Die for precision casting of aviation casting
By designing a mold for aviation castings, using the upper mold to move downwards and squeeze lubricant into it, the problem of the existing molds frequently applying release agent during stamping is solved, and the working efficiency and simplicity of operation is improved.
Patent Information
- Application Number
- CN202421032101.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-13
- Publication Date
- 2025-05-02
- Estimated Expiration
- 2034-05-13
AI Technical Summary
Existing board stamping molds need to frequently apply mold release agent during the stamping process, which affects working efficiency.
A mold for precision casting of aviation castings was designed. The lubricating oil was squeezed into the press mold by moving the upper mold downwards to immerse the surface of the workpiece to facilitate subsequent mold release.
It effectively improves work efficiency, reduces dependence on mold release agents, and simplifies the operation process.
Smart Images

Figure CN222817720U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of stamping dies, in particular to a die for precision casting of aviation castings. Background Art
[0002] Precision workpieces are usually stamped and formed by stamping equipment during casting. The stamping die is a key component in the stamping equipment. The use of different stamping dies directly affects the stamping quality and work efficiency.
[0003] The existing sheet metal stamping dies need to apply a release agent to the stamping end of the die during the stamping process to facilitate the removal of the workpiece. During actual operation, the user needs to apply the release agent continuously, which affects the work efficiency during use and has certain shortcomings. Utility Model Content
[0004] The utility model aims to solve the problems raised in the above-mentioned background technology and provides a mold for precision casting of aviation castings.
[0005] In order to achieve the above purpose, the utility model adopts the following technical solutions:
[0006] A mold for precision casting of aviation castings, comprising:
[0007] An upper mold and a lower mold;
[0008] A first pressing die is fixedly connected to the upper die;
[0009] A second pressing die is fixedly connected to the lower die;
[0010] The first die is located directly above the second die;
[0011] The upper mold and the lower mold are both fixedly connected with a driving cylinder;
[0012] The oil delivery pipe is fixedly connected to the driving cylinder.
[0013] Preferably, push rods are fixedly connected to the upper mold and the lower mold, a sliding plug is slidably connected in the driving cylinder, a sliding rod is fixedly connected to the sliding plug, and the sliding rod is connected to the push rod.
[0014] Furthermore, a first magnet is fixedly connected to the push rod, and a second magnet is fixedly connected to the slide rod, and the first magnet and the second magnet attract each other.
[0015] Preferably, an oil inlet pipe is fixedly connected to the side wall of the driving cylinder.
[0016] Furthermore, both the oil inlet pipe and the oil delivery pipe are provided with a one-way valve.
[0017] Furthermore, a spring is fixedly connected to the sliding plug, and one end of the spring away from the sliding plug is fixedly connected to the inner wall of the driving cylinder.
[0018] Furthermore, a limit plate is fixedly connected to the sliding rod, and the limit plate and the driving cylinder are against each other.
[0019] Compared with the prior art, the utility model provides a mold for precision casting of aviation castings, which has the following beneficial effects:
[0020] The parts not involved in the device are the same as the existing technology or can be implemented by using the existing technology. The utility model moves the upper mold in the device downward, and then squeezes the lubricating oil into the first die and the second die, and then can be immersed in the workpiece and the first die, the second die, so as to facilitate the subsequent demolding of the workpiece. The workpiece is lubricated by the device, which effectively improves the work efficiency. BRIEF DESCRIPTION OF THE DRAWINGS
[0021] Figure 1 This is a schematic diagram of the structure of a mold for precision casting of aviation castings proposed by the utility model;
[0022] Figure 2 A precision casting mold for aviation castings proposed by the utility model Figure 1 The structural diagram of part A in the figure;
[0023] Figure 3 A cross-sectional view of a mold for precision casting of aviation castings proposed by the utility model;
[0024] Figure 4 A precision casting mold for aviation castings proposed by the utility model Figure 3 The structural diagram of part B;
[0025] Figure 5 The utility model is an exploded view of a mold for precision casting of aviation castings.
[0026] In the figure: 1, upper mold; 101, first die; 2, lower mold; 201, second die; 3, drive cylinder; 301, spring; 302, slide plug; 4, oil inlet pipe; 5, one-way valve; 6, oil delivery pipe; 7, slide rod; 701, second magnet; 702, limit plate; 8, push rod; 801, first magnet. DETAILED DESCRIPTION
[0027] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.
[0028] Embodiment 1:
[0029] Reference Figure 1-Figure 5 , a mold for precision casting of aviation castings, comprising:
[0030] Upper mold 1 and lower mold 2;
[0031] The first die 101 is fixedly connected to the upper die 1;
[0032] The second pressing die 201 is fixedly connected to the lower die 2;
[0033] The first die 101 is located directly above the second die 201;
[0034] A driving cylinder 3 is fixedly connected to both the upper mold 1 and the lower mold 2;
[0035] The oil delivery pipe 6 is fixedly connected to the driving cylinder 3 .
[0036] A push rod 8 is fixedly connected to both the upper mold 1 and the lower mold 2 , a sliding plug 302 is slidably connected in the driving cylinder 3 , a sliding rod 7 is fixedly connected to the sliding plug 302 , and the sliding rod 7 is connected to the push rod 8 .
[0037] The push rod 8 is fixedly connected with a first magnet 801 , and the slide rod 7 is fixedly connected with a second magnet 701 . The first magnet 801 and the second magnet 701 attract each other.
[0038] Reference Figure 1-Figure 5 During use, the workpiece to be stamped is placed on the second die 201 of the lower die 2. After placement, the first die 101 is driven downward by the upper die 1. After the upper die 1 slides for a distance, the first die 101 and the workpiece are against each other. At this time, the upper die 1 continues to move downward. At this time, under the mutual extrusion of the first die 101 and the second die 201, the workpiece can be stamped into shape.
[0039] During the downward movement of the upper mold 1, the push rod 8 on the upper mold 1 will move downward synchronously. At this time, after the push rod 8 moves downward for a distance, the push rod 8 will collide with the slide bar 7. At this time, the first magnet 801 and the second magnet 701 attract each other. At this time, when the upper mold 1 continues to move downward, the slide bar 7 will move downward synchronously. The downwardly moved slide bar 7 will synchronously push the slide plug 302 to move downward. The downwardly moved slide plug 302 will squeeze out the lubricating oil in the driving cylinder 3. The extruded lubricating oil will be transported through the oil pipe 6. The transported lubricating oil will be sprayed on the second die 201. The lubricating oil sprayed on the second die 201 will flow and immerse into the workpiece surface, thereby facilitating the subsequent demolding of the workpiece.
[0040] Reference Figure 3When the upper mold 1 moves downward, the push rod 8 on the lower mold 2 will push the slide plug 302 to move, thereby squeezing the lubricating oil in the driving cylinder 3 into the first die 101, and the delivered lubricating oil will be sprayed on the second die 201. The lubricating oil sprayed on the second die 201 will flow and immerse into the surface of the workpiece, thereby facilitating the subsequent demolding of the workpiece.
[0041] The upper die 1 in the device moves downward, thereby squeezing the lubricating oil onto the first die 101 and the second die 201, and then can penetrate between the workpiece and the first die 101 and the second die 201, thereby facilitating the subsequent demoulding of the workpiece.
[0042] An oil inlet pipe 4 is fixedly connected to the side wall of the driving cylinder 3 .
[0043] Both the oil inlet pipe 4 and the oil delivery pipe 6 are provided with a one-way valve 5 .
[0044] The sliding plug 302 is fixedly connected with a spring 301 , and one end of the spring 301 away from the sliding plug 302 is fixedly connected to the inner wall of the driving cylinder 3 .
[0045] Reference Figure 4 The spring 301 is provided to enable the sliding plug 302 to be quickly reset. When the sliding plug 302 is reset, the driving cylinder 3 can draw external lubricating oil through the oil inlet pipe 4, so as to facilitate the next use.
[0046] The slide bar 7 is fixedly connected with a limit plate 702 , and the limit plate 702 and the driving cylinder 3 are against each other.
[0047] Reference Figure 4 By setting the limiting plate 702, when the push rod 8 pushes the slide rod 7 to slide down, it can prevent the slide rod 7 from excessively sliding and completely entering the driving cylinder 3.
[0048] The above is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent substitutions or changes within the technical scope disclosed by the present invention according to the technical solution and inventive concept of the present invention, which should be covered by the protection scope of the present invention.
Claims
1. A mold for precision casting of aviation castings, characterized in that: include: An upper mold (1) and a lower mold (2); A first pressing die (101) is fixedly connected to the upper die (1); A second pressing die (201) is fixedly connected to the lower die (2); The first die (101) is located directly above the second die (201); The upper mold (1) and the lower mold (2) are both fixedly connected with a driving cylinder (3); The oil delivery pipe (6) is fixedly connected to the driving cylinder (3).
2. A precision casting mold for aviation castings according to claim 1, characterized in that: The upper mold (1) and the lower mold (2) are both fixedly connected with a push rod (8), the driving cylinder (3) is slidably connected with a sliding plug (302), the sliding plug (302) is fixedly connected with a sliding rod (7), and the sliding rod (7) is connected to the push rod (8).
3. A precision casting mold for aviation castings according to claim 2, characterized in that: The push rod (8) is fixedly connected with a first magnet (801), and the sliding rod (7) is fixedly connected with a second magnet (701), and the first magnet (801) and the second magnet (701) attract each other.
4. The precision casting mold for aviation castings according to claim 1, characterized in that: An oil inlet pipe (4) is fixedly connected to the side wall of the driving cylinder (3).
5. The precision casting mold for aviation castings according to claim 4, characterized in that: Both the oil inlet pipe (4) and the oil delivery pipe (6) are provided with a one-way valve (5).
6. The precision casting mold for aviation castings according to claim 2, characterized in that: The sliding plug (302) is fixedly connected to a spring (301), and one end of the spring (301) away from the sliding plug (302) is fixedly connected to the inner wall of the driving cylinder (3).
7. The precision casting mold for aviation castings according to claim 6, characterized in that: A limit plate (702) is fixedly connected to the sliding rod (7), and the limit plate (702) and the driving cylinder (3) are in contact with each other.