Disassembling and assembling device for transition section of gas turbine
By designing the disassembly and assembly device of the transition section of the gas engine, the combination of the first frame, the second frame and the gripper is used to solve the problem of disassembly and assembly of the gas engine transition section, and the effect of facilitating disassembly and assembly is achieved.
Patent Information
- Application Number
- CN202422692440.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-05
- Publication Date
- 2025-08-19
- Estimated Expiration
- 2034-11-05
AI Technical Summary
When disassembling and assembling the transition section of the combustion chamber of the fuel engine, there are many pipelines around the combustion cylinder and are close to the inlet of the combustion chamber, making it difficult to disassemble and assembly.
A gas engine transition section disassembly and assembly device is designed, including a first frame, a second frame, a first moving part and a gripper. The gripper is rotatable and movable in the first direction, and the second frame and gripper are driven to move in the first direction through the first moving part to facilitate disassembly and assembly of the gas engine transition section.
It realizes the transition section of the gas engine to facilitate disassembly and assembly, and improves the disassembly and assembly efficiency and convenience.
Smart Images

Figure CN223235547U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of workpiece disassembly and assembly, in particular to a combustion engine transition section disassembly and assembly device. Background Art
[0002] During the secondary disassembly and assembly of the combustion chamber transition section of the gas turbine, it is difficult to disassemble and assemble the components because there are many pipelines around the combustion cylinder and it is close to the combustion chamber inlet. Utility Model Content
[0003] The present invention aims to solve at least one of the technical problems in the related art to a certain extent. To this end, an embodiment of the present invention provides a combustion engine transition section disassembly and assembly device.
[0004] The combustion engine transition section disassembly and assembly device of the embodiment of the utility model comprises:
[0005] a first frame having a first preset size in a first direction;
[0006] a second frame, the second frame being movably disposed on the first frame along the first direction;
[0007] a first moving portion, the first moving portion being disposed on the first frame and capable of driving the second frame to move in the first direction;
[0008] A gripper is used to grip the transition section. The gripper is connected to the second frame. The gripper can rotate relative to the second frame. The extension direction of the rotation axis of the gripper is the first direction.
[0009] Therefore, the combustion engine transition section disassembly and assembly device according to the embodiment of the utility model has the advantage of facilitating the disassembly and assembly of the combustion engine transition section.
[0010] In some embodiments, a second movable portion is provided on the second frame, the second movable portion is connected to the gripper, the second movable portion can drive the gripper to move in the first direction, and the gripper can rotate relative to at least part of the second movable portion.
[0011] In some embodiments, the second movable portion includes a second lead screw and a second handle, the length direction of the second lead screw is the first direction, and when the second handle is rotated, it can drive the second lead screw to move in the first direction relative to the second frame. The gripper is arranged on the outer peripheral side of the second lead screw, and the internal thread on the inner side of the gripper is threadedly connected with the external thread on the outer peripheral side of the second lead screw.
[0012] In some embodiments, the second moving portion includes a second lead screw, a second limiting portion, a second nut and a second handle. The second nut is rotatably provided on the second frame. The second nut is sleeved on the outer peripheral side of the second lead screw. The internal thread on the inner side of the second nut is threadedly connected with the external thread on the outer peripheral side of the second lead screw. The second limiting portion cooperates with the second lead screw to limit the second lead screw to move along the first direction. The second handle is connected to the second nut to drive the second nut to rotate.
[0013] In some embodiments, the outer surface of the second lead screw has a limiting groove, and the limiting groove extends along the first direction;
[0014] The second limiting portion is provided on the second frame, and the second limiting portion includes a limiting block extending into the limiting groove. The shape and size of the limiting block are adapted to the shape and size of the limiting groove, and the limiting block is slidably connected to the limiting groove in the first direction.
[0015] In some embodiments, the second screw is threadedly connected to the second frame, and the second handle is connected to the second screw to drive the second screw to rotate.
[0016] In some embodiments, the first frame includes a connecting support, a fixed support and a plurality of first connecting rods, the first connecting rods extend along the first direction, the connecting support and the fixed support are both annular, the connecting support and the fixed support are connected through a plurality of first connecting rods, the plurality of first connecting rods are arranged at intervals along the circumferential direction, and the connecting support is used to be connected to the combustion engine.
[0017] In some embodiments, the length of the first frame is greater than or equal to 1 meter and less than or equal to 2 meters;
[0018] The diameter of the second screw is greater than or equal to 0.1 meter and less than or equal to 0.4 meter;
[0019] The connecting support has a plurality of connecting holes arranged at intervals along the circumferential direction, and the connecting holes penetrate the connecting support along the first direction;
[0020] The second frame is slidably connected to the first connecting rods in a one-to-one correspondence via a plurality of connecting plates.
[0021] In some embodiments, the first moving portion includes a first screw and a first nut, the first screw extending along the first direction, the first screw being rotatably disposed on the connecting support and the fixed support, the first screw being provided with a first handle, the first handle being capable of driving the first screw to rotate, the first handle and the second handle being located on a side of the fixed support facing away from the connecting support, the first screw being threadedly connected to the first nut, and the first nut being connected to the second frame;
[0022] At least part of the second screw is located in the first frame, the axial position of the second screw is the same as the axial position of the connecting support, and the first movable part and the second movable part cooperate to drive the gripper to move to the side of the connecting support facing away from the fixed support.
[0023] In some embodiments, the gripper includes a gripping plate and a plurality of claws, the gripping plate is connected to the second frame, the gripping plate can rotate relative to the second frame, the extension direction of the rotation axis of the gripping plate is the first direction, each of the claws has a slot opening facing inward, and at least one of the plurality of claws is detachably connected to the gripping plate. BRIEF DESCRIPTION OF THE DRAWINGS
[0024] Figure 1 It is a schematic diagram of a gas turbine transition section disassembly and assembly device according to an embodiment of the utility model.
[0025] Figure 2 It is a schematic diagram of a gas turbine transition section disassembly and assembly device according to an embodiment of the utility model.
[0026] Figure 3 Schematic diagram of the second lead screw according to an embodiment of the present utility model.
[0027] Reference numerals:
[0028] 1. First frame, 11. Connecting support, 12. Fixed support, 13. First connecting rod, 14. Connecting hole;
[0029] 2. Second frame, 21. Connecting plate;
[0030] 3. gripper, 31. gripping plate, 32. claw;
[0031] 4. first screw, 41. first handle;
[0032] 5. Second lead screw, 51. Second handle, 52. Second limiting portion. DETAILED DESCRIPTION
[0033] The embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the accompanying drawings. The embodiments described below with reference to the accompanying drawings are exemplary and intended to be used to explain the present invention, but should not be understood as limiting the present invention.
[0034] The following describes the combustion engine transition section disassembly and assembly device according to the embodiment of the utility model with reference to the accompanying drawings. Figures 1 to 3 As shown, the combustion engine transition section disassembly and assembly device according to an embodiment of the present utility model includes a first frame 1, a second frame 2, a first moving part and a gripper 3.
[0035] The first frame 1 has a first predetermined dimension in a first direction. The second frame 2 is movably mounted on the first frame 1 along the first direction. A first movable portion is mounted on the first frame 1 and can drive the second frame 2 to move in the first direction. A gripper 3 is used to grasp the transition section. The gripper 3 is connected to the second frame 2 and can rotate relative to the second frame 2, with the rotation axis of the gripper 3 extending in the first direction.
[0036] According to an embodiment of the present invention, the gripper 3 of the gas turbine transition section assembly and disassembly device can grasp the transition section, and the first frame 1 can be connected to the gas turbine. The first movable portion can drive the second frame 2 to move in a first direction, thereby enabling the gripper 3 to move in the first direction and also driving the transition section on the gripper 3 to move in the first direction. The gripper 3 can also rotate relative to the second frame 2 to rotate the transition section so that it can be aligned with the gas turbine installation position, thereby facilitating the assembly and disassembly of the gas turbine transition section.
[0037] Therefore, the combustion engine transition section disassembly and assembly device according to the embodiment of the utility model has the advantage of facilitating the disassembly and assembly of the combustion engine transition section.
[0038] like Figure 1 and Figure 2 As shown, in some embodiments, the second frame 2 is provided with a second movable portion, which is connected to the gripper 3. The second movable portion can drive the gripper 3 to move in the first direction, and the gripper 3 can rotate relative to at least a portion of the second movable portion. In other words, the second frame 2 is provided with a second movable portion that can drive the gripper 3 to move in the first direction, allowing the gripper 3 to perform a second movement, thereby further increasing the range of movement of the gripper 3 in the first direction, thereby facilitating the disassembly of the transition section of the combustion engine.
[0039] In some embodiments, the diameter of the second screw 5 is greater than or equal to 0.1 meter and less than or equal to 0.4 meter. The larger diameter of the second screw 5 can facilitate supporting the gripper 3. For example, the diameter of the second screw 5 is 0.2 meter.
[0040] like Figure 1 and Figure 2As shown, in some embodiments, the second movable portion includes a second screw 5 and a second handle 51. The length of the second screw 5 is oriented in the first direction. Rotating the second handle 51 can cause the second screw 5 to move relative to the second frame 2 in the first direction. Specifically, the axis of the second screw 5 coincides with the center of the second frame 2. A staff member rotates the second handle 51, thereby causing the second screw 5 to rotate and move in the first direction.
[0041] like Figure 1 and Figure 2 As shown, in some embodiments, the second moving portion includes a second screw 5 , a second limiting portion 52 , a second nut and a second handle 51 .
[0042] The second nut is rotatably provided on the second frame 2, and the second nut is sleeved on the outer circumference of the second lead screw 5. The internal thread on the inner side of the second nut is threadedly connected to the external thread on the outer circumference of the second lead screw 5. The second limiting portion 52 cooperates with the second lead screw 5 to limit the second lead screw 5 to move in the first direction, and the second handle 51 is connected to the second nut to drive the second nut to rotate. Specifically, the second nut is threadedly connected to the second lead screw 5, and the second limiting portion 52 can limit the second lead screw 5 so that the second lead screw 5 can only move in the first direction. When the second handle 51 drives the second nut to rotate, the second nut is threadedly connected to the second lead screw 5, thereby driving the second lead screw 5 to move in the first direction.
[0043] In some embodiments, the outer surface of the second lead screw 5 has a limiting groove, and the limiting groove extends along the first direction. The second limiting portion 52 is provided on the second frame 2, and the second limiting portion 52 includes a limiting block extending into the limiting groove. The shape and size of the limiting block are adapted to the shape and size of the limiting groove, and the limiting block is slidably connected to the limiting groove in the first direction. Specifically, the limiting groove is a groove body concave on the outer surface of the second lead screw 5, and the limiting block is located on the inner side of the second limiting portion 52. The second limiting portion 52 is fixed on the second frame 2, so that the limiting block can be fixed relative to the second frame 2. The limiting block extends into the limiting groove to limit the second lead screw 5 and prevent the second lead screw 5 from rotating, so that the second lead screw 5 can move in the first direction when the second nut rotates. For example, the outer peripheral contour of the projection of the limiting groove and the limiting block in the cross section perpendicular to the first direction is a rectangle.
[0044] In some embodiments, the outer peripheral contour of the projection of the cross section of the limiting groove and the limiting block in a direction perpendicular to the first direction is a trapezoid, and the longer bottom side (lower bottom) of the cross section of the limiting groove and the limiting block is adjacent to the axis position of the second lead screw 5 .
[0045] In some embodiments, the second screw 5 is threadedly connected to the second frame 2, and the second handle 51 is connected to the second screw 5 to drive the second screw 5 to rotate. Specifically, the second screw 5 is directly threadedly connected to the second frame 2, and the second screw 5 can move relative to the second frame 2 in the first direction when rotating.
[0046] In some embodiments, the first frame 1 includes a connecting support 11 , a fixing support 12 and a plurality of first connecting rods 13 .
[0047] The first connecting rod 13 extends in the first direction, and the connecting support 11 and the fixed support 12 are both annular. The connecting support 11 and the fixed support 12 are connected by multiple first connecting rods 13, and the multiple first connecting rods 13 are arranged at intervals along the circumference. The connecting support 11 is used to connect to the fuel engine. Specifically, the connecting support 11 and the fixed support 12 are both circular rings. The connecting support 11 has multiple connecting holes 14 arranged at intervals along the circumference, and the connecting holes 14 pass through the connecting support 11 in the first direction. The connecting support 11 is connected to the flange on the fuel engine through the multiple connecting holes 14 and multiple bolts, so that the first frame 1 can be detachably connected to the fuel engine. For example, the first connecting rod 13 is a round rod extending in the first direction.
[0048] In some embodiments, the length of the first frame 1 is greater than or equal to 1 meter and less than or equal to 2 meters. For example, the length of the first frame 1 is equal to 1.5 meters.
[0049] like Figure 1 and Figure 2 As shown, in some embodiments, the second frame 2 is slidably connected to the plurality of first connecting rods 13 via a plurality of connecting plates 21. Specifically, the second frame 2 includes a frame body and a plurality of connecting plates 21, and the connecting plates 21 are slidably connected to corresponding first connecting rods 13, thereby allowing the second frame 2 to slide relative to the first frame 1 in a first direction.
[0050] In some embodiments, the first movable portion includes a first screw 4 and a first nut. The first screw 4 extends along a first direction. The first screw 4 is rotatably mounted on the connecting support 11 and the fixed support 12. The first screw 4 is provided with a first handle 41, which can drive the first screw 4 to rotate. The first handle 41 and the second handle 51 are both located on the side of the fixed support 12 facing away from the connecting support 11. The first screw 4 is threadedly connected to the first nut, which is connected to the second frame 2. Specifically, the first nut is fixed to a connecting plate 21 of the second frame 2. The first handle 41 can drive the first screw 4 to rotate, thereby driving the first nut to move in the first direction, thereby driving the second frame 2 to move in the first direction.
[0051] At least part of the second screw 5 is located inside the first frame 1. The axis of the second screw 5 is located at the same position as the axis of the connecting support 11. The first movable portion and the second movable portion cooperate to drive the gripper 3 to move to the side of the connecting support 11 facing away from the fixed support 12. This facilitates the movement of the transition section to the outside of the first frame 1 and installation in the combustion engine.
[0052] The gripper 3 is sleeved on the outer circumference of the second lead screw 5, and the inner internal thread of the gripper 3 is threadedly connected to the outer external thread of the outer circumference of the second lead screw 5. Specifically, the gripper 3 includes a gripping disc 31 and a plurality of claws 32. The gripping disc 31 is connected to the second frame 2 (via the second movable portion), and the gripping disc 31 is threadedly connected to the second lead screw 5. The gripping disc 31 can rotate relative to the second frame 2, and the extension direction of the rotation axis of the gripping disc 31 is the first direction. Each claw 32 has a slot with an opening facing inward, and at least one of the plurality of claws 32 is detachably connected to the gripping disc 31. Thus, after one claw 32 is removed, the transition section can be clamped into the slots of the remaining plurality of claws 32, and then the last claw 32 can be installed on the gripping disc 31 to fix the transition section. For example, three claws 32 are provided on the circumference of the gripping disc 31, and the shaft of the claw 33 is detachably connected to the gripping disc 31 by bolts.
[0053] In some embodiments, at least one claw 32 is adjustable in the radial direction of the gripping disc 31. For example, the gripping disc 31 is provided with a movable groove extending along its radial direction, and the shaft of the claw 32 is fitted into the movable groove.
[0054] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like to indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation to the present invention.
[0055] Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of the technical features being referred to. Thus, a feature specified as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of this utility model, "plurality" means at least two, such as two, three, etc., unless otherwise specifically defined.
[0056] In this utility model, unless otherwise specified or limited, the terms "installed," "connected," "connect," "fixed," etc. should be understood in a broad sense. For example, they can refer to fixed connection, detachable connection, or integration; mechanical connection, electrical connection, or communication; direct connection or indirect connection through an intermediate medium; internal communication between two elements or interaction between two elements, unless otherwise specified. For those skilled in the art, the specific meanings of the above terms in this utility model can be understood according to specific circumstances.
[0057] In the present invention, unless otherwise expressly specified or limited, when a first feature is "above" or "below" a second feature, it may mean that the first and second features are in direct contact, or the first and second features are in indirect contact through an intermediary. Furthermore, when a first feature is "above," "above," or "above" a second feature, it may mean that the first feature is directly above or diagonally above the second feature, or simply means that the first feature is at a higher level than the second feature. When a first feature is "below," "below," or "below" a second feature, it may mean that the first feature is directly below or diagonally below the second feature, or simply means that the first feature is at a lower level than the second feature.
[0058] In the present invention, the terms "one embodiment", "some embodiments", "example", "specific example", or "some examples" mean that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present invention. In this specification, the schematic expressions of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner. In addition, those skilled in the art can combine and combine different embodiments or examples described in this specification and the features of different embodiments or examples without contradiction.
[0059] Although the above embodiments have been shown and described, it is understood that the above embodiments are illustrative and cannot be understood as limitations on the present invention. Changes, modifications, substitutions and variations of the above embodiments made by ordinary technicians in this field are all within the scope of protection of the present invention.
Claims
1. A gas turbine transition section disassembly and assembly device, characterized in that: include: a first frame having a first preset size in a first direction; a second frame, the second frame being movably disposed on the first frame along the first direction; a first moving portion, the first moving portion being disposed on the first frame and capable of driving the second frame to move in the first direction; A gripper is used to grip the transition section. The gripper is connected to the second frame. The gripper can rotate relative to the second frame. The extension direction of the rotation axis of the gripper is the first direction.
2. The gas turbine transition section disassembly and assembly device according to claim 1, characterized in that: The second frame is provided with a second moving part, which is connected to the gripper. The second moving part can drive the gripper to move in the first direction, and the gripper can rotate relative to at least part of the second moving part.
3. The gas turbine transition section disassembly and assembly device according to claim 2, characterized in that: The second movable part includes a second screw and a second handle. The length direction of the second screw is the first direction. When the second handle is rotated, it can drive the second screw to move in the first direction relative to the second frame. The gripper is arranged on the outer peripheral side of the second screw, and the internal thread on the inner side of the gripper is threadedly connected with the external thread on the outer peripheral side of the second screw.
4. The gas turbine transition section disassembly and assembly device according to claim 3, characterized in that: The second moving part includes a second lead screw, a second limiting part, a second nut and a second handle. The second nut is rotatably provided on the second frame. The second nut is sleeved on the outer peripheral side of the second lead screw. The internal thread on the inner side of the second nut is threadedly connected with the external thread on the outer peripheral side of the second lead screw. The second limiting part cooperates with the second lead screw to limit the second lead screw to move along the first direction. The second handle is connected to the second nut to drive the second nut to rotate.
5. The gas turbine transition section disassembly and assembly device according to claim 4, characterized in that: The outer surface of the second lead screw has a limiting groove, and the limiting groove extends along the first direction; The second limiting portion is provided on the second frame, and the second limiting portion includes a limiting block extending into the limiting groove. The shape and size of the limiting block are adapted to the shape and size of the limiting groove, and the limiting block is slidably connected to the limiting groove in the first direction.
6. The gas turbine transition section disassembly and assembly device according to claim 3, characterized in that: The second screw is threadedly connected to the second frame, and the second handle is connected to the second screw to drive the second screw to rotate.
7. The gas turbine transition section disassembly and assembly device according to any one of claims 3 to 6, characterized in that: The first frame includes a connecting support, a fixed support and a plurality of first connecting rods, the first connecting rods extending along the first direction, the connecting support and the fixed support are both annular, the connecting support and the fixed support are connected through a plurality of first connecting rods, the plurality of first connecting rods are arranged at intervals along the circumferential direction, and the connecting support is used to be connected to the combustion engine.
8. The gas turbine transition section disassembly and assembly device according to claim 7, characterized in that: The length of the first frame is greater than or equal to 1 meter and less than or equal to 2 meters; The diameter of the second screw is greater than or equal to 0.1 meter and less than or equal to 0.4 meter; The connecting support has a plurality of connecting holes arranged at intervals along the circumferential direction, and the connecting holes penetrate the connecting support along the first direction; The second frame is slidably connected to the first connecting rods in a one-to-one correspondence via a plurality of connecting plates.
9. The gas turbine transition section disassembly and assembly device according to claim 8, characterized in that: The first movable portion includes a first screw and a first nut, the first screw extending along the first direction, the first screw being rotatably disposed on the connecting support and the fixed support, the first screw being provided with a first handle, the first handle being capable of driving the first screw to rotate, the first handle and the second handle being both located on a side of the fixed support facing away from the connecting support, the first screw being threadedly connected to the first nut, and the first nut being connected to the second frame; At least part of the second screw is located in the first frame, the axial position of the second screw is the same as the axial position of the connecting support, and the first movable part and the second movable part cooperate to drive the gripper to move to the side of the connecting support facing away from the fixed support.
10. The gas turbine transition section disassembly and assembly device according to claim 1, characterized in that: The gripper includes a gripping plate and a plurality of claws, wherein the gripping plate is connected to the second frame and can rotate relative to the second frame. The extension direction of the rotation axis of the gripping plate is the first direction. Each of the claws has a slot with an opening facing inward, and at least one of the plurality of claws is detachably connected to the gripping plate.