阅读说明：本技术 一种钛合金横孔的激光选区熔化无支撑成形方法 (Laser selective melting support-free forming method for titanium alloy transverse hole ) 是由 于永泽 何江涛 董蓉桦 王乐 于 2020-06-05 设计创作，主要内容包括：本发明一种钛合金横孔的激光选区熔化无支撑成形方法,对含有横孔结构的三维模型进行缺陷检测,对检测出缺陷进行修复后,得到修复后的有横孔结构的三维模型；确定修复后的有横孔结构的三维模型的摆放位置,不对横孔结构添加工艺支撑；设定激光选区熔化工艺参数,在设定的激光选区熔化工艺参数控制下,对模型进行分层切片处理,得到分层切片后的横孔结构的三维模型；将分层切片后的横孔结构的三维模型导入到激光选区熔化成形设备,采用钛合金粉末,通过在基板上逐层铺粉与激光选区熔化的方式,完成横孔结构的无支撑成形,得到成形零件；步骤四、对成形零件进行清理、退火热处理及线切割,最终得到含有横孔结构的钛合金零件,实现无支撑成形。(The invention relates to a laser selective melting unsupported forming method of a titanium alloy transverse hole, which comprises the steps of carrying out defect detection on a three-dimensional model containing a transverse hole structure, and repairing the detected defect to obtain a repaired three-dimensional model with the transverse hole structure; determining the placement position of the repaired three-dimensional model with the transverse hole structure, and adding no process support to the transverse hole structure; setting selective laser melting technological parameters, and carrying out layered slicing treatment on the model under the control of the set selective laser melting technological parameters to obtain a three-dimensional model of the cross hole structure after layered slicing; guiding the three-dimensional model of the cross hole structure subjected to layered slicing into selective laser melting forming equipment, and finishing unsupported forming of the cross hole structure by adopting titanium alloy powder in a mode of spreading powder on a substrate layer by layer and melting in the selective laser melting forming equipment to obtain a formed part; and fourthly, cleaning, annealing heat treatment and linear cutting are carried out on the formed part, and the titanium alloy part with the transverse hole structure is finally obtained, so that the unsupported forming is realized.)

1. A laser selective melting unsupported forming method of a titanium alloy transverse hole is characterized by comprising the following steps:

the method comprises the following steps of firstly, carrying out defect detection on a three-dimensional model with a transverse hole structure, and repairing the detected defects to obtain a repaired three-dimensional model with the transverse hole structure; determining the placement position of the repaired three-dimensional model with the transverse hole structure according to the transverse hole axis and the powder spreading direction in the repaired three-dimensional model with the transverse hole structure, and obtaining the three-dimensional model with the transverse hole structure to be layered without adding process support to the transverse hole structure;

step two, setting selective laser melting technological parameters, and carrying out layered slicing treatment on the three-dimensional model with the transverse hole structure to be layered, which is obtained in the step one, under the control of the set selective laser melting technological parameters to obtain a layered and sliced three-dimensional model with the transverse hole structure;

step three, guiding the three-dimensional model of the cross hole structure subjected to layered slicing into selective laser melting forming equipment, and finishing unsupported forming of the cross hole structure by adopting titanium alloy powder in a mode of spreading powder on a substrate layer by layer and melting in the selective laser melting, so as to obtain a formed part;

and fourthly, cleaning, annealing heat treatment and linear cutting are carried out on the formed part, and finally the titanium alloy part with the transverse hole structure is obtained.

2. The laser selective melting unsupported forming method of a titanium alloy cross bore according to claim 1, characterized in that: the titanium alloy is Ti6Al 4V.

3. The laser selective melting unsupported forming method of a titanium alloy cross bore according to claim 1, characterized in that: the diameter range of the transverse hole structure is 6 mm-15 mm, and the wall thickness is more than 0.6 mm.

4. The laser selective melting unsupported forming method of a titanium alloy cross bore according to claim 1, characterized in that: the model defects that need to be repaired are one or more of the following defects, including: inverted triangular patches, bad edges and false contours, gaps, holes, interfering shells, multiple shells, overlapping and intersecting triangular patches.

5. The laser selective melting unsupported forming method of a titanium alloy cross bore according to claim 1, characterized in that: in the first step, the placing direction of the model is such that the included angle between the axis of the transverse hole and the powder spreading direction is less than 45 degrees.

6. The laser selective melting unsupported forming method of a titanium alloy cross bore according to claim 1, characterized in that: in the third step, the particles of the titanium alloy powderThe degree distribution D10 is 15 mm-25 mm, D50 is 30 mm-40 mm, D90 is 45 mm-55 mm, the fluidity is less than 30s/50g, and the loose packed density is more than 2.2g/cm³Tap density of more than 2.6g/cm³The powder is spherical or approximately spherical and has a mass fraction of not less than 97%.

7. The laser selective melting unsupported forming method of a titanium alloy cross bore according to claim 1, characterized in that: in the third step, a metal scraper is used for powder paving; the selective laser melting process is carried out in an argon atmosphere protective environment; and cooling the formed part to room temperature in the forming chamber after the formed part is processed.

8. The selective laser melting unsupported forming method for titanium alloy cross bore according to claim 1, wherein in the fourth step, the floating powder on the inner and outer surfaces of the formed part is cleaned up by using a high pressure air gun and then is subjected to annealing heat treatment together with the substrate, and the heat treatment process parameter is that the vacuum degree is lower than 2 × 10^-2Pa, the temperature is 750-850 ℃, the heat preservation time is 4-6 h, and the furnace cooling is carried out.

9. The laser selective melting unsupported forming method of a titanium alloy cross bore according to claim 1, characterized in that: laser selective melting forming data preparation software, preferably Magics software.

10. The laser selective melting unsupported forming method of a titanium alloy cross bore according to claim 1, characterized in that: the three-dimensional model containing the transverse hole structure is imported into the laser selection melting forming data preparation software, and the file format of the three-dimensional model is a Standard Triangle Language (STL) file.

Technical Field

The invention relates to a selective laser melting and unsupported forming method for a titanium alloy transverse hole, and belongs to the technical field of selective laser melting and forming.

Background

The titanium alloy valve body type part containing the complex inner flow passage structure needs to realize high-pressure transmission and effective regulation and control of different medium fluids in a limited space, has higher requirements on the shape and performance indexes of an inner cavity, and is a core connecting part of precision control and power units in the fields of aerospace, nuclear power military industry and the like. The existing titanium alloy valve body manufacturing process mainly comprises casting, die forging, machining and welding, and due to material characteristics and process constraints, the valve body structure has to adopt a structural form with a simple inner cavity and a regular shape, and meanwhile, the defects of multiple processing procedures, low utilization rate of raw materials, difficulty in controlling process quality and the like exist.

The Selective Laser Melting (SLM) forming technique uses high-energy Laser as a heat source, and by selectively Melting metal powder bed regions, processes layer-by-layer stacking, and further realizes the processing and forming of any complex three-dimensional structure. The technology frees the traditional process constraint, further improves the material use efficiency, and provides possibility for the structure and function integrated design and manufacture of valve body parts. However, because the structure of the flow channel in the valve body part is complex, a horizontal hole structure still exists by adjusting the placing posture of the model. When the SLM is formed, an auxiliary supporting structure needs to be added to a transverse hole structure with the diameter exceeding 6mm, or the cross section of a round hole is changed into a water-drop shape, so that the suspended feature is stacked and formed, and the risk of warping and deformation of parts is reduced. The auxiliary support is added, so that an auxiliary support structure in the complex flow channel cannot be removed, and the original design performance of the valve body flow channel is changed by modifying the cross section shape of the flow channel.

Therefore, it is a problem to be solved by those skilled in the art to find a laser selective melting unsupported forming method capable of realizing a titanium alloy cross-hole structure, and to provide a manufacturing application with optimal structural design results for a valve body.

Disclosure of Invention

The technical problem solved by the invention is as follows: the defects of the prior art are overcome, the laser selective melting unsupported forming method of the titanium alloy transverse hole is provided, and the integral unsupported manufacturing forming of the complex inner runner structure is realized.

The technical scheme of the invention is as follows: a laser selective melting unsupported forming method of a titanium alloy transverse hole comprises the following steps:

the method comprises the following steps of firstly, carrying out defect detection on a three-dimensional model with a transverse hole structure, and repairing the detected defects to obtain a repaired three-dimensional model with the transverse hole structure; determining the placement position of the repaired three-dimensional model with the transverse hole structure according to the transverse hole axis and the powder spreading direction in the repaired three-dimensional model with the transverse hole structure, and obtaining the three-dimensional model with the transverse hole structure to be layered without adding process support to the transverse hole structure;

step two, setting selective laser melting technological parameters, and carrying out layered slicing treatment on the three-dimensional model with the transverse hole structure to be layered, which is obtained in the step one, under the control of the set selective laser melting technological parameters to obtain a layered and sliced three-dimensional model with the transverse hole structure;

step three, guiding the three-dimensional model of the cross hole structure subjected to layered slicing into selective laser melting forming equipment, and finishing unsupported forming of the cross hole structure by adopting titanium alloy powder in a mode of spreading powder on a substrate layer by layer and melting in the selective laser melting, so as to obtain a formed part;

and fourthly, cleaning, annealing heat treatment and linear cutting are carried out on the formed part, and finally the titanium alloy part with the transverse hole structure is obtained.

Preferably, the titanium alloy is Ti6Al 4V.

Preferably, the diameter of the transverse hole structure ranges from 6mm to 15mm, and the wall thickness is more than 0.6 mm.

Preferably, the model defect to be repaired is one or more of the following defects: inverted triangular patches, bad edges and false contours, gaps, holes, interfering shells, multiple shells, overlapping and intersecting triangular patches.

Preferably, in the first step, the placing direction of the model is such that the included angle between the axis of the transverse hole and the powder spreading direction is less than 45 degrees.

Preferably, in the third step, the titanium alloy powder has a particle size distribution D10 (diameter range corresponding to particles with volume content of 10% in the powder particle size cumulative distribution diagram) of 15-25 mm, a particle size distribution D50 (diameter range corresponding to particles with volume content of 50% in the powder particle size cumulative distribution diagram) of 30-40 mm, a particle size distribution D90 (diameter range corresponding to particles with volume content of 90% in the powder particle size cumulative distribution diagram) of 45-55 mm, a flowability of less than 30s/50g, and a loose packed density of more than 2.2g/cm³Tap density of more than 2.6g/cm³The powder is spherical or approximately spherical and has a mass fraction of not less than 97%.

Preferably, in the third step, a metal scraper is used for powder paving; the selective laser melting process is carried out in an argon atmosphere protective environment; and cooling the formed part to room temperature in the forming chamber after the formed part is processed.

Preferably, in the fourth step, floating powder on the inner surface and the outer surface of the formed part is cleaned by using a high-pressure air gun and then is subjected to annealing heat treatment together with the substrate, wherein the heat treatment process parameter is that the vacuum degree is lower than 2 × 10^-2Pa, the temperature is 750-850 ℃, the heat preservation time is 4-6 h, and the furnace cooling is carried out.

Preferably, the laser selective melting formation data preparation software is Magics software.

Preferably, the three-dimensional model containing the transverse hole structure introduced into the laser selective melting and forming data preparation software is in a Standard Triangle Language (STL) file format.

Compared with the prior art, the invention has the beneficial effects that:

(1) according to the process principle and the forming characteristics of the selective laser melting forming technology, the unsupported printing forming of the titanium alloy cross hole structure with the diameter of 6-15 mm is realized by optimizing the placing direction of the cross hole structure, and the problem that the supporting structure in the cross hole is difficult to remove is solved.

(2) The method adopts a linear cross entity scanning strategy of interlayer rotation of 30-90 degrees, improves the support strength of the entity structure around the overhung surface of the transverse hole, effectively reduces the buckling deformation of the edge of the entity, and realizes the support-free forming of the arc overhung surface of the titanium alloy transverse hole with the diameter of 6-15 mm in the forming process.

(3) According to the titanium alloy cross hole laser selective melting support-free forming method, the support-free direct forming of the hole structure in the horizontal direction is adopted, the capacity of forming the pipeline structure by the laser selective melting technology is improved, and a solution is provided for realizing support-free integral forming of the complicated inner flow passage structure of the valve body part.

Drawings

FIG. 1 is a flow chart of a forming method provided by the present invention;

fig. 2 is a schematic view of the structure and the placement direction of the present invention.

Detailed Description

The invention is described in further detail below with reference to the figures and specific embodiments.

The invention relates to a laser selective melting unsupported forming method of a titanium alloy transverse hole, which comprises the following steps of firstly, carrying out defect detection on a three-dimensional model containing a transverse hole structure, and repairing the detected defect to obtain a repaired three-dimensional model with the transverse hole structure; determining the placement position of the repaired three-dimensional model with the transverse hole structure according to the transverse hole axis and the powder spreading direction in the repaired three-dimensional model with the transverse hole structure, and adding no process support to the transverse hole structure; step two, setting selective laser melting technological parameters, and carrying out layered slicing treatment on the three-dimensional model with the transverse hole structure repaired in the step one under the control of the set selective laser melting technological parameters to obtain a layered sliced three-dimensional model with the transverse hole structure; step three, guiding the three-dimensional model of the cross hole structure subjected to layered slicing into selective laser melting forming equipment, and finishing unsupported forming of the cross hole structure by adopting titanium alloy powder in a mode of spreading powder on a substrate layer by layer and melting in the selective laser melting, so as to obtain a formed part; and fourthly, cleaning, annealing heat treatment and linear cutting are carried out on the formed part, and finally the titanium alloy part with the transverse hole structure is obtained.

The valve body with the multi-channel structure integrates structural design and functions and is a key part in a pipeline precision control unit. The method is limited by the feasibility of the traditional manufacturing process, the optimal configuration of the flow passage structure in the valve body cannot be realized, only a simple form of plane layout and straight hole connection can be adopted, the processing procedure is complex, the utilization rate of raw materials is low, and the process quality is difficult to control.

The Selective Laser Melting (SLM) forming technology has the characteristics of high forming freedom degree, quick response and high material utilization rate, gets rid of the constraint of a die and a tool, and provides possibility for directly forming valve body parts with complicated inner flow passage structures such as arc bending and three-dimensional layout. However, for a complicated inner runner structure with the diameter larger than 6mm, the following technical problems exist in the selective laser melting forming process: (1) a process support needs to be added into the transverse hole structure, and the support structure inside the bent transverse hole cannot be removed; (2) the cross section of the cross hole is changed into a water drop shape, so that the optimal structural design and function realization of the valve body flow passage cannot be realized.

According to the laser selective melting and support-free forming method for the titanium alloy cross hole, provided by the invention, the support-free laser selective melting and forming of the titanium alloy cross hole structure with the diameter of 6-15 mm can be realized by optimizing the arrangement direction of the cross hole structure and adopting a linear crossed entity scanning strategy of interlayer rotation of 30-90 degrees, and a solution is provided for support-free integral forming of a complex inner flow channel structure of a valve body part.

As shown in FIG. 1, a laser selective melting unsupported forming method for titanium alloy transverse holes, which preferably comprises the following steps:

the method comprises the following steps of firstly, carrying out defect detection on a three-dimensional model with a transverse hole structure, and repairing the detected defects to obtain a repaired three-dimensional model with the transverse hole structure; determining the placement position of the repaired three-dimensional model with the transverse hole structure according to the transverse hole axis and the powder spreading direction in the repaired three-dimensional model with the transverse hole structure, and obtaining the three-dimensional model with the transverse hole structure to be layered without adding process support to the transverse hole structure; the preferred scheme is as follows:

the defect detection is preferably performed by introducing the three-dimensional model having the transverse hole structure into laser selective melting molding data preparation software.

A cross-bore structure defined as: and after the forming direction and the placing position of the model are determined, the holes with the axes vertical to the layer-by-layer stacking and height increasing direction (the Z direction shown in figure 2) of the molten material in the selected laser area are formed.

As shown in fig. 2, the Z direction refers to: in the process of forming the materials by stacking layer by layer, the normal direction of the layers, namely the direction of the first layer pointing to the subsequent layer.

The powder spreading direction is as follows: the front side of the selective laser melting device is seen, and the front side faces the left-to-right direction and the right-to-left direction of the forming space.

According to the embodiment of the model structure shown in fig. 2, a three-dimensional model containing a cross-hole structure is preferably, but not limited to, established by using three-dimensional modeling software; and after modeling is completed, converting the three-dimensional model containing the transverse hole structure into a Standard Triangle Language (STL) file which can be identified by laser selective melting modeling data preparation software Magics.

The model has the problems of surface precision reduction and structural body information loss in the conversion process. Therefore, after the three-dimensional model with the transverse hole structure is introduced into the selective laser melting formation data preparation software Magics, the three-dimensional model with the transverse hole structure needs to be automatically detected for defects, and the specific detection contents are as follows: inverted triangular patches, bad edges and false contours, gaps, holes, interfering shells, multiple shells, overlapping and intersecting triangular patches.

And automatically repairing the detected model defects correspondingly.

And after the repairing is finished, automatically detecting and repairing the defects of the three-dimensional model containing the transverse hole structure again. Repeating the detection and repair process until the detection result shows that: the whole model has no reverse triangular surface patch, bad edge and wrong contour, gap, hole, overlapped and crossed triangular surface patch, 1 shell, no interference shell and multiple shells. At this time, the repair of the three-dimensional model with the transverse hole structure is completed, and the repaired three-dimensional model with the transverse hole structure is obtained. The probability of errors of the repaired three-dimensional model in the subsequent layering process is lower, and the printing success rate of the transverse hole structure is improved.

According to the transverse hole axis and the powder spreading direction in the repaired three-dimensional model with the transverse hole structure, the placement position of the repaired three-dimensional model with the transverse hole structure is determined, and the method specifically comprises the following steps: setting the powder spreading direction as the left-to-right and right-to-left directions (the powder spreading direction shown in fig. 2) when the powder spreading direction is seen from the front of the selective laser melting equipment and faces the forming space; the relationship between the axis of the transverse hole and the powder spreading direction is as follows: the direction from left to right facing the forming space is designated as the forward dusting direction as viewed from the front of the selective laser melting apparatus, and the angle between the axis of the transverse bore and the forward dusting direction is preferably less than 40 °. In the selective laser melting and forming process, the smaller the included angle between the axis of the transverse hole and the forward powder spreading direction is, and the smaller the contact area between the formed solid structure and the metal scraper is in the powder spreading process. When the overhanging part of the row of the transverse hole structure is formed, the formed solid structure is not easy to be damaged by the metal scraper, and the smooth forming without support of selective laser melting of the transverse hole structure is further ensured.

The method does not add process support to the transverse hole structure, and specifically comprises the following steps: original structural characteristics inside the cross hole structure are kept, and process supports connected with the lower surface of the cross hole are not added to the suspended part of the upper surface of the cross hole.

Step two, setting selective laser melting technological parameters, and carrying out layered slicing treatment on the three-dimensional model with the transverse hole structure to be layered, which is obtained in the step one, under the control of the set selective laser melting technological parameters to obtain a layered and sliced three-dimensional model with the transverse hole structure; the preferred scheme is as follows:

setting the melting technological parameters of the selected laser area, which specifically comprises the following steps: the preferred laser power of entity scanning is 380W-420W, the preferred speed of entity scanning is 1000-1200 mm/s, the preferred interval of entity scanning is 0.06-0.09 mm, the preferred scanning strategy is a linear scanning mode of interlayer rotation 60-90 degrees, the preferred laser power of outline scanning is 180-230W, the preferred speed of outline scanning is 1300-1500 mm/s, and the preferred thickness of layering is 0.04-0.06 mm, so as to improve the forming quality.

As the titanium alloy powder is subjected to periodic, violent, unstable and cyclic heating and cooling of the laser beam in the selective laser melting forming process, the formed solid structure has larger thermal stress, the formed solid structure is warped and cracked, and the unsupported forming failure of the transverse hole structure is caused. The invention adopts a linear scanning mode of interlayer rotation of 60-90 degrees, can effectively balance the interlayer stress of a formed entity, reduce the buckling deformation amount of the edge of the entity, improve the self-supporting strength of the entity structure around the overhanging surface of the transverse hole structure and realize the laser selective melting and unsupported forming of the transverse hole structure.

Taking the titanium alloy cross-hole structure shown in fig. 2 as an example, when a thick-wall large-diameter cross-hole structure with the wall thickness of more than 1mm and the cross-hole diameter of more than 15mm is to be formed in a selective laser melting mode, the setting parameters are preferably as follows: the parameters of the entity scanning laser power are preferably 380W-400W, the entity scanning speed is preferably 1000-1100 mm/s, the entity scanning interval is preferably 0.06-0.075 mm, the preferred scanning strategy is a linear scanning mode with 80-90 degrees of interlayer rotation, the profile scanning laser power is preferably 180-200W, the profile scanning speed is preferably 1300-1400 mm/s, the layering thickness is preferably 0.04-0.05 mm, and the forming quality is further improved.

When a thin-wall small-diameter transverse hole structure with the diameter of a transverse hole being more than 6mm and less than 10mm and the wall thickness being more than 0.6mm and less than 1mm is to be subjected to selective laser melting and unsupported forming, the set optimal parameters are as follows: the preferred physical scanning laser power is 410W-420W, the preferred physical scanning speed is 1000-1200 mm/s, the preferred physical scanning interval is 0.08-0.09 mm, the preferred scanning strategy is a linear scanning mode of interlayer rotation of 60-80 degrees, the preferred contour scanning laser power is 210-230W, the preferred contour scanning speed is 1300-1500 mm/s, the preferred layering thickness is 0.05-0.06 mm, and the forming quality is further improved.

Carrying out layered slicing treatment on the three-dimensional model with the cross hole structure to be layered obtained in the step one, wherein the specific requirements of the layered slicing are as follows: according to the set layering thickness value, layering and slicing the three-dimensional model with the transverse hole structure to be layered along the Z direction shown in figure 2; and obtaining the laser scanning path and power data of the profile scanning and the entity filling of each layer according to the profile and the entity section information of each layer after slicing and the set relevant process parameters.

Step three, guiding the three-dimensional model of the cross hole structure subjected to layered slicing into selective laser melting forming equipment, and finishing unsupported forming of the cross hole structure by adopting titanium alloy powder in a mode of spreading powder on a substrate layer by layer and melting in the selective laser melting, so as to obtain a formed part; the preferred scheme is as follows:

the preferable scheme of the selection of the titanium alloy powder is as follows: the titanium alloy powder has a particle size distribution D10 (diameter range corresponding to particles with volume content of 10% in the powder particle size cumulative distribution diagram) of 15-25 mm, D50 (diameter range corresponding to particles with volume content of 50% in the powder particle size cumulative distribution diagram) of 30-40 mm, D90 (diameter range corresponding to particles with volume content of 90% in the powder particle size cumulative distribution diagram) of 45-55 mm, fluidity of less than 30s/50g, and loose packing density of more than 2.2g/cm³Tap density of more than 2.6g/cm³The powder is spherical or approximately spherical, the mass fraction is not less than 97%, and the forming quality is further improved.

The method comprises the following steps of completing the unsupported forming of a transverse hole structure by a mode of spreading powder layer by layer on a substrate and melting in a selective laser area, and specifically comprises the following steps: importing the three-dimensional model of the cross hole structure after layered slicing into control software of selective laser melting forming equipment; argon with the purity of 99.999 percent is filled into equipment for spreading powder layer by layer and melting in a selective laser area; preferably, when the oxygen content in the equipment is stabilized below 1000ppm, a layer of flat titanium alloy powder is laid on the surface of the substrate by the metal scraper, laser scans according to the section information of the current layer, the titanium alloy powder in the scanning area is melted and solidified under the action of the laser to form a solid structure, then the substrate is lowered by one layer thickness, a layer of new titanium alloy powder is laid by the metal scraper, and the new titanium alloy powder is scanned again by the laser to be melted and formed, so that the reciprocating circulation is performed, and the unsupported forming of the transverse hole structure is finally completed through layer-by-layer superposition, so that a formed part is obtained, and the forming quality is further improved.

Step four, cleaning, annealing heat treatment and linear cutting are carried out on the formed part, and finally the titanium alloy part with the transverse hole structure is obtained, wherein the preferable scheme is as follows:

cleaning, annealing heat treatment and wire cutting are carried out on the formed part, the preferable scheme is that compressed air with the pressure of 0.5-0.8 MPa is preferably used for repeatedly carrying out gas flushing on the surface of the formed part and the interior of the transverse hole until no floating powder exists on the surface of the part and the interior of the transverse hole, the formed part and the substrate are placed into a vacuum annealing furnace, and the preferable scheme is that when the vacuum degree in the furnace is lower than 2 × 10^-2Heating is started after Pa, the heating time is preferably 75-85 minutes, the temperature is preferably raised to 750-850 +/-10 ℃, the heat preservation time is preferably 4-6 hours, and the air is preferably taken after the furnace is cooled to below 150 ℃; the method comprises the steps of adopting slow-running wire cut electrical discharge machining with the flushing pressure of 0.6-1.0 MPa preferably, the pulse interval of 20-30 mus preferably, the pulse width of 15-25 mus preferably, the open circuit voltage of 90-110V preferably, the peak current of 20-30A preferably, the diameter of 0.2mm brass wire preferably, the wire running speed of 100-110 mm/s preferably, and the wire tension of 8-12N preferably, cutting and separating the part from a substrate at a position 0-2 mm away from the upper surface of the substrate preferably, finally obtaining the titanium alloy part with the transverse hole structure, and further improving the final quality of the part.

The invention realizes the further proposal of improving the mechanical property of the transverse hole structure: let the laser power of the physical scan be P₁And the entity scanning interval is L, the layering thickness is H, and when the optimization meets the following requirements:

0.7＜P₁/(L×H×10⁶)＜1.5

under the preferable constraint conditions, the compactness of the titanium alloy transverse hole structure part formed by selective laser melting can reach more than 99.57%, the yield strength of the product can reach 962MPa, the tensile strength can reach 1031MPa, the elongation rate is close to 17%, and the mechanical property of the titanium alloy transverse hole structure formed by selective laser melting without support can be effectively improved.

The invention realizes the further proposal of improving the surface roughness of the transverse hole structure: let the laser power of the physical scan be P₁The physical scanning speed is V₁And the entity scanning interval is L, the layering thickness is H, and when the optimization meets the following requirements:

0.22＜(0.865P₁×V₁×L)/(7.8π×H²×10⁶)＜1

when the optimal constraint condition is adopted, the roughness of the overhanging surface of the titanium alloy transverse hole structure formed by selective laser melting can reach Ra 15, and the further improvement of the surface roughness of the titanium alloy transverse hole structure formed by selective laser melting without support can be realized.

According to the process principle and the forming characteristics of the selective laser melting forming technology, the unsupported printing forming of the diameter titanium alloy transverse hole structure is realized by optimizing the arrangement direction of the transverse hole structure, and the problem that the support structure in the transverse hole is difficult to remove is solved. And a linear crossed entity scanning strategy of interlayer rotation is adopted, so that the supporting strength of the entity structure around the overhung surface of the transverse hole is improved, the buckling deformation of the edge of the entity is effectively reduced, and the unsupported forming of the arc overhung surface of the titanium alloy transverse hole in the forming process is realized.

According to the titanium alloy cross hole laser selective melting support-free forming method, the support-free direct forming of the hole structure in the horizontal direction is adopted, the capacity of forming the pipeline structure by the laser selective melting technology is improved, and a solution is provided for realizing support-free integral forming of the complicated inner flow passage structure of the valve body part.