Rotor welding auxiliary positioning device
Patent Information
- Application Number
- CN202522479686.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-11-24
- Publication Date
- 2026-09-22
- Estimated Expiration
- 2035-11-24
AI Technical Summary
[0002]特高压/大功量电机使用到的电机转子相对微型电机体积较大,该电机一般设计有主轴、翼板等结构,转子在加工过程中需要将翼板焊接在主轴上,由于转子体积较大,目前的加工方式是依据焊接工人的经验进行单片翼板的焊接固定,然后转换位置对下一片翼板进行焊接固定,由于需要转换位置,故整体精度不好管控
[0009]本实用新型的有益效果是:通过设计第一夹板、第二夹板,从而可对主轴、翼板进行多个方位的同时限位固定,无需再转换转子的位置及方向;通过设计第一支撑柱、第二支撑柱,从而可对两个夹板的高度进行调整,从而适应不同高度规格的转子;第一夹板对翼板的纵向直边进行固定,第二夹板则对翼板的斜边进行固定,从而可保障各个翼板的准确牢固的固定。
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Figure CN224779766U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to an auxiliary processing device for motor rotors used in ultra-high voltage / high power motors, specifically a device for assisting in the positioning and welding of rotors. Background Technology
[0002] The rotors used in ultra-high voltage / high-power motors are relatively large compared to micro motors. These motors are generally designed with structures such as a main shaft and wing plates. During the processing of the rotor, the wing plates need to be welded to the main shaft. Due to the large size of the rotor, the current processing method is to weld and fix each wing plate individually based on the experience of the welding workers, and then change the position to weld and fix the next wing plate. Because the position needs to be changed, the overall accuracy is difficult to control. Utility Model Content
[0003] The purpose of this utility model is to provide a rotor welding auxiliary positioning device, and the technical problem to be solved is: how to provide an auxiliary positioning device that can complete the welding and fixing of the wing plate without switching the position of the rotor.
[0004] A rotor welding auxiliary positioning device includes: The first clamping plate has a first shaft hole and a first wing hole inside, which respectively position and fix the main shaft and the longitudinal straight edge of the wing plate at one end of the rotor; The second clamping plate has a second shaft hole and a second wing hole inside, which respectively position and fix the main shaft and the inclined edge of the wing plate at the other end of the rotor. The length of the second wing hole is less than the length of the first wing hole. The first shaft hole, the first wing hole, the second shaft hole, and the second wing hole are all aligned in position. The first support column is fixed on a base plate to support the first clamping plate; The second support column is fixed to the aforementioned base plate to support the second clamping plate; The base plate has positioning holes for positioning and fixing the spindle head; The base column is fixed below the base plate to support it.
[0005] The first clamping plate is a plate-shaped structure, the first shaft hole is a round hole and is located in the middle, and the first wing hole is a square hole and extends laterally outward along the edge of the first shaft hole.
[0006] The second clamping plate is a plate-shaped structure. The second shaft hole is a round hole and is located in the middle. The shaft center of the second shaft hole is the same as the shaft center of the first shaft hole, and also keeps the shaft center of the main shaft in the same center. The second wing hole is a square hole and extends laterally outward along the edge of the second shaft hole. The second wing hole is aligned with the first wing hole.
[0007] The first support column is a lifting cylinder, which has multiple cylinders evenly arranged below the first clamping plate to drive the first clamping plate to rise and fall.
[0008] The second support column is a lifting cylinder, which has multiple cylinders evenly arranged below the second clamping plate to drive the second clamping plate to rise and fall.
[0009] The beneficial effects of this utility model are as follows: by designing the first clamping plate and the second clamping plate, the main shaft and the wing plate can be simultaneously limited and fixed in multiple directions without having to change the position and direction of the rotor; by designing the first support column and the second support column, the height of the two clamping plates can be adjusted to accommodate rotors of different height specifications; the first clamping plate fixes the longitudinal straight edge of the wing plate, and the second clamping plate fixes the oblique edge of the wing plate, thereby ensuring the accurate and firm fixation of each wing plate. Attached Figure Description
[0010] Figure 1 This is a schematic diagram of the rotor welding auxiliary positioning device and rotor assembly; Figure 2 This is a schematic diagram showing the rotor welding auxiliary positioning device and the rotor assembly from the front view. Figure 3 yes Figure 1 A schematic diagram of the rotor welding auxiliary positioning device and the rotor in disassembled state; Figure 4 This is a schematic diagram of the first clamping plate; Figure 5 This is a schematic diagram of the second clamping plate; In the picture 1. First clamping plate; 11. First shaft hole; 12. First wing hole; 2. First supporting column; 3. Second clamping plate; 31. Second shaft hole; 32. Second wing hole; 4. Second support column; 5. Base plate; 51. Positioning holes; 6. Bottom column; 7. Spindle; 71. Spindle head; 8. Wing plate. Detailed Implementation
[0011] Please refer to Figures 1 to 5 The rotor welding auxiliary positioning device in the figure is mainly designed with a first clamping plate 1, a second clamping plate 3, a first support column 2, a second support column 4, a bottom column 6, and a bottom plate 5. In this case, the main shaft 7 and multiple wing plates 8 are positioned simultaneously by two clamping plates. In practical applications, the above components can be further optimized, such as by modifying, replacing or adding elements such as shape, structure, quantity and material.
[0012] The first clamping plate 1 in the figure is designed as a plate structure, which positions and fixes the upper middle part of the rotor, thus ensuring the vertical placement of the rotor. The first clamping plate 1 has a cavity forming a first shaft hole 11 and a first wing hole 12, which respectively positions and fixes the longitudinal straight edge of the main shaft 7 and the wing plate 8 at one end of the rotor. The shaft center of the first shaft hole 11 is ensured to be on the same axis as the shaft center of the rotor. The first shaft hole 11 is a circular hole that fits in close contact with the circular outer wall of the main shaft 7. The first wing hole 12 adopts a design of four square holes, which are evenly arranged and extend laterally along the edge of the first shaft hole 11, thus corresponding to the overall shape of the rotor and ensuring tight and precise assembly. In practical applications, the local design of the first clamping plate 1 can be optimized as needed, such as changing the number of first wing holes 12 according to different types of rotors.
[0013] The second clamping plate 3 in the figure is also designed as a plate structure, which positions and fixes the lower middle part of the rotor, thus ensuring the vertical placement of the rotor. The second clamping plate 3 has a cavity forming a second shaft hole 31 and a second wing hole 32, which respectively positions and fixes the main shaft 7 and the inclined edge of the wing plate 8 at the other end of the rotor. The inclined edge here can ensure the positioning of the wing plate 8 in both the horizontal and vertical directions. The shaft center of the second shaft hole 31 is ensured to be on the same axis as the shaft center of the rotor. The second shaft hole 31 is a circular hole that fits in close contact with the circular outer wall of the main shaft 7. The second wing hole 32 adopts a design of four square holes, which are evenly arranged and extend laterally along the edge of the second shaft hole 31, thus corresponding to the overall shape of the rotor and ensuring tight and precise assembly. In the figure, the second wing hole 32 is aligned with the first wing hole 12 and the length of the second wing hole 32 is less than the length of the first wing hole 12. In practical applications, the partial design of the second clamping plate 3 can be optimized as needed, such as changing the number of second wing holes 32 according to different types of rotors.
[0014] The first support column 2 in the figure has multiple fixed on the base plate 5 and below the first clamping plate 1 to support and fix the first clamping plate 1. The first support column 2 can be designed as a fixed type or a cylinder lifting type. If it is designed as a cylinder lifting type, it can drive the first clamping plate 1 to rise and fall.
[0015] The second support column 4 in the figure has multiple fixed on the base plate 5 and below the second clamping plate 3 to support and fix the second clamping plate 3. The second support column 4 can be designed as a fixed type or a cylinder lifting type. If it is designed as a cylinder lifting type, it can drive the second clamping plate 3 to rise and fall.
[0016] The base plate 5 in the figure is a conventional plate structure with a positioning hole 51 in the center, which is a cavity structure, so as to facilitate the positioning and fixing of the shaft head 71 at the bottom end of the rotor.
[0017] The base column 6 in the figure has multiple columns and is fixed below the base plate 5 to support the base plate 5. Its overall cylindrical design ensures sufficient support.
[0018] The specific embodiments described above are merely illustrative of the present technical solution and are not intended to limit the present technical solution. In the description of the present technical solution, it should be noted that terms such as "upper" and "inner" indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. These terms are only for the convenience of describing the present technical solution and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on the present technical solution.
[0019] Furthermore, in the description of this technical solution, it should be noted that, unless otherwise explicitly specified and limited, the terms "fixed" and "fitting" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal communication of two components or the interaction between two components. Those skilled in the art can understand the specific meaning of the above terms in this technical solution according to the specific circumstances.
[0020] Although embodiments of the present technical solution have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present technical solution, the scope of which is defined by the appended claims and their equivalents.
Claims
1. A rotor welding auxiliary positioning device, comprising: characterized in that: The first clamping plate (1) has a first shaft hole (11) and a first wing hole (12) inside, which respectively position and fix the longitudinal straight edge of the main shaft (7) and the wing plate (8) at one end of the rotor; The second clamping plate (3) has a second shaft hole (31) and a second wing hole (32) inside, which respectively position and fix the inclined side of the main shaft (7) and the wing plate (8) at the other end of the rotor. The length of the second wing hole (32) is less than the length of the first wing hole (12). The first shaft hole (11), the first wing hole (12), the second shaft hole (31), and the second wing hole (32) are all aligned. The first support column (2) is fixed on a base plate (5) to support the first clamping plate (1); The second support column (4) is fixed on the base plate (5) to support the second clamping plate (3); The base plate (5) has positioning holes (51) to position and fix the shaft head (71) of the spindle (7); The base column (6) is fixed below the base plate (5) to support the base plate (5).
2. The rotor welding auxiliary positioning device according to claim 1, characterized in that: The first clamping plate (1) is a plate-shaped structure. The first shaft hole (11) is a round hole structure and is located in the middle position. The first wing hole (12) is a square hole structure and extends laterally outward along the edge of the first shaft hole (11).
3. The rotor welding auxiliary positioning device according to claim 2, characterized in that: The second clamping plate (3) is a plate-shaped structure. The second shaft hole (31) is a round hole structure and is located in the middle. The shaft center of the second shaft hole (31) is the same as the shaft center of the first shaft hole (11) and is also the same as the shaft center of the main shaft (7). The second wing hole (32) is a square hole structure and extends laterally outward along the edge of the second shaft hole (31). The second wing hole (32) is aligned with the first wing hole (12).
4. The rotor welding auxiliary positioning device according to claim 3, characterized in that: The first support column (2) is a lifting cylinder, which has multiple cylinders and is evenly arranged below the first clamping plate (1) to drive the first clamping plate (1) to rise and fall.
5. The rotor welding auxiliary positioning device according to claim 4, characterized in that: The second support column (4) is a lifting cylinder, which has multiple cylinders and is evenly arranged below the second clamping plate (3) to drive the second clamping plate (3) to rise and fall.