阅读说明：本技术 一种采用钪铝合金成型尾翼搭载发动机壳体的方法及产品 (Method for forming empennage to carry engine shell by adopting scandium-aluminum alloy and product ) 是由 文世峰 陈柯宇 周燕 史玉升 陈道兵 洪青锋 李霏 王楠 于 2019-12-19 设计创作，主要内容包括：本发明属于3D打印领域,并公开了一种采用钪铝合金成型尾翼搭载发动机壳体的方法及产品。该方法包括下列步骤：(a)选取铝合金粉末和金属钪作为原料,将二者球磨混合,以此获得混合粉末；(b)构建待成形尾翼搭载发动机壳体的三维模型,将所述混合粉末采用选择性激光熔化成形方法按照所述三维模型进行成形,以此获得尾翼搭载发动机壳体；(c)对所述尾翼搭载发动机壳体进行热处理和后处理,以此获得所需的产品。同时本发明还公开了上述方法获得的产品。通过本发明,提高尾翼搭载发动机壳体的机械强度,避免焊缝的服役失效,安全高效。(The invention belongs to the field of 3D printing, and discloses a method and a product for carrying an engine shell by adopting a scandium-aluminum alloy forming empennage. The method comprises the following steps: (a) selecting aluminum alloy powder and metal scandium as raw materials, and ball-milling and mixing the aluminum alloy powder and the metal scandium to obtain mixed powder; (b) constructing a three-dimensional model of the empennage-mounted engine shell to be formed, and forming the mixed powder according to the three-dimensional model by adopting a selective laser melting forming method so as to obtain the empennage-mounted engine shell; (c) and carrying out heat treatment and aftertreatment on the tail-mounted engine shell so as to obtain a required product. Meanwhile, the invention also discloses a product obtained by the method. By the aid of the method, mechanical strength of the tail carrying engine shell is improved, service failure of welding seams is avoided, and safety and high efficiency are achieved.)

1. A method for forming a tail wing carrying engine shell by using scandium-aluminum alloy is characterized by comprising the following steps:

(a) selecting aluminum alloy powder and metal scandium as raw materials, and ball-milling and mixing the aluminum alloy powder and the metal scandium to obtain mixed powder;

(b) constructing a three-dimensional model of the empennage-mounted engine shell to be formed, and forming the mixed powder according to the three-dimensional model by adopting a selective laser melting forming method so as to obtain the empennage-mounted engine shell;

(c) and carrying out heat treatment and aftertreatment on the tail-mounted engine shell so as to obtain a required product.

2. A method of forming a tail-mounted engine casing using an aluminum scandium alloy according to claim 1, wherein in step (a), the aluminum alloy powder is one or more of a6061, 702A and YL102 which are commercially available, and the particle size of the aluminum alloy powder is 20 μm to 60 μm; the mass fraction of scandium in the mixed powder is 0.05-0.5%.

3. The method for forming a tail wing mounted engine housing by using scandium-aluminum alloy according to claim 1, wherein in the step (a), the rotation speed of the ball mill is 200r/min to 300r/min, and the time is 5.5h to 6.5 h.

4. A method for forming a tail-mounted engine casing using an aluminum scandium alloy according to claim 1, wherein in the step (b), the selective laser melting forming is performed at a laser power of 200W to 300W, a scanning speed of 750mm/s to 1350mm/s, a layer thickness of 30 μm to 40 μm, and a scanning pitch of 70 μm to 110 μm.

5. A method of forming a tail-mounted engine casing using an aluminum scandium alloy according to claim 1, wherein in step (c), the heat treatment comprises holding the temperature at 400 ℃ to 450 ℃ for 5h to 6h, and then quenching the heat treated heat at 80 ℃ to 100 ℃ for 50h to 55 h.

6. A method of forming a tail wing mounted engine casing using scandium-aluminum alloy as set forth in claim 1, wherein in step (c), said post-treatment is shot-peening for a time period of 5 to 10 min.

7. A product obtained by the method of any one of claims 1 to 6.

Technical Field

The invention belongs to the field of 3D printing, and particularly relates to a method and a product for carrying an engine shell by adopting a scandium-aluminum alloy forming empennage.

Background

With the improvement of the requirement on the high maneuverability of the tactical missile, the flight speed of the missile in the atmosphere is further increased, so that the power device of the tactical missile, namely the solid rocket engine, has the characteristics of high mass ratio, high pneumatic heating, high overload and the like. The shell is used as an important component of an engine, is a propellant storage tank, is a propellant chemical reaction site and is a part of the elastomer, and provides support for other parts (such as a cable cover, wings and the like) of the elastomer. When the engine works, the shell is used as a thin-wall part and not only bears internal pressure of about 10MPa, but also needs to bear external loads from full elasticity, such as axial pressure, bending moment, shearing force and the like. Thus, the lightweight, thin-walled shell carries the combined effect of internal pressure and external load. And in certain tactical missile, because of the requirement of the missile body pneumatic structure, the tail wing is moved to the outer surface of the engine shell from the missile body cabin section, and the large pneumatic load is combined with the high internal pressure of the engine, so that the bearing condition of the shell is rapid and severe. The traditional titanium steel alloy material cannot meet the requirements of the service environment of the empennage-mounted engine shell on the light weight and high strength of the shell material, so that a new high-strength aluminum alloy material is urgently needed to be developed.

Scandium is a very active metal with a melting point of 1539 deg.C, a boiling point of 2832 deg.C and a density of 2.995g/cm³. Scandium forms a dispersed highly stable Al3Sc intermetallic phase with aluminum in the aluminum alloy, and the crystal structure and lattice constant of Al3Sc mass points are similar to those of aluminum, thereby playing the roles of a precipitation enhancer, a grain refiner and a recrystallization inhibitor in the aluminum alloy. Research shows that the Sc content in the alloy is 0.1-0.5%, and the room temperature tensile strength, the high temperature heat resistance and the grain boundary corrosion performance of the alloy are improved within the range of room temperature to 300 ℃. In addition, China has abundant scandium resources, has a certain foundation for research and production of scandium, and has a very wide prospect in advanced high-tech fields such as aerospace, ships, rocket missiles and the like.

Disclosure of Invention

Aiming at the defects or improvement requirements of the prior art, the invention provides a method and a product for forming the empennage-mounted engine shell by adopting scandium aluminum alloy, wherein metal scandium is selectively added into the empennage-mounted engine shell, so that the mechanical property of the structure of the obtained product is enhanced, meanwhile, the empennage-mounted engine shell is integrally formed by adopting 3D printing, the service failure of a welding line is effectively avoided, the safety and the high efficiency are realized, the combination mode and the internal structure of the empennage and the engine shell can be changed according to the service environment, and the flexibility is high.

To achieve the above object, according to one aspect of the present invention, there is provided a method of forming a tail wing-mounted engine casing using a scandium-aluminum alloy, the method including the steps of:

(a) selecting aluminum alloy powder and metal scandium as raw materials, and ball-milling and mixing the aluminum alloy powder and the metal scandium to obtain mixed powder;

(b) constructing a three-dimensional model of the empennage-mounted engine shell to be formed, and forming the mixed powder according to the three-dimensional model by adopting a selective laser melting forming method so as to obtain the empennage-mounted engine shell;

(c) and carrying out heat treatment and aftertreatment on the tail-mounted engine shell so as to obtain a required product.

Further preferably, in the step (a), the aluminum alloy powder is one or more of a6061, 702A and YL102 which are commonly used in industry, and the particle size of the aluminum alloy powder is 20-60 μm; the mass fraction of scandium in the mixed powder is 0.05-0.5%.

Further preferably, in the step (a), the rotation speed of the ball mill is 200 r/min-300 r/min, and the time is 5.5 h-6.5 h.

Further preferably, in the step (b), in the selective laser melting molding, the laser power is 200W to 300W, the scanning speed is 750mm/s to 1350mm/s, the layer thickness is 30 μm to 40 μm, and the scanning pitch is 70 μm to 110 μm.

Further preferably, in the step (c), the heat treatment comprises firstly keeping the temperature at 400-450 ℃ for 5-6 h, and then quenching at 80-100 ℃ for 50-55 h.

Further preferably, in the step (c), the post-treatment is shot peening, and the polishing time is 5min to 10 min.

According to another aspect of the present invention there is provided a product obtained by the method described above.

In general, compared with the prior art, the above technical solution contemplated by the present invention can achieve the following beneficial effects:

1. according to the invention, scandium metal is added into the raw material, then the empennage-mounted engine shell is formed in a 3D printing mode, and scandium and aluminum form dispersed highly stable Al in the aluminum alloy₃Sc intermetallic phase, Al₃Crystals of Sc particlesThe structure and the lattice constant are similar to those of aluminum, and a precipitation enhancer, a grain refiner and a recrystallization inhibitor are added in the aluminum alloy, so that the tensile strength, the high-temperature heat resistance and the grain boundary corrosion resistance of the obtained product are obviously improved;

2. the invention integrally forms the empennage-mounted engine shell by adopting a selective laser forming method, successfully meets the requirement of the service environment of the empennage-mounted engine shell on the light weight and high strength performance of materials, is integrally and directly formed, omits the process of welding the empennage and the shell, and has the advantages of simple flow, easy implementation, better flexibility, safety and reliability.

Drawings

FIG. 1 is a flow chart of a method of preparation constructed in accordance with a preferred embodiment of the present invention;

FIG. 2 is a perspective view of a prepared tail mounted engine housing constructed in accordance with a preferred embodiment of the invention;

fig. 3 is a schematic top view of a prepared tail-mounted engine housing constructed in accordance with a preferred embodiment of the invention.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention. In addition, the technical features involved in the embodiments of the present invention described below may be combined with each other as long as they do not conflict with each other.

Referring to fig. 1, fig. 2 and fig. 3, the 3D printing method for processing the scandium-containing aluminum alloy empennage-mounted engine casing provided by the invention mainly comprises the following steps:

firstly, selecting aluminum alloy powder and mechanical ball milling and mixing metal scandium to form mixed powder. The aluminum alloy powder adopts one or more of A6061, 702A and YL102 which are common in industry, and the particle size of the powder is as follows: 20-60 μm; the mass fraction of scandium element is 0.05-0.5%. The aluminum alloy powder and the scandium element simple substance are uniformly mixed by adopting a mechanical ball milling method, and the ball milling time is as follows: 5.5-6.5 h, the rotating speed is as follows: 200 to 300 r/min. The particle size range of the metal powder suitable for SLM forming is: 20-100 mu m, and considering the mixing effect with scandium and the requirement of laser spots on the particle size of the powder, the particle size of the selected aluminum alloy powder is not too large, so that the particle size is selected to be 20-60 mu m; the doping amount of the doping phase is not required to be too high when the second phase of the composite material is doped, otherwise, the second phase is agglomerated, the mixing effect is not ideal, and in combination with related references of aluminum alloy second phase reinforcement, more ideal addition content is selected as mass fraction: 0.05 percent to 0.5 percent; similarly, the ball milling mixing time is too short, the mixing effect is poor, the mechanical property of a formed sample is poor, the ball milling time is too long, the powder is easy to oxidize and modify, meanwhile, the powder is damaged, and the powder mixing time is selected to be 5.5-6.5 hours by combining the practical experience of mixing the aluminum alloy powder.

And step two, adopting SLM printing to form scandium-containing aluminum alloy empennage-carrying engine parts. The SLM process parameters are as follows: the laser power is 200W-300W, the scanning speed is 750 mm/s-1350 mm/s, the layer thickness is 30 μm-40 μm, and the scanning distance is 70-110 μm. Furthermore, the preheating temperature of the forming substrate is 200 ℃, and argon is introduced into the forming cavity to be used as protective gas. The laser power and the scanning speed are used as energy input sources, the metal powder can be completely melted through reasonable power and speed combination, the combination of large laser energy density (namely large laser power and low scanning speed) is selected in consideration of the characteristics of high melting point, large laser reflectivity and low energy absorption rate of the aluminum alloy powder when the SLM is used for forming the aluminum alloy powder, the laser power is selected to be 200-300W in combination with actual field experience and a large number of relevant references, and the scanning speed is selected to be 750-1350 mm/s; the layer thickness selection in SLM forming is usually determined by the average powder particle size of the metal powder, and as mentioned above, the distribution range of the powder particle size is 20-60 μm, so the average powder particle size is about 35 μm, and the layer thickness is slightly larger than this value, so the layer thickness is selected to be 30-40 μm; meanwhile, the determination of the scanning distance needs to ensure that the lap joint rate of each melting channel of the aluminum alloy is reasonable, and is easily determined to be 70-110 mu m by combining related experience.

And step three, carrying out heat treatment and post-treatment on the obtained part. The heat treatment process comprises the steps of preserving heat of the formed part for 5-6 hours at the temperature of 400-450 ℃, then quenching, and preserving heat for 50-55 hours at the temperature of 80-100 ℃ after quenching. The post-treatment process is shot blasting polishing, and the polishing time is 5-10 min. The heat preservation temperature is above the transition temperature, and the heating and heat preservation temperature is determined to be 400-450 ℃ in combination with the critical transition temperature of the aluminum alloy; the heat preservation time is selected to be 5-6 h to ensure that the workpiece is completely heated or the tissue transformation is basically completed; the quenching temperature is selected to be 80-100 ℃, and the steel plate is rapidly cooled at a speed higher than the critical cooling speed so as to obtain a desired tissue and achieve the expected internal tissue and hardness; the heat preservation time is selected to be 50-55 hours long enough to enable the tissue transformation to fully occur; the material of the aluminum alloy sample is soft, and the shot blasting time is not suitable for too long, so that the selection time is 5-10 min.

The invention is further illustrated in the following by means of several specific examples: