A gas turbine rotor transfer tooling

CN224739421UActive Publication Date: 2026-09-11CHENGDU CHENGFA SCI & TECH POWER ENG
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Patent Information

Application Number
CN202522413756.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-11-13
Publication Date
2026-09-11
Estimated Expiration
2035-11-13

AI Technical Summary

Technical Problem

[0003]本实用新型的目的在于提供一种燃气轮机转子转移工装,以解决现有的燃气轮机转子在存放以及转移过程中容易发生窜动且容易出现磨损的问题

Benefits of technology

在需要将燃气轮机的转子进行存放或者转移时,让夹持机构的定位通道处于开放状态,然后将转子的轴端两侧分别放置在夹持机构上开放的定位通道内,然后将定位通道封堵,让转子的轴端两侧分别被夹持在两定位通道内。完成后,将螺纹杆对准转子轴端的同轴螺纹孔内,通过转动螺纹杆,让螺纹杆装入转子的轴端,然后让螺纹杆与止动机构的主体定位连接,从而完成对转子的止动。在夹持机构和支撑机构的双重作用下,即便是在转运过程中,转子也不会发生轴线的窜动以及环绕轴线的转动。从而有效的避免了因为转子的转动和窜动,而造成转子轴端与夹持机构之间的磨损,极大的提高了转子的存放过程中以及转运过程中的稳定性以及完好性。

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Abstract

The utility model discloses a gas turbine rotor transfer frock relates to rotor positioning transfer technical field. The utility model discloses a mobile mechanism constructs with base plate and installs the lock universal wheel of moving part as the base plate bottom surface, support mechanism is located the top surface of base plate and is mutually symmetrical and is equipped with a pair, all are provided with clamping mechanism on its top, and the locating channel of coaxial arrangement is constructed on two clamping mechanisms respectively, stop mechanism is located the outside of one support mechanism, and the top constructs the stop portion, the stop portion constructs with the thread rod of coaxial arrangement with the locating channel, and the thread end of thread rod is toward locating channel, and the main body of stop mechanism is positioned and is connected with thread rod, to solve the problem that the current gas turbine rotor is easy to move and is easy to wear and tear in the storage and transfer process.
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Description

Technical Field

[0001] This utility model relates to the field of rotor positioning and transfer technology, specifically, a gas turbine rotor transfer tooling. Background Technology

[0002] The gas turbine rotor is the core component of the gas turbine, and it is expensive, structurally precise, and heavy. During manufacturing, maintenance, and storage, the rotor needs to be frequently hoisted, stored, and transferred within the plant. The traditional method is to place the rotor directly on a V-shaped iron block or a simple support, which has the following drawbacks: (1) The fixing is not secure, and it is easy to roll or move axially, posing a safety hazard of tipping over and injuring people; (2) There is a lack of effective buffering and protection measures, and the rotor surface (especially critical parts such as bearing journals and gear meshing surfaces) is easily damaged, scratched, or deformed due to rigid contact or collision; (3) Transfer is extremely inconvenient, usually requiring multiple hoisting operations with the help of overhead cranes and forklifts, which is cumbersome, inefficient, and poses a risk of secondary collisions. Therefore, there is an urgent need for a special tooling equipment that integrates storage, protection, and transfer functions to ensure the safety and ease of operation of the rotor. Utility Model Content

[0003] The purpose of this invention is to provide a gas turbine rotor transfer fixture to solve the problems of easy movement and wear of existing gas turbine rotors during storage and transfer.

[0004] To solve the above problems, the present invention adopts the following technical means: A gas turbine rotor transfer fixture, comprising: The moving mechanism comprises a base plate and a lockable universal wheel mounted on the bottom surface of the base plate as a moving part. A pair of support mechanisms are provided on the top surface of the substrate and are symmetrically arranged. Each of them is provided with a clamping mechanism at its top end, and each of the two clamping mechanisms is provided with a coaxially arranged positioning channel. A stop mechanism is provided on the outside of one of the support mechanisms, and a stop part is constructed at the top. The stop part is constructed with a threaded rod coaxially arranged with the positioning channel. The threaded end of the threaded rod faces the positioning channel, and the threaded rod is positioned and connected to the main body of the stop mechanism.

[0005] Preferably, a lifting plate is also installed on the top surface of the substrate, and the lifting plate is provided with through holes for positioning.

[0006] Furthermore, the support mechanism includes a straight rod installed on the top surface of the substrate, and support rods with their top ends inclined toward the top end of the straight rod are respectively provided on the front and rear sides of the straight rod. The bottom end of the support rod is connected to the top surface of the substrate, and a bearing platform is installed at the top end of the straight rod. The top end of the support rod is connected to the bottom surface of the bearing platform, and the clamping mechanism is installed on the top surface of the bearing platform.

[0007] Furthermore, the clamping mechanism includes a bearing plate installed at the top of the support mechanism. The top of the bearing plate is constructed with a first arc groove, and an arc plate is detachably installed on the top surface of the bearing plate. The arc surface of the arc plate is configured as a second arc groove with the opening facing downward. The first arc groove and the second arc groove are spliced ​​together to form the positioning channel for clamping the shaft end of the rotor.

[0008] Furthermore, rubber pads are attached and installed in the first arc groove and the second arc groove respectively.

[0009] Furthermore, the stopping mechanism includes a mounting plate installed on the outer side wall of the support mechanism. A positioning plate is installed on the top surface of the mounting plate. A horizontal threaded rod is installed on the top end of the positioning plate. The positioning part of the threaded rod slides through the positioning plate. Two clamping nuts are threadedly installed on the positioning part of the threaded rod. The positioning plate is clamped between the two clamping nuts.

[0010] Furthermore, a first reinforcing rib is installed at the corner where the bottom side of the positioning plate connects to the mounting plate, and a second reinforcing rib is installed at the vertically extending position of the positioning plate.

[0011] This utility model has the following beneficial effects during use: When storing or transferring a gas turbine rotor, the positioning channels of the clamping mechanism are opened. The rotor shaft ends are then placed into the open positioning channels of the clamping mechanism, and the channels are sealed, clamping the rotor shaft ends into the two positioning channels respectively. Afterward, the threaded rod is aligned with the coaxial threaded hole on the rotor shaft end. By rotating the threaded rod, it is inserted into the rotor shaft end, and then the threaded rod is positioned and connected to the main body of the stop mechanism, thus stopping the rotor. Under the combined action of the clamping and support mechanisms, even during transfer, the rotor will not experience axial movement or rotation around its axis. This effectively avoids wear between the rotor shaft end and the clamping mechanism caused by rotor rotation and movement, greatly improving the stability and integrity of the rotor during storage and transfer. Attached Figure Description

[0012] Figure 1 This is a first-view structural diagram of the present invention.

[0013] Figure 2 This is a schematic diagram of the second-view structure of the present invention.

[0014] Among them, 1-base plate, 2-moving part, 3-threaded rod, 4-lifting plate, 5-straight rod, 6-support rod, 7-bearing platform, 8-bearing plate, 9-first arc groove, 10-arc plate, 11-second arc groove, 12-rubber pad, 13-mounting plate, 14-positioning plate, 15-compression nut, 16-first reinforcing rib, 17-second reinforcing rib. Detailed Implementation

[0015] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. The components of the embodiments of this utility model described and shown in the accompanying drawings can typically be arranged and designed in various different configurations.

[0016] Therefore, the following detailed description of the embodiments of the present invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely to illustrate selected embodiments of the invention. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without inventive effort are within the scope of protection of the present invention.

[0017] It should be noted that, where there is no conflict, the embodiments and features in the embodiments of this utility model can be combined with each other.

[0018] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0019] In the description of this utility model, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship commonly used when the product of this utility model is in use, or the orientation or positional relationship commonly understood by those skilled in the art. They are only used for the convenience of describing this utility model 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 this utility model. In addition, the terms "first," "second," etc., are only used to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0020] In the description of this utility model, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set," "install," "connect," and "link" 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 mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0021] Please refer to Figure 1 and Figure 2 As shown, a gas turbine rotor transfer fixture includes: The moving mechanism comprises a base plate 1 and a lockable universal wheel mounted on the bottom surface of the base plate 1 as a moving part 2; A pair of support mechanisms are provided on the top surface of the substrate 1 and are symmetrically arranged. Each of them is provided with a clamping mechanism at its top, and the two clamping mechanisms are respectively provided with a coaxially arranged positioning channel. A stop mechanism is provided on the outside of one of the support mechanisms, and a stop part is constructed at the top. The stop part is constructed with a threaded rod 3 coaxially arranged with the positioning channel. The threaded end of the threaded rod 3 faces the positioning channel, and the threaded rod 3 is positioned and connected to the main body of the stop mechanism.

[0022] In this way, when the gas turbine rotor needs to be stored or transferred, the positioning channels of the clamping mechanism are kept open, and the two sides of the rotor shaft end are placed in the open positioning channels of the clamping mechanism. Then, the positioning channels are sealed, so that the two sides of the rotor shaft end are clamped in the two positioning channels respectively. After completion, the threaded rod 3 is aligned with the coaxial threaded hole of the rotor shaft end. By rotating the threaded rod 3, it is inserted into the rotor shaft end. Then, the threaded rod 3 is positioned and connected to the main body of the stop mechanism, thereby stopping the rotor. Under the dual action of the clamping mechanism and the support mechanism, even during the transfer process, the rotor will not experience axial movement or rotation around the axis. This effectively avoids wear between the rotor shaft end and the clamping mechanism caused by rotor rotation and axial movement, greatly improving the stability and integrity of the rotor during storage and transfer.

[0023] To facilitate movement, a lifting plate 4 is also installed on the top surface of the substrate 1, and the lifting plate 4 is provided with through holes for positioning.

[0024] In this way, in addition to transferring the rotor by pushing, the hoisting mechanism can also be used to hoist the entire tooling and rotor by connecting the hoisting part of the hoisting mechanism with the through hole of the hoisting plate 4. Even if shaking occurs during the hoisting process, the rotor can be prevented from rotating or shifting due to the clamping and stopping mechanisms, thus ensuring the stability and integrity of the hoisting process.

[0025] Furthermore, the support mechanism includes a straight rod 5 installed on the top surface of the substrate 1. Support rods 6 with their top ends inclined towards the top of the straight rod 5 are respectively provided on the front and rear sides of the straight rod 5. The bottom end of the support rod 6 is connected to the top surface of the substrate 1. A bearing platform 7 is installed on the top of the straight rod 5. The top end of the support rod 6 is connected to the bottom surface of the bearing platform 7. The clamping mechanism is installed on the top surface of the bearing platform 7.

[0026] Furthermore, the clamping mechanism includes a bearing plate 8 installed at the top of the support mechanism. The top of the bearing plate 8 is constructed with a first arc groove 9. An arc plate 10 is detachably installed on the top surface of the bearing plate 8. The arc surface of the arc plate 10 is configured as a second arc groove 11 with the opening facing downward. The first arc groove 9 and the second arc groove 11 are spliced ​​together to form the positioning channel for clamping the shaft end of the rotor.

[0027] Thus, when the bearing plate 8 is separated from the arc plate 10, the positioning channel is in an open state. When the arc plate 10 and the bearing plate 8 are in close contact through bolts, so that the first arc groove 9 and the second arc groove 11 are spliced ​​to form a complete circular channel, the positioning channel is in a clamped state, and the shaft end of the rotor is locked by the clamping of the first arc groove 9 and the second arc groove 11.

[0028] Furthermore, rubber pads 12 are respectively attached and installed in the first arc groove 9 and the second arc groove 11.

[0029] In this way, the rubber pad 12 not only further avoids hard contact between the rotor shaft end and the inner wall of the positioning channel, but also allows the relatively fixed positioning channel to stably clamp rotor shaft ends of different diameters by removing and installing rubber pads 12 of different thicknesses.

[0030] Furthermore, the stopping mechanism includes a mounting plate 13 installed on the outer wall of the support mechanism. A positioning plate 14 is installed on the top surface of the mounting plate 13. A horizontal threaded rod 3 is installed on the top end of the positioning plate 14. The positioning part of the threaded rod 3 slides through the positioning plate 14. Two clamping nuts 15 are threadedly installed on the positioning part of the threaded rod 3. The positioning plate 14 is clamped between the two clamping nuts 15.

[0031] Thus, when the threaded rod 3 is rotated, the two deposit nuts are loosened, allowing the threaded rod 3 to rotate normally, thereby enabling it to be inserted into or removed from the rotor shaft end. After the threaded rod 3 is inserted, the two deposit nuts are used to clamp the positioning plate 14, thereby achieving a positioning connection between the threaded rod 3 and the positioning plate 14, and thus stopping the rotor shaft end. This prevents the rotor from axially shifting or rotating around its axis during transfer.

[0032] Furthermore, a first reinforcing rib 16 is installed at the corner where the bottom side of the positioning plate 14 connects to the mounting plate 13, and a vertically extending second reinforcing rib 17 is installed at the vertically extending position of the positioning plate 14.

[0033] Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.

Claims

1. A gas turbine rotor transfer fixture, characterized in that, include: The moving mechanism is constructed with a base plate (1) and a moving part (2) mounted on the bottom surface of the base plate (1). A pair of support mechanisms are provided on the top surface of the substrate (1) and are symmetrically arranged with each other. Each of them is provided with a clamping mechanism at its top, and the two clamping mechanisms are respectively provided with a positioning channel arranged coaxially. A stop mechanism is provided on the outside of one of the support mechanisms, and a stop part is constructed at the top. The stop part is constructed with a threaded rod (3) coaxially arranged with the positioning channel. The threaded end of the threaded rod (3) faces the positioning channel, and the threaded rod (3) is positioned and connected to the main body of the stop mechanism.

2. The gas turbine rotor transfer fixture according to claim 1, characterized in that, The top surface of the substrate (1) is also equipped with a lifting plate (4), and the lifting plate (4) is provided with through holes for positioning.

3. The gas turbine rotor transfer fixture according to claim 1, characterized in that, The support mechanism includes a straight rod (5) installed on the top surface of the substrate (1). Support rods (6) with their top ends inclined toward the top of the straight rod (5) are respectively provided on the front and rear sides of the straight rod (5). The bottom end of the support rod (6) is connected to the top surface of the substrate (1). A bearing platform (7) is installed on the top of the straight rod (5). The top end of the support rod (6) is connected to the bottom surface of the bearing platform (7). The clamping mechanism is installed on the top surface of the bearing platform (7).

4. The gas turbine rotor transfer fixture according to claim 1, characterized in that, The clamping mechanism includes a bearing plate (8) installed on the top of the support mechanism. The top of the bearing plate (8) is constructed with a first arc groove (9). An arc plate (10) is detachably installed on the top surface of the bearing plate (8). The arc surface of the arc plate (10) is set as a second arc groove (11) with the opening facing downward. The first arc groove (9) and the second arc groove (11) are spliced ​​together to form the positioning channel for clamping the shaft end of the rotor.

5. The gas turbine rotor transfer fixture according to claim 4, characterized in that, Rubber pads (12) are respectively attached to and installed in the first arc groove (9) and the second arc groove (11).

6. The gas turbine rotor transfer fixture according to claim 1, characterized in that, The stopping mechanism includes a mounting plate (13) installed on the outer side wall of the support mechanism. A positioning plate (14) is installed on the top surface of the mounting plate (13). A horizontal threaded rod (3) is installed on the top end of the positioning plate (14). The positioning part of the threaded rod (3) slides through the positioning plate (14). Two clamping nuts (15) are threadedly installed on the positioning part of the threaded rod (3). The positioning plate (14) is clamped between the two clamping nuts (15).

7. The gas turbine rotor transfer fixture according to claim 6, characterized in that, A first reinforcing rib (16) is installed at the corner where the bottom side of the positioning plate (14) connects to the mounting plate (13), and a vertically extending second reinforcing rib (17) is installed at the vertical extension position of the positioning plate (14).