Hole site arrangement design method of porous part, terminal equipment and readable storage medium

Abstract

The invention provides a hole site arrangement design method of a porous part, terminal equipment and a readable storage medium, the hole site arrangement design method of the porous part comprises the following steps: in a theoretical design drawing, selecting three theoretical hole site columns as theoretical reference columns, the theoretical reference columns and the theoretical contour of the part having a constant relationship; in the part adjustment contour, according to a constant relation, completing creation of three adjustment reference columns corresponding to the theoretical reference column; a row datum curve is made through the corresponding adjusting hole position of each adjusting reference datum column, wherein the curvature of the row datum curve is the same as the boundary curvature of the part adjusting contour; on each row reference curve, a plurality of adjusting hole positions are created at equal intervals, and adjusting hole position columns with the same number as the preset number are formed. According to the method, the outline of the multi-hole fan-shaped part and the position relation of all the hole sites in the multi-hole fan-shaped part can be correspondingly adjusted, so that the design size of the adjusted part and the relation of the hole site positions meet the design requirements.

Description

Technical Field

[0001] The present invention relates to the field of aviation manufacturing design technology, and more specifically, to a hole arrangement design method for porous parts, a terminal device and a readable storage medium. Background Art

[0002] In the field of aviation manufacturing, it is often necessary to prepare multiple acoustic lining holes on the corresponding structure to obtain porous parts to meet the design requirements of specific functions of the aircraft. Porous parts are mostly made of metal. When welding or other heat treatments are performed on them, under the action of thermal stress, the treated parts will have differences relative to the design dimensions of the parts. In order to ensure that the contour of the parts produced in the final batch and the deviation of each hole position meet the design requirements, it is necessary to adjust the design dimensions in a targeted manner and test them in combination with the specific process before batch production. So that the contour of the porous parts prepared with the adjusted design dimensions and their hole position deviations meet the design requirements. Therefore, on the basis of the initial design dimensions of the parts, how to adjust its contour and quickly arrange the holes therein so that the relationship between the design dimensions of the adjusted parts and their hole positions meets the design requirements is a problem that needs to be solved urgently. Summary of the invention

[0003] 1. Technical issues to be resolved

[0004] The technical problem to be solved by the present invention is how to adjust the contour and the positions of each hole of the part based on the initial design size of the part so that the relationship between the design size of the part and the positions of its holes after adjustment meets the design requirements.

[0005] (II) Technical solution

[0006] To achieve the above object, the technical solution adopted by the present invention is:

[0007] In a first aspect, the present invention provides a method for designing the hole arrangement of a porous part, wherein the porous sector-shaped part is provided with a preset number of hole rows spaced apart in a radial direction, and the method for designing the hole arrangement of the porous part comprises the following steps:

[0008] S1. In the theoretical design drawing, three columns of theoretical hole positions are selected as theoretical reference datum columns, and there is a constant relationship between the theoretical reference datum columns and the theoretical contour of the part;

[0009] S2. In the part adjustment profile, according to the constant relationship, complete the creation of three adjustment reference datum columns corresponding to the theoretical reference datum columns;

[0010] S3, making a row reference curve through the corresponding adjustment hole positions of each column of the adjustment reference datum column, wherein the curvature of the row reference curve is the same as the boundary curvature of the part adjustment contour;

[0011] S4. On each of the row reference curves, create a plurality of adjustment holes at equal intervals to form a column of adjustment holes having the same number as the preset number.

[0012] Preferably, the constant relationship includes: the theoretical contour of the part forms a fan-shaped closed figure, wherein one column of the theoretical reference datum columns is located on the axis of symmetry of the fan-shaped closed figure, and the other two columns of the theoretical reference datum columns are located at both ends of the fan-shaped closed figure and the distance between each adjustment hole position and the boundary of the theoretical contour of the part is a fixed value.

[0013] Preferably, step S2 comprises the following steps:

[0014] In each theoretical reference datum column, each hole position center of the theoretical reference datum column is connected to form a theoretical hole center curve, a hole position center of an end point of the theoretical hole center curve is selected as a theoretical reference hole position, and the length ratio relationship between the theoretical reference hole position and the remaining theoretical hole positions on the theoretical hole center curve is calculated;

[0015] In the part adjustment profile, the positions of the adjustment hole centers of the two end points are determined according to the fixed values, and the adjustment hole center curve is established;

[0016] On the adjustment hole center curve, a terminal hole position center corresponding to the theoretical reference hole position is used as the terminal reference hole position, and the remaining adjustment hole positions are created on the adjustment hole center curve according to the length ratio relationship to obtain an adjustment reference datum column;

[0017] The above steps are repeated until three adjustment reference datum columns corresponding to the theoretical reference datum columns are created.

[0018] Preferably, the length ratio relationship Xn=Ln / S, wherein S is the total length of the theoretical hole center curve, and Ln is the length of the distance between the remaining theoretical hole positions and the theoretical reference hole position along the direction of the theoretical hole center curve.

[0019] Preferably, on each of the row reference curves, the distance between two adjacent adjustment hole positions along the direction of the row reference curve is Yn=C / Z, wherein C is the total length of the row reference curve, and Z is the preset number of hole position columns.

[0020] Preferably, before step S1, the method further includes the following steps:

[0021] Prepare sample parts according to the theoretical design drawings;

[0022] Welding the sample parts, and obtaining the experimental parts after cooling;

[0023] measuring a boundary offset between the sample part and the test part;

[0024] The part adjusted contour is obtained based on the theoretical contour of the part and combined with the boundary offset.

[0025] Preferably, the boundary offset includes an X-direction offset and a Y-direction offset.

[0026] Preferably, the step of obtaining the part adjusted contour based on the part theoretical contour and combining the boundary offset comprises the following steps:

[0027] In the theoretical contour of the part, multiple boundary theoretical hole positions are selected as first reference holes, wherein the boundary theoretical hole position center is the theoretical hole position center closest to the boundary of the theoretical contour of the part, and the distance between the boundary theoretical hole position center and the boundary of the theoretical contour of the part is a preset value;

[0028] Taking the XY coordinates of the centers of the theoretical holes of the multiple boundaries as references and combining them with their corresponding boundary offsets, multiple boundary adjustment hole centers are obtained;

[0029] The adjustment contour of the porous part is obtained by taking the centers of the plurality of boundary adjustment holes as a reference and combining the preset values.

[0030] In a second aspect, the present invention also provides a terminal device, comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein when the processor executes the computer program, the method for designing the hole arrangement of porous parts as described in any one of the above technical solutions is implemented.

[0031] In a third aspect, the present invention further provides a readable storage medium, wherein the readable storage medium stores a computer program, and when the computer program is executed by a processor, the method for designing the hole arrangement of a porous part described in any one of the above technical solutions is implemented.

[0032] (III) Beneficial effects

[0033] The above technical solution of the present invention has at least the following advantages:

[0034] In the present invention, the theoretical boundary vertex of the theoretical contour of the porous part is used as the first reference point, and the first reference point is used as the benchmark. According to the relative position relationship between the centers of the theoretical holes and the first reference point in the theoretical contour of the porous part, the positions of the centers of the adjusted holes in the adjusted contour of the porous part are determined, so as to realize the batch design of the holes in the part after the contour is adjusted, so that the adjusted part contour and the positions of the holes in the part meet the design requirements. At the same time, when the hole position adjustment method of the porous part provided by the present invention is run through the corresponding computer program, the automatic adjustment of multiple holes of the porous part can be realized, which can significantly improve the design efficiency compared with the method of manually adjusting each hole in turn. BRIEF DESCRIPTION OF THE DRAWINGS

[0035] In order to more clearly illustrate the technical solutions in the embodiments of the present invention, 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 invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0036] Figure 1 It is a flow chart of a method for designing hole arrangement of a porous part provided in an embodiment of the present invention.

[0037] Figure 2 It is a schematic diagram of the structure of a porous sector-shaped part provided in an embodiment of the present invention.

[0038] Figure 3 It is a schematic diagram of the design dimensions of the sample parts provided in the embodiment of the present invention.

[0039] Figure 4 It is a size comparison diagram of the sample part and the experimental part provided in the embodiment of the present invention.

[0040] Figure 5 It is a schematic diagram of setting a theoretical reference column provided by an embodiment of the present invention.

[0041] Figure 6 It is a schematic diagram of setting the theoretical hole center curve provided in an embodiment of the present invention.

[0042] Figure 7 It is a schematic diagram of setting the adjustment reference datum column provided in an embodiment of the present invention.

[0043] Figure 8 It is a schematic diagram of setting a row reference curve provided by an embodiment of the present invention.

[0044] Fig. 9 It is a schematic diagram of setting the hole position adjustment provided in an embodiment of the present invention.

[0045] Fig.10This is the adjusted parts design drawing provided by the embodiment of the present invention.

[0046] The reference numerals in the figures are:

[0047] 1. First boundary; 2. Second boundary; 3. Third boundary; 4. Fourth boundary; 5. Theoretical reference datum column on the left; 6. Theoretical reference datum column in the middle; 7. Theoretical reference datum column on the right; 8. Theoretical hole center curve; 9. Adjust the hole position center by the first endpoint; 10. Adjust the hole position center by the second endpoint; 11. Adjust the hole center curve; 12. Row datum curve; 13. Adjust the hole position; 51. Adjust the reference datum column on the left; 61. Adjust the reference datum column in the middle; 71. Adjust the reference datum column on the right. DETAILED DESCRIPTION

[0048] In order to make the technical problems, technical solutions and beneficial effects to be solved by the present invention more clearly understood, the present invention is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention and are not intended to limit the present invention.

[0049] It should be noted that when an element is referred to as being "fixed to" or "disposed on" another element, it may be directly located on the other element or indirectly located on the other element. When an element is referred to as being "connected to" another element, it may be directly connected to the other element or indirectly connected to the other element.

[0050] It should be understood that the terms "length", "width", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside" and "outside" etc., indicating directions or positional relationships, are based on the directions or positional relationships shown in the accompanying drawings and are only for the convenience of describing the present invention, and do not indicate that a device or element must have a specific direction, be constructed and operated in a specific direction, and therefore should not be understood as a limitation on the present invention.

[0051] In addition, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating relative importance or indicating the number of technical features. In the description of the present invention, the meaning of "multiple" is two or more, unless otherwise clearly and specifically defined. The specific implementation of the present invention is described in more detail below in conjunction with specific embodiments:

[0052] like Figure 1 As shown, an embodiment of the present invention provides a hole arrangement design method for a porous part, wherein a porous sector-shaped part is provided with a preset number of hole rows spaced apart in a radial direction, and the hole arrangement design method for a porous part comprises the following steps:

[0053] S1. In the theoretical design drawing, three columns of theoretical hole positions are selected as theoretical reference datum columns. There is a constant relationship between the theoretical reference datum columns and the theoretical contour of the part.

[0054] S2. In the part adjustment profile, according to the constant relationship, complete the creation of three adjustment reference datum columns corresponding to the theoretical reference datum columns;

[0055] S3, making a row reference curve through the corresponding adjustment hole position of each column of the adjustment reference datum column, wherein the curvature of the row reference curve is the same as the boundary curvature of the part adjustment contour;

[0056] S4. On each row reference curve, create multiple adjustment holes at equal intervals to form a column of adjustment holes having the same number as the preset number.

[0057] Preferably, the constant relationship includes: the theoretical contour of the part forms a fan-shaped closed figure, wherein one column of theoretical reference datum columns is located on the axis of symmetry of the fan-shaped closed figure, and the other two columns of theoretical reference datum columns are located at both ends of the fan-shaped closed figure and the distance between each adjustment hole position and the boundary of the theoretical contour of the part is a fixed value.

[0058] Preferably, step S2 comprises the following steps:

[0059] In each theoretical reference datum column, each hole position center of the theoretical reference datum column is connected to form a theoretical hole center curve, a hole position center of an end point of the theoretical hole center curve is selected as the theoretical reference hole position, and the length ratio relationship between the theoretical reference hole position and the remaining theoretical hole positions on the theoretical hole center curve is calculated;

[0060] In the part adjustment profile, determine the positions of the two end points to adjust the hole center according to the fixed value, and establish the adjustment hole center curve;

[0061] On the adjustment hole center curve, the center of an end hole position corresponding to the theoretical reference hole position is used as the end hole reference hole position, and the remaining adjustment hole positions are created on the adjustment hole center curve according to the length ratio relationship to obtain the adjustment reference datum column;

[0062] Repeat the above steps until three adjustment reference datum columns corresponding to the theoretical reference datum columns are created.

[0063] Preferably, the length ratio relationship is Xn=Ln / S, wherein S is the total length of the theoretical hole center curve, and Ln is the length of the distance between the remaining theoretical hole positions and the theoretical reference hole position along the direction of the theoretical hole center curve.

[0064] Preferably, on each row reference curve, the distance between two adjacent adjustment hole positions along the row reference curve direction is Yn=C / Z, wherein C is the total length of the row reference curve, and Z is the preset number of hole position columns.

[0065] Preferably, before step S1, the method further includes the following steps:

[0066] Prepare sample parts according to the theoretical design drawings;

[0067] Weld the sample parts and obtain the experimental parts after cooling;

[0068] Measure the boundary offset between the sample part and the test part;

[0069] Based on the theoretical contour of the part and combined with the boundary offset, the adjusted contour of the part is obtained.

[0070] Preferably, the boundary offset includes an X-direction offset and a Y-direction offset.

[0071] Preferably, taking the theoretical contour of the part as a reference and combining the boundary offset, obtaining the adjusted contour of the part includes the following steps:

[0072] In the theoretical contour of the part, multiple boundary theoretical hole positions are selected as the first reference hole positions, wherein the boundary theoretical hole position center is the theoretical hole position center closest to the boundary of the theoretical contour of the part, and the distance between the boundary theoretical hole position center and the boundary of the theoretical contour of the part is a preset value;

[0073] Taking the XY coordinates of the centers of the theoretical holes of the multiple boundaries as references and combining them with their corresponding boundary offsets, multiple boundary adjustment hole centers are obtained;

[0074] The adjustment contour of the porous part is obtained by taking the centers of the hole positions adjusted by multiple boundaries as the reference and combining the preset values.

[0075] by Figure 2 A certain engine thin plate part (porous fan-shaped part) is shown as an example for explanation. The outline of the porous part is fan-shaped. There are multiple small holes with a diameter of φD (D ranges from 0.5-1.5mm) distributed on the porous fan-shaped part according to a certain rule. The number of holes is about 5000-15000. The small holes form a preset number of hole columns, and the preset number of hole columns are spaced apart along the radial direction. The thickness of the porous fan-shaped part is δ. For ease of understanding and clear expression of the drawings, a smaller number of holes is used for illustration in the attached drawings.

[0076] (1) First, prepare the sample parts according to the theoretical design drawing; for this porous sector-shaped part, Figure 3The four boundary theoretical hole positions shown ("hole 1", "hole 2", "hole 3", "hole 4") and the theoretical contour of the porous part (solid line segments in the figure, including the first boundary 1, the second boundary 2, the third boundary 3 and the fourth boundary 4 respectively) must satisfy the following relationship: the distance dimension from the axis of "hole 2" to the first boundary 1 is V2, the distance dimension from the axis of "hole 1" to the second boundary 2 is V1, the distance dimension from the axis of "hole 1" to the fourth boundary 4 is H1; the distance dimension from the axis of "hole 2" to the fourth boundary 4 is H2; "hole 3" and "hole 1" are symmetrical relative to the midline, and "hole 4" and "hole 2" are symmetrical relative to the midline. The remaining small holes are distributed according to a certain rule within the dotted line range of "hole 1", "hole 2", "hole 3", and "hole 4".

[0077] (2) Weld the sample parts and obtain the experimental parts after cooling; specifically, overlap the two sample parts, put the solder on the contact surface in advance, heat them to a certain temperature in a diffusion welding furnace, and under a certain pressure, diffusion connection occurs on the contact surface of the two sample parts to complete the welding process. After welding, cool and obtain the experimental parts. Contour comparison of the sample parts and the experimental parts Figure 4 As shown, the contour boundary shown by the solid line in the figure is the contour boundary of the sample part, and the contour boundary shown by the dotted line in the figure is the contour boundary of the experimental part. It can be found that, relative to the sample part, the contour boundary of the experimental part obtained after cooling during welding heat treatment shrinks.

[0078] (3) Measure the boundary offset between the sample part and the experimental part; specifically, take the "zero point" as the measurement reference, and the "zero point" of the experimental part coincides with the "zero point" of the sample part. The X-direction offset of "Point 1" is represented by "X1", and the Y-direction offset is represented by "Y1". The X-direction offset difference of "Point 2" is represented by "X2", and the Y-direction offset is represented by "Y2". "Point 3" is a symmetrical point relative to "Point 1", and "Point 4" is a symmetrical point relative to "Point 2". The dimensional deviation of "Point 5" is represented only by the Y-direction offset "Y5". Measure the values ​​of X1, Y1, X2, Y2 and Y5 respectively to obtain the boundary offset.

[0079] (4) Taking the theoretical contour of the part as a reference and combining the boundary offset, the adjusted contour of the part is obtained, which specifically includes the following steps:

[0080] (4-1) In the theoretical contour of the part, multiple boundary theoretical hole positions (i.e., "hole 1", "hole 2", "hole 3", "hole 4") are selected as the first reference hole positions, wherein the boundary theoretical hole position center is the theoretical hole position center closest to the boundary of the theoretical contour of the part, and the distance between the boundary theoretical hole position center and the boundary of the theoretical contour of the part is a preset value (i.e., V1, V2, H1, H2).

[0081] (4-2) Taking the XY coordinates of the centers of the theoretical holes at the boundaries as the reference, respectively combine the corresponding boundary offsets (i.e., X1, Y1, X2, Y2, and Y5), that is, add the X coordinate of the corresponding hole center to its X-direction offset, and add the Y coordinate of the corresponding hole center to its Y-direction offset, to obtain the XY coordinates of the centers of the adjusted holes at the boundaries;

[0082] (4-3) Based on the positions of the centers of multiple boundary adjustment holes and combined with preset values ​​(i.e., V1, V2, H1, H2), the part adjustment contour is obtained. That is, based on the XY coordinates of the boundary adjustment hole center, the corresponding preset values ​​are offset to determine the coordinates of the vertices of the part adjustment contour, and then combined with the curvature shape of each boundary of the part theoretical contour, the XY coordinates of the boundary adjustment hole center are used as the basis for proportional offset to obtain the boundary of the part adjustment contour, and finally the part adjustment contour is obtained. The final determined part adjustment contour is as follows: Figure 5 As shown (the boundary of the adjusted contour of the porous part is the solid line segment shown in the figure).

[0083] (5) In the theoretical design drawing, select three columns of theoretical hole positions as theoretical reference columns (such as Figure 5 As shown, the three columns of theoretical reference datum columns are respectively the left theoretical reference datum column 5, the middle theoretical reference datum column 6 and the right theoretical reference datum column 7), and there is a constant relationship between the theoretical reference datum columns and the theoretical contour of the part; the theoretical contour of the part forms a fan-shaped closed figure, wherein one column of theoretical reference datum columns is located on the symmetry axis of the fan-shaped closed figure (such as the middle theoretical reference datum column 6 in this embodiment), and the other two columns of theoretical reference datum columns (such as the left theoretical reference datum column 5 and the right theoretical reference datum column 7) are located at both ends of the fan-shaped closed figure and the distance between each adjustment hole position and the boundary of the part theoretical contour is a fixed value, that is, the vertical distance between each theoretical hole position on the left theoretical reference datum column 5 and the third boundary 3 is a fixed value, and the vertical distance between each theoretical hole position on the right theoretical reference datum column 7 and the fourth boundary 4 is a fixed value.

[0084] (6) In the part adjustment profile, according to the constant relationship, the creation of three adjustment reference datum columns corresponding to the theoretical reference datum columns is completed; specifically, the following steps are included (hereinafter referred to as Figures 6 to 10 The embodiment shown is used for explanation):

[0085] (6-1) In each theoretical reference column, connect each hole position center of the theoretical reference column to form a theoretical hole center curve 8, and select a hole position center at one end point of the theoretical hole center curve 8 (such as Figure 6 The hole 1 position shown in FIG. 1 is used as the theoretical reference hole position, and the length ratio relationship between the theoretical reference hole position and the remaining theoretical hole positions on the theoretical hole center curve 8 is calculated; the length ratio relationship X n =Ln / S, where S is the total length of the theoretical hole center curve 8, L n The remaining theoretical holes and theoretical reference holes (such as Figure 6 The length of the distance along the direction of the theoretical hole center curve 8 (the hole 1 position shown in FIG).

[0086] (6-2) In the part adjustment profile, determine the two end points to adjust the hole center according to the fixed value (such as Figure 7 The positions of the first endpoint adjustment hole center 9 and the second endpoint adjustment hole center 10) are shown, and the adjustment hole center curve 11 is established;

[0087] (6-3) On the adjustment hole center curve 11, an endpoint hole position center corresponding to the theoretical reference hole position is used as the endpoint reference hole position (such as the first endpoint adjustment hole position center 9), and the remaining adjustment hole positions are created on the adjustment hole center curve 11 according to the length ratio relationship to obtain the adjustment reference datum column.

[0088] (6-4) Repeat the above steps (6-1) to (6-3) until the creation of three adjustment reference columns corresponding to the theoretical reference columns is completed. Figure 5 As shown, the three adjustment reference datum columns are respectively the left adjustment reference datum column 51, the middle adjustment reference datum column 61 and the right adjustment reference datum column 71, wherein the position of the left adjustment reference datum column 51 corresponds to the position of the left theoretical reference datum column 5, the position of the middle adjustment reference datum column 61 corresponds to the position of the middle theoretical reference datum column 6, and the position of the right adjustment reference datum column 71 corresponds to the position of the right theoretical reference datum column 7.

[0089] (7) Figure 8 As shown, a row reference curve 12 is made through the corresponding adjustment hole positions of each adjustment reference reference column, wherein the curvature of the row reference curve 12 is the same as the boundary curvature of the part adjustment contour, that is, the curvature of the row reference curve 12 is consistent with the curvature of the outer edge arc of the fan-shaped closed figure;

[0090] (8) Fig. 9 As shown, on each row reference curve 12, multiple adjustment holes 13 are created at equal intervals to form a preset number of adjustment hole columns. Specifically, on each row reference curve 12, the distance Y between two adjacent adjustment holes 13 along the row reference curve 12 is n =C / Z, where C is the total length of the row reference curve 12 and Z is the preset number of hole position columns. Fig.10 As shown, a hole is made at each adjustment hole position 13 to obtain an adjusted part design drawing.

[0091] Specifically, a script can be designed by programming, and the script can run a cyclic calculation algorithm. The script is run in the corresponding design software to repeat the above steps until each adjustment hole position setting is completed on each row reference curve 12, which significantly improves the design efficiency. The specific computer program and its design principle involved in the script are prior art well known to those skilled in the art, and this application will not repeat them. When the hole position arrangement design method of the porous part provided in this embodiment is run using a corresponding computer program, after the part profile is adjusted, the hole positions of all small holes can be automatically arranged, thereby improving the small hole arrangement design efficiency and shortening the development cycle of the porous sector-shaped part.

[0092] (9) Cut the parts according to the adjusted part design drawing obtained in step (8), and punch holes according to the positions corresponding to the positions of the adjustment holes 13 to obtain the adjusted sample parts, weld the adjusted sample parts, and obtain the adjusted experimental parts after cooling. The preparation process of the adjusted experimental parts is the same as the above step (2). Then measure the contour deviation value of the adjusted experimental parts relative to the theoretical contour of the parts, as well as the deviation values ​​of the positions of the holes. If the deviation values ​​meet the design requirements, the parts are manufactured and mass-produced according to the corresponding part adjustment contour and hole positions. As long as the contour size and welding process parameters of the parts are consistent, the outer contour size changes of the porous fan-shaped parts after mass production are basically consistent. If the deviation value does not meet the design requirements, repeat steps (4) to (8) again, and use a deviation value different from the last adjustment to adjust the part adjustment contour again until the deviation value meets the design requirements.

[0093] An embodiment of the present invention also provides a terminal device, including a memory, a processor, and a computer program stored in the memory and executable on the processor. When the processor executes the computer program, a hole arrangement design method for a porous part as described in any of the above embodiments is implemented.

[0094] The terminal device may be a computing device such as a desktop computer, a notebook, a PDA, or a cloud server. The terminal device may include, but is not limited to, a processor and a memory. Those skilled in the art will appreciate that the terminal device may include more or fewer components, or a combination of certain components, or different components, such as an input / output device, a network access device, etc.

[0095] The processor may be a central processing unit (CPU), or other general-purpose processors, digital signal processors (DSP), application-specific integrated circuits (ASIC), field-programmable gate arrays (FPGA) or other programmable logic devices, discrete gate or transistor logic devices, discrete hardware components, etc. A general-purpose processor may be a microprocessor or any conventional processor, etc.

[0096] In some embodiments, the memory may be an internal storage unit of the terminal device, such as a hard disk or memory of the terminal device. In other embodiments, the memory may also be an external storage device of the terminal device, such as a plug-in hard disk equipped on the terminal device, a smart memory card (Smart Media Card, SMC), a secure digital (Secure Digital, SD) card, a flash card (Flash Card), etc. Further, the memory may also include both an internal storage unit of the terminal device and an external storage device. The memory is used to store an operating system, an application program, a boot loader (BootLoader), data, and other programs, such as program codes of a computer program, etc. The memory may also be used to temporarily store data that has been output or is to be output.

[0097] The embodiment of the present invention further provides a readable storage medium, which stores a computer program, and when the computer program is executed by a processor, any of the hole arrangement design methods for porous parts in the above embodiments is implemented. The readable storage medium is specifically a computer readable storage medium.

[0098] If the integrated unit is implemented in the form of a software functional unit and sold or used as an independent product, it can be stored in a computer-readable storage medium. Based on this understanding, the present application implements all or part of the processes in the above-mentioned embodiment method, which can be completed by instructing the relevant hardware through a computer program. The computer program can be stored in a computer-readable storage medium. When the computer program is executed by the processor, the steps of the above-mentioned method embodiments can be implemented. Among them, the computer program includes computer program code, and the computer program code can be in source code form, object code form, executable file or some intermediate form. The computer-readable medium may at least include: any entity or device that can carry the computer program code to the camera / terminal device, a recording medium, a computer memory, a read-only memory (ROM, Read-Only Memory), a random access memory (RAM, Random Access Memory), an electric carrier signal, a telecommunication signal, and a software distribution medium. For example, a USB flash drive, a mobile hard disk, a magnetic disk or an optical disk. In some jurisdictions, according to legislation and patent practice, computer-readable media cannot be electric carrier signals and telecommunication signals.

[0099] An embodiment of the present application provides a computer program product. When the computer program product runs on a mobile terminal, the mobile terminal can implement the steps in the above-mentioned method embodiments when executing the computer program product.

[0100] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions and improvements made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A method for designing hole arrangement of a porous part, wherein a porous sector-shaped part is provided with a preset number of hole rows spaced apart in a radial direction, characterized in that: The hole arrangement design method of the porous part comprises the following steps: S1. In the theoretical design drawing, three columns of theoretical hole positions are selected as theoretical reference datum columns, and there is a constant relationship between the theoretical reference datum columns and the theoretical contour of the part; S2. In the part adjustment profile, according to the constant relationship, complete the creation of three adjustment reference datum columns corresponding to the theoretical reference datum columns; S3, making a row reference curve through the corresponding adjustment hole positions of each column of the adjustment reference datum column, wherein the curvature of the row reference curve is the same as the boundary curvature of the part adjustment contour; S4. On each of the row reference curves, create a plurality of adjustment holes at equal intervals to form a column of adjustment holes having the same number as the preset number.

2. The hole arrangement design method of a porous part according to claim 1, characterized in that: The constant relationship includes: the theoretical contour of the part forms a fan-shaped closed figure, wherein one column of the theoretical reference datum columns is located on the axis of symmetry of the fan-shaped closed figure, and the other two columns of the theoretical reference datum columns are located at both ends of the fan-shaped closed figure, and the distance between each adjustment hole position and the boundary of the theoretical contour of the part is a fixed value.

3. The hole arrangement design method of a porous part according to claim 1, characterized in that: Step S2 includes the following steps: In each theoretical reference datum column, each hole position center of the theoretical reference datum column is connected to form a theoretical hole center curve, a hole position center of an end point of the theoretical hole center curve is selected as a theoretical reference hole position, and the length ratio relationship between the theoretical reference hole position and the remaining theoretical hole positions on the theoretical hole center curve is calculated; In the part adjustment profile, the positions of the adjustment hole centers of the two end points are determined according to the fixed values, and the adjustment hole center curve is established; On the adjustment hole center curve, a terminal hole position center corresponding to the theoretical reference hole position is used as the terminal reference hole position, and the remaining adjustment hole positions are created on the adjustment hole center curve according to the length ratio relationship to obtain an adjustment reference datum column; The above steps are repeated until three adjustment reference datum columns corresponding to the theoretical reference datum columns are created.

4. The hole arrangement design method of a porous part according to claim 3, characterized in that: The length ratio X n =L n / S, where S is the total length of the theoretical hole center curve, L n It is the length of the distance between the remaining theoretical hole positions and the theoretical reference hole position along the direction of the theoretical hole center curve.

5. The hole arrangement design method of a porous part according to claim 1, characterized in that: On each row reference curve, the distance Y between two adjacent adjustment holes along the row reference curve direction is n =C / Z, wherein C is the total length of the row reference curve, and Z is the preset number of hole position columns.

6. The hole arrangement design method of a porous part according to claim 1, characterized in that: Before step S1, the method further includes the following steps: Prepare sample parts according to the theoretical design drawings; Welding the sample parts, and obtaining the experimental parts after cooling; measuring a boundary offset between the sample part and the test part; The part adjusted contour is obtained based on the theoretical contour of the part and combined with the boundary offset.

7. The hole arrangement design method of a porous part according to claim 6, characterized in that: The boundary offset includes an X-direction offset and a Y-direction offset.

8. The hole arrangement design method of a porous part according to claim 6, characterized in that: The method of obtaining the part adjusted contour based on the part theoretical contour and combining the boundary offset comprises the following steps: In the theoretical contour of the part, multiple boundary theoretical hole positions are selected as first reference holes, wherein the boundary theoretical hole position center is the theoretical hole position center closest to the boundary of the theoretical contour of the part, and the distance between the boundary theoretical hole position center and the boundary of the theoretical contour of the part is a preset value; Taking the XY coordinates of the centers of the theoretical holes of the multiple boundaries as references and combining them with their corresponding boundary offsets, multiple boundary adjustment hole centers are obtained; The adjustment contour of the porous part is obtained by taking the centers of the plurality of boundary adjustment holes as a reference and combining the preset values.

9. A terminal device, comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, characterized in that: When the processor executes the computer program, the hole arrangement design method for a porous part as described in any one of claims 1 to 8 is implemented.

10. A readable storage medium storing a computer program, characterized in that: When the computer program is executed by a processor, the method for designing hole arrangement of a porous part as described in any one of claims 1 to 8 is implemented.

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