A method for designing a die set of a high-temperature alloy blade lying-forging aggregate blank
By designing a blank die set for horizontal forging of high-temperature alloy blades, the problems of long preparation cycle and large amount of waste in high-temperature alloy blade preparation were solved, achieving the effect of simplifying forging steps and shortening preparation cycle, while protecting technical secrets.
Patent Information
- Application Number
- CN202411715828.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-27
- Publication Date
- 2026-01-20
- Estimated Expiration
- 2044-11-27
AI Technical Summary
The preparation process of high-temperature alloy blades is lengthy, involves complicated steps, and generates a lot of waste, which affects their service life.
A mold assembly for horizontal forging of high-temperature alloy blade blanks is designed using 3D software. By constructing a target horizontal forging model, dividing the blank model, and designing sub-molds for each forging step according to the horizontal forging parameters, the shape of the forging hole in the sub-mold blank is consistent with the final shape during each forging step, thus avoiding the generation of waste.
The forging process was simplified, waste was reduced, the preparation cycle was shortened, and the trade secrets were protected by manufacturing through contract manufacturers.
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Figure CN119903606B_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to the technical field of metal material processing, in particular to a design method of a die set for a high-temperature alloy blade's upsetting gathered blank. BACKGROUND
[0002] High-temperature alloy is widely used in key equipment such as aero-engine and gas turbine due to its excellent high-temperature performance and corrosion resistance. In these equipment, the high-temperature alloy blade as a key component directly affects the operation efficiency and safety of the entire equipment.
[0003] Due to the harsh working environment of the high-temperature alloy blade and the material itself, various damages such as cracks, pores and wear are likely to occur during use, which reduces the service life of the blade. In order to ensure the service life of the high-temperature alloy blade, an integrated forming method such as forging is usually used to prepare the high-temperature alloy blade to reduce the possibility of blade damage. The high-temperature alloy blade is usually prepared by die forging. In the preparation, the blank is usually subjected to multi-step forging until the final target blade is formed. The entire preparation process has a long preparation cycle, and different dies are used in each step of forging. The waste material is removed during forging. The steps are complicated and a lot of waste material is generated. SUMMARY
[0004] Therefore, a design method of a die set for a high-temperature alloy blade's upsetting gathered blank is provided to solve the above technical problems.
[0005] The present application provides a design method of a die set for a high-temperature alloy blade's upsetting gathered blank, which is designed by using three-dimensional software, comprising the following steps:
[0006] S1, constructing a target upsetting gathered blank model according to a target blade model, the target upsetting gathered blank model comprising a blade tip upsetting gathered part, a blade body upsetting gathered part and a blade root upsetting gathered part;
[0007] S2, determining the size of a blank model based on the target upsetting gathered blank model and dividing the blank model into a blade tip blank part, a blade body blank part and a blade root blank part;
[0008] The blank model is cylindrical, and the volumes of the blade tip blank part, the blade body blank part and the blade root blank part are equal to the volumes of the blade tip upsetting gathered part, the blade body upsetting gathered part and the blade root upsetting gathered part, respectively;
[0009] S3, constructing the blade tip blank part of the blank model into a structure with the same shape and size as the blade tip upsetting gathered part to obtain a blade tip upsetting gathered blank model, and adding upsetting parameters to the blade tip upsetting gathered blank model to obtain a blade tip upsetting gathered blank hole shape;
[0010] S4, judging whether the blade root blanking part on the blade tip upset assembly model satisfies the upset local upsetting first rule, if yes, adding upset parameters to the target upset assembly model to obtain a target upset assembly blank hole shape; otherwise, entering the next step;
[0011] S5, adjusting the part volume of the blade root blanking part on the blade tip upset assembly model unchanged, increasing the shaft diameter by M times to obtain an intermediate upset assembly model, adding upset parameters to the intermediate upset assembly model to obtain an intermediate upset assembly blank hole shape, and returning to step S4 with the intermediate upset assembly model as a new blade tip upset assembly model until the blade root blanking part on the new blade tip upset assembly model satisfies the upset local upsetting first rule and then entering the next step;
[0012] S6, preparing a sub-mold based on each blank hole shape, and all sub-molds constitute a mold set of the upset assembly blank.
[0013] In one of the embodiments, constructing the target upset assembly model according to the target blade model includes the following steps:
[0014] S11, constructing a target blade forging model according to the target blade model;
[0015] S12, selecting several different sections in the axial direction on the target blade forging model and calculating the areas of the sections;
[0016] S13, converting the sections into circles with equal areas and combining the circles in the axial direction to form the target upset assembly model.
[0017] In one of the embodiments, the size of the blanking part model is that the shaft diameter of the blade body upset assembly part of the target upset assembly model is the blanking part diameter, and the length of the target upset assembly model and the length calculated by the volume of a cylinder formula are the blanking part length.
[0018] In one of the embodiments, the added upset parameters are the increased thermal coefficient and the draft angle.
[0019] In one of the embodiments, 1.10≤M≤1.25.
[0020] In one of the embodiments, the stamping hole of the sub-mold prepared based on the blade tip upset assembly blank hole shape is coaxially provided with a first punch accommodating hole and a blade tip upset assembly blank hole in sequence, and the blade tip end of the blade tip upset assembly blank hole communicates with the first punch accommodating hole.
[0021] The stamping hole of the sub-mold prepared based on the shape of the intermediate upsetting aggregate blank forging hole is sequentially coaxially provided with a first rear top position accommodating hole and an intermediate upsetting aggregate blank forging hole, and the blade tip end of the intermediate upsetting aggregate blank forging hole is in communication with the first rear top position accommodating hole;
[0022] The stamping hole of the sub-mold prepared based on the shape of the target upsetting aggregate model blank forging hole is sequentially coaxially provided with a second rear top position accommodating hole, a target upsetting aggregate model blank forging hole and a second punch accommodating hole, the blade tip end of the intermediate upsetting aggregate blank forging hole is in communication with the second rear top position accommodating hole, and the blade root end of the intermediate upsetting aggregate blank forging hole is in communication with the second punch accommodating hole.
[0023] In one of the embodiments, each sub-mold comprises an upper module and a lower module, the bottom of the upper module is provided with a first stamping groove, the top of the lower module is provided with a second stamping groove, the openings of the first stamping groove and the second stamping groove are opposite, and the first stamping groove and the second stamping groove constitute a stamping hole after the upper module and the lower module are aligned and abutted.
[0024] The present application has the following advantages:
[0025] (1) The mold set design method of the intermediate upsetting aggregate blank of the high-temperature alloy blade of the present application can design a sub-mold for each step of forging from the blank to the intermediate upsetting aggregate blank, and the shape of the blank forging hole of each sub-mold is the same as the shape and size finally generated in the step of forging, so that the use of the above-mentioned sub-mold for each step of forging will not produce waste and simplify the forging steps.
[0026] (2) The mold set obtained by using the present application can be prepared by a subcontracting enterprise, and then the subsequent preparation is prepared by the enterprise, which can shorten the preparation period of the enterprise. BRIEF DESCRIPTION OF DRAWINGS
[0027] Figure 1 It is a structural schematic diagram of a three-dimensional model of an A blade provided in the embodiments of the present application;
[0028] Figure 2 It is a structural schematic diagram of an A blade forging model provided in the embodiments of the present application;
[0029] Figure 3 It is a schematic diagram of a section on an A blade forging model provided in the embodiments of the present application;
[0030] Figure 4 It is a schematic diagram of a section conversion equivalent circle provided in the embodiments of the present application;
[0031] Figure 5 It is a structural schematic diagram of an A blade upsetting aggregate model provided in the embodiments of the present application;
[0032] Figure 6This is a schematic diagram of the structure of the blanking part model provided in the embodiment of the present invention;
[0033] Figure 7 This is a schematic diagram of the structure of the blade tip horizontal forging aggregate model provided in an embodiment of the present invention;
[0034] Figure 8 This is a schematic diagram of the structure of the intermediate horizontal forging aggregate model provided in the embodiment of the present invention;
[0035] Figure 9 This is a schematic diagram of the lower mold of the sub-mold used to prepare the forging hole shape of the blade tip horizontal forging aggregate blank, as provided in an embodiment of the present invention.
[0036] Figure 10 This is a schematic diagram of the upper mold of the sub-mold prepared based on the forging hole shape of the blade tip horizontal forging aggregate blank provided in an embodiment of the present invention;
[0037] Figure 11 This is a schematic diagram of the structure of the lower mold of one of the sub-molds prepared based on the forging hole shape of the intermediate horizontal forging aggregate blank provided in an embodiment of the present invention;
[0038] Figure 12 This is a schematic diagram of the structure of the upper mold of one of the sub-molds prepared based on the forging hole shape of the intermediate horizontal forging aggregate blank provided in an embodiment of the present invention;
[0039] Figure 13 This is a schematic diagram of the structure of the lower mold of the sub-mold prepared based on the forging hole shape of the blank of the target horizontal forging aggregate model provided in an embodiment of the present invention;
[0040] Figure 14 This is a schematic diagram of the upper mold of the sub-mold prepared based on the forging hole shape of the blank of the target horizontal forging aggregate model, provided in an embodiment of the present invention.
[0041] Explanation of reference numerals in the attached drawings: 100, blade tip horizontal forging assembly; 110, blade body horizontal forging assembly; 120, blade root horizontal forging assembly; 200, first punch receiving hole; 210, blade tip horizontal forging assembly blank forging hole; 300, first rear top receiving hole; 310, intermediate horizontal forging assembly blank forging hole; 400, second rear top receiving hole; 410, target horizontal forging assembly blank forging hole; 420, second punch receiving hole. Detailed Implementation
[0042] To make the objectives, technical solutions, and advantages of this invention clearer, the invention will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative and not intended to limit the invention.
[0043] In one embodiment, a die design method of a high-temperature alloy blade's upsetting cluster blank is provided, which is designed by using a three-dimensional software, which can be but is not limited to PRO / E and SolidWorks.
[0044] The die design method of the high-temperature alloy blade's upsetting cluster blank of the embodiment comprises the following steps:
[0045] S1, a target upsetting cluster model is constructed according to a target blade model, the target upsetting cluster model comprising a blade tip upsetting cluster part 100, a blade body upsetting cluster part 110 and a blade root upsetting cluster part 120.
[0046] The target upsetting cluster model is constructed according to the target blade model, comprising the following steps:
[0047] S11, a target blade forging model is constructed according to the target blade model.
[0048] Specifically, the target blade forging model is constructed according to the target blade model according to different die forging requirements, for example, the target blade forging model is obtained by converting the blade forging blank according to the principle of keeping the precision forging part unchanged and increasing the remaining part by 2mm on one side. The conversion process is well known to those skilled in the art and will not be described here.
[0049] S12, a plurality of different cross sections are selected axially on the target blade forging model and the areas of the cross sections are calculated.
[0050] It should be noted that the number of cross sections is equal to the ratio of the axial length of the target blade forging model to ΔL, and 3mm≤ΔL≤5mm.
[0051] S13, each cross section is converted into a circle with equal area and each circle is combined axially in sequence to form the target upsetting cluster model.
[0052] The blade tip upsetting cluster part 100, the blade body upsetting cluster part 110 and the blade root upsetting cluster part 120 are divided axially in equal length on the target upsetting cluster model according to the blade tip, the blade body and the blade root of the target blade.
[0053] S2, the size of a blank model is determined based on the target upsetting cluster model and the blank model is divided into a blade tip blank part, a blade body blank part and a blade root blank part.
[0054] The blank model is cylindrical, and the volumes of the blade tip blank part, the blade body blank part and the blade root blank part are equal to the volumes of the blade tip upsetting cluster part 100, the blade body upsetting cluster part 110 and the blade root upsetting cluster part 120, respectively.
[0055] Specifically, the size of the blanking piece model is set as the shaft diameter of the blade body lying forging aggregation part 110 of the target lying forging aggregation piece model as the diameter of the blanking piece, and the length of the target lying forging aggregation piece model and the shaft diameter of the blade body lying forging aggregation part 110 calculated by the cylinder volume formula as the length of the blanking piece.
[0056] S3, the blade tip blanking part of the blanking piece model is configured as a structure with the same shape and size as the blade tip lying forging aggregation part 100 to obtain a blade tip lying forging aggregation piece model, and the lying forging parameters are added to the blade tip lying forging aggregation piece model to obtain the shape of the blade tip lying forging aggregation piece rough forging hole 210.
[0057] The lying forging parameters are the increase of the thermal coefficient and the draft angle, and specifically, the size of the blade tip lying forging aggregation piece model is overall enlarged based on the thermal coefficient. The reason for increasing the thermal coefficient is that the material needs to be heated during the process of putting the blanking piece or the aggregation piece into the mold for forging, and the size of the aggregation piece will increase after heating.
[0058] S4, it is judged whether the blade root blanking part on the blade tip lying forging aggregation piece model satisfies the lying forging local upsetting first rule, if yes, the lying forging parameters are added to the target lying forging aggregation piece model to obtain the shape of the target lying forging aggregation piece rough forging hole 410; otherwise, the next step is entered.
[0059] Whether the lying forging local upsetting first rule is satisfied refers to whether the ratio of the length and the diameter of the blade root blanking part is less than 3, if yes, the lying forging local upsetting first rule is satisfied.
[0060] S5, the part of the volume of the blade root blanking part on the blade tip lying forging aggregation piece model is adjusted to be unchanged, and the shaft diameter is increased by M times to obtain an intermediate lying forging aggregation piece model, the lying forging parameters are added to the intermediate lying forging aggregation piece model to obtain the shape of the intermediate lying forging aggregation piece rough forging hole 310, and the intermediate lying forging aggregation piece model is taken as a new blade tip lying forging aggregation piece model, and then the step S4 is returned until the blade root blanking part on the new blade tip lying forging aggregation piece model satisfies the lying forging local upsetting first rule and then the next step is entered.
[0061] When the ratio of the length and the diameter of the blade root blanking part is greater than 3, due to the limitation of the forging machine or the material, etc., the blade root lying forging aggregation shape cannot be formed by one-time forging, so multiple times of forging are needed.
[0062] Specifically, 1.10≤M≤1.25.
[0063] S6, one sub-mold is prepared based on each rough forging hole shape, and all the sub-molds constitute a mold group of the lying forging aggregation piece rough.
[0064] The die design method of the high-temperature alloy blade lying forging aggregate blank of the embodiment can design each sub-die at each step of blanking to lying forging aggregate blank, and the shape of the blank hole of each sub-die is the same as the shape and size finally generated at the step of forging, so that no waste is generated by using the above-mentioned sub-die at each step of forging, and the forging step is simplified.
[0065] The punch hole of the sub-die prepared based on the shape of the blade tip lying forging aggregate blank hole 210 is coaxially provided with the first punch containing hole 200 and the blade tip lying forging aggregate blank hole 210 in sequence, and the blade tip end of the blade tip lying forging aggregate blank hole 210 is in communication with the first punch containing hole 200; the punch hole of the sub-die prepared based on the shape of the intermediate lying forging aggregate blank hole 310 is coaxially provided with the first rear top position containing hole 300 and the intermediate lying forging aggregate blank hole 310 in sequence, and the blade tip end of the intermediate lying forging aggregate blank hole 310 is in communication with the first rear top position containing hole 300; the punch hole of the sub-die prepared based on the shape of the target lying forging aggregate model blank hole 410 is coaxially provided with the second rear top position containing hole 400, the target lying forging aggregate model blank hole 410 and the second punch containing hole 420 in sequence, the blade tip end of the intermediate lying forging aggregate blank hole 310 is in communication with the second rear top position containing hole 400, and the blade root end of the intermediate lying forging aggregate blank hole 310 is in communication with the second punch containing hole 420.
[0066] The lengths of the punch containing hole and the rear top position containing hole can be specifically set according to different materials.
[0067] In addition, the die set prepared by the method of the embodiment is handed over to a contract manufacturing enterprise for preparation, and then the subsequent preparation is prepared by the enterprise, which can shorten the preparation period of the enterprise. In the process of shortening the preparation period, the final blade structure can be protected from being disclosed, and the protection of technical secrets is realized.
[0068] In one of the embodiments, each sub-die includes an upper die block and a lower die block, the first punch slot is provided through the bottom of the upper die block, the second punch slot is provided on the top of the lower die block, the first punch slot and the second punch slot are opposite in opening, and the first punch slot and the second punch slot constitute a punch hole after the upper die block and the lower die block are aligned and abutted.
[0069] Specifically, the upper die and the lower die of each sub-die are provided with fastening members that can be matched and installed.
[0070] In a specific embodiment, the die set for the lying forging aggregate blank of the A blade as shown in FIG. 1 is designed with the raw material brand of Inconel 718, the standard of AMS 5662, and the finish of Ra 0.40 (μm). Figure 1 The die design method of the high-temperature alloy blade lying forging aggregate blank of the embodiment can design each sub-die at each step of blanking to lying forging aggregate blank, and the shape of the blank hole of each sub-die is the same as the shape and size finally generated at the step of forging, so that no waste is generated by using the above-mentioned sub-die at each step of forging, and the forging step is simplified.
[0071] The mold set design method of the high-temperature alloy blade's upsetting aggregate blank in the embodiment is carried out in SolidWorks, and includes the following steps:
[0072] (1) a three-dimensional model of the A blade is established as shown in the figure, Figure 1 and a A blade forging model is constructed according to the three-dimensional model of the A blade as shown in the figure. Figure 2
[0073] (2) as shown in the figures, Figure 3 and Figure 4 a plurality of different sections are selected on the A blade forging model in the axial direction, the areas of the sections are calculated, the sections are converted into circles with equal areas, and the circles are combined in sequence to form an A blade upsetting aggregate model as shown in the figure. Figure 5
[0074] (3) the volume of the A blade upsetting aggregate model is calculated, a blanking piece model is constructed with the axial diameter of the blade body upsetting aggregate part 110 of the A blade upsetting aggregate model as the diameter and the ratio of the volume of the A blade upsetting aggregate model to the axial diameter of the blade body upsetting aggregate part 110 as the length as shown in the figure. Figure 6
[0075] (4) after the blade tip blanking part of the blanking piece model is constructed into a structure with the same shape and size as the blade tip upsetting aggregate part 100, a blade tip upsetting aggregate model is obtained as shown in the figure. Figure 7 The overall size of the blade tip upsetting aggregate model is adjusted to be expanded by 1.012 times, and a draft angle is added to obtain the shape of the blade tip upsetting aggregate blank forging hole 210.
[0076] (5) it is judged whether the ratio of the length to the diameter of the blade root blanking part on the blade tip upsetting aggregate model is less than 3, if yes, the A blade upsetting aggregate model is added with upsetting parameters to obtain the shape of the A blade upsetting aggregate blank forging hole. Otherwise, the next step is entered.
[0077] (6) the partial volume of the blade root blanking part on the blade tip upsetting aggregate model is adjusted to be unchanged, and the axial diameter is increased by 1.12 times to obtain an intermediate upsetting aggregate model as shown in the figure. Figure 8 The intermediate upsetting aggregate model is added with upsetting parameters to obtain the shape of the intermediate upsetting aggregate blank forging hole 310, and the intermediate upsetting aggregate model is taken as a new blade tip upsetting aggregate model and returned to step (5) until the blade root blanking part on the new blade tip upsetting aggregate model satisfies the upsetting local upsetting first rule and enters the next step.
[0078] (8) one sub-mold is prepared based on each blank forging hole shape, and all the sub-molds constitute the mold set of the upsetting aggregate blank. Among them, the lower mold of the sub-mold prepared based on the shape of the blade tip upsetting aggregate blank forging hole 210 is as shown in the figure.Figure 9 As shown in the figure, the upper die is as shown in the figure Figure 10 As shown in the figure, the lower die of one of the sub-dies prepared based on the shape of the intermediate upsetting aggregate blank forging hole 310 is as shown in the figure Figure 11 As shown in the figure, the upper die is as shown in the figure Figure 12 As shown in the figure, the lower die of one of the sub-dies prepared based on the shape of the intermediate upsetting aggregate blank forging hole 310 is as shown in the figure Figure 13 As shown in the figure, the upper die is as shown in the figure Figure 14 As shown in the figure.
[0079] The die set design method of the high-temperature alloy blade upsetting aggregate blank of the present embodiment can design the sub-die for each step of the blanking piece to the upsetting aggregate blank, and the shape of the blank forging hole of each sub-die is the same as the shape and size finally generated in the step of forging, so that the sub-die in the forging process will not produce waste, and the forging process can be simplified.
[0080] The above-described embodiments only express several embodiments of the present application, and the description is more specific and detailed, but it cannot be understood as limiting the scope of the patent of the present application. It should be noted that for ordinary skilled in the art, without departing from the concept of the present application, a number of modifications and improvements can be made, which are all within the scope of protection of the present application. Therefore, the scope of protection of the present application should be subject to the appended claims.
Claims
1. A method for designing a die assembly for a horizontal forging blank of a high-temperature alloy blade, characterized in that, The design process using 3D software includes the following steps: S1. Construct a target horizontal forging aggregate model based on the target blade model. The target horizontal forging aggregate model includes a blade tip horizontal forging aggregate (100), a blade body horizontal forging aggregate (110), and a blade root horizontal forging aggregate (120). S2. Based on the target horizontal forging aggregate model, determine the size of the blanking part model and divide the blanking part model into the blade tip blanking part, the blade body blanking part and the blade root blanking part; The blanking part model is cylindrical, and the volumes of the blade tip blanking part, the blade body blanking part, and the blade root blanking part are equal to the volumes of the blade tip horizontal forging gathering part (100), the blade body horizontal forging gathering part (110), and the blade root horizontal forging gathering part (120), respectively. S3. After constructing the blade tip blanking part of the blanking part model into a structure with the same shape and size as the blade tip horizontal forging gathering part (100), a blade tip horizontal forging gathering part model is obtained. Horizontal forging parameters are added to the blade tip horizontal forging gathering part model to obtain the shape of the blade tip horizontal forging gathering part blank forging hole (210). Increasing the horizontal forging parameters increases the thermal coefficient and draft angle; S4. Determine whether the blade root blanking part on the blade tip horizontal forging aggregate model meets the first rule of local upsetting in horizontal forging. If yes, add horizontal forging parameters to the target horizontal forging aggregate model to obtain the shape of the forging hole of the target horizontal forging aggregate blank; otherwise, proceed to the next step. The first rule for local upsetting in horizontal forging refers to the ratio of the length to the diameter of the blade root blank being less than 3; S5. Adjust the volume of the blade root blanking part on the blade tip horizontal forging aggregate model to remain unchanged, increase the shaft diameter by M times to obtain the intermediate horizontal forging aggregate model, add horizontal forging parameters to the intermediate horizontal forging aggregate model to obtain the shape of the forging hole (310) of the intermediate horizontal forging aggregate blank, and return to step S4 after using the intermediate horizontal forging aggregate model as the new blade tip horizontal forging aggregate model until the blade root blanking part on the new blade tip horizontal forging aggregate model meets the first rule of horizontal forging local upsetting and then proceed to the next step; 1.10≤M≤1.25; S6. Prepare a sub-mold based on the shape of each blank forging hole, and all sub-molds constitute a mold group for horizontal forging aggregate blanks.
2. The die assembly design method for horizontal forging of high-temperature alloy blade blanks according to claim 1, characterized in that, The process of constructing the target horizontal forging assembly model based on the target blade model includes the following steps: S11. Construct the target blade forging model based on the target blade model; S12. Select several different sections axially on the target blade forging model and calculate the area of each section; S13. Convert each cross section into a circle with equal area and combine each circle axially in sequence to form the target horizontal forging assembly model.
3. The die assembly design method for horizontal forging of high-temperature alloy blade blanks according to claim 1, characterized in that, The dimensions of the blanking part model are based on the diameter of the blade horizontal forging agglomeration part (110) of the target horizontal forging agglomeration part model as the blanking part diameter, and the blanking part length is calculated by the cylinder volume formula using the volume of the target horizontal forging agglomeration part model and the diameter of the blade horizontal forging agglomeration part (110).
4. The method for designing a die assembly for a horizontally forged aggregate blank of a high-temperature alloy blade according to any one of claims 1 to 3, characterized in that, The punching holes of the sub-mold prepared based on the shape of the forging hole (210) of the blade tip horizontal forging aggregate blank are arranged coaxially with the first punch receiving hole (200) and the blade tip horizontal forging aggregate blank forging hole (210). The blade tip end of the blade tip horizontal forging aggregate blank forging hole (210) is connected to the first punch receiving hole (200). The stamping holes of the sub-mold prepared based on the shape of the forging hole (310) of the intermediate horizontal forging aggregate blank are sequentially and coaxially provided with the first rear top receiving hole (300) and the intermediate horizontal forging aggregate blank forging hole (310). The tip end of the intermediate horizontal forging aggregate blank forging hole (310) is connected to the first rear top receiving hole (300). The sub-mold, prepared based on the shape of the forging hole (410) of the target horizontal forging aggregate model blank, has a second rear top receiving hole (400), the target horizontal forging aggregate model blank forging hole (410), and the second punch receiving hole (420) arranged coaxially in sequence. The tip end of the blade of the intermediate horizontal forging aggregate blank forging hole (310) is connected to the second rear top receiving hole (400), and the root end of the blade of the intermediate horizontal forging aggregate blank forging hole (310) is connected to the second punch receiving hole (420).
5. The die assembly design method for horizontal forging of high-temperature alloy blade blanks according to claim 4, characterized in that, Each sub-mold includes an upper module and a lower module. The bottom of the upper module is provided with a first stamping groove, and the top of the lower module is provided with a second stamping groove. The openings of the first stamping groove and the second stamping groove are opposite each other. After the upper module and the lower module are aligned and abutted together, the first stamping groove and the second stamping groove form a stamping hole.
Citation Information
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