阅读说明：本技术 一种NiAl合金复杂薄壁中空构件的成形方法 (Forming method of NiAl alloy complex thin-wall hollow component ) 是由 王东君 刘钢 苑世剑 于 2020-07-09 设计创作，主要内容包括：本发明涉及中空构件成形技术领域,尤其涉及一种NiAl合金复杂薄壁中空构件的成形方法。本发明对Ni箔进行热处理,可以降低Ni箔中位错等缺陷密度,降低Ni箔的屈服强度、提高延伸率,优化叠层原料的变形均匀协调性,进而有利于得到壁厚均匀、性能优异的复杂薄壁中空构件；本发明在成形前对第一叠层箔的重叠区进行压制,重叠区的Ni箔和A1箔之间可以形成扩散冶金结合的重叠区叠层箔,在后续成形复杂薄壁中空构件时变形更均匀协调,不容易窜动和分层,成形性能更好；本发明采用错层搭接的方式制备复杂薄壁中空构件,无需焊接,可确保搭接缝成分与构件其他部分成分一致,使用安全可靠性更高,壁厚均匀性更好、构件精度高。(The invention relates to the technical field of hollow member forming, in particular to a forming method of a NiAl alloy complex thin-wall hollow member. According to the invention, the Ni foil is subjected to heat treatment, so that the density of defects such as dislocation and the like in the Ni foil can be reduced, the yield strength of the Ni foil is reduced, the elongation is improved, the deformation uniformity and harmony of the laminated raw materials are optimized, and further, the complex thin-wall hollow component with uniform wall thickness and excellent performance can be obtained; according to the invention, the overlapping region of the first laminated foil is pressed before forming, and the Ni foil and the A1 foil in the overlapping region can form the overlapped region laminated foil combined by diffusion metallurgy, so that the deformation is more uniform and coordinated when a complex thin-wall hollow member is formed subsequently, the shifting and layering are not easy to occur, and the forming performance is better; the invention adopts the staggered lapping way to prepare the complex thin-wall hollow component, does not need welding, can ensure that the composition of the lapping seam is consistent with that of other parts of the component, and has the advantages of higher use safety and reliability, better wall thickness uniformity and high component precision.)

1. A forming method of a NiAl alloy complex thin-wall hollow component is characterized by comprising the following steps:

(1) calculating the thickness ratio of the Ni foil to the A1 foil according to the atomic number ratio of the Ni atoms to the A1 atoms in the NiA1 alloy; determining the actual thickness of the Ni foil and the Al foil according to the calculated thickness ratio of the Ni foil to the A1 foil; carrying out heat treatment on the needed Ni foil to obtain a heat-treated Ni foil; the temperature of the heat treatment is 600-800 ℃, and the time is 30-120 min;

(2) stacking a plurality of the heat-treated Ni foils and a1 foils alternately, and then dividing the resulting laminated foil into two in the thickness direction, with an upper laminated foil on the top and a lower laminated foil on the bottom, the upper and lower laminated foils constituting a first laminated foil; a dislocation exists between the upper laminated foil and the lower laminated foil, and the first laminated foil is divided into an overlapping area and two dislocation areas;

(3) pressing the overlapping area of the first laminated foil to obtain a second laminated foil; the second laminated foil comprises an overlapped area laminated foil formed after the overlapping area is pressed and two parts of staggered area laminated foils positioned on two staggered areas;

(4) and pressing the second laminated foil into a lower die by using a built-in die, overlapping two staggered areas of the second laminated foil around the built-in die, pressing the overlapped second laminated foil by using an upper die, connecting the overlapped areas under the combined action of the upper die, the lower die and the built-in die, and taking out the overlapped areas after forming to obtain the NiAl alloy complex thin-wall hollow component.

2. The forming method as claimed in claim 1, wherein the atomic number ratio of Ni atoms and a1 atoms in the NiA1 alloy in step (1) is 45:55 to 59:41 under a standard atmospheric pressure and room temperature environment.

3. The forming method according to claim 1, wherein the heat treatment in step (1) is performed under vacuum conditions.

4. The forming method according to claim 1, wherein the condition for pressing the overlapping area of the first laminated foil in step (3) includes: vacuum degree of 1.0X 10^-3～5.0×10^-3Pa, the temperature is 550-600 ℃, the pressure is 15-25 MPa, and the pressing time is 0.5-3 h.

5. The forming method according to claim 1, wherein the conditions for pressing the overlapped second laminated foil in the step (4) include: vacuum degree of 1.0X 10^-3～5.0×10^-3Pa, the temperature is 550-600 ℃, the pressure is 15-25 MPa, and the pressing time is 0.5-3 h.

6. The forming method according to claim 1 or 5, wherein in the step (4), the pressing of the second laminated foil into the lower mold using the built-in mold is performed at room temperature and normal atmospheric pressure.

7. The method of claim 1, wherein pressing the second laminated foil into the lower mold further comprises pressing a two-part staggered laminated foil of the second laminated foil.

8. The forming method according to claim 1, wherein the NiAl alloy complex thin-walled hollow member has a wall thickness of 1 to 3 mm.

9. The forming method according to claim 1, wherein a cross-sectional circumference ratio of both end surfaces of the NiAl alloy complex thin-walled hollow member is 1.5 or more.

10. A forming method according to claim 1, 8 or 9, wherein both end faces of the NiAl alloy complex thin-walled hollow member are different in shape.

Technical Field

The invention relates to the technical field of hollow member forming, in particular to a forming method of a NiAl alloy complex thin-wall hollow member.

Background

In the industrial fields of national defense equipment and the like, the closed-section hollow thin-wall type components are widely applied, such as a high-speed aircraft isolation section, an air inlet channel, a spray pipe, an outlet pipe and the like. Because the service temperature is as high as above 800 ℃, the components are often manufactured by adopting high-temperature resistant materials, and the high-temperature resistant alloy material widely applied at present is Ni-based high-temperature alloy.

In recent years, with the further improvement of the flight speed of the aircraft, the service temperature of key components is also greatly improved, and the service temperature of the key components of the new generation of high-speed aircraft reaches the service temperature limit of high-temperature alloy. In addition, the Ni-based high-temperature alloy has high density, and the forced cutting requirement of lightweight and weight reduction of a new generation of aircraft is severely limited. The density of the NiAl alloy is 2/3 of that of the Ni-based high-temperature alloy, the upper limit of the use temperature is expected to reach about 1250 ℃, and the temperature is improved by about 150-200 ℃ compared with the existing Ni-based high-temperature alloy. In addition, the NiAl alloy has high thermal conductivity which is 70-80W/m.K within the range of 20-1100 ℃, is 4-8 times of that of the common Ni-based high-temperature alloy, is applied to a higher Mach number component, and can enhance the active cooling effect besides reducing weight and improving the use temperature. However, the NiAl alloy is difficult to deform, the production cost is high, and the period is long; aiming at the complex thin-wall hollow components, the forming difficulty is particularly outstanding, and the forming precision and the structure performance are difficult to control.

The invention patent with the publication number of CN110142332A provides a forming and property control integrated method for a NiAl alloy thin-wall pipe fitting, which can obtain the NiAl alloy thin-wall pipe fitting, but still has some technical problems to be solved aiming at the preparation and forming of a thin-wall hollow component with a complex shape, such as large change of the shape of a cross section, large change of the perimeter of the cross section and the like. This is mainly reflected in: (1) the deformed Ni foil raw material is not subjected to heat treatment, so that the deformation uniformity and coordination of the Ni/Al laminated foil are reduced, and the member forming performance is further reduced. (2) The welding method is adopted to process the butt joint of the Ni/Al laminated foil pipe, so that a welding seam exists, and the use safety and reliability are reduced; in addition, alloy components in a local area of the welding seam may deviate from the NiAl single-phase area component requirements, material performance difference in an area near the welding seam is caused, and the instability possibility of the welding seam is increased.

Disclosure of Invention

The invention aims to provide a method for forming a NiAl alloy complex thin-wall hollow component, which can form the complex thin-wall hollow component with large change of section shape, large change of section perimeter and the like, has good wall thickness uniformity, good forming uniformity (few defects), high safety and reliability, easy operation, easy automatic production, high component precision and excellent performance, and does not need welding.

In order to achieve the above object, the present invention provides the following technical solutions:

the invention provides a forming method of a NiAl alloy complex thin-wall hollow component, which comprises the following steps:

(1) calculating the thickness ratio of the Ni foil to the A1 foil according to the atomic number ratio of the Ni atoms to the A1 atoms in the NiA1 alloy; determining the actual thickness of the Ni foil and the Al foil according to the calculated thickness ratio of the Ni foil to the A1 foil; carrying out heat treatment on the needed Ni foil to obtain a heat-treated Ni foil; the temperature of the heat treatment is 600-800 ℃, and the time is 30-120 min;

(2) stacking a plurality of the heat-treated Ni foils and a1 foils alternately, and then dividing the resulting laminated foil into two in the thickness direction, with an upper laminated foil on the top and a lower laminated foil on the bottom, the upper and lower laminated foils constituting a first laminated foil; a dislocation exists between the upper laminated foil and the lower laminated foil, and the first laminated foil is divided into an overlapping area and two dislocation areas;

(3) pressing the overlapping area of the first laminated foil to obtain a second laminated foil; the second laminated foil comprises an overlapped area laminated foil formed after the overlapping area is pressed and two parts of staggered area laminated foils positioned on two staggered areas;

(4) and pressing the second laminated foil into a lower die by using a built-in die, overlapping two staggered areas of the second laminated foil around the built-in die, pressing the overlapped second laminated foil by using an upper die, connecting the overlapped areas under the combined action of the upper die, the lower die and the built-in die, and taking out the overlapped second laminated foil after forming to obtain the NiAl alloy complex thin-wall hollow component.

Preferably, the atomic number ratio of the Ni atom to the A1 atom in the NiA1 alloy in step (1) is 45:55 to 59:41 under a standard atmospheric pressure and room temperature environment.

Preferably, the heat treatment in step (1) is performed under vacuum.

Preferably, in the step (3), the pressing conditions for the overlapping area of the first laminated foil include: vacuum degree of 1.0X 10^-3～5.0×10^-3Pa, the temperature is 550-600 ℃, the pressure is 15-25 MPa, and the pressing time is 0.5-3 h.

Preferably, in the step (4), the pressing condition of the overlapped second laminated foil includes: vacuum degree of 1.0X 10^-3～5.0×10^-3Pa, the temperature is 550-600 ℃, the pressure is 15-25 MPa, and the pressing time is 0.5-3 h.

Preferably, in the step (4), the process of pressing the second laminated foil into the lower mold using the built-in mold is performed at room temperature and normal atmospheric pressure.

Preferably, before pressing the second laminated foil into the lower mold, the method further includes pressing the two-part staggered area laminated foil of the second laminated foil.

Preferably, the wall thickness of the NiAl alloy complex thin-wall hollow component is 1-3 mm.

Preferably, the cross-sectional perimeter ratio of the two end surfaces of the NiAl alloy complex thin-walled hollow member is more than 1.5.

Preferably, both end surfaces of the NiAl alloy complex thin-walled hollow member are different in shape.

The invention provides a forming method of a NiAl alloy complex thin-wall hollow component, which comprises the following steps: (1) calculating the thickness ratio of the Ni foil to the A1 foil according to the atomic number ratio of the Ni atoms to the A1 atoms in the NiA1 alloy; determining the actual thickness of the Ni foil and the Al foil according to the calculated thickness ratio of the Ni foil to the A1 foil; carrying out heat treatment on the needed Ni foil to obtain a heat-treated Ni foil; the temperature of the heat treatment is 600-800 ℃, and the time is 30-120 min; (2) stacking a plurality of the heat-treated Ni foils and a1 foils alternately, and then dividing the resulting laminated foil into two in the thickness direction, with an upper laminated foil on the top and a lower laminated foil on the bottom, the upper and lower laminated foils constituting a first laminated foil; a dislocation exists between the upper laminated foil and the lower laminated foil, and the first laminated foil is divided into an overlapping area and two dislocation areas; (3) pressing the overlapping area of the first laminated foil to obtain a second laminated foil; the two laminated foils comprise an overlapped area laminated foil formed after the overlapping area is pressed and two partial staggered area laminated foils positioned on two staggered areas; (4) and pressing the second laminated foil into a lower die by using a built-in die, overlapping two staggered layer regions of the second laminated foil around the built-in die, pressing the overlapped second laminated foil by using an upper die, connecting the overlapped regions under the combined action of the upper die, the lower die and the built-in die, and taking out the overlapped regions after forming to obtain the NiAl alloy complex thin-wall hollow component.

The yield strength of pure Ni is 3-4 times of that of pure Al, the Ni foil is subjected to heat treatment for 30-120 min at the temperature of 600-800 ℃, and the density of defects such as dislocation and the like in the Ni foil can be reduced, so that the yield strength of the Ni foil is reduced, the elongation is improved, the deformation uniformity and harmony of a laminated material are optimized, and further, a complex thin-wall hollow component with uniform wall thickness and excellent performance is obtained;

according to the invention, the overlapping region of the first laminated foil is pressed before forming, and the overlapped region laminated foil combined by diffusion metallurgy can be formed between the Ni foil and the A1 foil in the overlapping region, so that compared with the prior art in which the laminated foil is directly formed without pressing, the laminated foil in the overlapping region deforms more uniformly and coordinately when a complex thin-wall hollow component is formed subsequently, is not easy to move and delaminate, and has better forming performance;

the invention adopts the staggered-layer lap joint mode to prepare the complex thin-wall hollow component, does not need welding, can form two lap joints which are not positioned at the same axial position in the component after pressing, and can ensure that the components of the lap joints are consistent with the components of other parts of the component compared with the welding seam formed by the welding method, the use safety and reliability are higher, the uniformity of the wall thickness is better, and the component precision is high.

In addition, the invention can flexibly design the shape, the block dividing mode and the like of the built-in die required in the preparation process according to the shape and the size of the final component, is convenient for obtaining the component with the complex shape, can conveniently and quickly demold and take out the built-in die, and has high efficiency and easy batch production.

Furthermore, the invention controls the atomic number ratio of Ni atoms and A1 atoms in the NiA1 alloy to be 45:55 to 59:41, and the atomic number ratio falls in a single-phase region of the NiA1 alloy, so that the components of the obtained NiAl alloy complex thin-wall hollow component are all in the single-phase region, the components are more uniform, and the performance difference of different parts of the component is prevented. In addition, the prior art emphasizes that the atomic ratio of Ni to Al is 1:1, and NiAl is formed, so that the high requirements on the quality and the operation of raw materials are met, and the mass production is not facilitated. The method optimizes the thickness ratio of the Ni foil to the Al foil based on the NiAl single-phase region composition range, has the advantages that the atomic number ratio of Ni atoms to A1 atoms in the NiAl single-phase region composition range is 45: 55-59: 41 under the standard room temperature environment, the range is wider, the thickness deviation of the actual foil raw materials and certain influence possibly caused by experimental operation and the like are considered, and the method is more convenient to operate and automatically produce.

Further, the invention controls the vacuum degree of the pressing to be 1.0 x 10 when the overlapping area of the first laminated foil is pressed and the overlapping area of the second laminated foil is pressed^-3～5.0×10^-3Pa, gas between the raw material foils can be fully removed, so that the interface bonding and lap seam bonding states are good, and no air holes exist. Therefore, the formed member has good uniformity, less defects and excellent member use performance.

Drawings

FIG. 1 is a schematic view showing an alternate stacking of Ni foil and Al foil;

FIG. 2 is a schematic view of an overlap region and two fault regions of a first laminated foil;

FIG. 3 is a schematic view of a lap seam;

FIG. 4 is a schematic structural view of a complicated thin-walled hollow member made of NiAl alloy according to example 1;

FIG. 5 is a tensile test stress-strain curve at different temperatures for laminated foils prepared using heat treated Ni foils and non-heat treated Ni foils;

FIG. 6 (a) is a schematic view of pressing a trapezoidal laminated foil, and FIG. 6 (b) is a schematic view of upper and lower two-part staggered layers of the trapezoidal laminated foil;

FIG. 7 is a microstructure view of a rectangular laminated foil;

FIG. 8 is a tensile test stress-strain curve for a rectangular laminated foil at different temperatures;

FIG. 9 is a photograph of a fracture after a tensile test of a rectangular laminated foil;

fig. 10 (a) is a schematic view of a rectangular laminated foil bending performance test mold, fig. 10 (b) is a photograph of a rectangular laminated foil before a bending test, and fig. 10 (c) is a photograph of a rectangular laminated foil after the bending test;

FIG. 11 (a) is a schematic view of an inner mold of example 1, and FIG. 11 (b) is a schematic view of an upper mold, a lower mold and a pressing process of a member of example 1;

FIG. 12 (a) is a schematic view of the "lap seam" formed during the pressing process of the member of example 1, and FIG. 12 (b) is a schematic view of the final-formed NiAl alloy complex thin-walled hollow member of example 1.

Detailed Description

The invention provides a forming method of a NiAl alloy complex thin-wall hollow component, which comprises the following steps:

(1) calculating the thickness ratio of the Ni foil to the A1 foil according to the atomic number ratio of the Ni atoms to the A1 atoms in the NiA1 alloy; determining the actual thickness of the Ni foil and the Al foil according to the calculated thickness ratio of the Ni foil to the A1 foil; carrying out heat treatment on the needed Ni foil to obtain a heat-treated Ni foil; the temperature of the heat treatment is 600-800 ℃, and the time is 30-120 min;

(2) stacking a plurality of the heat-treated Ni foils alternately with the same number of a1 foils, and then dividing the resulting laminated foil into two in the thickness direction, with an upper laminated foil on the top and a lower laminated foil on the bottom, the upper and lower laminated foils constituting a first laminated foil; a dislocation exists between the upper laminated foil and the lower laminated foil, and the first laminated foil is divided into an overlapping area and two dislocation areas;

(3) pressing the overlapping area of the first laminated foil to obtain a second laminated foil; the second laminated foil comprises an overlapped area laminated foil formed after the overlapping area is pressed and two parts of staggered area laminated foils positioned on two staggered areas;

(4) and pressing the second laminated foil into a lower die by using a built-in die, overlapping two staggered areas of the second laminated foil around the built-in die, pressing the overlapped second laminated foil by using an upper die, connecting the overlapped areas under the combined action of the upper die, the lower die and the built-in die, and taking out the overlapped second laminated foil after forming to obtain the NiAl alloy complex thin-wall hollow component.

The thickness ratio of the Ni foil and the A1 foil was calculated from the atomic number ratio of Ni atoms to A1 atoms in the NiA1 alloy. The method for calculating the thickness ratio of the Ni foil and the a1 foil according to the present invention is not particularly limited, and the calculation may be performed by a method known in the art. In the present invention, the atomic number ratio of Ni atoms to a1 atoms in the NiA1 alloy is preferably 45:55 to 59: 41.

In the present invention, the method of calculating the thickness ratio of the Ni foil and the Al foil is specifically as follows:

N＝n×N_Aformula (i)

M ═ nxm formula (ii)

h is m/(ρ × S) formula (iii)

Wherein N is the number of atoms, N is the amount of substance, N_AIs the avogalois constant, M is the mass, M is the molar mass of the material, h is the foil thickness, ρ is the density, and S is the cross-sectional area; rho_Ni＝8.902g/cm³， M_Ni＝58.69g/mol，ρ_Al＝2.70g/cm³，M_Al＝26.98g/mol。

H can be theoretically calculated according to the atomic number ratio of Ni atoms to A1 atoms in the NiA1 alloy and the formulas (i), (ii) and (iii)_Ni：h_AlIn the range of 1:1.04 to 1: 1.83.

Under the environment of standard atmospheric pressure and room temperature, the component range of the atomic percentage content of Ni between 45 and 59 percent is in a NiAl single-phase region, the number ratio of atoms of Ni atoms and A1 atoms in the NiA1 alloy is controlled to be 45:55 to 59:41, the number ratio of the atoms falls in the single-phase region of the NiA1 alloy, the components of the obtained NiAl alloy complex thin-wall hollow component can be ensured to be in the single-phase region, the components are more uniform, and the performance difference of different parts of the component is prevented. Compared with the prior art, the method emphasizes that the atomic ratio of Ni to Al is 1:1, has wider range, considers the thickness deviation of the actual foil raw material and certain influence possibly caused by experimental operation, and the like, and is more convenient to operate and automatically produce.

After the thickness ratio of the Ni foil and the A1 foil is obtained, the present invention determines the actual thicknesses of the Ni foil and the Al foil based on the calculated thickness ratio of the Ni foil and the A1 foil. When the raw materials are actually purchased, the Ni foil and the Al foil are made of materials with different thicknesses, the foil raw materials with standard thicknesses (industrially produced in large quantities) are cheap, and the foil raw materials with customized thicknesses are expensive. In the present invention, it is preferable that the actual thicknesses of the Ni foil and the Al foil are flexibly selected according to the actual situation, and the thickness ratio of the two foils is within the calculated range. The invention preferably selects h_Ni：h_AlPreferably, the ratio (c) is in the range of 1:1.2 to 1:1.6, so as to avoid the influence of slight deviation of the actual foil thickness or actual operation, and the ratio is beyond the calculated range.

After the actual thickness of the Ni foil and the Al foil is determined, the required Ni foil is subjected to heat treatment to obtain the heat-treated Ni foil. In the invention, the temperature of the heat treatment is 600-800 ℃, preferably 650-750 ℃, and more preferably 670-720 ℃; the time of the heat treatment is 30-120 min, preferably 40-100 min, and more preferably 50-80 min. In the present invention, the heat treatment is preferably performed under vacuum conditions, and the degree of vacuum is preferably 1.0X 10^-1～1.0×10^-2Pa. The yield strength of pure Ni is 3-4 times of that of pure Al, the Ni foil is subjected to heat treatment for 30-120 min at the temperature of 600-800 ℃, and the density of defects such as dislocation and the like in the Ni foil can be reduced, so that the yield strength of the Ni foil is reduced, the elongation is improved, the deformation uniformity and harmony of a laminated material are optimized, and the complex laminated material with uniform wall thickness and excellent performance can be obtainedA thin-walled hollow member.

After obtaining the heat-treated Ni foil, the present invention alternately stacks a plurality of the heat-treated Ni foils and a1 foils as shown in fig. 1, and then divides the resulting laminated foil into two in the thickness direction, the upper laminated foil being an upper laminated foil and the lower laminated foil being a lower laminated foil, the upper laminated foil and the lower laminated foil constituting a first laminated foil; a misalignment exists between the upper and lower laminated foils, dividing the first laminated foil into an overlap region and two misalignment regions, as shown in fig. 2.

The invention has no special requirements on the shapes of the A1 foil and the Ni foil, and can select a proper shape according to the shape of the finally formed NiAl alloy complex thin-wall hollow component. In an embodiment of the invention, the a1 foil and the Ni foil are trapezoidal foils. The invention has no special requirements on the total quantity of the heat-treated Ni foil and the A1 foil, can be flexibly adjusted and is only required to be more than 2 layers.

In the present invention, the bottom layer of the laminated foil obtained by the alternate stacking is a heat-treated Ni foil, the top layer is an Al foil, or both the bottom layer and the top layer may be heat-treated Ni foils. It is preferred in the present invention that both the bottom and top layers are heat treated Ni foils. When both the bottom layer and the top layer were heat-treated Ni foils, although the atomic number ratio of Ni atoms and a1 atoms slightly deviated from the theoretical atomic number ratio, the atomic number ratio of Ni atoms and a1 atoms did not affect the falling in the single-phase region of the NiA1 alloy.

In the present invention, the thickness of the alternating stack (overlap region thickness) is determined according to the final wall thickness of the NiAl alloy complex thin-walled hollow member. Specifically, it can be determined by a simple stacked raw material hot pressing experiment; a fitting database and the like can also be established, and the subsequent re-pressing can be directly invoked, and the process of determining the thickness of the alternate stack according to the final wall thickness of the NiAl alloy complex thin-wall hollow component is common knowledge in the field and is not described herein again. In the invention, the wall thickness of the NiAl alloy complex thin-wall hollow component is preferably 1-3 mm, and more preferably 1.5-2.5 mm.

The present invention preferably divides the resulting first laminated foil into an overlap region and two dislocation regions by moving the upper laminated foil and/or the lower laminated foil such that a dislocation between the upper laminated foil and the lower laminated foil occurs. The invention has no special requirements on the dislocation direction and distance, and can be flexibly designed according to the actual shape and requirements of the component. In the present invention, the thickness ratio of the upper laminated foil to the lower laminated foil is preferably (0.8 to 1.2): 1.

after the first laminated foil is obtained, the present invention presses the overlapping area of the first laminated foil (as shown in fig. 2) to obtain a second laminated foil. In the present invention, the conditions for pressing the overlapping area of the first laminated foil preferably include: vacuum degree of 1.0X 10^-3～5.0×10^-3Pa, the temperature is 550-600 ℃, the pressure is 15-25 MPa, and the pressing time is 0.5-3 h; the degree of vacuum is more preferably 2.0X 10^-3～4.0×10^-3Pa, the temperature is preferably 560-585 ℃, the pressure is preferably 17-23 MPa, and the pressing time is preferably 1-2.5 h. The invention preferably uses a graphite mold for pressing.

The invention controls the vacuum degree of the pressing to be 1.0 multiplied by 10^-3～5.0×10^-3Pa, gas between the Ni foil and the A1 foil can be fully removed, so that the interface bonding state is good, no air hole exists, and the NiAl alloy complex thin-wall hollow component with few defects and good uniformity can be obtained.

After the pressing is finished, the Ni foil and the A1 foil in the overlapping area are in diffusion metallurgical bonding, a transition layer is formed between the Ni foil and the A1 foil, and the composition range of the transition layer is Ni₂₅Al₇₅(atomic%) to Ni₆₀Al₄₀(atomic percent) and the thickness of the transition layer is 5-15 μm. According to the invention, the overlapping region of the first laminated foil is pressed before forming, and the Ni foil and the A1 foil in the overlapping region can form the overlapped region laminated foil combined by diffusion metallurgy.

After the pressing of the overlap area is completed, the second laminated foil obtained by the present invention includes an overlap area laminated foil formed after the pressing of the overlap area and two partial staggered area laminated foils located at two staggered areas. One skilled in the art can choose not to press or to press the two-part, staggered area laminated foil depending on the specific shape of the component.

In the present invention, when the shape of the final-formed NiAl alloy complex thin-walled hollow component is relatively simple (e.g. no small round corners), the present invention can press the two-part staggered area laminated foil, and then obtain the complete diffusion metallurgically bonded second laminated foil. In the present invention, when it is desired to press the two-part fault-layer laminated foil, the pressing conditions are the same as those of the first laminated foil overlap region, and will not be described herein again. When the shape of the finally formed NiAl alloy complex thin-wall hollow component is more complex, the laminated foils of the two staggered areas are not pressed before the second laminated foil is pressed into the lower die, at the moment, the staggered areas in the figure 2 are layered foil raw materials, so that adjustment in the subsequent forming process is facilitated (after forming, the staggered areas can be pressed again together with the lap seams, and the use performance is not influenced).

After the second laminated foil is obtained, the second laminated foil is pressed into a lower die by using a built-in die, then two staggered areas of the second laminated foil bypass the built-in die to be lapped, the lapped second laminated foil is pressed by using an upper die, the connection of a lapping area is realized under the combined action of the upper die, the lower die and the built-in die, and the second laminated foil is taken out after forming, so that the NiAl alloy complex thin-wall hollow component is obtained.

The invention has no special requirements on the specific shapes of the built-in die, the upper die and the lower die, and the technical personnel in the field can select and design according to the shape of the NiAl alloy complex thin-wall hollow component. In the invention, the built-in die can be in an integral type or in a block combined type, and a person skilled in the art can flexibly design the shape, the block dividing mode and the like of the built-in die required in the preparation process according to the shape and the size of the NiAl alloy complex thin-wall hollow component, so that the complex-shaped component can be conveniently obtained, the built-in die can be conveniently and quickly demolded and taken out, the efficiency is high, and the mass production is easy.

In the present invention, the upper mold, the lower mold, and the inner mold are preferably made of graphite, and the strength of the graphite is preferably 50 to 100 MPa. The invention adopts the graphite mold, and has the advantages of low price, high temperature resistance and easy demolding.

In the present invention, the process of pressing the second laminated foil into the lower mold using the built-in mold is preferably performed at room temperature and normal atmospheric pressure.

The invention has no special requirement on the lapping mode of the two parts of the staggered-layer laminated foils, and the two parts of the staggered-layer laminated foils are completely overlapped after lapping. For a component with a complex shape, the size of the foil can be increased appropriately, and the residual part can be removed after overlapping.

The overlapped second laminated foil is pressed by the upper die, the connection of the overlapped area is realized under the combined action of the upper die, the lower die and the built-in die, and the overlapped second laminated foil is taken out after forming to obtain the NiAl alloy complex thin-wall hollow component.

In the present invention, the conditions for pressing the overlapped second laminated foil preferably include: vacuum degree of 1.0X 10^-3～5.0×10^-3Pa, the temperature is 550-600 ℃, the pressure is 15-25 MPa, and the pressing time is 0.5-3 h; the degree of vacuum is more preferably 2.0X 10^-3～4.0×10^-3Pa, the temperature is preferably 560-585 ℃, the pressure is preferably 17-23 MPa, and the pressing time is preferably 1-2.5 h. The invention controls the vacuum degree of pressing during forming to be 1.0 multiplied by 10^-3～5.0×10^-3Pa, good bonding state of the lap seam can be ensured, and no air holes exist.

The invention adopts a staggered-layer lap joint mode to prepare a complex thin-wall hollow component, welding is not needed, two lap joints which are not positioned at the same axial line position can be formed in the component after pressing, and the two lap joints have non-through property in the wall thickness direction of the component, as shown in figure 3; compared with a welding seam formed by a welding method, the composition of the lap joint can be ensured to be consistent with that of other parts of the component, the use safety and reliability are higher, the uniformity of the wall thickness is better, and the precision of the component is high.

The method of the invention can be used for forming the NiAl alloy complex thin-wall hollow member with large change of the section shape and large change of the section perimeter. In the invention, the ratio of the cross section circumferences of the two end surfaces of the NiAl alloy complex thin-wall hollow component can be more than 1.5; the sections of two ends of the NiAl alloy complex thin-wall hollow component can be in different shapes, such as: one end of the cross section is round, and the other end of the cross section is rectangular.

The following will describe the forming method of the NiAl alloy complex thin-walled hollow member provided by the present invention in detail with reference to the examples, but they should not be construed as limiting the scope of the present invention.