Control assembly for gas turbine

By designing a gas turbine control assembly with adjustable height and supporting brackets, the operating blind spots of gas turbines are solved during assembly, and efficient assembly and processing operations are achieved.

CN223130665UActive Publication Date: 2025-07-22JIANGSU HUADIAN YIZHENG THERMOELECTRICITY CO LTD
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Patent Information

Application Number
CN202422431419.4
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-10-09
Publication Date
2025-07-22
Estimated Expiration
2034-10-09

AI Technical Summary

Technical Problem

When assembling existing gas turbines, one side of the control assembly needs to be fixed to the mounting plate, resulting in blind spots in operation and low assembly efficiency.

Method used

A control assembly including a machining seat, a movable seat and a support bracket is designed to achieve stable support and angle adjustment of the gas turbine through a height-adjustable movable seat and a support bracket combined with a pallet set and a drive motor.

Benefits of technology

It improves the assembly efficiency of the gas turbine, facilitates the fixing and processing operation of the gas turbine, and enhances flexibility and operation convenience.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of machining equipment for gas turbines, in particular to a control assembly for a gas turbine, which comprises a machining seat, the machining seat comprises a seat plate, a first positioning shell and a second positioning shell, and the first positioning shell and the second positioning shell are vertically mounted on two sides of the upper end face of the seat plate. The first positioning shell and the second positioning shell are fixedly connected with the seat plate, a movable seat is slidably mounted in the first positioning shell, a supporting bracket is slidably mounted in the second positioning shell, and an electric cylinder for supporting the first positioning shell and the second positioning shell is fixedly mounted on the seat plate. The movable seat with the adjustable height and the supporting bracket are installed on the machining seat, the tray set is installed on the movable seat, the gas turbine set can be stably supported easily through cooperation of the tray set and the arc-shaped supporting plate, in this way, the gas turbine can be lowered when installed, the gas turbine can be conveniently and easily fixed to equipment, and the machining efficiency of the gas turbine is improved. And then the device can be lifted up in the machining process.
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Description

Technical Field

[0001] The utility model relates to the technical field of processing equipment for gas turbines, and particularly relates to a control component for a gas turbine. Background Technique

[0002] A gas turbine uses continuously flowing gas as the working medium to drive the impeller to rotate at a high speed, converting the internal energy of the fuel into mechanical energy, and is a rotating impeller type thermal engine.

[0003] The existing Chinese patent with the publication number of CN204565554U discloses a gas turbine assembly vehicle, which includes a vehicle frame, a rotating assembly, a power device and an angle control assembly. The rotating assembly includes a main rotating bracket arranged on one side of the vehicle frame, an auxiliary rotating bracket arranged on the other side of the vehicle frame and a mounting plate. The main rotating bracket and the auxiliary rotating bracket are arranged opposite to each other, the mounting plate is arranged between the main rotating bracket and the auxiliary rotating bracket, the power device is connected to the main rotating bracket, and the angle control assembly is connected to the rotating assembly. During use, the gas turbine to be assembled is installed on the mounting plate, the power device is connected to the main rotating bracket, and the main rotating bracket is driven to drive the entire rotating assembly to rotate.

[0004] In view of the above related technologies, it is found that the control component used during the assembly of the above gas turbine needs to be fixed on one side of the mounting plate, so that the assembly of the side mounted on the mounting plate cannot be carried out during operation, and it is necessary to disassemble and operate after other parts are installed, thus there are working dead angles and relatively low assembly efficiency. Content of the Utility Model

[0005] The utility model solves the problems in the related technologies and provides a control component for a gas turbine.

[0006] In order to solve the above technical problems, the utility model is realized through the following technical solutions:

[0007] A control component for a gas turbine includes a processing seat, and the processing seat includes a seat plate, a first positioning shell and a second positioning shell. The first positioning shell and the second positioning shell are vertically installed on both sides of the upper end surface of the seat plate, and both the first positioning shell and the second positioning shell are fixedly connected to the seat plate. An activity seat is slidably installed in the first positioning shell, a support bracket is slidably installed in the second positioning shell, and an electric cylinder for supporting the first positioning shell and the second positioning shell is fixedly installed on the seat plate. A tray group is further installed in the activity seat, and a driving motor for driving the tray group to rotate is fixedly installed outside the activity seat.

[0008] As a preferred solution, the seat plate includes a bottom plate and an arc-shaped stabilizing plate. The arc-shaped stabilizing plate is arranged at both ends of the bottom plate, and the arc-shaped stabilizing plate is integrally formed with the bottom plate.

[0009] As a preferred solution, the movable seat includes a first sliding plate and a main frame housing. The first sliding plate is slidably installed in the first positioning housing, and the main frame housing is fixedly installed at the head of the first sliding plate.

[0010] As a preferred solution, a motor seat for installing a driving motor is provided on the outer side surface of the main frame housing, and the motor seat is fixedly connected to the main frame housing.

[0011] As a preferred solution, the support bracket includes a second sliding plate and an arc-shaped support plate. The second sliding plate is slidably installed in the second positioning housing, the arc-shaped support plate is fixedly installed at the head of the second sliding plate, and a limiting vertical plate is also fixedly installed on the arc-shaped support plate.

[0012] As a preferred solution, the tray group includes a tray shell and limiting arc plates. The number of the limiting arc plates is two, and both of the two limiting arc plates are snap-fitted and fixed in the tray shell.

[0013] As a preferred solution, a sleeve matched with the output shaft of the driving motor is also fixedly installed at the center of the outer side surface of the tray shell. Limiting grooves are opened on both sides of the sleeve, and a connecting shaft corresponding to the limiting grooves is fixedly installed on the output shaft of the driving motor.

[0014] Compared with the prior art, the beneficial effects of the present utility model are as follows: By installing a movable seat and a support bracket with adjustable height on the processing seat, and installing a tray group on the movable seat, it is easy to stably support the gas turbine group through the cooperation of the tray group and the arc-shaped support plate. In this way, when installing the gas turbine, it can be lowered, which is convenient for easily fixing the gas turbine on the equipment. Then, during the processing process, it can be raised, and the operating angle of the gas turbine can be flexibly adjusted by the driving motor, and the operation is very convenient. Description of the Drawings

[0015] Figure 1 is a schematic structural view of the device of the present utility model when clamping the gas turbine;

[0016] Figure 2 is Figure 1 the exploded structural view of the device shown;

[0017] Figure 3 is Figure 2 the front view of the device shown;

[0018] Figure 4 is a three-dimensional view of the tray group in the present utility model;

[0019] Figure 5 is Figure 4 the side view of the device shown.

[0020] In the figure: 1. Processing base; 11. Base plate; 111. Bottom plate; 112. Arc-shaped stabilizing plate; 12. First positioning shell; 13. Second positioning shell; 2. Movable base; 21. First sliding plate; 22. Main frame shell; 221. Motor base; 3. Support bracket; 31. Second sliding plate; 32. Arc-shaped supporting plate; 33. Limit vertical plate; 4. Electric cylinder; 5. Tray group; 51. Tray shell; 511. Sleeve; 512. Limit groove; 52. Limit arc plate; 6. Driving motor; 61. Connecting shaft; 7. Gas turbine. Specific implementation mode

[0021] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. The following description of at least one exemplary embodiment is actually only illustrative and in no way limits the present invention and its application or use. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0022] It should be noted that the terms used herein are only for describing specific implementation modes and are not intended to limit the exemplary implementation modes according to the present application. As used herein, unless otherwise clearly specified in the context, the singular form is also intended to include the plural form. In addition, it should be understood that when the terms "comprise" and / or "include" are used in this specification, they indicate the presence of features, steps, operations, devices, components, and / or combinations thereof.

[0023] Unless otherwise specifically stated, the relative arrangements, numerical expressions, and numerical values of the components and steps set forth in these embodiments do not limit the scope of the present invention. At the same time, it should be understood that for the convenience of description, the dimensions of the various parts shown in the drawings are not drawn in actual proportional relationships. Technologies, methods, and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, the technologies, methods, and devices should be regarded as part of the authorized specification. In all the examples shown and discussed here, any specific value should be interpreted as merely exemplary and not as a limitation. Therefore, other examples of the exemplary embodiments may have different values. It should be noted that similar reference numerals and letters indicate similar items in the following drawings. Therefore, once an item is defined in one drawing, it does not need to be further discussed in subsequent drawings.

[0024] In the description of the present utility model, it should be understood that the orientation or positional relationship indicated by orientation terms such as "front, rear, upper, lower, left, right", "lateral, vertical, perpendicular, horizontal", and "top, bottom", etc. is usually based on the orientation or positional relationship shown in the drawings. It is only for the convenience of describing the present utility model and simplifying the description. Without contrary description, these orientation terms do not indicate and imply that the device or component referred to must have a specific orientation or be constructed and operated in a specific orientation. Therefore, it cannot be understood as a limitation on the protection scope of the present utility model; the orientation terms "inside, outside" refer to the inside and outside relative to the contour of each component itself.

[0025] For the convenience of description, spatial relative terms can be used here, such as "above...", "over...", "on the upper surface of...", "upper...", etc., to describe the spatial positional relationship between a device or feature shown in the drawings and other devices or features. It should be understood that the spatial relative terms are intended to include different orientations in use or operation in addition to the orientation described in the drawings for the device. For example, if the device in the drawing is inverted, the device described as "above other devices or structures" or "over other devices or structures" will then be positioned as "below other devices or structures" or "under other devices or structures". Thus, the exemplary term "above..." can include both the orientations of "above..." and "below...". The device can also be positioned in other different ways (rotated 90 degrees or in other orientations), and corresponding interpretations are made for the spatial relative descriptions used here.

[0026] In addition, it should be noted that using words such as "first", "second", etc. to limit components is only for the convenience of distinguishing the corresponding components. Without separate statement, the above words have no special meaning. Therefore, it cannot be understood as a limitation on the protection scope of the present utility model.

[0027] Refer to Figure 1 、 Figure 2 and Figure 3As shown in the figure, a control component for a gas turbine includes a processing base 1. The processing base 1 includes a base plate 11, a first positioning shell 12, and a second positioning shell 13. The first positioning shell 12 and the second positioning shell 13 are vertically installed on both sides of the upper end surface of the base plate 11, and both the first positioning shell 12 and the second positioning shell 13 are fixedly connected to the base plate 11. A movable seat 2 is slidably installed in the first positioning shell 12, and a support bracket 3 is slidably installed in the second positioning shell 13. An electric cylinder 4 for supporting the first positioning shell 12 and the second positioning shell 13 is fixedly installed on the base plate 11. A tray group 5 is also installed in the movable seat 2, and a driving motor 6 for driving the tray group 5 to rotate is fixedly installed outside the movable seat 2. By setting the structure of the processing base 1, it is ensured that the first positioning shell 12 and the second positioning shell 13 are fixedly installed on the base plate 11. In this way, when in use, the movable seat 2 and the support bracket 3 can be installed through the first positioning shell 12 and the second positioning shell 13 respectively. During use, the support heights of the movable seat 2 and the support bracket 3 can be controlled by the electric cylinder 4. At the same time, by installing the tray group 5 in the movable seat 2, the two ends of the gas turbine 7 can be clamped and supported through the cooperation of the tray group 5 and the support bracket 3. In this way, when processing the gas turbine 7, the gas turbine 7 can be driven to rotate and adjust by the driving motor 6. The base plate 11 includes a bottom plate 111 and an arc-shaped stabilizing plate 112. The arc-shaped stabilizing plate 112 is arranged at both ends of the bottom plate 111, and the arc-shaped stabilizing plate 112 is integrally formed with the bottom plate 111. By setting the structure of the base plate 1, it is ensured that the arc-shaped stabilizing plate 112 can be fixedly installed at both ends of the bottom plate 111 during use, so that the equipment can be stably placed on the ground through the bottom plate 111 and the arc-shaped stabilizing plate 112.

[0028] Referring to Figure 2 and Figure 3 As shown in the figure, the movable seat 2 includes a first sliding plate 21 and a main frame shell 22. The first sliding plate 21 is slidably installed in the first positioning shell 12, and the main frame shell 22 is fixedly installed at the head of the first sliding plate 21. By setting the structure of the movable seat 2, it is ensured that the main frame shell 22 can be fixedly installed through the first sliding plate 21 during use. During use, the first sliding plate 21 can be installed in the first positioning shell 12, so that it can be ensured that the tray group 5 is installed through the main frame shell 22. A motor seat 221 for installing the driving motor 6 is arranged on the outer side surface of the main frame shell 22, and the motor seat 221 is fixedly connected to the main frame shell 22. At the same time, by setting the motor seat 221, it is ensured that the driving motor 6 is stably installed. During use, the driving motor 6 can drive the tray group 5 to rotate and adjust.

[0029] Referring to Figure 2As shown, the support bracket 3 includes a second sliding plate 31 and an arc-shaped support plate 32. The second sliding plate 31 is slidably installed in the second positioning shell 13. The arc-shaped support plate 32 is fixedly installed at the head of the second sliding plate 31, and a limiting vertical plate 33 is also fixedly installed on the arc-shaped support plate 32. By setting the structure of the support bracket 3, it is ensured that the arc-shaped support plate 32 can be supported and installed by the second sliding plate 31 during use, and it is easy to slidably install the second sliding plate 31 in the second positioning shell 13 during use, so that the gas turbine 7 can be supported by the arc-shaped support plate 32.

[0030] Referring to Figure 4 and Figure 5 As shown, the tray group 5 includes a tray shell 51 and limiting arc plates 52. The number of the limiting arc plates 52 is two, and both of the two limiting arc plates 52 are snap-fitted and fixed in the tray shell 51. A sleeve 511 that is matched with the output shaft of the driving motor 6 is fixedly installed at the center of the outer side surface of the tray shell 51. Limiting grooves 512 are opened on both sides of the sleeve 511, and a connecting shaft 61 corresponding to the limiting grooves 512 is fixedly installed on the output shaft of the driving motor 6. By setting the structure of the tray group 5, it is ensured that the tray shell 51 can be sleeved on the output end of the driving motor 6 through the sleeve 511 during use, and the connecting shaft 61 is fixedly installed on the output end, so that it can be ensured that the tray group 5 can slide and adjust on the output end of the driving motor 6. At the same time, it is easy to drive the tray group 5 to rotate and operate through the driving motor 6. After the tray group 5 is sleeved on the gas turbine 7, the gas turbine 7 can be limited by installing two limiting arc plates 52, ensuring that one end of the gas turbine 7 is fixedly installed in the tray group 5, and it is convenient to drive the gas turbine 7 to rotate and adjust through the tray group 5.

[0031] In this embodiment, during actual use, the processing seat can be used to support on the ground, and then the electric cylinders at both ends can be used to adjust the heights of the movable seats and the support brackets at both ends. After lowering the heights at both ends to the lowest, the gas turbine can be installed. Ensure that one end of the gas turbine is placed on the arc-shaped support plate, and the other end is sleeved with the tray shell on the other end of the gas turbine by sliding the tray group. Then, two limiting arc plates are installed on the tray shell to limit and fix the gas turbine, ensuring that the gas turbine is stably installed in the tray shell. Finally, start the electric cylinders at both ends to move synchronously to support the gas turbine. In this way, when processing is required, the driving motor can be started to drive the tray group and the gas turbine to rotate synchronously, which is easy to perform processing operations on different angles of the gas turbine just right.

[0032] The above is the preferred embodiment of the present invention. Those skilled in the art to which the present invention pertains can also make changes and modifications to the above embodiment. Therefore, the present invention is not limited to the above specific embodiments, and any obvious improvements, substitutions or variations made by those skilled in the art on the basis of the present invention all belong to the protection scope of the present invention.

Claims

1. A control component for a gas turbine, comprising a processing base (1), characterized in that: The processing seat (1) includes a seat plate (11), a first positioning shell (12) and a second positioning shell (13). The first positioning shell (12) and the second positioning shell (13) are vertically installed on both sides of the upper end surface of the seat plate (11), and both the first positioning shell (12) and the second positioning shell (13) are fixedly connected to the seat plate (11). An activity seat (2) is slidably installed in the first positioning shell (12), and a support bracket (3) is slidably installed in the second positioning shell (13). An electric cylinder (4) for supporting the first positioning shell (12) and the second positioning shell (13) is fixedly installed on the seat plate (11). A tray group (5) is also installed in the activity seat (2), and a driving motor (6) for driving the tray group (5) to rotate is fixedly installed outside the activity seat (2).

2. The control component for a gas turbine according to claim 1, wherein: The seat plate (11) includes a bottom plate (111) and an arc-shaped stabilizing plate (112). The arc-shaped stabilizing plate (112) is arranged at both ends of the bottom plate (111), and the arc-shaped stabilizing plate (112) is integrally formed with the bottom plate (111).

3. The control component for a gas turbine according to claim 2, characterized in that: The activity seat (2) includes a first sliding plate (21) and a main frame shell (22). The first sliding plate (21) is slidably installed in the first positioning shell (12), and the main frame shell (22) is fixedly installed at the head of the first sliding plate (21).

4. The control component for a gas turbine according to claim 3, characterized in that: A motor seat (221) for installing the driving motor (6) is arranged on the outer side surface of the main frame shell (22), and the motor seat (221) is fixedly connected to the main frame shell (22).

5. The control component for a gas turbine according to claim 4, characterized in that: The support bracket (3) includes a second sliding plate (31) and an arc-shaped support plate (32). The second sliding plate (31) is slidably installed in the second positioning shell (13), the arc-shaped support plate (32) is fixedly installed at the head of the second sliding plate (31), and a limiting vertical plate (33) is also fixedly installed on the arc-shaped support plate (32).

6. The control assembly for a gas turbine according to claim 5, wherein: The tray group (5) includes a tray shell (51) and limiting arc plates (52). The number of the limiting arc plates (52) is two, and both the two limiting arc plates (52) are snap-fitted and fixed in the tray shell (51).

7. A control component for a gas turbine according to claim 6, characterized in that: A sleeve (511) matched with the output shaft of the driving motor (6) is fixedly installed at the center of the outer side surface of the tray shell (51). Limiting grooves (512) are opened on both sides of the sleeve (511), and a connecting shaft (61) corresponding to the limiting grooves (512) is fixedly installed on the output shaft of the driving motor (6).

Citation Information

Patent Citations

  • Gas turbine assembles car

    CN204565554U