High-temperature alloy material combined limiting assembly
By designing a combination limiting component of high-temperature alloy material and adopting arc limiting grooves and fastening hole structures, the accuracy and stability problems of mechanical parts of high-temperature alloy material are solved, and efficient combined connection and disassembly and assembly operations are achieved.
Patent Information
- Application Number
- CN202422552621.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-22
- Publication Date
- 2025-07-22
- Estimated Expiration
- 2034-10-22
AI Technical Summary
When splicing existing high-temperature alloy mechanical parts, it is difficult to ensure the coordination accuracy and connection efficiency between components, resulting in difficulty in installation and disassembly and maintenance, affecting the stability of later use.
A high-temperature alloy material combination limit assembly is designed, including the main body support placing plate and a symmetrical main body matching combination frame, and the arc-shaped limit groove and fastening hole are set to achieve accurate limit and interlaced combination connections, improving assembly accuracy and stability.
It improves the assembly position accuracy and combined connection stability of mechanical parts of high-temperature alloy materials, simplifies the disassembly and assembly process, improves the installation and disassembly efficiency, and enhances the durability for later use.
Smart Images
Figure CN223136566U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of mechanical parts, in particular to a combined limit component made of superalloy materials. Background Technique
[0002] Superalloy materials are important materials in the production of mechanical parts. The mechanical products processed by them can ensure more stable performance of the components during use. Due to the high hardness, quality, etc. of superalloy materials, when multiple mechanical parts are spliced and matched during installation, the matching accuracy between them has an important impact on the performance during later use. When the existing splicing components are installed, they are matched by fastening different components. It is difficult to ensure the matching accuracy between different assembled components, and the connection efficiency during combination is relatively low. It is difficult to ensure the accuracy during installation and later disassembly and maintenance. Content of the Utility Model
[0003] The purpose of the utility model is to provide a combined limit component made of superalloy materials, which can accurately limit and match the splicing components at different positions during use, can ensure higher position accuracy when assembling mechanical parts made of superalloy materials, and the installation positions can achieve the combined connection effect of staggered combination in different directions, ensuring better overall combined connection stability, more convenient overall operation during disassembly and assembly, higher efficiency during assembly and disassembly, more guaranteed mutual matching accuracy, and stronger durability during later use.
[0004] The technical solution of the utility model is as follows:
[0005] A combined limit component made of superalloy materials, characterized in that: it includes a main body support placement plate in the horizontal direction, a set of symmetric main body cooperation combination frames are respectively arranged on the front and rear sides of the main body support placement plate, a circular arc-shaped first cooperation limit groove is arranged at the upper right end of the main body cooperation combination frame, a circular arc-shaped second cooperation limit groove is arranged at the upper left end of the main body cooperation combination frame, a placement cooperation stable groove is formed at the lower end of the main body cooperation combination frame, an overall fastening combination hole communicating with the first cooperation limit groove is arranged on the main body cooperation combination frame, a second cooperation placement frame is integrally formed at the front and rear positions on the right side of the main body support placement plate, a circular arc-shaped third cooperation limit groove is arranged on the right side of the second cooperation placement frame, a placement reinforcement combination safety groove is formed between the lower end of the second cooperation placement frame and the right side of the main body cooperation combination frame, a splicing stable placement frame is arranged at the position between the two second cooperation placement frames on the right side of the main body support placement plate, and a circular arc-shaped fourth cooperation limit groove is arranged on the right side of the splicing stable placement frame.
[0006] Further, the upper end surface of the main body mating combination rack is on the same plane as the upper end surfaces of the main body support placement plate and the assembled stable placement rack.
[0007] Further, the right side of the assembled stable placement rack is on the same plane as the right side of the second mating placement rack.
[0008] Further, the height of the second mating placement rack in the up and down direction on the right side is greater than the height of the main body mating combination rack in the up and down direction on the right side.
[0009] Further, both the third mating limit groove and the fourth mating limit groove are composed of a plurality of placement combination grooves evenly distributed in the front and back.
[0010] Further, the height of the assembled stable placement rack is less than the height of the second mating placement rack.
[0011] Advantages of the present utility model:
[0012] When in use, the present utility model can simultaneously perform precise limit fitting on splicing components at different positions, ensuring higher position accuracy when assembling mechanical parts made of superalloy materials. The installation positions can achieve a mating connection effect of staggered combination in different directions, ensuring better overall combination connection stability. The overall operation during disassembly and assembly is relatively convenient, with higher efficiency during assembly and disassembly, more guaranteed mutual fitting accuracy, and stronger durability during later use. Description of the Drawings
[0013] Figure 1 is a three-dimensional structural schematic diagram of the present utility model;
[0014] Figure 2 is a front view schematic diagram of the present utility model;
[0015] Figure 3 is a left side view schematic diagram of the present utility model;
[0016] Figure 4 is a right side view schematic diagram of the present utility model;
[0017] Figure 5 is a top view schematic diagram of the present utility model;
[0018] Figure 6 is a bottom view schematic diagram of the present utility model;
[0019] Figure 7 is a three-dimensional structural schematic diagram of the present utility model in the second direction;
[0020] In the figure: 1. Main body support placement plate, 2. Main body fitting combination rack, 3. First fitting limit groove, 4. Second fitting limit groove, 5. Overall fastening combination hole, 6. Second fitting placement rack, 7. Third fitting limit groove, 8. Assembly stable placement rack, 9. Fourth fitting limit groove. Detailed implementation method
[0021] As Figures 1 to 7 shown, a combined limit component for superalloy materials includes a horizontal main body support placement plate 1. On the front and back sides of the main body support placement plate 1, a set of symmetric main body fitting combination racks 2 are respectively provided. At the upper right position of the main body fitting combination rack 2, an arc-shaped first fitting limit groove 3 is provided. At the upper left position of the main body fitting combination rack 2, an arc-shaped second fitting limit groove 4 is provided. During use, it can be fitted and connected with the combination made of superalloy materials at the upper end. The arc-shaped structure can make the fitting area between them larger and the fitting stability better. The arc angles of the two fitting limit grooves can be set to different angles to make the stability during fitting better. A placement fitting stable groove is formed at the lower end of the main body fitting combination rack 2, enabling stable combination with the components to be fitted at the lower end during fitting. On the main body fitting combination rack 2, an overall fastening combination hole 5 communicating with the first fitting limit groove 3 is provided, which can be used to fasten and connect during overall combination with fastening bolts. At the front and back positions on the right side of the main body support placement plate 1, an integrally formed second fitting placement rack 6 is provided. The right side of the second fitting placement rack 6 is an arc-shaped third fitting limit groove 7, which can provide precise limit fitting for the components spliced on the right side. A placement reinforcement combination safety groove is formed between the lower end of the second fitting placement rack 6 and the right side of the main body fitting combination rack 2. At the position between the two second fitting placement racks 6 on the right side of the main body support placement plate 1, an assembly stable placement rack 8 is provided. The right side of the assembly stable placement rack 8 is an arc-shaped fourth fitting limit groove 9, ensuring precise fitting of the splicing components in the middle position on the right side, and ensuring precise assembly between the splicing components in the front and back directions and the middle position on the right side. The structural stability of the fitting position is better. During use, it can simultaneously perform precise limit fitting on the splicing components at different positions, ensuring higher position accuracy when assembling mechanical parts made of superalloy materials. The installation position can achieve the fitting connection effect of staggered combination in different directions, ensuring better overall combination connection stability, more convenient overall operation during disassembly and assembly, higher efficiency during assembly and disassembly, more guaranteed mutual fitting accuracy, and stronger durability during later use.
[0022] Preferably, the upper end surfaces of the main body fitting combination rack 2, the main body support placement plate 1, and the assembly stable placement rack 8 are on the same plane, making the overall flatness at the upper end better and the fitting safety during use also better.
[0023] Preferably, the right side of the assembled stable placement rack 8 is on the same plane as the right side of the second mating placement rack 6, so that the structural strength at the right side position is higher.
[0024] Preferably, the height of the second mating placement rack 6 in the up-and-down direction on the right side is greater than the height of the main body mating combination rack 2 in the up-and-down direction on the right side, so that when the lower positions of the left and right side structures are in use, they can be in limit fit with the structure at the installation position, ensuring that the fit stability at the lower position is more reliable.
[0025] Preferably, both the third mating limit groove 7 and the fourth mating limit groove 9 are composed of a plurality of placement combination grooves evenly distributed in the front and rear directions, so that the mating accuracy during combination is better. At the same time, it can meet the splicing and mating use of multiple components, and the flexibility during use is stronger, as long as the number of mating components at the splicing position does not exceed the number of placement combination grooves.
[0026] Preferably, the height of the assembled stable placement rack 8 is less than the height of the second mating placement rack 6, so that the structure at the lower right side position can form an anti-loosening staggered combination effect during mating, further improving the combination safety at the lower position. The overall fit stability is stronger.
[0027] The above is the preferred embodiment of the present utility model. It should be noted that for those of ordinary skill in the art of this technology, without departing from the principle described in the present utility model, several improvements or replacements can still be made, and these improvements or replacements should also be regarded as the protection scope of the present utility model.
Claims
1. A combined limit component for a superalloy material, characterized in that: It includes a main body support placement plate (1) in the horizontal direction. On the front and rear sides of the main body support placement plate (1), there is a set of symmetric main body mating combination frames (2) respectively. At the upper right position of the main body mating combination frame (2), there is an arc-shaped first mating limit groove (3). At the upper left position of the main body mating combination frame (2), there is an arc-shaped second mating limit groove (4). At the lower end of the main body mating combination frame (2), a placement mating stable groove is formed. On the main body mating combination frame (2), there is an integral fastening combination hole (5) communicating with the first mating limit groove (3). At the front and rear positions on the right side of the main body support placement plate (1), there is an integrally formed second mating placement frame (6). The right side of the second mating placement frame (6) is an arc-shaped third mating limit groove (7). Between the lower end of the second mating placement frame (6) and the right side of the main body mating combination frame (2), a placement reinforcement combination safety groove is formed. At the position between the two second mating placement frames (6) on the right side of the main body support placement plate (1), there is an assembly stable placement frame (8). On the right side of the assembly stable placement frame (8), there is an arc-shaped fourth mating limit groove (9).
2. The combined limit component of a superalloy material according to claim 1, wherein: The upper end surface of the main body mating combination frame (2) is on the same plane as the upper end surfaces of the main body support placement plate (1) and the assembly stable placement frame (8).
3. The combined limit component of a superalloy material according to claim 1, characterized in that: The right side of the assembly stable placement frame (8) is on the same plane as the right side of the second mating placement frame (6).
4. The combined limit component of a superalloy material according to claim 1, characterized in that: The height of the second mating placement frame (6) in the up and down direction on the right side is greater than the height of the main body mating combination frame (2) in the up and down direction on the right side.
5. The combined limit assembly of a superalloy material according to claim 1, characterized in that: Both the third mating limit groove (7) and the fourth mating limit groove (9) are composed of a plurality of placement combination grooves evenly distributed in the front and back.
6. The combined limit component of a superalloy material according to claim 1, characterized in that: The height of the assembly stable placement frame (8) is less than the height of the second mating placement frame (6).