Detection device for engine compressor blade
By designing a multi-dimensional synchronous detection component and linkage frame, synchronous multi-dimensional detection of the upper surface, left side, and right side of the engine compressor blades is achieved, solving the problem of low detection efficiency in existing technologies and improving detection efficiency and accuracy.
Patent Information
- Application Number
- CN202510932713.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-07-07
- Publication Date
- 2025-11-14
AI Technical Summary
Existing technologies make it difficult to achieve simultaneous multi-dimensional detection of irregular curved paths on the upper, left, and right sides of engine compressor blades, resulting in low detection efficiency.
It adopts a multi-dimensional synchronous detection component, including an upper sleeve column, a side sliding rod, a side sleeve column, and an infrared detection probe. The movement of the linkage frame drives the probe to perform synchronous detection along different tracks. Combined with a drive motor and controller, it achieves efficient detection.
It enables simultaneous multi-dimensional inspection of the upper, left, and right surfaces of engine compressor blades, improving inspection efficiency, reducing blind spots, enhancing inspection accuracy, and saving power.
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Figure CN120948548A_ABST
Abstract
Description
Technical Field
[0001] This invention relates to the field of optical inspection technology, and more specifically, to an inspection device for engine compressor blades. Background Technology
[0002] In the process of testing new materials for engine compressor blades, optical methods, especially infrared light detection devices, have the advantages of being non-contact, real-time, covering the entire field, and highly sensitive. They can comprehensively evaluate the structural defects of new material engine compressor blades and determine whether the engine compressor blades are qualified products.
[0003] Among the existing publicly available technical documents, patent publication number CN108489984A discloses a detection device for aero-engine compressor blades. This technology involves a detection frame placed on a detection base, with one end of a connecting frame connected to the detection frame via a connecting block, and the other end connected to a connecting box via a connecting head. The connecting head is placed on the connecting box, which is positioned above a blade transfer device. A 3D scanner is placed inside the connecting box, and a remote control is electrically connected to the 3D scanner; a computing device is also electrically connected to the 3D scanner. The beneficial effects of this invention are: by detecting blades using instruments, human error is reduced, manpower input is reduced, and detection accuracy is increased. However, this technology still has the following problems.
[0004] In the process of inspecting new materials for engine compressor blades, infrared detection probes are needed to detect surface defects. However, there are irregular gaps between adjacent engine compressor blades, and the upper surface and both sides of each engine compressor blade are irregular curved surfaces. To inspect each engine compressor blade, it is necessary to first inspect each point on the curved surface, and then inspect each point on the other surfaces. It is difficult to simultaneously and multidimensionally inspect the irregular paths on the upper surface and both sides of the engine compressor blade based on the gap position of the engine compressor blade, which greatly reduces the inspection efficiency of engine compressor blades. Summary of the Invention
[0005] To overcome the above-mentioned defects of the prior art, the present invention provides the following technical solution: a detection device for engine compressor blades, including a bracket and a controller, wherein a linkage frame is provided on one side of the bracket, and a multi-dimensional synchronous detection component is installed on the inner wall of the linkage frame, the multi-dimensional synchronous detection component including: an upper sleeve column, which is slidably connected to the inner wall of the linkage frame, and a side slide rod is provided on one side of the upper sleeve column, and the side slide rod is slidably connected to the linkage frame; An arc-shaped sleeve is fixedly connected to the bottom end of the side slide rod. A first infrared detection probe is fixedly connected to one side of the inner wall of the arc-shaped sleeve, and an arc-shaped guide rail is slidably connected to the outer wall of the arc-shaped sleeve. The second infrared detection probe is fixedly installed at the bottom of the upper sleeve column. The upper sleeve column is slidably connected to the upper curved track on the outer wall and the lower surface of the linkage frame. The upper sleeve column is used to drive the second infrared detection probe to move along the curved path of the inner wall of the upper curved track. A side sleeve column is located on the other side of the upper sleeve column. The side sleeve column is slidably connected to the linkage frame. A side curved track is slidably connected to the outer wall of the side sleeve column. A third infrared detection probe is slidably connected to the inner wall of the side curved track. The side sleeve column is used to drive the third infrared detection probe to move along the curved path of the inner wall of the side curved track.
[0006] In a preferred embodiment, both the arc-shaped guide rail and the upper curved rail are fixedly connected to the bracket, and the side curved rail is fixedly connected to the bracket.
[0007] In a preferred embodiment, the side slide rod is slidably connected to the arc-shaped guide rail, the linkage frame is slidably connected to the upper curved track, and the third infrared detection probe is fixedly connected to the side sleeve column. The first and second infrared detection probes are both electrically connected to the controller, and the third infrared detection probe is electrically connected to the controller.
[0008] In a preferred embodiment, a guide rod is slidably connected to the inner wall of the arc-shaped sleeve, and both ends of the guide rod are fixedly connected to the same arc-shaped guide rail.
[0009] In a preferred embodiment, a rubber sleeve is fixedly connected to the inner wall of the upper sleeve column, and a curved column is slidably connected to the inner wall of the rubber sleeve, with both ends of the curved column fixedly connected to the same upper curved track.
[0010] In a preferred embodiment, a silicone sleeve is fixedly connected to the inner wall of the side sleeve column, and a curved rod is slidably connected to the inner wall of the silicone sleeve, with both ends of the curved rod fixedly connected to the same side curved track.
[0011] In a preferred embodiment, the top of the bracket is provided with a linkage component, the linkage component comprising: A support frame is fixedly connected to the top of the bracket, and a screw is rotatably installed on the inner wall of the support frame; A socket strip is slidably connected to the inner wall of the support frame. The socket strip is threadedly connected to the screw rod. The bottom end of the socket strip is fixedly connected to the linkage frame. The socket strip is slidably connected to the support frame. A drive motor is installed at one end of the support frame. The drive motor is used to drive the screw to rotate and is electrically connected to the controller.
[0012] In a preferred embodiment, an electric cylinder is mounted on the lower surface of the support frame, the electric cylinder is electrically connected to the controller, and the output end of the electric cylinder is fixedly connected to the support frame. A mounting plate is fixedly connected to one side of the outer wall of the electric cylinder. A stepper motor is installed on the upper surface of the mounting plate near its center point. A positioning seat is fixedly connected to the output end of the stepper motor.
[0013] In a preferred embodiment, a compressor shaft head is placed on the inner wall of the positioning seat, and multiple blades are fixedly connected to the outer wall of the compressor shaft head.
[0014] In a preferred embodiment, the stepper motor is used to drive the positioning seat to rotate, and the stepper motor is electrically connected to the controller.
[0015] The technical effects and advantages of this invention are as follows: 1. This invention utilizes a multi-dimensional synchronous detection component. By moving the linkage frame to the right, the upper sleeve, side sliding rod, and side sleeve move synchronously. In this way, the upper sleeve drives the second infrared detection probe to perform curved path movement detection on the upper surface of the blade along the upper curved track. The side sliding rod drives the first infrared detection probe to perform multi-dimensional movement detection on the right side of the blade along the inner wall of the arc-shaped guide rail. The side sleeve drives the third infrared detection probe to perform curved path movement detection on the left side of the blade along the inner wall of the side curved track. By working synchronously with the first, second, and third infrared detection probes, synchronous multi-dimensional detection of irregular curved paths on the upper surface, left side, and right side of the blade can be achieved, significantly improving detection efficiency.
[0016] 2. This invention employs a multi-dimensional synchronous detection component. The rightward movement of the linkage frame drives the upper sleeve, side sliding rod, and side sleeve to move synchronously. In this way, the second infrared detection probe performs large-area irregular curved path detection on the upper surface of the blade along the upper curved track, the first infrared detection probe performs large-area multi-dimensional moving detection on the right side of the blade along the arc-shaped guide rail, and the third infrared detection probe performs large-area irregular curved path detection on the left side of the blade along the side curved track. This allows for large-area detection at different positions on the upper, left, and right sides of the blade, effectively reducing detection blind spots and achieving high-precision and efficient detection.
[0017] 3. This invention employs a linkage component and a multi-dimensional synchronous detection component. The controller starts the drive motor, and the screw and sleeve thread transmission achieve stable rightward movement of the linkage frame, thereby driving the upper sleeve column, side sliding rod, and side sleeve column to move synchronously. Only a single power source, the drive motor, is needed to drive the second infrared detection probe to perform irregular curve path detection on the upper surface of the blade, the first infrared detection probe to perform multi-dimensional movement detection on the right side of the blade, and the third infrared detection probe to perform irregular curve path detection on the left side of the blade. The drive motor's driving power is fully integrated to achieve efficient driving, effectively save detection power source, and make the detection process more energy-saving and environmentally friendly. Attached Figure Description
[0018] Figure 1 This is a schematic diagram of the overall structure of the engine compressor blade detection device of the present invention.
[0019] Figure 2 This is a partial structural diagram of the connection between the bracket and the linkage frame of the present invention.
[0020] Figure 3 This is a partial structural diagram of the connection between the bracket and the support frame of the present invention.
[0021] Figure 4 This is a partial structural diagram of the connection between the bracket and the arc-shaped guide rail of the present invention.
[0022] Figure 5 This is a partial structural diagram of the connection between the second infrared detection probe and the upper sleeve column of the present invention.
[0023] Figure 6 This is a schematic diagram of a partial cut-off structure at the connection between the curved column and the upper curved track of the present invention.
[0024] Figure 7 This is a partial structural diagram of the connection between the side sleeve column and the side curved track of the present invention.
[0025] Figure 8 This is a partial structural diagram of the connection between the side sleeve post and the silicone sleeve of the present invention.
[0026] Figure 9 This is a partial structural diagram of the connection between the support frame and the drive motor of the present invention.
[0027] The attached diagram is labeled as follows: 1. Bracket; 2. Linkage frame; 3. Upper sleeve column; 4. Side slide rod; 5. Arc sleeve; 6. First infrared detection probe; 7. Arc guide rail; 8. Second infrared detection probe; 9. Upper curved track; 10. Side sleeve column; 11. Side curved track; 12. Third infrared detection probe; 13. Guide rod; 14. Rubber sleeve; 15. Curved column; 16. Silicone sleeve; 17. Curved rod; 18. Support frame; 19. Screw; 20. Connecting strip; 21. Drive motor; 22. Electric cylinder; 23. Mounting plate; 24. Controller; 25. Stepper motor; 26. Positioning seat; 27. Compressor shaft head; 28. Blade. Detailed Implementation
[0028] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.
[0029] As attached Figure 1 - Appendix Figure 9 The invention relates to a detection device for engine compressor blades. The device is equipped with a multi-dimensional synchronous detection component. The multi-dimensional synchronous detection component enables the first infrared detection probe 6, the second infrared detection probe 8, and the third infrared detection probe 12 to work synchronously. This allows for synchronous multi-dimensional detection of the upper surface, the irregular curved path on the left side, and the irregular path on the right side of the blade 28, significantly improving detection efficiency. The specific structural configuration of the multi-dimensional synchronous detection component is as follows.
[0030] In this embodiment, as shown in the appendix Figure 1 - Appendix Figure 8As shown, the multi-dimensional synchronous detection component includes: an upper sleeve 3, slidably connected to the inner wall of the linkage frame 2, with a side sliding rod 4 on one side of the upper sleeve 3, and the side sliding rod 4 slidably connected to the linkage frame 2; an arc-shaped sleeve 5, fixedly connected to the bottom end of the side sliding rod 4, with a first infrared detection probe 6 fixedly connected to one side of the inner wall of the arc-shaped sleeve 5, and an arc-shaped guide rail 7 slidably connected to the outer wall of the arc-shaped sleeve 5; a second infrared detection probe 8, fixedly installed at the bottom end of the upper sleeve 3, with an upper curved track 9 slidably connected to the outer wall of the upper sleeve 3 and located on the lower surface of the linkage frame 2, the upper sleeve 3 being used to drive the second infrared detection probe 8 to move along the curved path of the inner wall of the upper curved track 9; and a side sleeve 10, located on the other side of the upper sleeve 3, slidably connected to the linkage frame 2, with a side curved track 11 slidably connected to the outer wall of the side sleeve 10, and a third infrared detection probe 12 slidably connected to the inner wall of the side curved track 11, the side sleeve 10 being used to drive the third infrared detection probe 12 to move along the curved path of the inner wall of the side curved track 11. Both the arc-shaped guide rail 7 and the upper curved track 9 are fixedly connected to the bracket 1, and the side curved track 11 is fixedly connected to the bracket 1. The side slide rod 4 is slidably connected to the arc-shaped guide rail 7, the linkage frame 2 is slidably connected to the upper curved track 9, and the third infrared detection probe 12 is fixedly connected to the side sleeve column 10; the first infrared detection probe 6 and the second infrared detection probe 8 are both electrically connected to the controller 24, and the third infrared detection probe 12 is electrically connected to the controller 24. So that when the linkage frame 2 moves to the right, it will drive the upper sleeve column 3 to move to the right. The upper sleeve column 3 will drive the rubber sleeve 14 to move along the outer wall of the curved column 15 in a curved path, so that the second infrared detection probe 8 can perform curved path movement detection on the upper surface of the blade 28. At the same time, when the linkage frame 2 moves to the right, it will drive the side sliding rod 4 to move to the right in sync. The arc sleeve 5 will move to the right along the outer wall of the guide rod 13, and the side sliding rod 4 will also move to the right along the inner wall of the arc guide rail 7. The arc sleeve 5 will drive the first infrared detection probe 6 to perform multi-dimensional movement detection on the right side of the blade 28. At the same time, when the linkage frame 2 moves to the right, it will drive the side sleeve column 10 to move to the right in sync. The side sleeve column 10 will drive the silicone sleeve 16 to move along the outer wall of the curved rod 17 in a curved path. The side sleeve column 10 will drive the third infrared detection probe 12 to perform curved path movement detection along the left side gap of the blade 28. In this way, synchronous multi-dimensional detection is achieved, which greatly improves the detection efficiency.
[0031] In this embodiment, as shown in the appendix Figure 4 As shown, a guide rod 13 is slidably connected to the inner wall of the arc-shaped sleeve 5. Both ends of the guide rod 13 are fixedly connected to the same arc-shaped guide rail 7 so that the arc-shaped sleeve 5 can move to the right along the outer wall of the guide rod 13. The guide rod 13 provides stable guidance for the arc-shaped sleeve 5, ensuring that the arc-shaped sleeve 5 moves along the specified path.
[0032] In this embodiment, as shown in the appendix Figure 6As shown, a rubber sleeve 14 is fixedly connected to the inner wall of the upper sleeve 3, and a curved column 15 is slidably connected to the inner wall of the rubber sleeve 14. Both ends of the curved column 15 are fixedly connected to the same upper curved track 9, so that the upper sleeve 3 can drive the rubber sleeve 14 to move along the outer wall of the curved column 15 in a curved path, ensuring that the upper sleeve 3 moves stably along the curved path.
[0033] In this embodiment, as shown in the appendix Figure 8 As shown, a silicone sleeve 16 is fixedly connected to the inner wall of the side sleeve column 10, and a curved rod 17 is slidably connected to the inner wall of the silicone sleeve 16. Both ends of the curved rod 17 are fixedly connected to the same side curved track 11, so that the side sleeve column 10 can drive the silicone sleeve 16 to move along the outer wall of the curved rod 17 in a curved path, ensuring that the side sleeve column 10 moves stably according to the specified curved path.
[0034] In this embodiment, as shown in the appendix Figure 1 - Appendix Figure 9 As shown, the top of the bracket 1 is provided with a linkage assembly, which includes: a support frame 18, fixedly connected to the top of the bracket 1, with a screw 19 rotatably mounted on the inner wall of the support frame 18; a sleeve 20, slidably connected to the inner wall of the support frame 18, with a threaded connection between the sleeve 20 and the screw 19, a fixed connection between the bottom end of the sleeve 20 and the linkage frame 2, and a slidable connection between the sleeve 20 and the support frame 18; and a drive motor 21, installed at one end of the support frame 18, which drives the screw 19 to rotate. The drive motor 21 is electrically connected to the controller 24 so that the controller 24 can start the drive motor 21 to ensure that the drive motor 21 drives the screw 19 to rotate. Under the action of the threaded transmission force, the sleeve 20 moves to the right along the inner wall of the support frame 18, stabilizing the sleeve 20 to guide it to move to the right, and the sleeve 20 drives the linkage frame 2 to move to the right stably.
[0035] In this embodiment, as shown in the appendix Figure 1 - Appendix Figure 9As shown, an electric cylinder 22 is mounted on the lower surface of the support frame 18. The electric cylinder 22 is electrically connected to the controller 24, and the output end of the electric cylinder 22 is fixedly connected to the support frame 18. A mounting plate 23 is fixedly connected to one side of the outer wall of the electric cylinder 22. A stepper motor 25 is mounted on the upper surface of the mounting plate 23 near its center point. A positioning seat 26 is fixedly connected to the output end of the stepper motor 25. A compressor shaft head 27 is placed on the inner wall of the positioning seat 26. Multiple blades 28 are fixedly connected to the outer wall of the compressor shaft head 27. The stepper motor 25 is used to drive the positioning seat 26 to rotate, and the stepper motor 25 is electrically connected to the controller 24. So that the stepper motor 25 can be started by the controller 24, so that the stepper motor 25 drives the positioning seat 26 to rotate the compressor shaft head 27. The compressor shaft head 27 drives the blades 28 to rotate. The electric cylinder 22 will drive the support frame 18 to move down. The bracket 1 drives the side curved track 11 to be located at the left gap position of the next blade 28, the arc guide rail 7 to be located at the right gap position of the next blade 28, and at the same time the upper curved track 9 is located above the next blade 28. In this way, the switching detection of multiple blades 28 is repeated.
[0036] The working principle of the engine compressor blade detection device of the present invention is as follows: First, during the installation of this invention, in the process of new material testing of multiple blades 28, the compressor shaft head 27 is placed on the inner wall of the positioning seat 26, and multiple blades 28 are supported by the compressor shaft head 27. One blade 28 is located below the linkage frame 2, while the second infrared detection probe 8 is located above the blade 28, the first infrared detection probe 6 is located on the right side of the blade 28, and the third infrared detection probe 12 is located on the left side of the blade 28.
[0037] Secondly, when the present invention is linked, the controller 24 starts the drive motor 21, the drive motor 21 drives the screw 19 to rotate, the screw 19 drives the socket 20 to move to the right under the action of the thread transmission force, the socket 20 moves to the right along the inner wall of the support frame 18, the socket 20 drives the linkage frame 2 to move to the right, at the same time the mounting plate 23 supports the electric cylinder 22, the output end of the electric cylinder 22 supports the support frame 18, the support frame 18 supports the bracket 1, the bracket 1 supports the upper curved track 9, the bracket 1 supports the arc guide rail 7, and the bracket 1 supports the side curved track 11, increasing the stability of the arc guide rail 7, the upper curved track 9 and the side curved track 11, ensuring that the socket 20 stably drives the linkage frame 2 to move to the right.
[0038] Simultaneously, during multi-dimensional synchronous detection, when the linkage frame 2 moves to the right, it drives the upper sleeve 3 to move to the right. The upper sleeve 3 slides on the linkage frame 2, and at the same time, the upper sleeve 3 drives the rubber sleeve 14 to move along the outer wall of the curved column 15 along a curved path. During this curved path movement, the rubber sleeve 14 undergoes deformation. The upper sleeve 3 is used to drive the second infrared detection probe 8 to move along the inner wall of the upper curved track 9 along a curved path, ensuring that the second infrared detection probe 8 performs curved path movement detection on the upper surface of the blade 28. When the distance value sensed by the second infrared detection probe 8 is different from the value set by the controller 24, there is a defect on the upper surface of the blade 28, and the detection data is unqualified. When the distance value sensed by the second infrared detection probe 8 is the same as the value set by the controller 24, there is no defect on the upper surface of the blade 28, and the detection data is qualified.
[0039] Simultaneously, as the linkage frame 2 moves to the right, it also drives the side slide rod 4 to move to the right. The side slide rod 4 drives the arc sleeve 5 to move to the right, and the arc sleeve 5 moves to the right along the outer wall of the guide rod 13. At the same time, the arc sleeve 5 moves to the right along the inner wall of the arc guide rail 7, and the side slide rod 4 also moves to the right along the inner wall of the arc guide rail 7. Thus, the arc sleeve 5 moves to the right along the inner wall of the arc guide rail 7, and the arc sleeve 5 drives the first infrared detection probe 6 to move to the right along the right side gap of the blade 28 for detection. The first infrared detection probe 6 performs multi-dimensional movement detection on the right side of the blade 28. When the distance value sensed by the first infrared detection probe 6 is different from the value set by the controller 24, there is a defect on the right side of the blade 28, and the right side of the blade 28 is in an unqualified state. When the distance value sensed by the first infrared detection probe 6 is the same as the value set by the controller 24, there is no defect on the right side of the blade 28, and the right side of the blade 28 is in a qualified state.
[0040] Simultaneously, the rightward movement of the linkage frame 2 causes the side sleeve column 10 to move synchronously to the right. The side sleeve column 10 slides along the linkage frame 2, and at the same time, it drives the silicone sleeve 16 to move along the outer wall of the curved rod 17 in a curved path. Simultaneously, the side sleeve column 10 guides the movement along the inner wall of the side curved track 11 in a curved path. Furthermore, the silicone sleeve 16 can deform during this curved path movement along the outer wall of the curved rod 17, ensuring that the side sleeve column 10 can move along the curved path on the outer wall of the curved rod 17. This causes the side sleeve column 10 to drive the third infrared detection probe 12 to move along a curved path, and the third infrared detection probe 12 detects this movement along the gap on the left side of the blade 28. When the distance value sensed by the third infrared detection probe 12 is different from the value set by the controller 24, there is a defect on the left side of the blade 28, and the left side of the blade 28 is considered unqualified. When the distance value sensed by the third infrared detection probe 12 is the same as the value set by the controller 24, there is no defect on the left side of the blade 28, and the left side of the blade 28 is in a qualified state. This allows for the detection of movement along a curved path on the upper surface of the blade 28, as well as the detection of movement along a curved path on the left side of the blade 28 and the detection of movement along a multi-dimensional path on the right side of the blade 28.
[0041] Finally, during the linkage switching of this invention, after the detection is completed, the controller 24 starts the electric cylinder 22. The output end of the electric cylinder 22 pushes the support frame 18 upward, the support frame 18 drives the bracket 1 upward, the bracket 1 drives the side curved track 11 upward, and at the same time, the bracket 1 drives the upper curved track 9 upward, and the bracket 1 drives the arc-shaped guide rail 7 upward. In this way, both the side curved track 11 and the arc-shaped guide rail 7 create a large gap with the blade 28. Then, the controller 24 starts the stepper motor 25, the stepper motor 25 drives the positioning seat 26 to rotate, and the positioning seat 26 drives the compressor shaft head. 27 rotates, the compressor shaft head 27 drives the blade 28 to rotate, and the next blade 28 is located below the upper curved track 9. At the same time, the controller 24 starts the electric cylinder 22, the electric cylinder 22 drives the support frame 18 to move down, the support frame 18 drives the bracket 1 to move down, the bracket 1 drives the side curved track 11 to be located at the left gap position of the next blade 28, the arc guide rail 7 is located at the right gap position of the next blade 28, and at the same time the upper curved track 9 is located above the next blade 28, and the next blade 28 continues to be synchronously multi-dimensionally detected.
[0042] All contents not described in detail in the specification are existing technologies known to those skilled in the art, and the model parameters of each electrical appliance are not specifically limited; conventional equipment can be used. Electrical control components not mentioned in this technical solution are not shown in the figures because they are existing technologies, and will not be described here.
[0043] The above description is merely a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.
Claims
1. A detection device for engine compressor blades, comprising a bracket (1) and a controller (24), wherein a linkage frame (2) is provided on one side of the bracket (1), and a multi-dimensional synchronous detection component is installed on the inner wall of the linkage frame (2), characterized in that: The multi-dimensional synchronous detection component includes: The upper sleeve column (3) is slidably connected to the inner wall of the linkage frame (2). A side slide rod (4) is provided on one side of the upper sleeve column (3), and the side slide rod (4) is slidably connected to the linkage frame (2). An arc-shaped sleeve (5) is fixedly connected to the bottom end of the side slide rod (4). A first infrared detection probe (6) is fixedly connected to one side of the inner wall of the arc-shaped sleeve (5), and an arc-shaped guide rail (7) is slidably connected to the outer wall of the arc-shaped sleeve (5). The second infrared detection probe (8) is fixedly installed at the bottom of the upper sleeve column (3). The upper sleeve column (3) is slidably connected to the upper curved track (9) on the outer wall of the upper sleeve column (3) and on the lower surface of the linkage frame (2). The upper sleeve column (3) is used to drive the second infrared detection probe (8) to move along the curved path of the inner wall of the upper curved track (9). The side sleeve column (10) is located on the other side of the upper sleeve column (3). The side sleeve column (10) is slidably connected to the linkage frame (2). The outer wall of the side sleeve column (10) is slidably connected to the side curved track (11). The inner wall of the side curved track (11) is slidably connected to the third infrared detection probe (12). The side sleeve column (10) is used to drive the third infrared detection probe (12) to move along the curved path of the inner wall of the side curved track (11).
2. The detection device for engine compressor blades according to claim 1, characterized in that: The arc-shaped guide rail (7) and the upper curved rail (9) are both fixedly connected to the bracket (1), and the side curved rail (11) is fixedly connected to the bracket (1).
3. The detection device for engine compressor blades according to claim 1, characterized in that: The side slide rod (4) is slidably connected to the arc-shaped guide rail (7), the linkage frame (2) is slidably connected to the upper curved track (9), and the third infrared detection probe (12) is fixedly connected to the side sleeve column (10). The first infrared detection probe (6) and the second infrared detection probe (8) are both electrically connected to the controller (24), and the third infrared detection probe (12) is electrically connected to the controller (24).
4. The detection device for engine compressor blades according to claim 1, characterized in that: The inner wall of the arc sleeve (5) is slidably connected to a guide rod (13), and both ends of the guide rod (13) are fixedly connected to the same arc guide rail (7).
5. The detection device for engine compressor blades according to claim 1, characterized in that: The inner wall of the upper sleeve column (3) is fixedly connected to a rubber sleeve (14), and the inner wall of the rubber sleeve (14) is slidably connected to a curved column (15), both ends of the curved column (15) are fixedly connected to the same upper curved track (9).
6. The detection device for engine compressor blades according to claim 1, characterized in that: The inner wall of the side sleeve column (10) is fixedly connected to a silicone sleeve (16), and the inner wall of the silicone sleeve (16) is slidably connected to a curved rod (17), both ends of the curved rod (17) being fixedly connected to the same side curved track (11).
7. The detection device for engine compressor blades according to claim 1, characterized in that: The top of the bracket (1) is provided with a linkage component, the linkage component including: A support frame (18) is fixedly connected to the top of the bracket (1), and a screw (19) is rotatably installed on the inner wall of the support frame (18). A socket strip (20) is slidably connected to the inner wall of the support frame (18). The socket strip (20) is threadedly connected to the screw (19). The bottom end of the socket strip (20) is fixedly connected to the linkage frame (2). The socket strip (20) is slidably connected to the support frame (18). A drive motor (21) is installed at one end of the support frame (18). The drive motor (21) is used to drive the screw (19) to rotate. The drive motor (21) is electrically connected to the controller (24).
8. The detection device for engine compressor blades according to claim 7, characterized in that: An electric cylinder (22) is installed on the lower surface of the support frame (18). The electric cylinder (22) is electrically connected to the controller (24). The output end of the electric cylinder (22) is fixedly connected to the support frame (18). A mounting plate (23) is fixedly connected to one side of the outer wall of the electric cylinder (22). A stepper motor (25) is installed on the upper surface of the mounting plate (23) near its center point. A positioning seat (26) is fixedly connected to the output end of the stepper motor (25).
9. The detection device for engine compressor blades according to claim 8, characterized in that: The inner wall of the positioning seat (26) is provided with a compressor shaft head (27), and the outer wall of the compressor shaft head (27) is fixedly connected with multiple blades (28).
10. The detection device for engine compressor blades according to claim 8, characterized in that: The stepper motor (25) is used to drive the positioning seat (26) to rotate, and the stepper motor (25) is electrically connected to the controller (24).
Citation Information
Patent Citations
Detection device for aero-engine compressor blades
CN108489984A