Turbine measuring point blade fixing device

CN224621552UActive Publication Date: 2026-08-11SHANGHAI ELECTRIC POWER GENERATION EQUIPMENT CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-07-23
Publication Date
2026-08-11

AI Technical Summary

Technical Problem

[0002]燃气轮机的透平测点叶片表面布置有传感器,而且传感器线束需要穿过各级透平轮盘线束孔并引出到转子外面,因此需要将透平测点叶片在各级透平轮盘竖直叠加到转子之前安装到透平轮盘上,而这种特殊的安装顺序致使透平测点叶片在透平轮盘翻转过程中极易发生掉落

Benefits of technology

[0023] The first aspect of this application provides a turbine measuring point blade fixing device, including a support component for abutting the lower side of the turbine measuring point blade, a first pull block embedded in a first blade root groove, and a second pull block embedded in a second blade root groove. By hooking the first end of the first pull block to the end face of the first blade root groove and connecting its second end to the support component, and hooking the first end of the second pull block to the end face of the second blade root groove and connecting its second end to the support component, the device can provide good support and fixation for the turbine measuring point blade when it is installed, and can effectively solve the problem of the turbine measuring point blade falling off during the turbine wheel rotation process.

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Abstract

This application discloses a turbine measuring point blade fixing device, including a support assembly, a first pull block, a second pull block, and a clamping assembly. The support assembly is used to abut the lower side of the turbine measuring point blade. The first pull block is embedded in the first blade root groove, with its first end hooked to the end face of the first blade root groove and its second end connected to the support assembly. The second pull block is embedded in the second blade root groove, with its first end hooked to the end face of the second blade root groove and its second end connected to the support assembly. Overall, this device can effectively solve the problem of turbine measuring point blades falling off during turbine wheel rotation.
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Description

Technical Field

[0001] This utility model relates to the field of gas turbine technology, and in particular to a turbine measuring point blade fixing device for a gas turbine. Background Technology

[0002] Sensors are arranged on the surface of the turbine measuring blades of the gas turbine, and the sensor wiring harness needs to pass through the wiring harness holes of each stage of the turbine disk and lead out to the outside of the rotor. Therefore, the turbine measuring blades need to be installed on the turbine disks before each stage of the turbine disks are vertically stacked on the rotor. This special installation sequence makes the turbine measuring blades very easy to fall off during the rotation of the turbine disks.

[0003] Currently, traditional clamps can no longer meet the special installation requirements of turbine measuring blades, especially when other components on both sides of the turbine disk block the blade root groove, making traditional clamps unusable. Therefore, there is an urgent need to develop a special fixing device that can meet the special installation requirements of turbine measuring blades. Utility Model Content

[0004] In view of the deficiencies of the prior art, the purpose of this application is to provide a turbine measuring point blade fixing device to meet the special installation requirements of turbine measuring point blades.

[0005] To achieve the above objectives, the embodiments of this application adopt the following technical solutions:

[0006] In a first aspect, embodiments of this application provide a turbine measuring point blade fixing device for fixing a turbine measuring point blade to a turbine disk, the turbine disk including a first blade root groove and a second blade root groove, comprising:

[0007] A support assembly for abutting against the underside of the turbine measuring point blade;

[0008] A first pull block is embedded in the first leaf root groove, with a first end hooked to the end face of the first leaf root groove, and a second end connected to the support assembly.

[0009] The second pull block is embedded in the second leaf root groove. The first end of the second pull block is hooked to the end face of the second leaf root groove, and the second end of the second pull block is connected to the support component.

[0010] In some embodiments of the first aspect of this application, the support assembly includes a support plate and a first fastener, the first fastener being screwed to the support plate, the support plate being connected to the second end of the first pull block and the second end of the second pull block, and the first fastener being used to abut against the lower side of the turbine measuring point blade.

[0011] In some embodiments of the first aspect of this application, the support plate is arc-shaped, the first pull block is inclinedly disposed on the arc-shaped support plate, and the second pull block is inclinedly disposed on the arc-shaped support plate.

[0012] In some embodiments of the first aspect of this application, the number of turbine measuring blades and the number of the first fasteners are each three, with each first fastener corresponding to one turbine measuring blade.

[0013] In some embodiments of the first aspect of this application, a clamping assembly is further included, the clamping assembly including a clamping plate and a second fastener, the second fastener being screwed to the clamping plate, the clamping plate being connected to a first end of the first pull block and a first end of the second pull block, and the second fastener being used to abut against the upper side of the turbine measuring point blade.

[0014] In some embodiments of the first aspect of this application, the number of turbine measuring blades and the number of second fasteners are each three, with each second fastener corresponding to one turbine measuring blade.

[0015] Secondly, embodiments of this application provide a turbine measuring point blade fixing device for fixing a turbine measuring point blade to a turbine disk, wherein the turbine disk includes a first blade root groove and a second blade root groove, comprising:

[0016] Support member, used to support the turbine measuring point blade;

[0017] The first locking block assembly is locked in the first leaf root groove, the first end of the first locking block assembly is hooked to the end face of the first leaf root groove, and the second end of the first locking block assembly is connected to the support member.

[0018] The second locking block assembly is locked in the second leaf root groove. The first end of the second locking block assembly is hooked to the end face of the second leaf root groove, and the second end of the second locking block assembly is connected to the support member.

[0019] In some embodiments of the second aspect of this application, the first locking block assembly includes a third pull block and a first plug block, the second end of the third pull block is connected to the support member, the first end of the third pull block is hooked to the end face of the first leaf root groove, and the first plug block is used to lock the third pull block in the first leaf root groove.

[0020] In some embodiments of the second aspect of this application, the second locking block assembly includes a fourth pull block and a second plug block, the second end of the fourth pull block is connected to the support member, the first end of the fourth pull block is hooked to the end face of the second leaf root groove, and the second plug block is used to lock the fourth pull block in the second leaf root groove.

[0021] In some embodiments of the second aspect of this application, a third fastener is further included for securing the support member to the second end of the first block assembly and the second block assembly.

[0022] This application has the following beneficial effects:

[0023] The first aspect of this application provides a turbine measuring point blade fixing device, including a support component for abutting the lower side of the turbine measuring point blade, a first pull block embedded in a first blade root groove, and a second pull block embedded in a second blade root groove. By hooking the first end of the first pull block to the end face of the first blade root groove and connecting its second end to the support component, and hooking the first end of the second pull block to the end face of the second blade root groove and connecting its second end to the support component, the device can provide good support and fixation for the turbine measuring point blade when it is installed, and can effectively solve the problem of the turbine measuring point blade falling off during the turbine wheel rotation process.

[0024] The second aspect of this application provides a turbine measuring point blade fixing device, which can also achieve the aforementioned good technical effects, and will not be described in detail here. Attached Figure Description

[0025] Figure 1 This is a schematic diagram of the turbine measuring point blade fixing device provided in some embodiments of this application;

[0026] Figure 2 Schematic diagram of the usage state of the turbine measuring point blade fixing device provided in some embodiments of this application Figure 1 ;

[0027] Figure 3 Schematic diagram of the usage state of the turbine measuring point blade fixing device provided in some embodiments of this application Figure 2 ;

[0028] Figure 4 This is a schematic diagram of the turbine measuring point blade fixing device provided in some other embodiments of this application;

[0029] Figure 5 This is a schematic diagram of the first card block component structure in some other embodiments of this application;

[0030] Figure 6 This is a schematic diagram of the second card block component structure in some other embodiments of this application;

[0031] Figure 7 This is a schematic diagram illustrating the installation of the first and second card block components according to other embodiments of this application;

[0032] Figure 8 A schematic diagram showing the usage state of the turbine measuring point blade fixing device provided in some other embodiments of this application.

[0033] Figure label:

[0034] 100-Turbine measuring point blade;

[0035] 200-Turbine roulette wheel;

[0036] 201-First leaf root groove;

[0037] 202-Second leaf root groove;

[0038] 30 - Support components;

[0039] 31-Support plate;

[0040] 32 - First fastener;

[0041] 40 - First pull block;

[0042] 41-First hook section;

[0043] 50 - Second pull block;

[0044] 51-Second hook part;

[0045] 60 - Clamping component;

[0046] 61-Securing plate;

[0047] 62 - Second fastener;

[0048] 70 - Support component;

[0049] 81-First Card Block Component;

[0050] 811 - Third pull block;

[0051] 8111-Third hook section;

[0052] 812 - First stopper block;

[0053] 813 - Fifth Pull Block;

[0054] 8131 - Fourth hook section;

[0055] 82-Second Card Block Component;

[0056] 821 - Fourth Pull Block;

[0057] 8211 - Fifth hook section;

[0058] 822 - Second stopper block;

[0059] 823 - Sixth Pull Block;

[0060] 8231 - Sixth hook section;

[0061] 83 - Third fastener. Detailed Implementation

[0062] The following specific embodiments illustrate the implementation of this application. Those skilled in the art can easily understand other advantages and effects of this application from the content disclosed in this specification.

[0063] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. The present application will now be described in detail with reference to the accompanying drawings and embodiments. To enable those skilled in the art to better understand the solutions of this application, the technical solutions in the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only a part of the embodiments of this application, and not all of them. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort should fall within the scope of protection of this application.

[0064] It should be noted that the terms "first," "second," etc., in the specification, claims, and accompanying drawings of this application are used to distinguish similar objects and are not necessarily used to describe a specific order or sequence. Furthermore, the terms "comprising" and "having," and any variations thereof, are intended to cover a non-exclusive inclusion; for example, a process, method, system, product, or device that includes a series of steps or units is not necessarily limited to those steps or units explicitly listed, but may include other steps or units not explicitly listed or inherent to these processes, methods, products, or devices.

[0065] It should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "linking" should be interpreted broadly. For example, they can refer to fixed connections, detachable connections, or integral connections; they can refer to mechanical connections or electrical connections; they can refer to direct connections or indirect connections through an intermediate medium; and they can refer to the internal connection between two components. Those skilled in the art can understand the specific meaning of the above terms in this application based on the specific circumstances.

[0066] In the embodiments of this application, the words "exemplary," "exemplarily," or "for example" are used to indicate examples, illustrations, or descriptions. Any embodiment or design described as "exemplary," "exemplarily," or "for example" in the embodiments of this application should not be construed as being more preferred or advantageous than other embodiments or designs; rather, the use of the words "exemplary" or "for example" is intended to present the relevant concepts in a specific manner.

[0067] A first aspect of this application provides a turbine measuring point blade fixing device for fixing a turbine measuring point blade 100 to a turbine disk 200, the turbine disk including a first blade root groove 201 and a second blade root groove 202. Figure 1-3 As shown, in some embodiments, the turbine measuring point blade fixing device includes a support assembly 30, a first pull block 40, a second pull block 50, and a clamping assembly 60.

[0068] The support component 30 is used to abut the lower side of the turbine measuring point blade 100. The first pull block 40 is embedded in the first blade root groove 201. The first end of the first pull block 40 is hooked to the end face of the first blade root groove 201, and the second end of the first pull block 40 is connected to the support component 30.

[0069] The second pull block 50 is embedded in the second leaf root groove 202. The first end of the second pull block 50 is hooked to the end face of the second leaf root groove 202, and the second end of the second pull block 50 is connected to the support component 30.

[0070] Specifically, such as Figure 1 As shown, the second end of the first pull block 40 is connected to the first side of the support assembly 30; for example, the second end of the first pull block 40 can be detachably connected to the first side of the support assembly 30 by bolts, facilitating the disassembly and installation of the first pull block 40 and the support assembly 30. The second end of the second pull block 50 is connected to the second side of the support assembly 30; for example, the second end of the second pull block 50 can be detachably connected to the second side of the support assembly 30 by bolts, facilitating the disassembly and installation of the second pull block 50 and the support assembly 30.

[0071] In the embodiments of this application, such as Figure 2 and 3 As shown, the support assembly 30 is used to abut against the lower side of the turbine measuring point blade 100 to support the turbine measuring point blade 100 and prevent it from falling.

[0072] For example, such as Figure 2 and 3 As shown, three turbine measuring blades 100 need to be installed on the turbine disk 200. The first pull block 40 can be embedded in the first blade root groove 201, and then the first end of the first pull block 40 is hooked to the end face of the first blade root groove 201, and the second end of the first pull block 40 is connected to the support component 30. Correspondingly, the second pull block 50 is embedded in the second blade root groove 202, and the first end of the second pull block 50 is hooked to the end face of the second blade root groove 202, and the second end of the second pull block 50 is connected to the support component 30. Then, three turbine measuring blades 100 are installed in the three blade root grooves between the first blade root groove 201 and the second blade root groove 202.

[0073] Since the first end of the first pull block 40 is hooked to the end face of the first blade root groove 201, the first end of the second pull block 50 is hooked to the end face of the second blade root groove 202, and the first end of the first pull block 40 and the second end of the second pull block 50 are respectively connected to the first and second sides of the support assembly 30, the support assembly 30 provides good support and fixation for the three turbine measuring blades 100, and can prevent the turbine measuring blades 100 from falling off during the rotation of the turbine wheel 200.

[0074] In this embodiment, the support component 30, the first pull block 40, and the second pull block 50 are made of rigid materials; for example, the support component 30, the first pull block 40, and the second pull block 50 can be made of stainless steel, which can meet the requirements for supporting and fixing the turbine measuring point blade 100.

[0075] The first aspect of this application provides a turbine measuring point blade fixing device, including a support component 30 for abutting the lower side of the turbine measuring point blade 100, a first pull block 40 embedded in a first blade root groove 201, and a second pull block 50 embedded in a second blade root groove 202. By hooking the first end of the first pull block 40 to the end face of the first blade root groove 201 and connecting its second end to the support component 30, and by hooking the first end of the second pull block 50 to the end face of the second blade root groove 202 and connecting its second end to the support component 30, the device can provide good support and fixing for the turbine measuring point blade 100 when it is installed on the turbine wheel 200, effectively solving the problem of the turbine measuring point blade 100 falling off during the rotation of the turbine wheel 200.

[0076] like Figure 1 As shown, in order to enable the first end of the first pull block 40 and the first end of the second pull block 50 to be stably hooked onto the end face of the first leaf root groove 201 and the end face of the second leaf root groove 202 respectively, a first hooking part 41 is provided at the first end of the first pull block 40 and extends toward the end face of the first leaf root groove 201, and a second hooking part 51 is provided at the first end of the second pull block 50 and extends toward the end face of the second leaf root groove 202.

[0077] like Figure 1 As shown, in some embodiments, the support assembly 30 includes a support plate 31 and a first fastener 32. The first fastener 32 is screwed to the support plate 31. The support plate 31 is connected to the second end of the first pull block 40 and the second end of the second pull block 50. The first fastener 32 is used to abut against the lower side of the turbine measuring blade 100. The support plate 31 can be detachably connected to the second end of the first pull block 40 and the second end of the second pull block 50 respectively by bolts for disassembly and installation. By setting the first fastener 32, the turbine measuring blade 100 can be pressed upward, which can prevent the turbine measuring blade 100 from moving during the flipping process.

[0078] Based on the actual circumferential curved surface structure design of the turbine disk 200, in some embodiments, the support plate 31 has an arc-shaped structure, with the first pull block 40 inclinedly disposed on the arc-shaped support plate 31 and the second pull block 50 inclinedly disposed on the arc-shaped support plate 31. By designing the support plate 31 as arc-shaped, the support plate 31 can be adapted to different turbine disk 200 structures.

[0079] like Figure 2 and 3 As shown, in some embodiments, the number of turbine measuring blades 100 and the number of first fasteners 32 are each three, with each first fastener 32 corresponding to one turbine measuring blade 100. It is understood that when a larger number of turbine measuring blades 100 need to be installed, an appropriate length of the support assembly 30 can be set to meet the support function for the larger number of turbine measuring blades 100.

[0080] like Figure 1 As shown, to prevent the turbine measuring blade 100 from moving during the rotation of the turbine disk 200, in some embodiments, the turbine measuring blade fixing device further includes a clamping component 60. The clamping component 60 includes a clamping plate 61 and a second fastener 62. The second fastener 62 and the clamping plate 61 are screwed together. The clamping plate 61 is connected to the first end of the first pull block 40 and the first end of the second pull block 50. The second fastener 62 is used to abut against the upper side of the turbine measuring blade 100. The clamping plate 61 can be detachably connected to the first end of the first pull block 40 and the first end of the second pull block 50 by bolts, which facilitates the installation and removal of the clamping plate 61 from the first end of the first pull block 40 and the first end of the second pull block 50. By setting the second fastener 62, the turbine measuring blade 100 can be clamped downwards, and in cooperation with the first fastener 32 in the aforementioned embodiment, the positional movement of the turbine measuring blade 100 during the rotation can be effectively prevented.

[0081] like Figure 2 and 3 As shown, in some embodiments, the number of turbine measuring blades 100 and the number of second fasteners 62 are each three, with each second fastener 62 corresponding to one turbine measuring blade 100. It is understood that when a larger number of turbine measuring blades 100 need to be installed, an appropriate length of the second fastener 62 can be set to meet the clamping effect on the larger number of turbine measuring blades 100.

[0082] Based on the same inventive concept, a second aspect of this application provides a turbine measuring point blade fixing device for fixing a turbine measuring point blade 100 to a turbine disk 200, the turbine disk including a first blade root groove 201 and a second blade root groove 202. Figure 4-8As shown, in some embodiments, the turbine measuring point blade fixing device includes a support 70, a first locking block assembly 81, and a second locking block assembly 82.

[0083] Among them, the support member 70 is used to support the turbine measuring point blade 100, the first locking block assembly 81 is locked in the first blade root groove 201, the first end of the first locking block assembly 81 is hooked to the end face of the first blade root groove 201, and the second end of the first locking block assembly 81 is connected to the support member 70.

[0084] The second locking component 82 is locked in the second leaf root groove 202. The first end of the second locking component 82 is hooked to the end face of the second leaf root groove 202, and the second end of the second locking component 82 is connected to the support member 70.

[0085] Specifically, such as Figure 1 and 7 As shown, the support member 70 is used to support and fix the turbine measuring blade 100. The second end of the first locking block assembly 81 can be detachably connected to the first side of the support member 70 via bolts, facilitating the disassembly and installation of the first locking block assembly 81 and the support member 70. The second end of the second locking block assembly 82 can be detachably connected to the second side of the support member 70 via bolts, facilitating the disassembly and installation of the second locking block assembly and the support member 70. By locking the first locking block assembly 81 and the second locking block assembly 82 into the first blade root groove 201 and the second blade root groove 202 respectively, and hooking the first end of the first locking block assembly 81 and the first end of the second locking block assembly 82 to the end faces of the first blade root groove 201 and the second blade root groove 202 respectively, the support member 70 can provide good support and fixation for the turbine measuring blade 100.

[0086] In this embodiment, the support member 70, the first locking block assembly 81, and the second locking block assembly 82 are made of rigid materials; for example, the support member 70, the first locking block assembly 81, and the second locking block assembly 82 can be made of stainless steel, which can meet the requirements for supporting and fixing the turbine measuring point blade 100.

[0087] The second aspect of this application provides a turbine measuring point blade fixing device, including a support member 70 for supporting the turbine measuring point blade 100, a first locking block assembly 81 locked in a first blade root groove 201, and a second locking block assembly 82 locked in a second blade root groove 202. By hooking the first end of the first locking block assembly 81 to the end face of the first blade root groove 201 and connecting its second end to the support member 70, and by hooking the first end of the second locking block assembly 82 to the end face of the second blade root groove 802 and connecting its second end to the support member 70, the device can provide good support and fixing for the turbine measuring point blade 100 when it is installed, and can effectively prevent the turbine measuring point blade 100 from falling off during the rotation of the turbine wheel 200.

[0088] like Figure 4-8 As shown, in order to enable the first end of the first locking block assembly 81 and the first end of the second locking block assembly 82 to be stably hooked onto the end face of the first leaf root groove 201 and the end face of the second leaf root groove 202 respectively, a hooking member is provided at the first end of the first locking block assembly 81 and extends toward the end face of the first leaf root groove 201, and a second hooking member is provided at the first end of the second locking block assembly 82 and extends toward the end face of the second leaf root groove 202.

[0089] like Figure 4 and 5 As shown, in some embodiments, the first locking block assembly 81 includes a third pull block 811 and a first plug block 812. The second end of the third pull block 811 is connected to the support member 70, and the first end of the third pull block 811 is hooked onto the end face of the first blade root groove 201. The first plug block 812 is used to lock the third pull block 811 into the first blade root groove 201. The second end of the third pull block 811 can be detachably connected to the first side of the support member 70 by bolts, which facilitates the disassembly and installation between the third pull block 811 and the support member 70. By setting the first plug block 812, the third pull block 811 can be locked into the first blade root groove 201, and the third hooking part 8111 provided on the first end of the third pull block 811 is hooked onto the end face of the first blade root groove 201, which enables the support member 70 to provide good support and fixation for the turbine measuring point blade 100.

[0090] like Figure 5 As shown, in some embodiments, the first locking block assembly 81 further includes a fifth pulling block 813. The first end of the fifth pulling block 813 is hooked onto the end face of the first leaf root groove 201, and the second end of the fifth pulling block 813 is detachably connected by bolts and a support member 70. The first end of the fifth pulling block 813 is also provided with a fourth hooking portion 8131 extending towards the end face of the first leaf root groove 201, which allows the fifth pulling block 813 to be stably hooked onto the end face of the first leaf root groove 201. A first plug block 812 is engaged between the third pulling block 811 and the fifth pulling block 813 to secure the third pulling block 811 and the fifth pulling block 813 in the first leaf root groove 201, preventing the hooking contact between the third pulling block 811 and the fifth pulling block 813 and the end face of the first leaf root groove 201 from loosening.

[0091] During installation, such as Figure 7As shown, the third pull block 811 and the fifth pull block 813 are first inserted into both sides of the first leaf root groove 201, and the third hook part 8111 on the first end of the third pull block 811 and the fourth hook part 8131 on the first end of the fifth pull block 813 are hooked to the end faces on both sides of the first leaf root groove 201, respectively. Then, the first plug 812 is inserted between the third pull block 811 and the fifth pull block 813, so that the third pull block 811 and the fifth pull block 813 are stably hooked to the end faces of the first leaf root groove 201, respectively. The support member 70 is fixed to the second end of the third pull block 811 and the second end of the fifth pull block 813 by fixing screws. Finally, insert the turbine measuring blade 100 into the other blade root grooves between the first blade root groove 201 and the second blade root groove 202. After the turbine disk 200 is stacked on the rotor and the rotor is flipped to a horizontal state, first loosen the fixing screws and remove the support 70. Then, use the pin puller to remove the first plug 812 and disassemble the third pull block 811 and the fifth pull block 813.

[0092] like Figure 4 and 6 As shown, in some embodiments, the second locking block assembly 82 includes a fourth pull block 821 and a second plug block 822. The second end of the fourth pull block 821 is connected to the support member 70, and the first end of the fourth pull block 821 is hooked onto the end face of the second leaf root groove 202. The second plug block 822 is used to lock the fourth pull block 821 into the second leaf root groove 202. The second end of the fourth pull block 821 can be detachably connected to the second side of the support member 70 by bolts, facilitating the disassembly and installation of the fourth pull block 821 and the support member 70.

[0093] By setting the second stopper 822, the fourth pull block 821 can be locked in the second blade root groove 202, and the fifth hook part 8211 set on the first end of the fourth pull block 821 can be hooked to the end face of the second blade root groove 202, so that the support member 70 can play a good supporting and fixing role for the turbine measuring point blade 100.

[0094] like Figure 6 As shown, in some embodiments, the second locking block assembly 82 further includes a sixth pulling block 823. The first end of the sixth pulling block 823 is hooked onto the end face of the second leaf root groove 202, and the second end of the sixth pulling block 823 is detachably connected by bolts and a support member 70. The first end of the sixth pulling block 823 is also provided with a sixth hooking portion 8231 extending towards the end face of the second leaf root groove 202, which allows the sixth pulling block 823 to be stably hooked onto the end face of the second leaf root groove 202. The second plug 822 is engaged between the fourth pulling block 821 and the sixth pulling block 823 to secure the fourth pulling block 821 and the sixth pulling block 823 in the second leaf root groove 202, preventing the hooking contact between the fourth pulling block 821 and the sixth pulling block 823 and the end face of the second leaf root groove 202 from loosening.

[0095] During installation, such as Figure 7 As shown, firstly, the fourth pull block 821 and the sixth pull block 823 are inserted into both sides of the second leaf root groove 202, and the fifth hook part 8211 on the first end of the fourth pull block 821 and the sixth hook part 8231 on the first end of the sixth pull block 823 are hooked to the end faces on both sides of the second leaf root groove 202, respectively. Then, the second plug 822 is inserted between the fourth pull block 821 and the sixth pull block 823, so that the fourth pull block 821 and the sixth pull block 823 are stably hooked to the end faces of the second leaf root groove 202, respectively. The support member 70 is fixed to the second end of the fourth pull block 821 and the second end of the sixth pull block 823 by fixing screws. Finally, insert the turbine measuring blade 100 into the other blade root grooves between the first blade root groove 201 and the second blade root groove 202. After the turbine disk 200 is stacked on the rotor and the rotor is flipped to a horizontal state, first loosen the fixing screws and remove the support 70. Then, use the pin puller to remove the second plug 822 and disassemble the fourth pull block 821 and the sixth pull block 823.

[0096] like Figure 1 As shown, in some embodiments, the turbine measuring point blade fixing device further includes a third fastener 83, which is used to fix the support member 70 to the second end of the first locking block assembly 81 and the second end of the second locking block assembly 82. The third fastener 83 can detachably connect the first side of the support member 70 to the second end of the first locking block assembly 81 through a screw hole, and the third fastener 83 can detachably connect the second side of the support member 70 to the second end of the second locking block assembly 82 through a screw hole, facilitating the disassembly and installation of the third fastener 83 with the first locking block assembly 81 and the second locking block assembly 82.

[0097] The turbine measuring blade fixing device provided in the foregoing embodiments of this application can provide good support and fixation for the turbine measuring blade 100 when it is installed on the turbine disk 200, and can effectively solve the problem of the turbine measuring blade 100 falling off during the rotation of the turbine disk 200.

[0098] The above description is merely a specific embodiment of this application, but the scope of protection of this application is not limited thereto. All embodiments obtained by any modifications, alterations or equivalent substitutions made by those skilled in the art without departing from the technical concept of this application shall fall within the scope of protection of the claims of this application.

Claims

1. A turbine measuring point blade fixing device for fixing a turbine measuring point blade (100) to a turbine disk (200), the turbine disk (200) comprising a first blade root groove (201) and a second blade root groove (202), characterized in that, include: Support assembly (30) for abutting against the underside of the turbine measuring blade (100); A first pull block (40) is embedded in the first leaf root groove (201). The first end of the first pull block (40) is hooked to the end face of the first leaf root groove (201), and the second end of the first pull block (40) is connected to the support component (30). The second pull block (50) is embedded in the second leaf root groove (202). The first end of the second pull block (50) is hooked to the end face of the second leaf root groove (202), and the second end of the second pull block (50) is connected to the support assembly (30).

2. The turbine measuring point blade fixing device according to claim 1, characterized in that, The support assembly (30) includes a support plate (31) and a first fastener (32). The first fastener (32) and the support plate (31) are screwed together. The support plate (31) is connected to the second end of the first pull block (40) and the second end of the second pull block (50). The first fastener (32) is used to abut against the lower side of the turbine measuring point blade (100).

3. The turbine measuring point blade fixing device according to claim 2, characterized in that, The support plate (31) is arc-shaped, the first pull block (40) is inclinedly disposed on the arc-shaped support plate (31), and the second pull block (50) is inclinedly disposed on the arc-shaped support plate (31).

4. The turbine measuring point blade fixing device according to claim 2, characterized in that, The number of turbine measuring blades (100) and the number of the first fasteners (32) are three each, with each first fastener (32) corresponding to one turbine measuring blade (100).

5. The turbine measuring point blade fixing device according to claim 1, characterized in that, It also includes a clamping assembly (60), which includes a clamping plate (61) and a second fastener (62). The second fastener (62) is screwed to the clamping plate (61). The clamping plate (61) is connected to the first end of the first pull block (40) and the first end of the second pull block (50). The second fastener (62) is used to abut against the upper side of the turbine measuring point blade (100).

6. The turbine measuring point blade fixing device according to claim 5, characterized in that, The number of turbine measuring blades (100) and the number of the second fasteners (62) are three each, with each second fastener (62) corresponding to one turbine measuring blade (100).

7. A turbine measuring point blade fixing device for fixing a turbine measuring point blade (100) to a turbine disk (200), the turbine disk (200) comprising a first blade root groove (201) and a second blade root groove (202), characterized in that, include: Support member (70) for supporting the turbine measuring point blade (100); The first locking block assembly (81) is locked in the first leaf root groove (201). The first end of the first locking block assembly (81) is hooked to the end face of the first leaf root groove (201), and the second end of the first locking block assembly (81) is connected to the support member (70). The second locking block assembly (82) is locked in the second leaf root groove (202). The first end of the second locking block assembly (82) is hooked to the end face of the second leaf root groove (202), and the second end of the second locking block assembly (82) is connected to the support member (70).

8. The turbine measuring point blade fixing device according to claim 7, characterized in that, The first locking block assembly (81) includes a third pull block (811) and a first plug block (812). The second end of the third pull block (811) is connected to the support member (70), and the first end of the third pull block (811) is hooked to the end face of the first leaf root groove (201). The first plug block (812) is used to lock the third pull block (811) in the first leaf root groove (201).

9. The turbine measuring point blade fixing device according to claim 7, characterized in that, The second locking block assembly (82) includes a fourth pull block (821) and a second plug block (822). The second end of the fourth pull block (821) is connected to the support member (70), and the first end of the fourth pull block (821) is hooked to the end face of the second leaf root groove (202). The second plug block (822) is used to lock the fourth pull block (821) in the second leaf root groove (202).

10. The turbine measuring point blade fixing device according to claim 7, characterized in that, It also includes a third fastener (83) for securing the support (70) to the second end of the first locking block assembly (81) and the second end of the second locking block assembly (82).