A support tool for disassembling and assembling a rotating component of a gas turbine

By using a slide rail-supported transport structure and a split bracket design, the safety, precision, and efficiency issues in the disassembly and assembly of rotating gas turbine components have been resolved, enabling efficient and safe disassembly and assembly operations while reducing costs and manpower requirements.

CN122165332APending Publication Date: 2026-06-09QINHUANGDAO TURBINE TECHNOLOGY DEVELOPMENT CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
QINHUANGDAO TURBINE TECHNOLOGY DEVELOPMENT CO LTD
Filing Date
2026-04-30
Publication Date
2026-06-09

Smart Images

  • Figure CN122165332A_ABST
    Figure CN122165332A_ABST
Patent Text Reader

Abstract

This invention relates to the field of gas turbine maintenance technology and discloses a support fixture for disassembling and assembling rotating components of a gas turbine. It adopts a slide rail support and transport working structure. During operation, external traction assistance allows for convenient and quick lateral transport of the disassembled gas turbine. Compared to traditional hoisting and movement methods, it offers better operational convenience and stability. Furthermore, the slide rail support replaces manual assistance for stabilization, eliminating the need for operators to handle heavy objects. This significantly reduces manpower consumption during gas turbine disassembly and greatly improves operational safety. The connecting beam is designed as a split type, allowing for adjustment of the support width by replacing the beam. The support slide rail is guided by a limiting side seat and limited by limiting bolts for installation. The overall support length can be adjusted through telescopic adjustment, greatly enhancing the device's operational flexibility and enabling it to meet the disassembly and assembly support requirements of gas turbines of different sizes.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] This invention relates to the field of gas turbine maintenance technology, specifically a support fixture for disassembling and assembling rotating components of a gas turbine. Background Technology

[0002] Gas turbines, as core power equipment, are widely used in aviation, shipbuilding, power generation and industrial drive fields. Their core rotating components include compressor rotors, turbine rotors and power turbine rotors. These components have precise structures, large weights and extremely high assembly precision requirements.

[0003] Disassembly and assembly operations are a core part of the daily maintenance, troubleshooting, and overhaul of gas turbines, directly affecting the reliability and safety of equipment operation. Existing disassembly and assembly technologies have the following problems: 1) Insufficient safety: Relying on overhead cranes and manual positioning, there is a risk of component collision damage or falling due to shaking; 2) Low positioning accuracy: The temporary support has no guiding function, and manual adjustment of coaxiality is time-consuming (requiring 2-3 hours per time) and has large errors; 3) Inefficient: Traditional methods require 4-6 people to work together, and a single disassembly and assembly cycle takes more than 6 hours; 4) Poor versatility: Different models of components require customized special brackets, resulting in high equipment costs (annual maintenance costs increase by 30%).

[0004] Therefore, there is an urgent need for a special tooling that integrates stable support, precise guidance, and convenient movement functions to solve the above-mentioned technical pain points. To this end, a support tooling for disassembling and assembling rotating components of a gas turbine is proposed. Summary of the Invention

[0005] The purpose of this invention is to provide a support fixture for disassembling and assembling rotating components of a gas turbine, so as to solve the problems mentioned in the background art.

[0006] To achieve the above objectives, the present invention provides the following technical solution: a support fixture for disassembling and assembling rotating components of a gas turbine, comprising a support mechanism and a transport mechanism. The support mechanism includes a main support column, a secondary support column, a slide rail support, a support slide rail, and a connecting beam. The slide rail support and the support slide rail are arranged in pairs. The main support column and the secondary support column are both supported and installed on the lower part of the slide rail support. The lower part of the secondary support column is adjustablely equipped with telescopic support legs. The connecting beam is detachably installed between the two sets of main support columns. The support slide rail is movably and adjustablely installed on the upper part of the slide rail support. The transport mechanism includes roller seats and supporting rollers. Multiple roller seats are provided, and the roller seats are movably mounted on the upper part of the supporting slide rail by means of the supporting rollers.

[0007] Preferably, multiple main support columns are provided. The main support columns are vertically fixed to the lower rear side of the slide rail support by means of brackets. The secondary support columns are provided in pairs. The secondary support columns are vertically fixed to the lower front side of the slide rail support by means of brackets.

[0008] Preferably, the upper part of the telescopic support leg is fixedly installed with a docking support, which is fitted and supported by the lower groove side of the auxiliary support column.

[0009] Preferably, a fastening bolt is installed in the hole in the middle of the above-mentioned secondary support column, and a long slot is opened through the middle of the telescopic leg. The middle of the fastening bolt is movably fitted into the long slot. After installation, the telescopic leg is fixedly installed to the secondary support column by the fastening bolt.

[0010] Preferably, multiple connecting beams are provided, and each end of the connecting beam is fixedly installed with an installation end seat. The installation end seat is fixedly installed to the inner side of the main support column by bolts, and the middle of the installation end seat is provided with an elliptical groove for bolt installation.

[0011] Preferably, limiting side seats are fixedly installed on both sides of the slide rail support. Multiple limiting side seats are provided. The supporting slide rail is supported and installed on the upper part of the slide rail support. After installation, the edge of the supporting slide rail and the limiting side seats are slidably fitted and supported. An end limiting seat is fixed on the upper inner side of the limiting side seat.

[0012] Preferably, a connecting end seat is fixedly installed at the rear of the aforementioned support slide rail. The upper rear side of the slide rail support is provided with equidistant limit screw holes. The inner side of the limit screw holes is threaded with a limit bolt for locking the connecting end seat. The middle of the connecting end seat is provided with an elliptical groove for installing the limit bolt.

[0013] Preferably, the aforementioned support roller is rotatably mounted on the lower part of the roller seat via a rotating shaft, and the upper part of the roller seat is provided with a docking bolt hole and a traction docking hole.

[0014] Preferably, the above-mentioned support slide rail is provided with a guide groove cavity in the middle, the support roller is rolled and supported on the bottom side of the guide groove cavity, and inner limit supports are fixedly installed on both the front and rear sides of the guide groove cavity, and buffer rubber pads are fixedly installed on the inner side of the inner limit supports.

[0015] Preferably, both sets of the above-mentioned support slide rails are fixedly installed with mating side seats on the inner side of the front part, and the mating side seats have bolt mounting holes in the middle.

[0016] Compared with the prior art, the present invention, employing the above technical solution, has the following technical effects: The working structure adopts a sliding rail support and transportation type. The roller seat is used as the load-bearing support structure and is installed in conjunction with the lower part of the gas turbine. The roller seat is moved and supported by the support sliding rail. During operation, the side movement and transportation of the disassembled gas turbine can be completed conveniently and quickly with the help of external traction. The transportation structure is simple and the support is stable. Compared with the traditional hoisting and movement, it has better operation convenience and working stability. Moreover, the sliding rail support replaces manual assistance for stabilization. The operators do not need to touch the heavy objects. While reducing the manpower consumption of gas turbine disassembly operation, it can also greatly improve the operation safety.

[0017] The device adopts a split-type bracket installation structure, with the connecting crossbeam set as a split type. By replacing the connecting crossbeam, the support width of the device can be controlled and adjusted. Furthermore, the split-type support slide rail is supported and installed through slide rail supports. The support slide rail is guided by the limit side seat and limited by the limit bolt for working installation. The overall support length of the device can be adjusted by telescopic adjustment, which greatly improves the working flexibility of the device and enables the device to meet the disassembly and assembly support requirements of gas turbines of different sizes. Attached Figure Description

[0018] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0019] Figure 1 This is a schematic diagram of the upper structure of the overall working assembly of the present invention; Figure 2 This is a schematic diagram of the lower structure of the overall working assembly of the present invention; Figure 3 This is a schematic diagram of the working installation structure of the connecting beam of the present invention; Figure 4 This is a schematic diagram of the working installation structure of the supporting slide rail of the present invention; Figure 5 For the present invention Figure 1 Schematic diagram of the structure of region A in the middle; Figure 6 For the present invention Figure 1 Schematic diagram of the structure of region B in the middle.

[0020] Explanation of reference numerals in the attached diagram: 1. Main support column; 2. Secondary support column; 3. Slide rail support; 4. Support slide rail; 5. Connecting crossbeam; 6. Roller seat; 7. Telescopic support leg; 8. Connecting end seat; 9. Limiting bolt; 10. Inner limiting support; 11. Buffer rubber pad; 12. Limiting side seat; 13. Butt joint side seat; 14. Support roller. Detailed Implementation

[0021] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0022] It should be noted that the structures, proportions, sizes, etc., shown in the accompanying drawings of this specification are only for the purpose of assisting those skilled in the art in understanding and reading the content disclosed in the specification, and are not intended to limit the conditions under which this application can be implemented. Therefore, they have no substantial technical significance. Any modifications to the structure, changes in the proportions, or adjustments to the size should still fall within the scope of the technical content disclosed in this application, provided that they do not affect the effects and purposes that this application can produce. Example

[0023] Please see Figure 1-6 This invention provides a technical solution: a support fixture for disassembling and assembling rotating components of a gas turbine, comprising a support mechanism and a transport mechanism, specifically: The support structure is used for the load-bearing installation of the transport mechanism. The support structure includes a main support column 1, a secondary support column 2, a slide rail support 3, a support slide rail 4, and a connecting crossbeam 5, as shown in the attached diagram. Figure 1 As shown, the slide rail support 3 and the supporting slide rail 4 are both set in pairs. The main support column 1 and the auxiliary support column 2 are both installed on the lower part of the slide rail support 3 for installation support. Specifically, there are four main support columns 1, which are vertically fixed to the lower rear side of the slide rail support 3 by brackets. The auxiliary support columns 2 are set in pairs, and are vertically fixed to the lower front side of the slide rail support 3 by brackets. Both the main support columns 1 and the auxiliary support columns 2 are made of Q345B steel welded into a rectangular frame. To improve the stability of the support connection, a 10mm thick steel plate is welded to the bottom of the column. The bottom plate of the column is fitted with M30×150mm adjustable anchor bolts to achieve rapid movement and rigid fixation of the tooling. To facilitate the adjustment of the auxiliary support column 2 for connection support, see attached... Figure 4 As shown, a telescopic support leg 7 is adjustablely installed at the lower part of the secondary support column 2, and a docking support is fixedly installed at the upper part of the telescopic support leg 7. The docking support is fitted and supported by the slot side of the lower part of the secondary support column 2. In order to facilitate adjustment of the limit, a fastening bolt is installed in the hole opened in the middle of the secondary support column 2. A long slot is opened through the middle of the telescopic support leg 7, and the middle part of the fastening bolt is movably fitted with the long slot. After installation, the telescopic support leg 7 is fixedly installed to the secondary support column 2 by the fastening bolt.

[0024] The connecting beam 5 is detachably installed between the two sets of main support columns 1, and is used for the middle joint support connection of the two main support columns 1, as shown in the attached figure. Figure 3 As shown, there are four connecting beams 5. To facilitate the docking and installation, mounting end seats are fixedly installed at both ends of the connecting beams 5. The mounting end seats are fixedly installed to the inner side of the main support column 1 by bolts. The support width of the device can be controlled and adjusted by replacing the connecting beams 5. To facilitate the installation and adjustment, an elliptical groove for bolt installation is provided in the middle of the mounting end seat.

[0025] The support rail 4 is used for the moving support of the transport mechanism. The support rail 4 is movably and adjustablely installed on the upper part of the rail support 3, as shown in the attached figure. Figure 4 As shown, the slide rail support 3 uses thick channel steel as the supporting guide rail steel beam for the slide rail 4. The slide rail 4 is supported and installed on the upper part of the slide rail support 3. In order to improve the installation stability of the slide rail 4, limit seats 12 are fixedly installed on both sides of the slide rail support 3. The limit seats 12 are provided with multiple equidistantly distributed on the side of the slide rail support 3. After installation, the side of the slide rail 4 slides and fits into the limit seats 12 for support. To prevent the slide rail 4 from moving out, as shown in the attached figure... Figure 6 As shown, an end limit seat is fixed on the upper inner side of the limit seat 12. The connecting beam 5 is set as a split type. By replacing the connecting beam 5, the support width of the device can be controlled and adjusted. The split support slide rail 4 is supported and installed by the slide rail support 3. The support slide rail 4 is guided by the limit seat 12 and limited by the limit bolt 9 for working installation. The overall support length of the device can be adjusted by telescopic adjustment, which greatly improves the working flexibility of the device. The device can meet the disassembly and assembly support requirements of gas turbines of different sizes, reduce the procurement cost of special brackets by 60%, and reduce the annual maintenance cost by 250,000 yuan.

[0026] As attached Figure 6 As shown, in order to achieve the locking limit of the adjusted support slide rail 4, a connecting end seat 8 is fixedly installed at the rear of the support slide rail 4. For convenient adjustment and positioning of the support slide rail 4, see attached... Figure 4 As shown, equidistant limit screw holes are evenly spaced on the upper rear side of the slide rail support 3. The inner side of the limit screw holes is threaded with limit bolts 9 for locking the connecting end seat 8. To facilitate installation and adjustment, an elliptical groove for installing the limit bolts 9 is provided in the middle of the connecting end seat 8. To facilitate docking with the ground support point, docking side seats 13 are fixedly installed on the inner front side of both sets of support slide rails 4. The docking side seats 13 have bolt mounting holes in the middle.

[0027] The transport mechanism is used for disassembly, support, and docking of rotating components of the gas turbine. The transport mechanism includes roller seats 6 and support rollers 14. Four roller seats 6 are provided, as shown in the attached diagram. Figure 5 As shown, the support roller 14 is rotatably mounted on the lower part of the roller seat 6 via a rotating shaft. The roller seat 6 is movably mounted on the upper part of the support slide rail 4 via the support roller 14. Specifically, to achieve the guiding support of the roller seat 6, a guide groove is provided in the middle of the support slide rail 4. The support roller 14 is rolled and supported on the bottom side of the guide groove. A slide rail support and loading working structure is adopted, in which the roller seat 6 is used as a load-bearing support structure and docked with the lower part of the gas turbine. The support slide rail 4 provides movable support for the roller seat 6. During operation, the roller seat 6 is moved and supported by the support roller 14. External traction assistance facilitates the convenient and quick side-shifting and transport of the disassembled gas turbine. The transport structure is simple and stable, offering better operational convenience and stability compared to traditional hoisting methods. Furthermore, the use of sliding rails replaces manual assistance for stability, eliminating the need for personnel to handle heavy loads. This significantly reduces manpower consumption during gas turbine disassembly and greatly improves operational safety. In practice, the disassembly and assembly time per operation has been reduced from 6 hours to 2 hours, and the required workforce has been reduced from 6 to 2 people. For convenient docking and installation with gas turbine components, see attached... Figure 5 As shown, the upper part of the roller seat 6 is provided with docking bolt holes and traction docking holes. In order to realize the displacement support and limit of the roller seat 6, as shown in the attached figure... Figure 6 As shown, inner limit supports 10 are fixedly installed on both the front and rear sides inside the guide groove cavity. In order to improve the buffer support and protection of the inner limit supports 10, a buffer rubber pad 11 is fixedly installed on the inner side of the inner limit supports 10. Specifically, the buffer rubber pad 11 is a neoprene rubber soft pad with a thickness of 5mm.

[0028] Working principle or structural principle: Unit assembly: Select the corresponding connecting beam 5 according to the model and specifications of the gas turbine to be disassembled and assembled. Then, use bolts to connect and install multiple sets of connecting beams 5 between two adjacent sets of main support columns 1. Then, align and install the support slide rail 4 on the upper part of the slide rail support 3. Then, use the limit bolt 9 to lock and limit the installed support slide rail 4. Finally, support the roller seat 6 on the upper part of the support slide rail 4 to complete the assembly and installation of the unit. Device installation: The tooling is connected to the skid base with bolts to complete the overall installation and positioning of the device. Then, the bolts on the side of the telescopic support leg 7 at the bottom of the auxiliary support column 2 are loosened to make the base side of the telescopic support leg 7 stably contact the ground for support. After that, the bolts are tightened to complete the locking limit of the telescopic support leg 7 after adjustment, ensuring that the device is stably and fixedly supported and installed on the ground. Then, according to the longitudinal distance of the gas turbine, the support length of the support rail 4 is adjusted by horizontal sliding with the limit bolt 9 loosened. After adjustment, the bolt mounting hole in the middle of the docking side seat 13 at the front of the support rail 4 is aligned and overlapped with the screw hole on the upper part of the base. The docking side seat 13 is then docked and installed with the base with bolts. After completion, the adjusted support rail 4 is locked and limited by the limit bolt 9 to complete the installation of the device. Disassembly and Loading: The rotating components of the gas turbine are disassembled and separated. Then, the positions of the four sets of roller seats 6 are adjusted. After completion, the components are lifted by the lifting beam and placed on the upper part of the roller seats 6 in the middle of the support slide rail 4. After positioning, adjustment and installation are completed, and the components are locked with bolts. Then, two sets of hand chain hoists are installed on the front and rear sides of the device respectively. The disassembled components are moved and pulled by the two sets of hand chain hoists. One of the two hand chain hoists is pulled and the other is released. The two hand chain hoists work in sync. While realizing the lateral movement of the disassembled components, it can also prevent the device from slipping and moving. The device can complete the removal or pushing back of the components. During the process, the slide rail support replaces manual assistance for stabilization. The operators do not need to touch the heavy objects. This reduces the manpower consumption of gas turbine disassembly operations and greatly improves the operation safety.

[0029] In summary, the sliding rail-supported loading structure uses the roller seat 6 as the load-bearing support structure, which is connected and supported to the lower part of the gas turbine. The roller seat 6 is moved and supported by the support rail 4. During operation, the side-moving and loading of the disassembled gas turbine can be easily and quickly completed with the assistance of external traction. The transport structure is simple and the support is stable. Compared with the traditional hoisting and moving method, it has better operation convenience and working stability. Moreover, the sliding rail support replaces manual assistance for stabilization, and the operators do not need to touch the heavy objects. This reduces the manpower consumption of gas turbine disassembly operations and greatly improves the operation safety. The split bracket installation structure is adopted, and the connecting beam 5 is set as a split type. By replacing the connecting beam 5, the support width of the device can be controlled and adjusted. The split support rail 4 is supported and installed by the sliding rail support 3. The support rail 4 is guided by the limiting side seat 12 and limited by the limiting bolt 9 for working installation. The overall support length of the device can be adjusted by telescopic adjustment, which greatly improves the working flexibility of the device and enables the device to meet the disassembly and assembly support requirements of gas turbines of different sizes.

[0030] Those skilled in the art will understand that the features described in the various embodiments and / or claims of the present invention can be combined or combined in various ways, even if such combinations or combinations are not explicitly described in the present invention. In particular, the features described in the various embodiments and / or claims of the present invention can be combined or combined in various ways without departing from the spirit and teachings of the present invention. All such combinations and / or combinations fall within the scope of the present invention.

Claims

1. A support fixture for disassembling and assembling rotating components of a gas turbine, comprising a support mechanism and a transport mechanism, characterized in that, The support structure includes a main support column (1), a secondary support column (2), a slide rail support (3), a support slide rail (4), and a connecting beam (5). The slide rail support (3) and the support slide rail (4) are arranged in pairs. The main support column (1) and the secondary support column (2) are both supported and installed on the lower part of the slide rail support (3). The lower part of the secondary support column (2) is adjustablely equipped with telescopic support feet (7). The connecting beam (5) is detachably installed between the two sets of main support columns (1). The support slide rail (4) is movably and adjustablely installed on the upper part of the slide rail support (3). The transport mechanism includes a roller seat (6) and a support roller (14). Multiple roller seats (6) are provided, and the roller seats (6) are movably mounted on the upper part of the support slide rail (4) by the support rollers (14).

2. The support fixture for disassembling and assembling rotating components of a gas turbine according to claim 1, characterized in that, Multiple main support columns (1) are provided. The main support columns (1) are vertically fixed and installed on the lower rear side of the slide rail support (3) by means of brackets. The auxiliary support columns (2) are provided in pairs. The auxiliary support columns (2) are vertically fixed and installed on the lower front side of the slide rail support (3) by means of brackets.

3. The support fixture for disassembling and assembling rotating components of a gas turbine according to claim 2, characterized in that, The upper part of the telescopic support leg (7) is fixedly installed with a docking support, which is fitted and supported by the lower groove side of the auxiliary support column (2).

4. The support fixture for disassembling and assembling rotating components of a gas turbine according to claim 3, characterized in that, A fastening bolt is installed in the hole in the middle of the secondary support column (2). A long slot is opened through the middle of the telescopic support leg (7). The middle of the fastening bolt is movably fitted into the long slot. After installation, the telescopic support leg (7) is fixedly installed to the secondary support column (2) by the fastening bolt.

5. A support fixture for disassembling and assembling rotating components of a gas turbine according to claim 4, characterized in that, Multiple connecting beams (5) are provided. Both ends of the connecting beams (5) are fixedly installed with mounting end seats. The mounting end seats are fixedly installed to the inner side of the main support column (1) by bolts. The middle part of the mounting end seat is provided with an elliptical groove for bolt installation.

6. The support fixture for disassembling and assembling rotating components of a gas turbine according to claim 1, characterized in that, Both sides of the slide rail support (3) are fixedly installed with limiting side seats (12). Multiple limiting side seats (12) are provided. The supporting slide rail (4) is supported and installed on the upper part of the slide rail support (3). After installation, the side of the supporting slide rail (4) and the limiting side seat (12) are slidably fitted and supported. The upper inner side of the limiting side seat (12) is fixed with an end limiting seat.

7. A support fixture for disassembling and assembling rotating components of a gas turbine according to claim 6, characterized in that, The rear of the support slide rail (4) is fixedly installed with a connecting end seat (8). The upper rear side of the slide rail support (3) is evenly provided with equidistant limit screw holes. The inner side of the limit screw holes is threaded with a limit bolt (9) for locking the connecting end seat (8) for limiting. The middle part of the connecting end seat (8) is provided with an elliptical groove for installing the limit bolt (9).

8. A support fixture for disassembling and assembling rotating components of a gas turbine according to claim 7, characterized in that, The support roller (14) is rotatably mounted on the lower part of the roller seat (6) by means of a rotating shaft. The upper part of the roller seat (6) is provided with a docking bolt hole and a traction docking hole.

9. A support fixture for disassembling and assembling rotating components of a gas turbine according to claim 8, characterized in that, The middle part of the support slide rail (4) is provided with a guide groove cavity. The support roller (14) is rolled and supported on the bottom side of the guide groove cavity. The inner limit support (10) is fixedly installed on both the front and rear sides of the guide groove cavity. The inner side of the inner limit support (10) is fixedly installed with a buffer rubber pad (11).

10. A support fixture for disassembling and assembling rotating components of a gas turbine according to claim 9, characterized in that, Both sets of support slide rails (4) have a mating seat (13) fixedly installed on the inner side of the front part, and the mating seat (13) has a bolt mounting hole in the middle.