blade maintenance, and discloses a blade maintenance scheme generation method, equipment, equipment and a storage medium. The blade maintenance scheme generation method comprises the steps that the defect position of a blade is determined; determining a maintenance parameter and a reinforcement parameter according to the defect position; wherein the maintenance parameters comprise the first strength of the repair material; the reinforcing parameter comprises the second strength of the reinforcing material; checking the maintenance parameter and the reinforcement parameter according to a comparison result of a size relationship between the first strength and the second strength and a preset threshold value; and generating a maintenance scheme of the blade by using the corrected maintenance parameters and reinforcement parameters. The blade maintenance scheme is formulated through an automatic process, and related maintenance parameters and reinforcement parameters are verified before the maintenance scheme is generated, so that the accuracy of the maintenance scheme is improved while the generation efficiency of the maintenance scheme is improved.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of blade repair, in particular to a blade repair scheme generation method, equipment, device and storage medium. BACKGROUND

[0002] A fan converts wind energy into mechanical energy and then converts the mechanical energy into electrical energy by means of rotation of blades, thereby providing renewable energy for a power grid. As an important component of the fan, the blades are damaged, which affects the efficiency of wind power generation and may even cause safety hazards. However, the blades are relatively expensive, and replacing the blades directly after damage will cause unnecessary waste of resources. Therefore, repairing the damaged position of the blades is conducive to reducing costs and improving the utilization rate of the blades.

[0003] At present, after determining the defect position of the blade, the blade repair scheme is usually formulated and implemented according to artificial experience. However, the scheme formulated by humans is affected by subjective judgment, data calculation is prone to error, and the efficiency of manually formulating the repair scheme is not high. SUMMARY

[0004] The purpose of the embodiments of the present application is to provide a blade repair scheme generation method, equipment, device and storage medium, which realizes the formulation of the blade repair scheme through an automatic process, and checks the related repair parameters and reinforcement parameters before generating the repair scheme, thereby improving the efficiency of generating the repair scheme and the accuracy of the repair scheme.

[0005] To solve the above technical problems, the embodiments of the present application provide a blade repair scheme generation method, which comprises: determining a defect position of a blade; determining repair parameters and reinforcement parameters according to the defect position; wherein the repair parameters comprise a first strength of a repair material; the reinforcement parameters comprise a second strength of a reinforcement material; checking the repair parameters and the reinforcement parameters according to a comparison result of a size relationship between the first strength and the second strength and a preset threshold; and generating a repair scheme of the blade by using the corrected repair parameters and the reinforcement parameters.

[0006] The embodiments of the present application also provide a blade repair scheme generation device, which comprises: an input unit, a logic unit, a checking unit and an output unit; the input unit is used to determine a defect position of a blade; the logic unit is used to determine repair parameters and reinforcement parameters according to the defect position; wherein the repair parameters comprise a first strength of a repair material; the reinforcement parameters comprise a second strength of a reinforcement material; the checking unit is used to check the repair parameters and the reinforcement parameters according to a comparison result of a size relationship between the first strength and the second strength and a preset threshold; and the output unit is used to generate a repair scheme of the blade by using the corrected repair parameters and the reinforcement parameters.

[0007] The embodiment of the present application also provides an electronic device, comprising: at least one processor; and a memory connected with the at least one processor; wherein the memory stores instructions executable by the at least one processor, and the instructions are executed by the at least one processor to enable the at least one processor to execute the blade maintenance scheme generation method.

[0008] The embodiment of the present application also provides a computer readable storage medium, which stores a computer program, and the computer program is executed by a processor to implement the blade maintenance scheme generation method.

[0009] Compared with the prior art, the embodiment of the present application only needs to determine the defect position of the blade, and then automatically determines the maintenance parameter and the reinforcing parameter according to the defect position, and according to the first strength of the repair material in the maintenance parameter and the second strength of the reinforcing material in the reinforcing parameter, the accuracy of the maintenance parameter and the reinforcing parameter is verified through comparison of the size relationship between the first strength and the second strength and a preset threshold, and finally the maintenance scheme of the blade is generated by using the maintenance parameter and the reinforcing parameter after the verification. The accuracy of the generated maintenance scheme is improved while the efficiency of the maintenance scheme generation is improved.

[0010] In addition, before the maintenance parameter and the reinforcing parameter are checked, the method further comprises: calculating the sum of the strengths of each layer of material in all repair materials as the first strength, and the sum of the corresponding strengths of each layer of material in all reinforcing materials as the second strength.

[0011] In addition, the maintenance parameter comprises: the first specification of the repair material; and before the maintenance parameter and the reinforcing parameter are checked according to the comparison result of the size relationship between the first strength and the second strength and the preset threshold, the method comprises: determining the corresponding preset threshold according to the first specification.

[0012] In addition, the checking of the maintenance parameter and the reinforcing parameter according to the comparison result of the size relationship between the first strength and the second strength and the preset threshold comprises: comparing the ratio of the first strength to the second strength with the preset threshold; and if the ratio of the first strength to the second strength is greater than the preset threshold, the second strength is increased.

[0013] In addition, before the maintenance scheme of the blade is generated, the method comprises: drawing a graph corresponding to the maintenance scheme according to the size information of the blade, the size of the repair material and the size of the reinforcing material; and checking the size of the repair material and the size of the reinforcing material according to the arrangement rule of the first line representing the boundary of the repair material and the second line representing the boundary of the reinforcing material in the graph.

[0014] In addition, according to the arrangement rule of the first lines representing the boundary of the repair material and the second lines representing the boundary of the reinforcing material in the blade figure, the size of the repair material and the size of the reinforcing material are checked, including: if the first lines intersect each other, or the second lines intersect each other, or the first lines and the second lines intersect each other, then outputting that the check fails.

[0015] In addition, the defect position includes the total number of layers of the damaged material, the repair parameter includes the first number of layers of the repair material, the reinforcing parameter includes the second number of layers of the reinforcing material, and the determination of the repair parameter and the reinforcing parameter according to the defect position includes taking the total number of layers of the damaged material as the first number of layers and taking the product of the total number of layers of the damaged material and a preset reinforcing coefficient as the second number of layers. BRIEF DESCRIPTION OF DRAWINGS

[0016] One or more embodiments are illustrated by way of example in the figures that are part of this disclosure and which are illustrative, but not restrictive, of the embodiments, wherein elements having the same reference number designates like elements, unless otherwise stated, and wherein the figures are not necessarily to scale.

[0017] Figure 1 is a schematic diagram of an operation interface in a blade repair scheme generation method according to an embodiment of the present application;

[0018] Figure 2 is a flowchart of a blade repair scheme generation method according to an embodiment of the present application;

[0019] Figure 3 is a schematic diagram of related parameters in a blade repair scheme generation method according to an embodiment of the present application;

[0020] Figure 4 is a flowchart of a blade repair scheme generation method according to an embodiment of the present application;

[0021] Figure 5 is a schematic diagram of a derived figure in a blade repair scheme generation method according to an embodiment of the present application;

[0022] Figure 6 is a schematic diagram of related parameters in a blade repair scheme generation method according to an embodiment of the present application;

[0023] Figure 7 is a structural schematic diagram of an electronic device according to an embodiment of the present application. DETAILED DESCRIPTION

[0024] In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the embodiments of the present application will be described in detail below with reference to the drawings. However, those skilled in the art can understand that, in the embodiments of the present application, many technical details are presented in order to make the readers better understand the present application. However, the technical solutions claimed by the present application can be implemented even without these technical details and based on various changes and modifications of the following embodiments.

[0025] The division of the following embodiments is for the convenience of description, and should not constitute any limitation on the specific implementation modes of the present application. The embodiments can be combined and referenced with each other under the premise of no contradiction.

[0026] The embodiment of the present application relates to a blade repair scheme generation method, comprising: determining a defect position of a blade; determining a repair parameter and a reinforcement parameter according to the defect position; wherein the repair parameter comprises a first strength of a repair material; the reinforcement parameter comprises a second strength of a reinforcement material; according to a comparison result of a size relationship between the first strength and the second strength and a preset threshold, the repair parameter and the reinforcement parameter are checked; and a repair scheme of the blade is generated by using the checked repair parameter and reinforcement parameter. The formulation of the blade repair scheme is realized through an automatic process, and the related repair parameter and reinforcement parameter are checked before the generation of the repair scheme, which improves the repair scheme generation efficiency and improves the accuracy of the repair scheme. The implementation details of the blade repair scheme generation method of the present embodiment will be described in detail below. The following content only provides implementation details for easy understanding, and is not necessary for implementing the present scheme.

[0027] Compared with the prior art, the embodiment of the present application only needs to determine the defect position of the blade, and can automatically determine the repair parameter and the reinforcement parameter according to the defect position. According to the first strength of the repair material in the repair parameter and the second strength of the reinforcement material in the reinforcement parameter, the repair parameter and the reinforcement parameter are checked according to the comparison result of the size relationship between the first strength and the second strength and the preset threshold. The accuracy of the repair parameter and the reinforcement parameter is verified through the checking mode, and finally the repair scheme of the blade is generated by using the checked repair parameter and reinforcement parameter. The repair scheme generation efficiency is improved, and the accuracy of the generated repair scheme is improved.

[0028] The blade repair scheme generation method of the present application can be applied to a software operating system, and the operation interface of the operating system is as follows Figure 1As shown, after inputting the defect position of the blade on the operation interface, for example, inputting the axial position, chordwise position and damage layer number, the operation system determines the material specifications of each layer corresponding to the defect position according to the pre-stored position information of each specification material in the blade model, and outputs the material specifications corresponding to the defect position in the layer specification. After outputting the material specifications, the generated material specifications can also be adjusted and deleted through the damage specification determination option key and the delete specification function key. In response to the user's operation of clicking the wrong layer deduction, the operation system automatically generates a repair scheme according to the pre-set repair logic. In actual operation, part of the parameters in the generated repair scheme can be displayed on the operation interface for the staff to manually determine the reliability of the generated repair scheme, for example, the repair parameters and reinforcement parameters can be displayed on the operation interface, such as Figure 1 The double-axial damage and single-axial damage represent the first strength of the repair material, the double-axial 20% reinforcement and single-axial 20% reinforcement represent the target strength of the reinforcement material under the pre-set reinforcement rule, and the double-axial actual reinforcement and single-axial actual reinforcement represent the second strength of the reinforcement material in the generated scheme. In addition, related parameters of the repair scheme such as "repair glass fiber weight", "repair resin weight", "repair material quality moment", "repair proportion check" and the like can also be output to preliminarily understand the repair scheme by the staff. In addition, the accuracy of the related parameters in the repair scheme can be checked through the calculation check button. The generation and export of the CAD graph of the repair scheme can be realized through the export CAD button. When exporting the CAD graph, the label font size and font color of the CAD graph can be manually adjusted.

[0029] The following will be described in detail for the checking function and the export CAD graph function in the generation of the blade repair scheme.

[0030] The checking process in the blade repair scheme is as shown in Figure 2 The checking process in the blade repair scheme is as shown in

[0031] Step 201, determining the defect position of the blade.

[0032] Step 202, determining the repair parameters and reinforcement parameters according to the defect position; wherein the repair parameters include: the first strength of the repair material; and the reinforcement parameters include: the second strength of the reinforcement material.

[0033] Step 203, checking the repair parameters and reinforcement parameters according to the comparison result of the size relationship between the first strength and the second strength and the pre-set threshold value.

[0034] Step 204, generating the repair scheme of the blade by using the corrected repair parameters and reinforcement parameters.

[0035] In addition, when the number of layers of the repair material in the repair scheme is multiple, the sum of the strength of each layer of the repair material is calculated as the first strength, and the sum of the corresponding strength of each layer of the reinforcing material is calculated as the second strength.

[0036] In addition, the repair parameters include: the first specification of the repair material; before the repair parameters and the reinforcing parameters are checked according to the comparison result of the size relationship between the first strength and the second strength and the preset threshold, the first specification is used to determine the corresponding preset threshold. Then, the accuracy of the repair scheme is verified by using the preset threshold corresponding to the first specification. The checking of the repair parameters and the reinforcing parameters according to the comparison result of the size relationship between the first strength and the second strength and the preset threshold includes: comparing the ratio of the first strength to the second strength with the preset threshold; if the ratio of the first strength to the second strength is greater than the preset threshold, the second strength is increased.

[0037] For example, if the relevant parameters of the generated repair scheme are as shown in Figure 3 , the number of layers of the repair material in the generated repair scheme is 1 to 3 layers Figure 3 (the three rows of data in the original structure type), and the number of layers of the reinforcing material is 4 to 5 layers Figure 3 (the two rows of data in the reinforcing type). The first strength and the second strength are divided into the strength of the 0-degree material specification and the strength of the ±45-degree material specification. The strength of the 0-degree material specification of the 1 to 3 layers of the repair material corresponds to X1, X2, X3, and the strength of the ±45-degree material specification corresponds to Y1, Y2, Y3. The strength of the 0-degree material specification of the 4 to 5 layers of the reinforcing material corresponds to X2, X3, and the strength of the ±45-degree material specification corresponds to Y2, Y3. If (X1+X2+X3)×K1≤(X2+X3), and (Y1+Y2+Y3)×K2≤(Y2+Y3), it indicates that the generated repair scheme meets the requirements. K1 and K2 represent the preset threshold values under different material specifications, and the preset threshold values can be selected as any value between 10% and 20%. K1 and K2 can be selected as the same value.

[0038] The generation process of the CAD graph in the blade repair scheme is as shown in Figure 4 , and the process includes:

[0039] Step 401: Obtain the material position data in the repair scheme.

[0040] Step 402: Split the position data into X-direction data and Y-direction data.

[0041] Step 403: Call the drawing resource.

[0042] Step 404: Draw the graph according to the X-direction data and the Y-direction data.

[0043] The generated drawing graph is as shown inFigure 5 As shown, the material size gradually decreases from the outer layer to the inner layer. The accuracy of the generated repair scheme can be further checked according to the line distribution of the drawing graph. Specifically, according to the size information of the blade, the size of the repair material, and the size of the reinforcing material, a graph corresponding to the repair scheme is drawn; according to the arrangement rule of the first line representing the boundary of the repair material and the second line representing the boundary of the reinforcing material in the graph, the size of the repair material and the size of the reinforcing material are checked. If there is a cross between multiple first lines, or a cross between multiple second lines, or a cross between the first line and the second line, the check fails. In addition, it can also be judged whether the distance between adjacent lines of the first line representing the boundary of the repair material is uniformly distributed. If there is a non-uniform distribution, the check fails. The drawn graph can be presented to the staff for the staff to manually judge whether the repair scheme meets the requirements.

[0044] In addition, the first number of layers of repair material in the repair parameter and the second number of layers of reinforcing material in the reinforcing parameter can also be checked according to the total number of layers of damaged material. The checking logic is: taking the total number of layers of damaged material as the first number of layers, and taking the product of the total number of layers of damaged material and the preset reinforcing coefficient as the second number of layers. If the first number of layers is not equal to the total number of layers of damaged material, or the second number of layers is less than the product of the total number of layers of damaged material and the preset reinforcing coefficient, it indicates that the generated repair scheme is not accurate enough.

[0045] Before checking the repair scheme in any of the above ways, the related parameters of the repair scheme have been generated in the operating system, and the checking process is also implemented by using the related parameters to check the repair scheme. Only after the check passes, the complete repair scheme is exported for the staff to view. The exported repair scheme includes repair scheme related parameters such as Figure 6 As shown, including axial starting point, axial ending point, chordal starting point, chordal ending point, material specification, remarks, axial staggered layers, chordal staggered layers, layer length, layer width, and other related parameters. In addition, it can also include the strength parameters of each layer of material. The corresponding drawing is exported as shown in Figure 5 If the check of the repair scheme in any of the above ways fails, the generation logic of the repair scheme needs to be adjusted to generate the repair scheme again. When the check fails, the operation interface will highlight the related parameters that fail the check, so that the staff can know the type of inaccurate parameters.

[0046] The generation of the blade maintenance scheme is realized by the above method, compared with the traditional manual maintenance scheme, the generation of the maintenance scheme is automatically calculated according to the specific logic, and the stability and reliability of the generated scheme are higher. In addition, the accuracy of the related data in the generated maintenance scheme is automatically checked according to the set checking logic, the checking logic includes multiple dimensions and multiple ways of judgment logic, and the checking of the data is more comprehensive, which is beneficial to improve the accuracy of the maintenance scheme.

[0047] The step division of the above various methods is only for clear description, and can be combined into one step or some steps can be split and decomposed into multiple steps, as long as the same logical relationship is included, and all are within the protection scope of the patent; adding irrelevant modifications or introducing irrelevant designs in the algorithm or process, but not changing the core design of the algorithm and process are within the protection scope of the patent.

[0048] The embodiment of the application also relates to a blade maintenance scheme generation device, comprising: an input unit, a logic unit, a checking unit and an output unit; the input unit is used to determine the defect position of the blade; the logic unit is used to determine the maintenance parameter and the reinforcing parameter according to the defect position; wherein the maintenance parameter comprises a first strength of the repair material; the reinforcing parameter comprises a second strength of the reinforcing material; the checking unit is used to check the maintenance parameter and the reinforcing parameter according to the comparison result of the size relationship between the first strength and the second strength and the preset threshold value; and the output unit is used to generate the maintenance scheme of the blade by using the corrected maintenance parameter and the reinforcing parameter.

[0049] In addition, the checking unit is used to calculate the sum of the strengths of all layers of the repair material as the first strength and the sum of the corresponding strengths of all layers of the reinforcing material as the second strength before checking the maintenance parameter and the reinforcing parameter.

[0050] In addition, the checking unit is used to determine the corresponding preset threshold value according to the first specification.

[0051] In addition, the checking unit is used to compare the ratio of the first strength to the second strength with the preset threshold value; if the ratio of the first strength to the second strength is greater than the preset threshold value, the second strength is increased.

[0052] In addition, the checking unit is used to draw a graph corresponding to the maintenance scheme according to the size information of the blade, the size of the repair material and the size of the reinforcing material; and check the size of the repair material and the size of the reinforcing material according to the arrangement rule of the first line representing the boundary of the repair material and the second line representing the boundary of the reinforcing material in the graph.

[0053] In addition, if the first lines intersect each other, or the second lines intersect each other, or the first lines and the second lines intersect each other, the output is not passed.

[0054] In addition, the logic unit is configured to take the total number of layers of the damaged material as the first number of layers, and take the product of the total number of layers of the damaged material and a preset reinforcement coefficient as the second number of layers.

[0055] It is worth mentioning that each module involved in the embodiment is a logical module, and in actual application, one logic unit can be one physical unit, or a part of one physical unit, or a combination of multiple physical units. In addition, in order to highlight the innovative part of the application, units not closely related to solving the technical problems proposed in the application are not introduced in the embodiment, but this does not mean that there are no other units in the embodiment.

[0056] The embodiment can be implemented in combination with the method embodiments described above. The related technical details mentioned in the method embodiments are still valid in this embodiment, and in order to reduce repetition, they will not be described here. Correspondingly, the related technical details mentioned in this embodiment can also be applied to the above method embodiments.

[0057] The embodiment of the application relates to an electronic device, such as Figure 7 As shown in the figure, the electronic device comprises at least one processor 701 and a memory 702 connected with the at least one processor 701, wherein the memory 702 stores instructions executable by the at least one processor 701, and the instructions are executed by the at least one processor 701 to enable the at least one processor 701 to perform the blade maintenance scheme generation method described above.

[0058] The memory and the processor are connected in a bus mode, the bus can include any number of interconnected buses and bridges, and the bus connects various circuits of one or more processors and memories together. The bus can also connect various other circuits such as peripheral devices, voltage stabilizers and power management circuits together, which are well known in the art, and therefore, they will not be further described herein. The bus interface provides an interface between the bus and the transceiver. The transceiver can be one element or multiple elements such as multiple receivers and transmitters, which provide a unit for communicating with various other devices on the transmission medium. The data processed by the processor is transmitted on the wireless medium through the antenna, and further, the antenna also receives data and transmits the data to the processor.

[0059] The processor is responsible for managing the bus and general processing, and can also provide various functions, including timing, peripheral interface, voltage regulation, power management and other control functions. And the memory can be used to store the data used by the processor in the execution operation.

[0060] An embodiment of the present application relates to a computer readable storage medium storing a computer program. The computer program is executed by a processor to implement the method embodiments.

[0061] That is, a person skilled in the art can understand that all or part of the steps of the above-mentioned method embodiments can be completed by a program instructing relevant hardware, the program is stored in a storage medium, and the program includes a plurality of instructions for causing an apparatus (which can be a single-chip microcomputer, a chip, etc.) or a processor to execute all or part of the steps of the method described in each embodiment of the present application. The foregoing storage medium includes a U disk, a mobile hard disk, a read-only memory (ROM), a random access memory (RAM), a magnetic disk or an optical disk, and various storage media that can store program codes.

[0062] A person skilled in the art can understand that the above-mentioned embodiments are specific embodiments for implementing the present application, and in actual applications, various changes can be made in form and details without departing from the spirit and scope of the present application.

Claims

1. A blade repair scheme generation method, characterized by, The method comprises the following steps: determining a defect position of a blade; determining a repair parameter and a reinforcement parameter according to the defect position; wherein the repair parameter comprises a first strength of a repair material; and the reinforcement parameter comprises a second strength of a reinforcement material; checking the repair parameter and the reinforcement parameter according to a comparison result of a size relationship between the first strength and the second strength and a preset threshold value; generating a repair scheme of the blade by using the corrected repair parameter and the reinforcement parameter.

2. The blade repair concept generation method of claim 1, wherein, Before the checking of the repair parameter and the reinforcement parameter, the method further comprises the following steps: calculating a sum of strengths of each layer of material in all repair materials as the first strength, and a sum of corresponding strengths of each layer of material in all reinforcement materials as the second strength.

3. The blade repair concept generation method of claim 1, wherein, The repair parameter comprises a first specification of the repair material. Before the checking of the repair parameter and the reinforcement parameter according to the comparison result of the size relationship between the first strength and the second strength and the preset threshold value, the method comprises the following step: determining the corresponding preset threshold value according to the first specification.

4. The blade repair concept generation method of claim 3, wherein, The checking of the repair parameter and the reinforcement parameter according to the comparison result of the size relationship between the first strength and the second strength and the preset threshold value comprises the following steps: comparing a ratio of the first strength to the second strength with the preset threshold value; if the ratio of the first strength to the second strength is greater than the preset threshold value, increasing the second strength.

5. The blade repair concept generation method of claim 1, wherein, Before the generation of the repair scheme of the blade, the method comprises the following steps: drawing a graph corresponding to the repair scheme according to size information of the blade, a size of the repair material and a size of the reinforcement material; checking the size of the repair material and the size of the reinforcement material according to an arrangement rule of first lines representing boundaries of the repair material and second lines representing boundaries of the reinforcement material in the graph.

6. The blade repair concept generation method of claim 5, wherein, The checking of the size of the repair material and the size of the reinforcement material according to the arrangement rule of the first lines representing boundaries of the repair material and the second lines representing boundaries of the reinforcement material in the graph comprises the following step: if there is intersection between a plurality of first lines, or between a plurality of second lines, or between a first line and a second line, outputting a check failure.

7. The blade repair scheme generation method according to any one of claims 1 to 6, characterized in that, The defect position comprises a total number of layers of damaged material; the repair parameter comprises a first number of layers of repair material; and the reinforcement parameter comprises a second number of layers of reinforcement material. The determination of the repair parameter and the reinforcement parameter according to the defect position comprises the following steps: taking the total number of layers of damaged material as the first number of layers; taking a product of the total number of layers of damaged material and a preset reinforcement coefficient as the second number of layers.

8. A blade repair scheme generation apparatus, characterized by, The method comprises the following steps: an input unit, a logic unit, a checking unit and an output unit; the input unit is configured to determine a defect position of a blade; the logic unit is configured to determine a repair parameter and a reinforcement parameter according to the defect position; wherein the repair parameter comprises a first strength of a repair material; and the reinforcement parameter comprises a second strength of a reinforcement material; the checking unit is configured to check the repair parameter and the reinforcement parameter according to a comparison result of a size relationship between the first strength and the second strength and a preset threshold value; and the output unit is configured to generate a repair scheme of the blade by using the corrected repair parameter and the reinforcement parameter. The output unit is configured to generate a repair scheme for the blade by using the corrected repair parameter and the reinforcement parameter.

9. An electronic device, comprising: Comprise: at least one processor; and, a memory connected to the at least one processor in communication; wherein, the memory stores instructions executable by the at least one processor, and the instructions are executed by the at least one processor to enable the at least one processor to perform the blade repair scheme generation method according to any one of claims 1 to 7.

10. A computer readable storage medium storing a computer program, characterized in that, The computer program is executed by the processor to implement the blade repair scheme generation method according to any one of claims 1 to 7.

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