CN110849286B - Aircraft tire factory detection device - Google Patents
Aircraft tire factory detection device Download PDFInfo
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- CN110849286B CN110849286B CN201911178954.0A CN201911178954A CN110849286B CN 110849286 B CN110849286 B CN 110849286B CN 201911178954 A CN201911178954 A CN 201911178954A CN 110849286 B CN110849286 B CN 110849286B
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B11/00—Measuring arrangements characterised by the use of optical techniques
- G01B11/24—Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
- G01B21/20—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring contours or curvatures, e.g. determining profile
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- General Physics & Mathematics (AREA)
- Length Measuring Devices By Optical Means (AREA)
- Tires In General (AREA)
Abstract
The invention discloses an aircraft tire delivery detection device which comprises a detection box, a detection analyzer and sealing covers, wherein an intermediate motor is fixed at the middle position inside the detection box, the detection analyzer is installed inside the detection box, the sealing covers are symmetrically arranged on two sides of the outside of the detection box, built-in grooves are symmetrically reserved on two sides of the lower surface inside the detection box, internal sliding grooves are formed in two sides above the detection box, a pressure sensor is fixed at the middle position inside a roller, an internal motor is fixed inside an installation shaft, the installation shaft is connected with the detection box through a circular groove, and side sliding grooves are formed in the side surface of a fixture block. This aircraft tire dispatches from factory and detects automatic device of comparing of shape adopts neotype structural design for this device is convenient for quick accurate positioning finished product tire's position, and the device can be to the three-dimensional diversified comprehensive detection of finished product tire, and the testing result is comparatively accurate.
Description
Technical Field
The invention relates to the technical field of aircraft tire factory detection, in particular to an aircraft tire factory detection device.
Background
The airplane tire is a structure used for buffering the load of an airplane when the airplane slides on the ground, the airplane has high requirements on the bearing performance and the wear resistance of the airplane tire due to the large volume and weight of the airplane, the airplane tire is used directly in relation to the safety of the airplane in the operation process, the requirements on the production of the airplane tire are strict, and the external shape of the airplane tire needs to be detected, analyzed and screened strictly after the airplane tire is produced and delivered from a factory.
With the continuous use of the factory shape detection device of the airplane tire, the following problems are found in the use process:
1. some existing airplane tire delivery shape detection devices are inconvenient for rapidly positioning, loading and unloading tires, and positions placed during tire detection cannot be accurately positioned, so that detection results are affected.
2. And some existing aircraft tire delivery shape detection devices are inconvenient for simultaneously detecting tires in three dimensions and multiple directions, have limited detection range, and are not beneficial to detecting the influence of external shapes on the service performance of finished tires when the tires are in a static state in the detection process.
Therefore, the aircraft tire factory inspection device needs to be designed for solving the problems.
Disclosure of Invention
The invention aims to provide an aircraft tire factory detection device, which solves the problems that the existing aircraft tire factory shape detection devices in the background art are inconvenient to quickly and accurately position, assemble and disassemble a tire during detection, are inconvenient to simultaneously detect three-dimensional and multi-direction of the tire, and cannot detect the influence of the external shape on the service performance of the finished tire when the finished tire is dynamic.
In order to achieve the purpose, the invention provides the following technical scheme: an aircraft tire delivery detection device comprises a detection box, a detection analyzer and a sealing cover, wherein an intermediate motor is fixed at the inner intermediate position of the detection box, the lower end of the intermediate motor is rotatably connected with an intermediate rotating shaft, an intermediate gear is welded on the lower surface of the intermediate rotating shaft, the detection analyzer is installed in the detection box, a side rotating shaft is rotatably connected on the inner side of the detection box, a side gear is fixed at one end of the side rotating shaft, an installation shaft is fixed at the other end of the side rotating shaft, a finished tire is arranged outside the installation shaft, the sealing cover is symmetrically arranged on the two outer sides of the detection box, laser displacement sensors are installed in the sealing cover and the detection box, a beam expanding mirror is fixed on the outer side of the laser displacement sensors, built-in grooves are reserved on the two sides of the inner lower surface of the detection box symmetrically, and rollers are arranged in the, the outer side of the roller is connected with a positioning rod through an external rotating shaft, the inner parts of two sides of the positioning rod are rotatably connected with threaded rods, a fixed block is arranged below the threaded rods and is welded on the inner lower surface of the detection box, the inner sliding grooves are formed in the inner parts of two sides of the upper part of the detection box, the inner parts of the inner sliding grooves are rotatably connected with lead screws, a pressure sensor is fixed at the middle position of the inner part of the roller, the outer part of the pressure sensor is electrically connected with an induction probe, the induction probe is arranged on the inner side of the roller, an internal motor is fixed in the installation shaft, the upper end of the internal motor is rotatably connected with a disc, a lug is rotatably connected to one side of the upper surface of the disc, the lug is connected with a limiting block through a bottom sliding groove, the bottom sliding groove, and the circular groove is reserved in the detection box, penetrating grooves are reserved in the two sides of the mounting shaft symmetrically, a clamping block is arranged in each penetrating groove, side sliding grooves are formed in the side faces of the clamping blocks and are connected with the mounting shaft through side sliding blocks, the side sliding blocks are fixed on the inner side of the mounting shaft, movable plates are fixed on the side faces of the sealing covers, and threaded holes are formed in the movable plates.
Preferably, the middle gear is meshed with the side gear, and the side gear, the side rotating shaft and the mounting shaft are of an integrated structure.
Preferably, the sealing cover and the detection box form a sliding structure, the sealing cover is fixedly connected with the movable plate, and the movable plate is in threaded connection with the screw rod through a threaded hole.
Preferably, the laser displacement sensor is located on the left side and right side of the finished tire, and is electrically connected with the detection analyzer, the detection analyzer is in remote network induction connection with the pressure sensor, and the laser displacement sensor, the pressure sensor and the detection analyzer form an external shape induction detection system.
Preferably, the gyro wheel is located the installation axle under the position, and the gyro wheel rotates with the locating lever through outside pivot to the locating lever passes through the threaded rod and constitutes elevation structure with the fixed block.
Preferably, the bump forms a sliding structure with the limiting block through a bottom sliding groove, and the limiting block is connected with the mounting shaft in a sliding manner.
Preferably, the position of fixture block corresponds each other with the position of stopper, and the side of stopper and fixture block all is the slope column structure to the fixture block passes through side spout and side slider and installs the axle and constitute extending structure, and the outside of fixture block is cellular structure simultaneously.
Compared with the prior art, the invention has the beneficial effects that: the automatic shape comparison device for the delivery detection of the airplane tire adopts a novel structural design, so that the device can quickly and accurately position, assemble and disassemble the finished tire, can simultaneously detect the finished tire in three dimensions and multiple directions, and can detect the influence of the shape on the service performance of the finished tire when the finished tire is in a dynamic rotating state during detection;
1. the lug and the limiting block arranged on the sliding structure and the clamping block arranged on the telescopic structure can drive the disc to rotate by moving the internal rotating shaft, the lug moves in the limiting block to push the limiting block to move back and forth, the clamping block is pushed outwards by the inclined surface of the limiting block in the moving process of the limiting block, the clamping block is in interference fit with the shaft sleeve of the finished tire, the finished tire is quickly and accurately positioned outside the mounting shaft, and the accuracy of a detection result is improved;
2. the laser displacement sensors, the pressure sensor and the detection analyzer form a tire shape detection system, the laser displacement sensors are distributed at the left side, the right side and the right upper position of the finished tire, during the rotation process of the finished tire, the laser displacement sensor can comprehensively detect the external shape of the tire in the three-dimensional direction, detect whether the external part of the finished tire has the problem of protrusion or depression, and the tire pushes the roller to rotate in the rotating process, the pressure sensor arranged in the roller detects the pressure condition generated to the roller when the tire rotates in real time, this structure can detect whether there is the heterology in the outside shape of tire through the change of pressure value, can detect the tire developments simultaneously and rotate the homogeneity of in-process to outer atress, and the simulation detects the stationary degree of finished product tire developments rotation in-process, improves the pluralism that detects.
Drawings
FIG. 1 is a schematic cross-sectional front view of the present invention;
FIG. 2 is a side cross-sectional structural schematic view of the present invention;
FIG. 3 is a front cross-sectional structural view of the roller of the present invention;
FIG. 4 is a side cross-sectional view of the roller of the present invention;
FIG. 5 is a front sectional view of the mounting shaft of the present invention;
FIG. 6 is a schematic view of a bottom view of a limited block according to the present invention;
FIG. 7 is an enlarged view of the structure at A in FIG. 5 according to the present invention;
fig. 8 is a front sectional structural view of the movable plate of the present invention.
In the figure: 1. a detection box; 2. an intermediate motor; 3. an intermediate rotating shaft; 4. an intermediate gear; 5. a detection analyzer; 6. a side rotating shaft; 7. a side gear; 8. installing a shaft; 9. a finished tire is obtained; 10. a sealing cover; 11. a laser displacement sensor; 12. a beam expander; 13. a built-in groove; 14. a roller; 15. an external rotating shaft; 16. positioning a rod; 17. a threaded rod; 18. a fixed block; 19. an internal chute; 20. a screw rod; 21. a pressure sensor; 22. an inductive probe; 23. an internal motor; 24. a disc; 25. a bump; 26. a bottom chute; 27. a limiting block; 28. a circular groove; 29. penetrating a groove; 30. a clamping block; 31. a side chute; 32. a side slider; 33. a movable plate; 34. a threaded bore.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-8, the present invention provides a technical solution: an aircraft tire factory detection device comprises a detection box 1, a middle motor 2, a middle rotating shaft 3, a middle gear 4, a detection analyzer 5, a side rotating shaft 6, a side gear 7, a mounting shaft 8, a finished tire 9, a sealing cover 10, a laser displacement sensor 11, a beam expanding lens 12, an internal groove 13, a roller 14, an external rotating shaft 15, a positioning rod 16, a threaded rod 17, a fixing block 18, an internal sliding groove 19, a screw rod 20, a pressure sensor 21, an induction probe 22, an internal motor 23, a disc 24, a bump 25, a bottom sliding groove 26, a limiting block 27, a circular groove 28, a through groove 29, a clamping block 30, a side sliding groove 31, a side sliding block 32, a movable plate 33 and a threaded hole 34, wherein the middle motor 2 is fixed at the internal middle position of the detection box 1, the middle rotating shaft 3 is rotatably connected to the lower end of the middle motor 2, and the, the detection analyzer 5 is arranged in the detection box 1, the inner side of the detection box 1 is rotatably connected with a side rotating shaft 6, one end of the side rotating shaft 6 is fixed with a side gear 7, the other end of the side rotating shaft 6 is fixed with an installation shaft 8, a finished tire 9 is arranged outside the installation shaft 8, sealing covers 10 are symmetrically arranged at two sides of the outer part of the detection box 1, laser displacement sensors 11 are arranged in the sealing covers 10 and the detection box 1, a beam expanding lens 12 is fixed at the outer side of each laser displacement sensor 11, built-in grooves 13 are reserved at two sides of the inner lower surface of the detection box 1 symmetrically, rollers 14 are arranged in the built-in grooves 13, the outer sides of the rollers 14 are connected with a positioning rod 16 through an outer rotating shaft 15, threaded rods 17 are rotatably connected in two sides of the positioning rod 16, a fixing block 18 is arranged below the threaded rods 17, and the fixing block 18 is welded at, the inner sliding grooves 19 are formed in the two sides of the upper portion of the detection box 1, the lead screw 20 is rotatably connected to the inner portion of the inner sliding groove 19, the pressure sensor 21 is fixed at the middle position of the inner portion of the roller 14, the sensing probe 22 is electrically connected to the outer portion of the pressure sensor 21, the sensing probe 22 is installed on the inner side of the roller 14, the inner motor 23 is fixed inside the installation shaft 8, the disc 24 is rotatably connected to the upper end of the inner motor 23, the protruding block 25 is rotatably connected to one side of the upper surface of the disc 24, the protruding block 25 is connected with the limiting block 27 through the bottom sliding groove 26, the bottom sliding groove 26 is formed in the lower surface of the limiting block 27, the installation shaft 8 is connected with the detection box 1 through the circular groove 28, the circular groove 28 is reserved inside the detection box 1, the through grooves 29 are symmetrically reserved inside the two sides, the side sliding grooves 31 are formed in the side surfaces of the latch 30, the side sliding grooves 31 are connected with the mounting shaft 8 through side sliding blocks 32, the side sliding blocks 32 are fixed on the inner side of the mounting shaft 8, a movable plate 33 is fixed on the side surface of the sealing cover 10, and threaded holes 34 are formed in the movable plate 33.
In the embodiment, the middle gear 4 is meshed with the side gear 7, the side rotating shaft 6 and the mounting shaft 8 are of an integrated structure, and the mounting shaft 8 is driven to rotate through mechanical transmission due to the structural design;
the sealing cover 10 and the detection box 1 form a sliding structure, the sealing cover 10 is fixedly connected with the movable plate 33, the movable plate 33 is in threaded connection with the screw rod 20 through the threaded hole 34, and the structure is convenient for mounting the finished tire 9;
the laser displacement sensors 11 are positioned on the left side, the right side and the right upper side of the finished tire 9, the laser displacement sensors 11 are electrically connected with the detection analyzer 5, the detection analyzer 5 is in remote network induction connection with the pressure sensor 21, meanwhile, the laser displacement sensors 11, the pressure sensor 21 and the detection analyzer 5 form an external shape induction detection system, and the laser displacement sensors 11 can comprehensively detect the shape of the finished tire 9 in the three-dimensional direction;
the roller 14 is positioned right below the mounting shaft 8, the roller 14 is rotatably connected with the positioning rod 16 through an external rotating shaft 15, the positioning rod 16 and the fixing block 18 form a lifting structure through a threaded rod 17, and the height position of the roller 14 is adjusted through rotating the threaded rod 17 according to the mounting position of the finished tire 9, so that the roller 14 is in contact with the outer side of the finished tire 9;
the bump 25 and the limiting block 27 form a sliding structure through the bottom sliding groove 26, the limiting block 27 is connected with the mounting shaft 8 in a sliding manner, and the bump 25 pushes the limiting block 27 to move in the rotating process of the disc 24;
the position of fixture block 30 corresponds to the position of stopper 27 each other, and the side of stopper 27 and fixture block 30 all is the slope column structure to fixture block 30 passes through side spout 31 and side slider 32 and installs axle 8 and constitute extending structure, and the outside of fixture block 30 is the honeycomb structure simultaneously, and fixture block 30's setting can make its axle sleeve interference fit with finished tire 9, is convenient for fast accurate loading and unloading finished tire 9.
The working principle is as follows: when the device is used, firstly, according to the structure shown in fig. 1, fig. 2, fig. 5, fig. 6, fig. 7 and fig. 8, the screw rod 20 is rotated, the screw rod 20 is in threaded connection with the movable plate 33 through the threaded hole 34, so that the position of the movable plate 33 is driven to move in the process of rotating the screw rod 20, the sealing cover 10 moves on the side surface of the detection box 1 to expose the installation position of the finished tire 9 in the detection box 1, then the finished tire 9 is respectively installed outside the installation shaft 8 at two sides of the inner side of the detection box 1, the inner motor 23 is operated, the inner motor 23 drives the disc 24 to rotate, the lug 25 slides in the bottom sliding groove 26 when the disc 24 rotates to push the limit block 27 to move in the installation shaft 8, the limit block 27 pushes the fixture block 30 to move through the inclined surface at the side edge thereof, the fixture block 30 slides in the inner side edge sliding groove 31, continuously moving the position of the fixture block 30 until the fixture block 30 is in interference fit with the shaft sleeve of the finished tire 9, quickly and accurately positioning the finished tire 9 outside the mounting shaft 8, and stopping running the internal motor 23;
subsequently, according to the structure shown in fig. 1, 2 and 4, according to the installation position of the finished tire 9, the threaded rod 17 is rotated, the threaded rod 17 is in threaded connection with the fixed block 18, the threaded rod 17 drives the positioning rod 16 to move up and down in the rotating process, the positioning rod 16 adjusts the height position of the roller 14, the roller 14 is adjusted to be in contact with the lower surface of the finished tire 9 (the finished tire 9 is kept to rotate normally), and then the screw rod 20 is rotated to adjust the position of the sealing cover 10, so that the sealing cover 10 seals two sides of the detection box 1;
then, according to the structure shown in fig. 1, fig. 2 and fig. 3, operating the intermediate motor 2, the intermediate motor 2 driving the intermediate rotating shaft 3 and the intermediate gear 4 to rotate, the intermediate gear 4 meshing with the side gear 7 to drive the side gear 7, the side rotating shaft 6 and the mounting shaft 8 to rotate, the mounting shaft 8 driving the finished tire 9 outside to rotate, controlling the rotating speed of the finished tire 9 according to the detection requirement, starting the laser displacement sensor 11, the pressure sensor 21 and the detection analyzer 5, firstly, the laser beam of the laser displacement sensor 11 is transmitted to the surface of the finished tire 9 through the function of the beam expanding lens 12, according to the rotation condition of the finished tire 9, sensing and detecting the external shape of the three-dimensional position of the finished tire 9 more comprehensively, the laser beam can detect the external diameter and width of the finished tire 9, and the laser beam senses the part of the external local protrusion or depression of the finished tire 9 to form different, the finished tires 9 on the two sides in the device are detected simultaneously, the detection results can be analyzed and compared, meanwhile, the finished tire 9 drives the roller 14 to rotate through the external rotating shaft 15 in the process of dynamic rotation, the sensing probe 22 arranged in the roller 14 senses the pressure condition on the roller 14 in the process of rotation of the finished tire 9, the signal is transmitted to the pressure sensor 21, the pressure sensor 21 forms data and transmits the data to the detection analyzer 5, the detection analyzer 5 changes the data according to the feedback of the pressure sensor 21, whether the external shape of the finished tire 9 is qualified or not is analyzed, and if the external shape of the finished tire 9 is abnormal, the pressure of the roller 14 is changed, and the change of the pressure value can also detect the stress condition in the dynamic rotation process of the finished tyre 9, the stability of the finished tire 9 in the using and rotating process is simulated and detected, and the reference value of the detection and analysis data is increased.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an aircraft tire detection device that dispatches from factory, includes detection case (1), detection analysis appearance (5) and sealed lid (10), its characterized in that: the detection box comprises a detection box (1), a middle motor (2) is fixed at the middle position inside the detection box (1), a middle rotating shaft (3) is connected to the lower end of the middle motor (2) in a rotating mode, a middle gear (4) is welded on the lower surface of the middle rotating shaft (3), a detection analyzer (5) is installed inside the detection box (1), a side rotating shaft (6) is connected to the inner side of the detection box (1) in a rotating mode, a side gear (7) is fixed at one end of the side rotating shaft (6), an installation shaft (8) is fixed at the other end of the side rotating shaft (6), a finished tire (9) is arranged outside the installation shaft (8), sealing covers (10) are symmetrically arranged on two sides of the outer portion of the detection box (1), laser displacement sensors (11) are installed inside the sealing covers (10) and the detection box (1), and a beam expanding mirror (12) is fixed on the outer, the detection box is characterized in that built-in grooves (13) are reserved on two sides of the inner lower surface of the detection box (1) symmetrically, rollers (14) are arranged in the built-in grooves (13), the outer sides of the rollers (14) are connected with positioning rods (16) through outer rotating shafts (15), threaded rods (17) are connected to the inner portions of two sides of each positioning rod (16) in a rotating mode, fixing blocks (18) are arranged below the threaded rods (17), the fixing blocks (18) are welded on the inner lower surface of the detection box (1), inner sliding grooves (19) are formed in the inner portions of two sides of the upper portion of the detection box (1), lead screws (20) are connected to the inner portions of the inner sliding grooves (19) in a rotating mode, pressure sensors (21) are fixed to the inner middle positions of the rollers (14), inductive probes (22) are electrically connected to the outer portions of the pressure sensors (21), and the inductive probes, an internal motor (23) is fixed inside the mounting shaft (8), the upper end of the internal motor (23) is rotatably connected with a disc (24), one side of the upper surface of the disc (24) is rotatably connected with a convex block (25), the convex block (25) is connected with a limiting block (27) through a bottom sliding groove (26), the bottom sliding groove (26) is arranged on the lower surface of the limiting block (27), the mounting shaft (8) is connected with the detection box (1) through a circular groove (28), the circular groove (28) is reserved inside the detection box (1), penetrating grooves (29) are symmetrically reserved inside two sides of the mounting shaft (8), meanwhile, clamping blocks (30) are arranged inside the penetrating grooves (29), side sliding grooves (31) are arranged on the side surfaces of the clamping blocks (30), and the side sliding grooves (31) are connected with the mounting shaft (8) through side sliding blocks (32), and the side slide block (32) is fixed on the inner side of the mounting shaft (8), a movable plate (33) is fixed on the side surface of the sealing cover (10), and a threaded hole (34) is formed in the movable plate (33).
2. The aircraft tire factory inspection device of claim 1, wherein: the middle gear (4) is meshed with the side gear (7) and the side gear (7), the side rotating shaft (6) and the mounting shaft (8) are of an integrated structure.
3. The aircraft tire factory inspection device of claim 1, wherein: the sealing cover (10) and the detection box (1) form a sliding structure, the sealing cover (10) is fixedly connected with the movable plate (33), and the movable plate (33) is in threaded connection with the screw rod (20) through the threaded hole (34).
4. The aircraft tire factory inspection device of claim 1, wherein: laser displacement sensor (11) are located the left and right sides of finished tire (9) and are put directly over, and laser displacement sensor (11) and detection and analysis appearance (5) electric connection to detection and analysis appearance (5) and pressure sensor (21) remote network response are connected, and laser displacement sensor (11), pressure sensor (21) and detection and analysis appearance (5) constitute outside shape response detecting system simultaneously.
5. The aircraft tire factory inspection device of claim 1, wherein: the roller (14) is located under the installation shaft (8), the roller (14) is rotatably connected with the positioning rod (16) through an external rotating shaft (15), and the positioning rod (16) forms a lifting structure with the fixing block (18) through a threaded rod (17).
6. The aircraft tire factory inspection device of claim 1, wherein: the bump (25) forms a sliding structure with the limiting block (27) through the bottom sliding groove (26), and the limiting block (27) is connected with the mounting shaft (8) in a sliding mode.
7. The aircraft tire factory inspection device of claim 1, wherein: the position of fixture block (30) corresponds to the position of stopper (27) each other, and the side of stopper (27) and fixture block (30) all is the slope column structure to fixture block (30) form extending structure through side spout (31) and side slider (32) and installation axle (8), and the outside of fixture block (30) is cellular structure simultaneously.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911178954.0A CN110849286B (en) | 2019-11-27 | 2019-11-27 | Aircraft tire factory detection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911178954.0A CN110849286B (en) | 2019-11-27 | 2019-11-27 | Aircraft tire factory detection device |
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| Publication Number | Publication Date |
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| CN110849286A CN110849286A (en) | 2020-02-28 |
| CN110849286B true CN110849286B (en) | 2020-10-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201911178954.0A Active CN110849286B (en) | 2019-11-27 | 2019-11-27 | Aircraft tire factory detection device |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0547364A2 (en) * | 1991-12-16 | 1993-06-23 | Bridgestone Corporation | Method and apparatus for measuring irregular tread wear |
| CN1227629A (en) * | 1996-07-04 | 1999-09-01 | 太阳电英国有限公司 | Apparatus and method for tire condition assessment |
| CN1318487A (en) * | 2001-06-12 | 2001-10-24 | 西南交通大学 | Automatic geometric parameter measuring equipment for wheel pair of railroad carriage |
| RU2227908C2 (en) * | 2002-04-10 | 2004-04-27 | Московская железная дорога | Diagnostic stand for rail vehicle wheelsets |
| CN102778203A (en) * | 2012-07-06 | 2012-11-14 | 天津大学 | Online measuring device and measuring and controlling method for tread thickness of tire tread winding |
| CN105571781A (en) * | 2015-12-11 | 2016-05-11 | 山东永泰集团有限公司 | Detection device of dynamic balancing and uniformity of tire |
| CN106289097A (en) * | 2015-06-24 | 2017-01-04 | 住友橡胶工业株式会社 | Tire tread process for measuring shape and tire tread shape measuring apparatus |
| CN109843609A (en) * | 2017-12-29 | 2019-06-04 | 深圳配天智能技术研究院有限公司 | Tire monitor method, slip rate computing device, system, vehicle, storage device |
-
2019
- 2019-11-27 CN CN201911178954.0A patent/CN110849286B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0547364A2 (en) * | 1991-12-16 | 1993-06-23 | Bridgestone Corporation | Method and apparatus for measuring irregular tread wear |
| CN1227629A (en) * | 1996-07-04 | 1999-09-01 | 太阳电英国有限公司 | Apparatus and method for tire condition assessment |
| CN1318487A (en) * | 2001-06-12 | 2001-10-24 | 西南交通大学 | Automatic geometric parameter measuring equipment for wheel pair of railroad carriage |
| RU2227908C2 (en) * | 2002-04-10 | 2004-04-27 | Московская железная дорога | Diagnostic stand for rail vehicle wheelsets |
| CN102778203A (en) * | 2012-07-06 | 2012-11-14 | 天津大学 | Online measuring device and measuring and controlling method for tread thickness of tire tread winding |
| CN106289097A (en) * | 2015-06-24 | 2017-01-04 | 住友橡胶工业株式会社 | Tire tread process for measuring shape and tire tread shape measuring apparatus |
| CN105571781A (en) * | 2015-12-11 | 2016-05-11 | 山东永泰集团有限公司 | Detection device of dynamic balancing and uniformity of tire |
| CN109843609A (en) * | 2017-12-29 | 2019-06-04 | 深圳配天智能技术研究院有限公司 | Tire monitor method, slip rate computing device, system, vehicle, storage device |
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| Publication number | Publication date |
|---|---|
| CN110849286A (en) | 2020-02-28 |
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