CN213447223U - High-rigidity platform for heat treatment of large thin-wall light alloy castings - Google Patents
High-rigidity platform for heat treatment of large thin-wall light alloy castings Download PDFInfo
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- CN213447223U CN213447223U CN202020694738.3U CN202020694738U CN213447223U CN 213447223 U CN213447223 U CN 213447223U CN 202020694738 U CN202020694738 U CN 202020694738U CN 213447223 U CN213447223 U CN 213447223U
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- 229910001234 light alloy Inorganic materials 0.000 title claims abstract description 22
- 238000005266 casting Methods 0.000 title claims description 80
- 230000003014 reinforcing effect Effects 0.000 claims description 19
- 238000003825 pressing Methods 0.000 claims description 14
- 229910000831 Steel Inorganic materials 0.000 claims description 8
- 239000010959 steel Substances 0.000 claims description 8
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 230000032683 aging Effects 0.000 abstract description 7
- 238000003754 machining Methods 0.000 abstract description 3
- 239000006104 solid solution Substances 0.000 abstract description 2
- 238000007669 thermal treatment Methods 0.000 abstract 1
- 208000002740 Muscle Rigidity Diseases 0.000 description 76
- 238000000034 method Methods 0.000 description 10
- 230000008569 process Effects 0.000 description 6
- 239000000243 solution Substances 0.000 description 6
- 238000012937 correction Methods 0.000 description 3
- 230000000171 quenching effect Effects 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
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- 229910052751 metal Inorganic materials 0.000 description 1
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Abstract
The utility model provides a large-scale thin wall light alloy foundry goods thermal treatment is with high platform of having a firm basis, the platform of having a firm basis of height includes the platform body of having a firm basis of height, can dismantle on the platform body of having a firm basis of height and be equipped with a plurality of lever principles that utilize and apply to the high point of foundry goods out of tolerance with downforce or to the low point of foundry goods out of tolerance with the local loading device of upward pressure. The utility model discloses carry out external force loading to the yielding region of foundry goods, through solid solution and the ageing two-wheeled heat treatment of exerting pressure, the foundry goods plane degree is better, and it is not enough to have avoided the machining allowance that local deformation leads to, and is significant to the final weight of the foundry goods size precision and the control member product after finally guaranteeing the finish machining.
Description
Technical Field
The utility model belongs to the equipment of the large-scale light alloy thin wall component of spacecraft makes the field, especially relates to a large-scale light alloy casting heat treatment is with high platform of having a rigidity.
Background
For the aerospace field, the mass of the aircraft is reduced, and the launching cost of the effective load of the aircraft is greatly reduced. The magnesium alloy, aluminum alloy and other light metal large castings are widely applied to aerospace vehicles. The spacecraft casting structural part is characterized by being large, thin, light and precise, having complex and multiple processing surfaces, generally having the overall dimension larger than 2m and the wall thickness of 5mm, and having the technical difficulty higher than the national standard requirement. During the development process, the casting often has poor flatness and size, so that the product is rejected. Particularly, the large low frame type castings are easy to deform in the heat treatment process, the castings are easy to crack and have defects due to cold shape correction after heat treatment, products are scrapped, and the structural change is easy to cause reduction of mechanical properties due to repeated remelting and hot shape correction. Therefore, a device for ensuring the size, shape and position precision of the product in the heat treatment process is developed, and the device has important significance for ensuring the quality of large components of the spacecraft and improving the production efficiency.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model aims at providing a large-scale thin wall light alloy casting heat treatment is with high platform of having rigidity to overcome the defect that large-scale thin wall light alloy casting heat treatment process is very easily produced deformation.
In order to achieve the above purpose, the technical scheme of the utility model is realized like this:
a high-rigidity platform for heat treatment of large thin-wall light alloy castings comprises a high-rigidity platform body, wherein a plurality of local loading devices which apply downward pressure to a high point of casting out-of-tolerance or apply upward pressure to a low point of casting out-of-tolerance by utilizing the lever principle are detachably arranged on the high-rigidity platform body.
Furthermore, the local loading device comprises a support screw, a force application screw and a high-rigidity pressure plate, one side of the high-rigidity pressure plate is pressed against the over-tolerance part of the casting, the other side of the high-rigidity pressure plate is provided with a waist hole, the support screw and the force application screw are arranged in the waist hole in a penetrating way, the supporting screw rod is close to the high-rigidity pressure plate and is pressed against one side of the casting out-of-tolerance part, the force application screw rod is far away from the high-rigidity pressure plate and is pressed against one side of the casting out-of-tolerance part, the supporting screw rod is in threaded connection with a supporting point lower positioning nut and a supporting point upper positioning nut which are used for playing the role of a fulcrum, the force application screw rod is in threaded connection with a force application point lower nut and a force application point upper nut which are used for playing the role of a force application point, the supporting point lower positioning nut and the force application point lower nut are positioned below the high-rigidity pressing plate, and the supporting point upper positioning nut and the force application point upper nut are positioned above the high-rigidity pressing plate.
Furthermore, the high-rigidity platform comprises two high-rigidity platforms A and two high-rigidity platforms B.
Furthermore, the high-rigidity platform body is provided with at least two rows of threaded holes according to the outline of the casting, and the lower end of the support screw and the lower end of the force application screw are screwed into the threaded holes respectively.
Furthermore, the high-rigidity platform body and the high-rigidity pressing plate are made of HT250 or 20 steel.
Furthermore, the bottom of the high-rigidity platform body is provided with a plurality of annular reinforcing ribs and a plurality of linear reinforcing ribs, the annular reinforcing ribs are concentrically arranged, and the linear reinforcing ribs extend outwards from the annular reinforcing rib at the innermost side and are radially distributed.
Furthermore, the high-rigidity platform also comprises a plurality of weights, and the weights are placed on the upper plane of the casting.
Further, the weight is I-shaped steel.
Compared with the prior art, large-scale thin wall light alloy foundry goods heat treatment with high platform just have following advantage:
the high-rigidity platform has the characteristics of high rigidity and easy heat conduction, the high rigidity can ensure that the high-rigidity platform is not deformed in the heat treatment shape correction process, the deformation of a casting in the stress release process is easy to strictly control, and the size of the casting is further strictly controlled; the heat conduction is easy, the temperature uniformity of the tool and the casting can be ensured, and new deformation is avoided; through using a set of high rigidity platform, the local loading device on the high rigidity platform is cooperated to carry out external force loading on the easily deformable area of the casting, and the use methods of the high rigidity platform at different stages of heat treatment are combined to ensure the good dimensional accuracy of the large-scale light alloy thin-wall casting.
Drawings
The accompanying drawings, which form a part hereof, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention without undue limitation. In the drawings:
fig. 1 is a top view of a high rigidity platform for heat treatment of a large thin-wall light alloy casting according to embodiment 1 of the present invention;
FIG. 2 is a diagram showing a state of use of a high rigidity platform for heat treatment of a large thin-wall light alloy casting according to embodiment 1 of the present invention;
FIG. 3 is an enlarged view of a portion A of FIG. 2;
fig. 4 is a schematic bottom structure view of a high-rigidity platform for heat treatment of large thin-wall light alloy castings according to embodiment 1 of the present invention.
Description of reference numerals:
1. a high rigidity platform body; 2. a support screw; 3. a nut is positioned at the upper part of the supporting point; 4. a nut is positioned at the lower part of the supporting point; 5. a force application screw; 6. a nut at the upper part of the force application point; 7. a nut at the lower part of the force application point; 8. a high rigidity pressing plate; 9. pressing iron; 10. casting; 11. a waist hole; 13. a circular reinforcing rib; 14. straight line shaped reinforcing ribs.
Detailed Description
It should be noted that, in the present invention, the embodiments and features of the embodiments may be combined with each other without conflict.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are used merely for convenience of description and for simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
The present invention will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.
Example 1
A high-rigidity platform for heat treatment of large thin-wall light alloy castings comprises a high-rigidity platform body 1, and a plurality of local loading devices which apply downward pressure to high points of casting out-of-tolerance or upward pressure to low points of casting out-of-tolerance by utilizing the lever principle are detachably arranged on the high-rigidity platform body 1, as shown in figures 1-4.
The local loading device comprises a supporting screw rod 2, a force application screw rod 5 and a high-rigidity pressure plate 8, one side of the high-rigidity pressure plate 8 is pressed against the out-of-tolerance part of the casting 10, the other side of the high-rigidity pressure plate 8 is provided with a waist hole 11, the supporting screw rod 2 and the force application screw rod 5 are arranged in the waist hole 11 in a penetrating manner, the supporting screw rod 2 is close to one side of the over-tolerance part of the casting 10 pressed by the high-rigidity pressure plate 8, the force application screw rod 5 is far away from one side of the over-tolerance part of the casting 10 pressed by the high-rigidity pressure plate 8, the supporting screw rod 2 is in threaded connection with a supporting point lower positioning nut 4 and a supporting point upper positioning nut 3 which are used for playing the role of a fulcrum, the force application screw rod 5 is in threaded connection with a force application point lower nut 7 and a force application point upper nut 6 which are used for playing the role of a force application point, the supporting point lower positioning nut 4 and the force application point lower nut 7 are positioned below the high-rigidity pressing plate 8, the supporting point upper positioning nut 3 and the force application point upper nut 6 are positioned above the high-rigidity pressing plate 8.
The high-rigidity platform comprises two high-rigidity platforms, wherein the two high-rigidity platforms are completely identical in structure and are respectively called a high-rigidity platform A and a high-rigidity platform B. The high-rigidity stage A is used in solution treatment, and the high-rigidity stage B is used in aging treatment.
The high-rigidity platform body 1 is provided with at least two rows of threaded holes according to the outline of the casting 10, and the lower ends of the supporting screw rods 2 and the lower ends of the force application screw rods 5 are screwed into the threaded holes respectively. So set up, local loading device threaded connection is to high rigid platform body 1 on, conveniently adjusts local loading device's position according to the foundry goods 10 of different shapes or size, and the suitability is strong.
The high-rigidity platform body 1 and the high-rigidity pressing plate 8 are made of HT250 or 20 steel, and the HT250 or 20 steel is high in melting point and good in rigidity.
The high-rigidity platform comprises a high-rigidity platform body 1, and is characterized in that three circular ring-shaped reinforcing ribs 13 and eight linear reinforcing ribs 14 are arranged at the bottom of the high-rigidity platform body 1, the circular ring-shaped reinforcing ribs 13 are concentrically arranged, and the linear reinforcing ribs 14 extend outwards from the circular ring-shaped reinforcing rib 13 at the innermost side and are radially distributed. The circular ring-shaped reinforcing ribs 13 and the linear reinforcing ribs 14 enhance the structural strength of the whole high-rigidity platform body 1.
The high-rigidity platform further comprises a plurality of weights 9, the weights 9 are I-shaped steel, and the weights 9 are placed on the upper plane of the casting 10 to compact the casting 10 and avoid deformation of the casting 10.
Example 2
A use method of a high-rigidity platform for heat treatment of large thin-wall light alloy castings comprises the following steps:
a. five large thin-wall castings 10 (the size is phi 2.3m) are respectively numbered as No. 1, No. 2, No. 3, No. 4 and No. 5, a reference plane in the casting state is found out through preliminary scribing, rough machining leveling is carried out on the bottom surface, and high points and low points of the products in the five casting states, which are out of tolerance at different positions, are respectively found out through scribing.
b. Attaching a casting 10 to a high-rigidity platform (marked as a high-rigidity platform A), supporting by utilizing a support point upper positioning nut 3 configured on a support screw rod 2 according to a high point obtained by marking, upwards rotating a force application point lower nut 7 configured on a force application screw rod 5, and applying downward pressure to the high point on the casting 10 by utilizing a high-rigidity pressure plate 8 through a lever principle; according to the low point obtained by the marking result, a support point lower positioning nut 4 arranged on a support screw 2 is used for supporting, a force application point upper nut 6 arranged on a force application screw 5 is used for downwards rotating, and a high-rigidity pressure plate 8 is used for applying upward pressure to the high point on a casting 10 by utilizing the lever principle; uniformly placing the weights 9 on the upper plane of the casting 10 to compact the casting 10;
c. putting the pressed casting 10 together with the high-rigidity platform A into a heat treatment furnace, and carrying out solution treatment at 485 ℃ for 8 hours;
d. after solid solution, air cooling quenching is carried out, the casting 10 is rapidly separated from the high-rigidity platform A within the temperature of 250-350 ℃, the purpose of rapidly separating from the high-rigidity platform is to achieve good quenching effect, the problem that the casting 10 has poor chilling effect due to the heat dissipation of the high-rigidity platform A is avoided, the casting is transferred to another high-rigidity platform (marked as a high-rigidity platform B), and the weight 9 is rapidly and uniformly placed on the upper plane of the casting 10 to compact the casting 10;
e. after quenching, carrying out secondary press fitting on the high-rigidity platform B, marking high points and low points with different positions of the product out of tolerance by marking, supporting by using a positioning nut 3 at the upper part of a supporting point configured on a supporting screw rod 2 according to the high points obtained by marking, carrying out upward rotation on a nut 7 at the lower part of a force application point configured on a force application screw rod 5, and applying downward pressure on the high points on the casting 10 by using a high-rigidity pressure plate 8 by using a lever principle; according to the low point obtained by the marking result, a support point lower positioning nut 4 arranged on a support screw 2 is used for supporting, a force application point upper nut 6 arranged on a force application screw 5 is used for downwards rotating, and a high-rigidity pressure plate 8 is used for applying upward pressure to the high point on a casting 10 by utilizing the lever principle; uniformly placing the weights 9 on the upper plane of the casting 10 to compact the casting 10;
f. and putting the pressed casting 10 together with the high steel platform B into a heat treatment furnace, and carrying out aging treatment at 225 ℃ for 24 hours.
The flatness after the solution heat treatment and the flatness after the aging treatment of the five large thin-wall castings 10 are detected by adopting a height gauge scribing method, a UTM5105X electronic universal testing machine is adopted to stretch body sampling test pieces of the five large thin-wall castings 10, and the detection results are shown in table 1. As can be seen from Table 1, after multiple tests, the flatness of the casting 10 measured by a height gauge scribing method after the solution heat treatment under the condition of using a high-rigidity platform for applying force is generally controlled within 1.5-2mm, and the flatness after the aging treatment is controlled within 1 mm.
TABLE 1 Performance data Table for large thin-walled castings of example 2
Comparative example
Three large thin-wall castings (the sizes of which are phi 2.3m) are respectively numbered 6#, 7#, 8#, the castings are not assembled with a high-rigidity platform, the solution treatment at 485 ℃ for 8h and the aging treatment at 225 ℃ for 24h are directly carried out, the performance of the castings is detected, and the detection results are shown in table 2. As can be seen from Table 2, the flatness after the solution heat treatment is 10-20mm, the flatness after the aging treatment is 4-5mm, and the flatness performance is poor.
It can be seen from table 1 and table 2 that the tensile strength and elongation of the large thin-walled casting are not affected by whether the high-rigidity platform is used for press mounting.
TABLE 2 Performance data sheet for large thin-walled castings of the comparative examples
The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (7)
1. A high-rigidity platform for heat treatment of large thin-wall light alloy castings is characterized in that: the high-rigidity platform comprises a high-rigidity platform body, and a plurality of local loading devices which apply downward pressure to a high point of the casting out-of-tolerance or apply upward pressure to a low point of the casting out-of-tolerance by utilizing the lever principle are detachably arranged on the high-rigidity platform body;
the local loading device comprises a supporting screw rod, a force application screw rod and a high-rigidity pressing plate, wherein one side of the high-rigidity pressing plate is abutted to the casting out-of-tolerance part, the other side of the high-rigidity pressing plate is provided with a waist hole, the supporting screw rod and the force application screw rod are arranged in the waist hole in a penetrating mode, the supporting screw rod is close to one side of the high-rigidity pressing plate which is abutted to the casting out-of-tolerance part, the force application screw rod is far away from the high-rigidity pressing plate and abutted to one side of the casting out-of-tolerance part, a supporting point lower positioning nut and a supporting point upper positioning nut which are used for playing a fulcrum role are connected to the supporting screw rod in a threaded mode, a force application point lower nut and a force application point upper nut which are used for playing a force application point role are connected to the force application screw rod in a threaded mode, the supporting point lower positioning nut.
2. The high-rigidity platform for heat treatment of large thin-wall light alloy castings according to claim 1, characterized in that: the high-rigidity platform comprises two high-rigidity platforms A and two high-rigidity platforms B.
3. The high-rigidity platform for heat treatment of large thin-wall light alloy castings according to claim 1, characterized in that: the high-rigidity platform body is provided with at least two rows of threaded holes according to the outline of a casting, and the lower ends of the supporting screw rods and the force application screw rods are screwed into the threaded holes respectively.
4. The high-rigidity platform for heat treatment of large thin-wall light alloy castings according to claim 1, characterized in that: the high-rigidity platform body and the high-rigidity pressing plate are made of HT250 or 20 steel.
5. The high-rigidity platform for heat treatment of large thin-wall light alloy castings according to claim 1, characterized in that: the high-rigidity platform is characterized in that a plurality of annular reinforcing ribs and a plurality of linear reinforcing ribs are arranged at the bottom of the high-rigidity platform body, the annular reinforcing ribs are concentrically arranged, and the linear reinforcing ribs extend outwards from the innermost annular reinforcing rib and are radially distributed.
6. The high-rigidity platform for heat treatment of large thin-wall light alloy castings according to claim 1, characterized in that: the high-rigidity platform also comprises a plurality of weights, and the weights are placed on the upper plane of the casting.
7. The high-rigidity platform for heat treatment of large thin-wall light alloy castings according to claim 6, characterized in that: the weight is I-shaped steel.
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| CN202020694738.3U CN213447223U (en) | 2020-04-29 | 2020-04-29 | High-rigidity platform for heat treatment of large thin-wall light alloy castings |
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| CN202020694738.3U CN213447223U (en) | 2020-04-29 | 2020-04-29 | High-rigidity platform for heat treatment of large thin-wall light alloy castings |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111394564A (en) * | 2020-04-29 | 2020-07-10 | 天津航天机电设备研究所 | High-rigidity platform for heat treatment of large thin-wall light alloy castings and use method thereof |
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2020
- 2020-04-29 CN CN202020694738.3U patent/CN213447223U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111394564A (en) * | 2020-04-29 | 2020-07-10 | 天津航天机电设备研究所 | High-rigidity platform for heat treatment of large thin-wall light alloy castings and use method thereof |
| CN111394564B (en) * | 2020-04-29 | 2023-11-28 | 天津航天机电设备研究所 | High-rigidity platform for heat treatment of large thin-wall light alloy castings and application method thereof |
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