Workpiece thermal barrier coating performance detection device

By designing a thermal barrier coating performance detection device for turbine blades, combined with microscope and negative pressure testing, the problem of detecting coating adhesion is solved, the detection efficiency and accuracy are improved, and the damage and economic losses of turbine blades are prevented.

CN119246396AActive Publication Date: 2025-01-03CHINA MACHINE KAIBO SURFACE TECHNOLOGY (JIANGSU) CO LTD
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Patent Information

Application Number
CN202411530399.4
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-10-30
Publication Date
2025-01-03
Estimated Expiration
2044-10-30

AI Technical Summary

Technical Problem

The existing thermal barrier coating performance detection device is not convenient for testing the coating adhesion condition after corrosion by negative pressure during microscope detection. A small part of the peeled coating is not easily discovered, and the traditional direct scratch testing method is likely to damage the turbine. blades, causing scratches and economic losses.

Method used

A thermal barrier coating performance detection device for workpieces is designed, including a microscope base, corrosion regulator, isolation part, microscope adapter, angle adapter and coating protective stripper, and negative pressure testing and protective stripper are used to To detect the roots and thermal barrier coating of the turbine blades, prevent corrosion and scratches from corrosive fluid.

Benefits of technology

The comprehensive inspection of the roots of the turbine blades is achieved, which prevents excessive corrosion, improves detection efficiency and accuracy, avoids economic losses, and detects the adhesion performance of the thermal barrier coating through negative pressure suction, ensuring the integrity of the coating.

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Abstract

The invention discloses a workpiece thermal barrier coating performance detection device, and relates to the technical field of thermal barrier coating detection. Comprising a microscope base part, a corrosion adjusting piece is installed on the microscope base part, and the interior of the microscope base part is used for introducing corrosive liquid; an isolation part is mounted on the microscope base part; the isolation part is used for being attached to a turbine blade; a microscope adapter is mounted on the microscope base part; the microscope adapter is used for being in butt joint with a microscope lens; a detection separator is mounted at the bottom of the microscope adapter; a negative pressure suction mode is used for testing, so that a worker can comprehensively know the adhesion performance of the thermal barrier coating, and the thermal barrier coating which is only stripped but does not crack is prevented from being not found; the invention aims to solve the problems that the adhesion condition of a corroded coating is inconvenient to detect through negative pressure and a small part of stripped coating is not easy to discover when the existing thermal barrier coating performance detection device is used for microscope detection.
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Description

Technical Field

[0001] The invention relates to the technical field of thermal barrier coating detection, in particular to a device for detecting performance of thermal barrier coatings on a workpiece. Background Art

[0002] Thermal barrier coating is a layer of ceramic coating, which is deposited on the surface of high temperature resistant metal or super alloy. Thermal barrier coating plays a role of heat insulation for the base material and reduces the base temperature. In the actual production and manufacturing of turbine blades, because the working conditions of worm wheel blades are relatively extreme, thermal barrier coating is needed to improve the service life of the turbine. At present, in addition to extreme heating test, the quality inspection of worm wheel blade coating also needs to be carried out for corrosion resistance test, and the corrosion condition of the coating surface is observed microscopically with a microscope. Usually, the turbine blade is taken manually for corrosion soaking and then placed under a microscope for observation. The root of the turbine blade of the current thermal barrier coating performance testing device often does not have thermal barrier coating, which is not convenient for protecting the root of the turbine blade, and it is easy to cause excessive corrosion to the root of the turbine blade, causing the turbine blade substrate to be directly scrapped. It is not convenient to detect the adhesion of the coating after corrosion through negative pressure during microscope inspection. The peeled coating inside is not easy to be found, which is easy to cause detection omissions. At the same time, the traditional method of directly scratching the coating is very easy to damage the turbine blade because of the thin coating thickness, resulting in scratches, causing the turbine blade to need to be repaired, and deeper scratches will cause the worm wheel blade to be unable to continue to be used.

[0003] To this end, we propose a device for detecting the performance of thermal barrier coatings on workpieces. Summary of the invention

[0004] The purpose of the present invention is to provide a workpiece thermal barrier coating performance detection device to solve the problem mentioned in the above background technology that the current thermal barrier coating performance detection device is not convenient for detecting the coating adhesion after corrosion through negative pressure during microscope detection, and a small part of the peeled coating is not easy to be found.

[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a device for detecting the performance of thermal barrier coating of a workpiece, comprising a microscope base, a corrosion adjusting part is installed on the microscope base, and the interior of the microscope base is used to introduce a corrosion liquid; an isolation part is installed on the microscope base; the isolation part is used to fit a turbine blade; a microscope adapter is installed on the microscope base; the microscope adapter is used to dock a microscope lens; a detection isolation part is installed at the bottom of the microscope adapter; an angle adapter is installed at the bottom of the detection isolation part; the angle adapter is used to fit the thermal barrier coating of a turbine blade; the angle adapter is used to test the adhesion of the coating under negative pressure; a coating protection stripping part is installed on the angle adapter; the coating protection stripping part is used to fit the thermal barrier coating; the microscope base comprises: a microscope base plate and a mounting threaded barrel, a mounting threaded barrel is installed on the microscope base plate, and a thread is provided on the upper part of the mounting threaded barrel; the microscope base plate is used to be placed on a microscope stage.

[0006] Preferably, the coating protection stripping piece also includes: a downward pressure spring and a stripping scraper, the downward pressure spring is sleeved on the sliding column; one end of the downward pressure spring is connected to the top of the stripping sliding seat, and the other end of the downward pressure spring is connected to the sliding column; the downward pressure spring is used to pull the sliding column downward to press the thermal barrier coating; a circle of stripping scrapers is fixedly installed at the bottom of the sliding column, and the circle of stripping scrapers is used to scrape the bulging thermal barrier coating.

[0007] Preferably, the angle adapter also includes: a suction tube and a return spring, the suction tube is fixedly mounted on the rotating sleeve; the suction tube passes through the mounting threaded tube; the suction tube is externally connected to a vacuum pump; the rotating sleeve is used for negative pressure suction of the thermal barrier coating; a return spring is sleeved on the detection isolation tube; one end of the return spring is connected to the detection isolation tube, and the other end of the return spring is fixedly mounted on the rotating sleeve.

[0008] Preferably, the microscope base also includes: an electric heating plate, an adjusting worm and a guide tube, the electric heating plate is fixedly installed inside the microscope base plate; the adjusting worm is rotatably installed on the microscope base plate; the electric heating plate is located on the inner side of the mounting threaded tube; two guide tubes are fixedly installed on the microscope base plate, and valves are respectively provided on the two guide tubes; the upper guide tube is used for the inlet of corrosive liquid, and the lower guide tube is used for the outlet of corrosive liquid; a handwheel is provided on the side of the adjusting worm.

[0009] Preferably, the coating protection stripping member comprises: a stripping sliding seat and a sliding column, wherein the stripping sliding seat is fixedly mounted on the inner side of the rotating sleeve; a sliding column is slidably sleeved on the stripping sliding seat; and the bottom of the sliding column is an arc-shaped structure.

[0010] Preferably, the microscope adapter comprises: an upper cover, a corrugated sleeve, a plastic tube and a lifting spring, the upper cover is threadedly connected to the mounting threaded tube; a corrugated sleeve is fixedly mounted on the bottom of the upper cover; a plastic tube is fixedly mounted on the bottom of the corrugated sleeve; the plastic tube is used to sleeve the microscope lens; a lifting spring is fixedly mounted on the bottom of the upper cover, and the lifting spring is sleeved on the outside of the corrugated sleeve; a taper is provided between the lifting spring and the outside of the corrugated sleeve.

[0011] Preferably, the angle adapter comprises: a rotating sleeve, a fill light and a rubber ring, the rotating sleeve is sleeved on the spherical sleeve; the fill light is fixedly installed on the inner side of the rotating sleeve; the fill light is used to fill light for the thermal barrier coating; a rubber ring is fixedly installed on the bottom of the rotating sleeve, and the rubber ring is used to fit the thermal barrier coating.

[0012] Preferably, the detection isolation component includes: a detection isolation cylinder, a spherical cylinder and an isolation lens, the detection isolation cylinder is fixedly installed on the bottom of the plastic cylinder; the spherical cylinder is fixedly installed on the bottom of the detection isolation cylinder; the outer side of the spherical cylinder is a spherical structure; the inner side of the detection isolation cylinder is fixedly sleeved with an isolation lens; the isolation lens is used to seal and isolate the detection isolation cylinder.

[0013] Preferably, the corrosion adjustment part includes: a driving worm gear, a clamping plate and a clamping bolt, the driving worm gear is rotatably mounted on the microscope base plate; the driving worm gear is meshed with the adjusting worm; a clamping plate is fixedly mounted on the shaft end of the driving worm gear, and a row of arc-shaped protrusions are provided on the inner side of the bottom of the clamping plate; the row of arc-shaped protrusions on the inner side of the bottom of the clamping plate are used to fit and clamp the turbine blades; a clamping bolt is threadedly connected to the clamping plate, and a handwheel is provided on the top of the clamping bolt; the clamping plate is a U-shaped structure.

[0014] Preferably, the isolation part includes: an isolation plate, a sliding guide shaft, a fitting spring, an isolation rubber sheet and a fitting sealing ring, the isolation plate is located inside the microscope base plate; two sliding guide shafts are fixedly installed on the isolation plate; the two sliding guide shafts are slidably inserted inside the microscope base plate; the two sliding guide shafts are respectively sleeved with fitting springs; the isolation rubber sheet is fixedly installed on the top of the electric heating plate, and both sides of the isolation rubber sheet are fixedly installed inside the microscope base plate; the isolation plate is fixedly fitted with the isolation rubber sheet; a fitting sealing ring is fixedly installed on the isolation plate, and the fitting sealing ring is used to seal and fit on the end of the turbine blade.

[0015] Compared with the prior art, the present invention has the following beneficial effects:

[0016] The present invention adopts a corrosion adjustment member to facilitate the staff to quickly switch the detection position of the turbine blade, ensuring the comprehensiveness of the detection. The structure can fit and seal the root of the turbine blade to prevent the root of the turbine blade from being corroded by the corrosive liquid, resulting in reduced accuracy when the root of the turbine blade is installed on the turbine ring, and excessive corrosion caused by the lack of a thermal barrier coating on the root of the turbine blade, thereby preventing economic losses caused by the test.

[0017] By using a microscope adapter, the structure can be directly used for corrosion testing on the stage of the microscope, which can avoid the problem of dripping of corrosion liquid caused by taking and transferring the turbine blades, thereby preventing the problem of low test efficiency. At the same time, the structure uses an upper cover for sealing, combined with an isolation lens, which does not affect the observation test under the microscope and also plays a sealing role to prevent the residual corrosion liquid from evaporating and causing damage to the staff who are inspecting and observing on the microscope above.

[0018] The use of angle adapters can ensure that the structure has better adaptability to turbine blades with certain curved surfaces, and also ensure that the fill light can better fill in the light perpendicular to the detection surface to avoid side light affecting the staff's observation. Testing by negative pressure suction can better test the adhesion of the thermal barrier coating surface, which is convenient for staff to fully understand the adhesion performance of the thermal barrier coating. The locations where there is peeling in the thermal barrier coating will swell under the action of negative pressure, preventing the thermal barrier coating that has only peeled off but no cracks from being discovered.

[0019] The use of coating protection stripping parts can facilitate further separation of the coating at cracked and peeled locations, making it easier for workers to observe the corrosion of the turbine blade base at cracked and peeled locations under a microscope. The bottom end of the stripping scraper is higher than the sliding column, which can prevent the stripping scraper from scratching the turbine blade when rubbing the thermal barrier coating, thereby improving the protection effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 It is a schematic diagram of the overall structure of a device for detecting the performance of thermal barrier coatings on a workpiece according to the present invention;

[0021] Figure 2 It is a schematic diagram of the rear side structure of a device for detecting the performance of thermal barrier coatings on a workpiece according to the present invention;

[0022] Figure 3 This is a schematic diagram of the internal structure of a device for detecting the performance of thermal barrier coatings on a workpiece according to the present invention;

[0023] Figure 4 It is a schematic diagram of the structure of the microscope base of the present invention;

[0024] Figure 5 This is a schematic diagram of the structure of the corrosion regulating member of the present invention;

[0025] Figure 6 It is a schematic diagram of the isolation part structure of the present invention;

[0026] Figure 7 This is a schematic diagram of the installation position of the isolation part of the present invention;

[0027] Figure 8 This is a schematic diagram of the bottom structure of the microscope adapter of the present invention;

[0028] Fig. 9 For the present invention Figure 3 A magnified view of the structure of the middle B region;

[0029] Fig.10 This is a schematic diagram of the structure of the detection isolation element of the present invention;

[0030] Fig.11 For the present invention Fig.10 A magnified view of the structure of the middle C region;

[0031] Fig.12 For the present invention Figure 3 A magnified view of the structure in region D.

[0032] In the figure: 1. microscope base; 101. microscope base plate; 1011. mounting threaded cylinder; 1012. electric heating plate; 102. adjusting worm; 103. flow guide tube; 2. corrosion adjusting member; 201. driving worm gear; 202. clamping plate; 203. clamping bolt; 3. isolation part; 301. isolation plate; 3011. sliding guide shaft; 302. fitting spring; 303. isolation rubber sheet; 304. fitting sealing ring; 4. microscope adapter; 401. Upper cover; 402, corrugated sleeve; 403, plastic cylinder; 404, lifting spring; 5, detection isolation piece; 501, detection isolation cylinder; 5011, spherical cylinder; 502, isolation lens; 6, angle adapter; 601, rotating sleeve; 602, fill light; 603, rubber ring; 604, suction tube; 605, reset spring; 7, coating protection stripping piece; 701, stripping sliding seat; 702, sliding column; 7021, pressing spring; 703, stripping scraper. DETAILED DESCRIPTION

[0033] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0034] Example 1: Please refer to Figure 1-Figure 12 As shown:

[0035] The present invention provides a technical solution: a workpiece thermal barrier coating performance detection device, comprising a microscope base part 1, a corrosion adjustment part 2 is installed on the microscope base part 1, and the interior of the microscope base part 1 is used to introduce a corrosion liquid; an isolation part 3 is installed on the microscope base part 1; the isolation part 3 is used to fit a turbine blade; a microscope adapter 4 is installed on the microscope base part 1; the microscope adapter 4 is used to dock a microscope lens; a detection isolation part 5 is installed at the bottom of the microscope adapter 4; an angle adapter 6 is installed at the bottom of the detection isolation part 5; the angle adapter 6 is used to fit a thermal barrier coating of a turbine blade; the angle adapter 6 is used to test the adhesion of the coating under negative pressure; a coating protection stripping part 7 is installed on the angle adapter 6; the coating protection stripping part 7 is used to fit a thermal barrier coating; the microscope base part 1 comprises: a microscope base plate 101 and a mounting threaded barrel 1011, the microscope base plate 101 is installed with the mounting threaded barrel 1011, and the upper part of the mounting threaded barrel 1011 is provided with threads; the microscope base plate 101 is used to be placed on a microscope stage.

[0036] The microscope base 1 further comprises: an electric heating plate 1012, an adjusting worm 102 and a guide tube 103, wherein the electric heating plate 1012 is fixedly mounted inside the microscope base plate 101; the adjusting worm 102 is rotatably mounted on the microscope base plate 101; the electric heating plate 1012 is located on the inner side of the mounting threaded tube 1011; two guide tubes 103 are fixedly mounted on the microscope base plate 101, and valves are respectively arranged on the two guide tubes 103; the upper guide tube 103 is used for the inlet of the corrosive liquid, and the lower guide tube 103 is used for the outlet of the corrosive liquid; a hand wheel is arranged on the side of the adjusting worm 102; the corrosion adjusting member 2 comprises: a driving worm wheel 201, a clamping plate 202 and a clamping bolt 203, the driving worm wheel 201 is rotatably mounted on the microscope base plate 101; the driving worm wheel 201 is meshed with the adjusting worm 102; the driving worm wheel 201 shaft end is fixedly mounted with a clamping plate 202, and a row of arc-shaped protrusions are provided on the inner side of the bottom of the clamping plate 202; the row of arc-shaped protrusions on the inner side of the bottom of the clamping plate 202 is used to fit and clamp the turbine blades; the clamping plate 202 is threadedly connected with a clamping bolt 203, and a hand wheel is provided on the top of the clamping bolt 203; the clamping plate 202 is a U-shaped structure; the isolation part 3 includes: an isolation plate 301, a sliding guide shaft 3011, a fitting spring 302, an isolation rubber sheet 303 and a fitting sealing ring 304, and the isolation plate 301 is located at the microscope Inside the base plate 101; two sliding guide shafts 3011 are fixedly installed on the isolation plate 301; the two sliding guide shafts 3011 are slidably inserted into the inside of the microscope base plate 101; the two sliding guide shafts 3011 are respectively sleeved with fitting springs 302; the isolation rubber sheet 303 is fixedly installed on the top of the electric heating plate 1012, and the two sides of the isolation rubber sheet 303 are fixedly installed inside the microscope base plate 101; the isolation plate 301 is fixedly fitted with the isolation rubber sheet 303; a fitting sealing ring 304 is fixedly installed on the isolation plate 301, and the fitting sealing ring 304 is used to seal and fit on the end of the turbine blade, and the use of the corrosion adjustment member 2 can facilitate the staff to switch quickly The inspection position of the turbine blades can be freely controlled, which is more flexible and ensures comprehensive inspection. The microscope base 1 is used in conjunction with the isolation part 3 to immerse the turbine blades in corrosive liquid, so that the corrosion resistance of the turbine blades can be tested. At the same time, this structure can seal the roots of the turbine blades to prevent the roots of the turbine blades from being corroded by the corrosive liquid, which causes the accuracy of the turbine blade roots being reduced when installed on the turbine ring, and avoids excessive corrosion caused by the lack of a thermal barrier coating at the roots of the turbine blades. This structure is easy to install, and the flexible structure of the isolation rubber sheet 303, in conjunction with the fitting spring 302 to squeeze the isolation plate 301, can be elastically and tightly fitted on the turbine blades for sealing.

[0037] The microscope adapter 4 includes: an upper cover 401, a corrugated sleeve 402, a plastic tube 403 and a lifting spring 404. The upper cover 401 is threadedly connected to the mounting threaded tube 1011; the corrugated sleeve 402 is fixedly installed at the bottom of the upper cover 401; the plastic tube 403 is fixedly installed at the bottom of the corrugated sleeve 402; the plastic tube 403 is used to sleeve the microscope lens; the lifting spring 404 is fixedly installed at the bottom of the upper cover 401, and the lifting spring 404 is sleeved on the corrugated sleeve 402. The outer side of the sleeve 402; the lifting spring 404 and the outer side of the corrugated sleeve 402 are provided with a taper; the detection isolation member 5 comprises: a detection isolation cylinder 501, a spherical cylinder 5011 and an isolation lens 502, the detection isolation cylinder 501 is fixedly mounted on the bottom of the plastic cylinder 403; the bottom of the detection isolation cylinder 501 is fixedly mounted with a spherical cylinder 5011; the outer side of the spherical cylinder 5011 is a spherical structure; the inner side of the detection isolation cylinder 501 is fixedly sleeved with an isolation lens 502; the isolation lens 50 2 is used for sealing and isolating the detection isolation tube 501; the microscope adapter 4 is used to facilitate the corrosion test of the present structure directly on the storage table of the microscope, which can avoid the problem of dripping of corrosion liquid caused by taking and transferring turbine blades, and the problem of low test efficiency. At the same time, the present structure uses the upper cover 401 for sealing, and cooperates with the isolation lens 502, which does not affect the observation test of the microscope, and at the same time plays a sealing role to avoid the residual corrosion liquid from evaporating and causing damage to the staff who are inspecting and observing on the microscope above. At the same time, the present structure uses the flexible structure of the corrugated sleeve 402 to ensure the flexibility of the microscope lens during observation, and does not affect the adjustment of the observation direction of the microscope. The upper lifting spring 404 is also used to lift the corrugated sleeve 402, so that the isolation lens 502 can be stably attached to the front end of the microscope lens to ensure the stability of the lens during adjustment. The present structure also uses the isolation lens 502 to play an isolation role, which is convenient for subsequent negative pressure suction detection.

[0038] Among them, the angle adapter 6 includes: a rotating sleeve 601, a fill light 602 and a rubber ring 603, the rotating sleeve 601 is sleeved on the spherical cylinder 5011; the fill light 602 is fixedly installed on the inner side of the rotating sleeve 601; the fill light 602 is used to fill light for the thermal barrier coating; a rubber ring 603 is fixedly installed on the bottom of the rotating sleeve 601, and the rubber ring 603 is used to fit the thermal barrier coating; the angle adapter 6 also includes: a suction tube 604 and a reset spring 605, the suction tube 604 is fixedly installed on the rotating sleeve 601; the suction tube 604 passes through the mounting threaded cylinder 1011; the suction tube 604 is externally connected to a vacuum pump; the rotating sleeve 601 is used for negative pressure suction of the thermal barrier coating; the reset spring 605 is sleeved on the detection isolation cylinder 501; one end of the reset spring 605 is connected to the detection isolation cylinder 501, and the other end of the reset spring 605 is fixedly installed on the rotating sleeve An angle adapter 6 is used on the sleeve 601. On the one hand, it can ensure that the present structure has better adaptability to turbine blades with a certain curved surface, ensure that the rubber ring 603 can adaptively fit the surface of the turbine blade, and also ensure that the fill light 602 can better fill light perpendicular to the detection surface to avoid side light affecting the observation of the staff. On the other hand, the angle adapter 6 is used to test by negative pressure suction, which can better test the adhesion of the surface of the thermal barrier coating. When the negative pressure suction is performed, if the coating is peeled off, the coating will swell under the action of negative pressure, which can make it easier for the staff to observe and distinguish under a microscope, and have a more comprehensive understanding of the adhesion performance of the thermal barrier coating. Under the action of negative pressure, the location where the thermal barrier coating is peeled off will swell under the action of negative pressure, preventing the thermal barrier coating that is only peeled off but not cracked from being discovered.

[0039] Embodiment 2, on the basis of embodiment 1, the coating protection stripping member 7 comprises: a stripping sliding seat 701 and a sliding column 702, the stripping sliding seat 701 is fixedly mounted on the inner side of the rotating sleeve 601; the stripping sliding seat 701 is slidably sleeved with the sliding column 702; the bottom of the sliding column 702 is an arc-shaped structure; the coating protection stripping member 7 also comprises: a downward pressure spring 7021 and a stripping scraper 703, the downward pressure spring 7021 is sleeved on the sliding column 702; one end of the downward pressure spring 7021 is connected to the top of the stripping sliding seat 701, and the downward pressure spring 7021 is connected to the top of the stripping sliding seat 701. The other end of 021 is connected to the sliding column 702; the downward tension spring 7021 is used to pull the sliding column 702 downward to fit the thermal barrier coating; a circle of stripping scrapers 703 is fixedly installed at the bottom of the sliding column 702, and the circle of stripping scrapers 703 is used to scrape the bulging thermal barrier coating. The use of the coating protection stripping piece 7 can facilitate further separation of the coating at the cracked and stripped locations, so that it can be separated from the turbine blade substrate, which can facilitate the staff to observe the corrosion of the turbine blade substrate at the cracked and stripped hollow locations under a microscope. In order to more comprehensively understand the performance of the thermal barrier coating, the bottom end of the stripping scraper 703 used in this structure is higher than the sliding column 702, which can prevent the probability of the stripping scraper 703 scratching the turbine blade when rubbing the thermal barrier coating. The arc-shaped bottom of the sliding column 702 further prevents scratches on the turbine blade. This structure can prevent damage to the normal turbine blades that meet the standards and avoid increasing economic losses. The coating protection stripping piece 7 is used in conjunction with the angle adapter 6 to conduct a comprehensive test of the adhesion of the thermal barrier coating, which is also convenient for observation under a microscope to ensure the efficiency of the test. If cracks appear in the thermal barrier coating and it is corroded and peeled off, the peeling position will also be aggravated under the extrusion and friction of the sliding column 702, resulting in warping. During the movement of the sliding column 702, the stripping scraper 703 can be further separated from the position where the warping exists, which is convenient for the staff to observe the corrosion of the substrate under the thermal barrier coating of the turbine blade and understand the anti-permeability of the thermal barrier coating. The bottom of the sliding column 702 is used to support the stripping scraper 703 to prevent the stripping scraper 703 from directly scratching and damaging the substrate under the thermal barrier coating of the turbine blade.

[0040] The working principle of this embodiment is as follows: first, the microscope base plate 101 is placed on the microscope stage, the turbine blade is placed on the microscope base plate 101, the root of the turbine blade is placed on the clamping plate 202, and the clamping bolt 203 is tightened to clamp and position, the electric heating plate 1012 is powered on for heating, the upper guide tube 103 is connected to the corrosion liquid pump to introduce the corrosion liquid into the microscope base plate 101, and the valve of the lower guide tube 103 is opened when draining the liquid. After the corrosion is completed, the lower guide tube 103 can be connected to an external liquid tank for recycling, and the rotating adjustment worm 102 can engage the driving worm gear 201 set to rotate, driving the turbine blade clamped on the clamping plate 202 to rotate and adjust; insert the microscope lens into the plastic cylinder 403, at this time, the microscope lens can be lowered to approach the turbine blade, and the isolation lens 502 can be stably attached to the front end of the microscope lens during the process, and the microscope lens is controlled to move downward, driving the rubber ring 603 to fit on the surface of the workpiece and apply a certain pressure, and the rotating sleeve 601 will rotate in the spherical cylinder during the process. 5011 is rotated to adapt to the surface of the turbine blade, and the vacuum pump connected to the suction pipe 604 is started. At this time, under the action of negative pressure, the position where the thermal barrier coating is peeled off will swell under the action of negative pressure, and a microscopic inspection can be performed through a microscope; after the negative pressure test is performed through the angle adapter 6, the microscope lens is controlled to move up slightly to prevent the rubber ring 603 from rubbing the thermal barrier coating. Under the elastic extrusion of the reset spring 605, the rotating sleeve 601 can be elastically squeezed to rotate and reset on the spherical cylinder 5011. At the same time, under the pull of the downward tension spring 7021, the bottom of the sliding column 702 is elastically attached to the thermal barrier coating. The thermal barrier coating can be rubbed and squeezed through the bottom of the sliding column 702. If cracks appear in the thermal barrier coating and it is corroded and peeled off, the strength is reduced. Under the extrusion of the sliding column 702, the peeling position will also be aggravated, resulting in warping. During the movement of the sliding column 702, the peeling scraper 703 can further separate the position where the warping exists, so that the staff can observe the corrosion of the substrate under the thermal barrier coating of the turbine blade through a microscope.

[0041] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0042] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A device for detecting the performance of a thermal barrier coating of a workpiece, comprising a microscope base (1), on which a corrosion adjustment member (2) is mounted, characterized in that: The interior of the microscope base (1) is used for introducing a corrosive liquid; an isolation portion (3) is installed on the microscope base (1); the isolation portion (3) is used for fitting a turbine blade; A microscope adapter (4) is installed on the microscope base (1); the microscope adapter (4) is used to dock with a microscope lens; A detection isolation piece (5) is installed at the bottom of the microscope adapter (4); an angle adapter (6) is installed at the bottom of the detection isolation piece (5); the angle adapter (6) is used to adhere to the thermal barrier coating of the turbine blade; The angle adapter (6) is used for negative pressure testing of coating adhesion; The angle adapter (6) is provided with a coating protection stripping piece (7); the coating protection stripping piece (7) is used for bonding the thermal barrier coating; The microscope base part (1) comprises: a microscope base plate (101) and a mounting threaded barrel (1011); the microscope base plate (101) is mounted with the mounting threaded barrel (1011), and the upper part of the mounting threaded barrel (1011) is provided with threads; the microscope base plate (101) is used for being placed on a microscope stage.

2. A workpiece thermal barrier coating performance detection device according to claim 1, characterized in that: The microscope base (1) further comprises: an electric heating plate (1012), an adjusting worm (102) and a flow guide tube (103); the electric heating plate (1012) is fixedly mounted inside the microscope base plate (101); the adjusting worm (102) is rotatably mounted on the microscope base plate (101); the electric heating plate (1012) is located inside the mounting threaded cylinder (1011); two flow guide tubes (103) are fixedly mounted on the microscope base plate (101), and valves are respectively provided on the two flow guide tubes (103); the upper flow guide tube (103) is used for the inlet of etching liquid, and the lower flow guide tube (103) is used for the outlet of etching liquid; and a hand wheel is provided on the side of the adjusting worm (102).

3. A workpiece thermal barrier coating performance detection device according to claim 2, characterized in that: The corrosion adjustment member (2) comprises: a driving worm gear (201), a clamping plate (202) and a clamping bolt (203); the driving worm gear (201) is rotatably mounted on a microscope base plate (101); the driving worm gear (201) is meshed with an adjustment worm (102); a clamping plate (202) is fixedly mounted on the axial end of the driving worm gear (201), and a row of arc-shaped protrusions are provided on the inner side of the bottom of the clamping plate (202); the row of arc-shaped protrusions on the inner side of the bottom of the clamping plate (202) are used to fit and clamp turbine blades; a clamping bolt (203) is threadedly connected to the clamping plate (202), and a hand wheel is provided on the top of the clamping bolt (203); the clamping plate (202) is a U-shaped structure.

4. A workpiece thermal barrier coating performance detection device according to claim 2, characterized in that: The isolation part (3) comprises: an isolation plate (301), a sliding guide shaft (3011), a fitting spring (302), an isolation rubber sheet (303) and a fitting sealing ring (304); the isolation plate (301) is located inside the microscope base plate (101); two sliding guide shafts (3011) are fixedly mounted on the isolation plate (301); the two sliding guide shafts (3011) are slidably inserted inside the microscope base plate (101); the two sliding guide shafts (3011) are respectively sleeved with fitting springs (302); the isolation rubber sheet (303) is fixedly mounted on the top of the electric heating plate (1012), and both sides of the isolation rubber sheet (303) are fixedly mounted inside the microscope base plate (101); the isolation plate (301) is fixedly fitted with the isolation rubber sheet (303); a fitting sealing ring (304) is fixedly mounted on the isolation plate (301), and the fitting sealing ring (304) is used for sealing and fitting on the end of a turbine blade.

5. The device for detecting the performance of thermal barrier coatings on a workpiece according to claim 1, characterized in that: The microscope adapter (4) comprises: an upper cover (401), a corrugated sleeve (402), a plastic tube (403) and a lifting spring (404); the upper cover (401) is threadedly connected to the mounting threaded tube (1011); the corrugated sleeve (402) is fixedly mounted on the bottom of the upper cover (401); the plastic tube (403) is fixedly mounted on the bottom of the corrugated sleeve (402); the plastic tube (403) is used for sleeve-mounting a microscope lens; the upper cover (401) is fixedly mounted on the bottom of the upper cover (401), and the lifting spring (404) is sleeved on the outside of the corrugated sleeve (402); the lifting spring (404) and the outside of the corrugated sleeve (402) are provided with a taper.

6. A workpiece thermal barrier coating performance detection device according to claim 5, characterized in that: The detection isolation member (5) comprises: a detection isolation cylinder (501), a spherical cylinder (5011) and an isolation lens (502); the detection isolation cylinder (501) is fixedly mounted on the bottom of the plastic cylinder (403); the spherical cylinder (5011) is fixedly mounted on the bottom of the detection isolation cylinder (501); the outer side of the spherical cylinder (5011) is a spherical structure; the inner side of the detection isolation cylinder (501) is fixedly sleeved with the isolation lens (502); the isolation lens (502) is used for sealing and isolating the detection isolation cylinder (501).

7. A workpiece thermal barrier coating performance detection device according to claim 6, characterized in that: The angle adapter (6) comprises: a rotating sleeve (601), a fill light (602) and a rubber ring (603); the rotating sleeve (601) is sleeved on the spherical cylinder (5011); the fill light (602) is fixedly installed on the inner side of the rotating sleeve (601); the fill light (602) is used to fill light for the thermal barrier coating; the rubber ring (603) is fixedly installed on the bottom of the rotating sleeve (601), and the rubber ring (603) is used to fit the thermal barrier coating.

8. The device for detecting the performance of thermal barrier coatings on a workpiece according to claim 7, characterized in that: The angle adapter (6) further comprises: a suction pipe (604) and a return spring (605); the suction pipe (604) is fixedly mounted on the rotating sleeve (601); the suction pipe (604) passes through the mounting threaded cylinder (1011); the suction pipe (604) is externally connected to a vacuum pump; the rotating sleeve (601) is used for negative pressure suction of the thermal barrier coating; a return spring (605) is sleeved on the detection isolation cylinder (501); one end of the return spring (605) is connected to the detection isolation cylinder (501), and the other end of the return spring (605) is fixedly mounted on the rotating sleeve (601).

9. The device for detecting the performance of thermal barrier coatings on a workpiece according to claim 7, characterized in that: The coating protection stripping member (7) comprises: a stripping sliding seat (701) and a sliding column (702); the stripping sliding seat (701) is fixedly mounted on the inner side of the rotating sleeve (601); the sliding column (702) is slidably sleeved on the stripping sliding seat (701); and the bottom of the sliding column (702) is an arc-shaped structure.

10. A workpiece thermal barrier coating performance detection device according to claim 9, characterized in that: The coating protection stripping member (7) further comprises: a downward pressure tension spring (7021) and a stripping scraper (703), wherein the downward pressure tension spring (7021) is sleeved on the sliding column (702); one end of the downward pressure tension spring (7021) is connected to the top of the stripping sliding seat (701), and the other end of the downward pressure tension spring (7021) is connected to the sliding column (702); the downward pressure tension spring (7021) is used to pull the sliding column (702) downward to press the thermal barrier coating; a circle of stripping scrapers (703) is fixedly installed at the bottom of the sliding column (702), and the circle of stripping scrapers (703) is used to scrape the bulging thermal barrier coating.

Citation Information

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