CN211262143U - Automatic coaxiality debugging equipment - Google Patents
Automatic coaxiality debugging equipment Download PDFInfo
- Publication number
- CN211262143U CN211262143U CN201922386401.6U CN201922386401U CN211262143U CN 211262143 U CN211262143 U CN 211262143U CN 201922386401 U CN201922386401 U CN 201922386401U CN 211262143 U CN211262143 U CN 211262143U
- Authority
- CN
- China
- Prior art keywords
- motor
- fixed
- positioning
- installation
- connecting plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Abstract
The utility model discloses an automatic debugging equipment of axiality, include through the drive arrangement activity in the fixed frock of motor and the fixed frock of aircraft nose of installation station and butt joint station, the fixed frock fixed mounting of motor is in the frame, the fixed frock of aircraft nose passes through adjusting device and frame fixed, the fixed frock of motor and aircraft nose passes through the flange butt joint after adjusting for the axiality through laser sensor and adjusting device with motor and aircraft nose when being located the butt joint station simultaneously. In this way, the utility model discloses can guarantee that the precision of aircraft nose and motor axiality is high, reduce loaded down with trivial details operating procedure, alleviate workman's intensity of labour, can take notes operation process and measured data, improve the output in the unit interval.
Description
Technical Field
The utility model relates to an intelligence field of making especially relates to an automatic debugging equipment of axiality.
Background
Because the motor with the weight of about 300KG needs to be hoisted to a horizontal workbench manually, the other end of the motor is about 250KG of machine head, the machine head needs to be arranged on a hydraulic lifting trolley which is stepped on by feet, the butt joint position of the machine head and the motor is adjusted by the height of the lifting trolley and the method of moving the trolley, the coaxiality of a motor shaft and a machine head shaft is ensured by the motor flange and the spigot precision of the machine head flange, the installation of workers is difficult, the vibration of the motor after working is large, the noise is large, the service life of a shaft coupling of two shafts is greatly reduced, and the maintenance cost of products is increased.
Therefore, the data recording is difficult when the installation is difficult, the product quality is not high, and the maintenance cost is high.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the main technical problem who solves provides an automatic debugging equipment of axiality, can guarantee that the precision of aircraft nose and motor axiality is high, reduces loaded down with trivial details operating procedure, alleviates workman's intensity of labour, can take notes operation process and measured data, improves the output in the unit interval.
In order to solve the technical problem, the utility model discloses a technical scheme be: the utility model provides an automatic debugging equipment of axiality, includes the fixed frock of motor and the fixed frock of aircraft nose through drive arrangement activity in installation station and butt joint station, the fixed frock fixed mounting of motor is in the frame, the fixed frock of aircraft nose passes through adjusting device and frame fixed, the fixed frock of motor and aircraft nose passes through the flange butt joint after adjusting motor and aircraft nose for the axiality through laser sensor and adjusting device when being located the butt joint station simultaneously.
Further, adjusting device includes guiding mechanism and displacement mechanism, displacement mechanism is including fixing the linear motion subassembly in the symmetry of frame, be fixed with the mounting panel on the slider of linear motion subassembly, install guiding mechanism on the mounting panel, the last fixed frock of aircraft nose of installing of guiding mechanism.
Further, the motor fixing tool and the machine head fixing tool are the same in structure.
The motor fixing tool and the machine head fixing tool further comprise bottom plates driven by the driving device, displacement slide rails are symmetrically arranged on the bottom plates, connecting plates are fixedly arranged on sliders of the displacement slide rails, the bottom plates and the connecting plates respectively comprise three straight sides and an arc-shaped side, bayonets are arranged on the arc-shaped sides of the bottom plates and the straight sides opposite to the arc-shaped sides, and the bayonets when the bottom plates are positioned at the motor mounting station and the machine head mounting station are fixed through clamping blocks driven by the driving device; the positioning device comprises a connecting plate, positioning blocks, a driving device and an ejector rod, wherein the two straight edges of the connecting plate, which are connected with an arc edge, are fixedly provided with limiting blocks, the limiting blocks are provided with limiting grooves, the straight edges of the connecting plate, which are opposite to the arc edge, are fixedly provided with positioning plates, the positioning plates are provided with positioning holes, the positioning blocks are sequentially arranged on the periphery of the connecting plate and are fixed through a support, one positioning block is driven by the driving device, the ejector rod is driven by the driving device and can be inserted into the positioning holes, the positioning blocks are matched with the limiting grooves, when the positioning blocks are positioned at a motor installation station and a machine head installation station, ba; when the connecting plate is positioned at the motor installation station and the machine head installation station, the connecting plate is fixed by a positioning block fixed through a support and a positioning block driven by a driving device through opposite positions and matching with a limiting groove, and the ejector rod is inserted into the positioning hole through the driving device.
Further, the bottom plate is provided with symmetrical balance supports between the displacement slide rails, a plurality of guide rods are arranged between the balance supports, a stop block is arranged between the guide rods, a spring is arranged on the guide rod between the balance support and the stop block, and the stop block is fixedly connected with the connecting plate.
Further, the adjusting mechanism is a six-axis platform.
Further, the machine head installation tool and the motor installation tool are respectively fixed on the working installation plate, the working installation plate is provided with an installation hole and a bearing, and a driving shaft of the driving device is fixedly connected with the bottom plate.
Further, a dovetail groove is fixedly arranged on the upper end face of the connecting plate of the motor fixing tool, and a motor installation front plate and a motor installation rear plate are arranged on the dovetail groove.
Further, a fixed baffle is fixedly mounted on the upper end face of the connecting plate of the machine head fixing tool.
Further, the driving device is a driving motor; and/or a cylinder; and/or the telescopic rod of the cylinder drives the linear slide rail.
The utility model has the advantages that: the utility model discloses an automatic debugging equipment of axiality can guarantee that the precision of aircraft nose and motor axiality is high, reduces loaded down with trivial details operating procedure, alleviates workman's intensity of labour, can take notes operation process and measured data, improves the output in the unit interval.
Drawings
Fig. 1 is a schematic structural diagram of an automatic coaxiality debugging device of the present invention;
fig. 2 is an exploded schematic view of an automatic coaxiality debugging apparatus according to the present invention;
fig. 3 is a schematic structural view of a head fixing tool of the automatic coaxiality debugging device of the present invention;
fig. 4 is an exploded schematic view of a head fixing tool of the automatic coaxiality debugging device of the present invention;
fig. 5 is a schematic view of a state of a head fixing tool of the automatic coaxiality debugging apparatus of the present invention;
fig. 6 is a schematic view of a second state of the head fixing tool of the automatic coaxiality debugging device of the present invention;
fig. 7 is a schematic structural view of a motor fixing tool of the automatic coaxiality debugging device of the present invention;
fig. 8 is an exploded view of a motor fixing tool of the automatic coaxiality debugging device of the present invention;
fig. 9 is a schematic view of a state of a motor fixing tool of the automatic coaxiality debugging device of the present invention;
fig. 10 is a schematic view of a state two of the motor fixing tool of the automatic coaxiality debugging device of the present invention;
1. fixing a tool for the motor; 2. the machine head fixes the tool; 3. a frame; 4. an adjustment mechanism; 5. a displacement mechanism; 6. a linear motion assembly; 7. mounting a plate; 8. a laser sensor; 9. a motor; 10. a machine head; 11. a flange; 12. a base plate; 13. a displacement slide rail; 14. a connecting plate; 15. a bayonet; 16. a clamping block; 17. a limiting block; 18. positioning a plate; 19. a support; 20. positioning blocks; 21. a top rod; 22. a balance support; 23. a stopper; 24. a spring; 25. a bearing; 26. a dovetail groove; 27. the motor is provided with a front plate; 28. the motor is provided with a rear plate; 29. fixing a baffle plate; 30. a drive device; 31. and (7) working mounting plates.
Detailed Description
The following detailed description of the preferred embodiments of the present invention will be provided to enable those skilled in the art to more easily understand the advantages and features of the present invention, and to make clear and definite definitions of the protection scope of the present invention.
Referring to fig. 1 to 10, an embodiment of the present invention includes: the utility model provides an automatic debugging equipment of axiality, includes through drive arrangement activity in the fixed frock 1 of motor and the fixed frock 2 of aircraft nose and adjusting device of installation station and butt joint station, the fixed frock 1 fixed mounting of motor is in frame 3, adjusting device includes guiding mechanism 4 and displacement mechanism 5, displacement mechanism is including fixing the linear motion subassembly 6 in the symmetry of frame 1, be fixed with mounting panel 7 on the slider of linear motion subassembly 6, install guiding mechanism 4 on the mounting panel 7, the fixed frock 2 of aircraft nose is installed to guiding mechanism 4. When the motor fixing tool 1 and the machine head fixing tool 2 are simultaneously positioned at the butt joint station, the motor 9 and the machine head 10 are adjusted to be coaxial through the laser sensor 8 and the adjusting device and then are in butt joint through the flange 11. The motor fixing tool 1 and the machine head fixing tool 2 are identical in structure.
The motor fixing tool 1 and the machine head fixing tool 2 comprise bottom plates 12 driven by a driving device, displacement slide rails 13 are symmetrically arranged on the bottom plates 12, connecting plates 14 are fixedly arranged on sliders of the displacement slide rails 13, each of the bottom plates 12 and the connecting plates 14 comprises three straight sides and an arc-shaped side, bayonets 15 are arranged on the arc-shaped sides of the bottom plates 12 and the straight sides opposite to the arc-shaped sides, and the bayonets 15 when the bottom plates 12 are positioned at a motor mounting station and a machine head mounting station are fixed through clamping blocks 16 driven by the driving device; the positioning device comprises a connecting plate 14, positioning blocks 17, positioning blocks 20, an ejector rod 21, a positioning block 20 and a clamping block 16, wherein the two straight edges of the connecting plate 14, which are connected with the arc-shaped edges, are fixedly provided with limiting grooves, the straight edges of the connecting plate 14, which are opposite to the arc-shaped edges, are fixedly provided with the positioning plates 18, the positioning plates 18 are provided with positioning holes, the positioning device further comprises two positioning blocks 20, which are sequentially arranged on the periphery of the connecting plate 14 and are fixed through a support 19, the positioning blocks 20 are driven by a driving device, the ejector rod 21 is driven by the driving device and can be inserted into the positioning holes, the positioning blocks 20 are matched with the limiting grooves, when the positioning blocks are positioned at a motor mounting station and; when the connecting plate 14 is positioned at the motor installation station and the machine head installation station, the connecting plate is fixed by a positioning block 20 fixed through a support 19 and a positioning block 20 driven by a driving device which are opposite and matched with the limiting groove, and the ejector rod 21 is inserted into the positioning hole through the driving device.
Further, balance supports 22 are symmetrically arranged on the bottom plate 12 between the displacement slide rails 13, a plurality of guide rods are arranged between the balance supports 22, a stop 23 is arranged between the guide rods, a spring 24 is arranged on the guide rod between the balance support 22 and the stop 23, and the stop 23 is fixedly connected with the connecting plate 14.
Further, the machine head installation tool and the motor installation tool are respectively fixed on the work installation plate 31, the work installation plate 31 is provided with an installation hole and a bearing 25, and a driving shaft of the driving device is fixedly connected with the bottom plate 12.
Further, a dovetail groove 26 is fixedly installed on the upper end face of the connecting plate 14 of the motor fixing tool, and a motor installation front plate 27 and a motor installation rear plate 28 are installed on the dovetail groove 26.
Further, a fixed baffle 29 is fixedly mounted on the upper end face of the connecting plate 14 of the machine head fixing tool.
Further, the driving device 30 is a driving motor; and/or a cylinder; and/or the telescopic rod of the cylinder drives the linear slide rail. The adjusting mechanism 4 is a six-axis platform.
Further, the laser sensor 8 is a dual beam laser centering instrument.
The utility model relates to a working process of axiality automatic debugging equipment: the six-axis platform is adjusted to a specified position through a linear motion assembly, the machine head is placed on a machine head fixing tool, the position is placed on a mounting station position for positioning, a machine head flange is mounted, the motor is placed on a motor fixing tool, the position is placed on a mounting station position for positioning, the motor flange is mounted, after respective flanges are mounted, the machine head fixing tool and the motor fixing tool are placed on a butt joint station for positioning, a double-beam laser centering instrument fixing tool is respectively connected to the machine head shaft and the motor shaft, the laser centering instrument is mounted on the tool, and the six-axis platform is adjusted through software according to data fed back by the double-beam laser centering instrument, so that the coaxiality of the motor shaft and the machine head shaft reaches a preset range. And taking the laser centering instrument and the tool, adjusting the linear motion assembly to move the motor to the splicing position, and connecting the motor flange and the machine head flange through the bolt.
The dual beam operation of the dual beam laser centering instrument is as follows: the measurement technique allows for simultaneous measurement of displacement and angle with only one PSD;
1. opening a light beam 1, irradiating the light beam to a PSD, and measuring the central displacement;
2. the light beam 1 is closed, and the background light is calibrated;
3. the light beam 2 is opened, reflected by a prism, passes through a lens, reflected by a second prism and enters the PSD, and the angle is measured;
4. beam 2 is off and the second backlight is modified.
The utility model discloses an automatic debugging equipment of axiality can guarantee that the precision of aircraft nose and motor axiality is high, reduces loaded down with trivial details operating procedure, alleviates workman's intensity of labour, can take notes operation process and measured data, improves the output in the unit interval.
The above only is the embodiment of the present invention, not limiting the patent scope of the present invention, all the equivalent structures or equivalent processes that are used in the specification and the attached drawings or directly or indirectly applied to other related technical fields are included in the patent protection scope of the present invention.
Claims (10)
1. The utility model provides an automatic debugging equipment of axiality which characterized in that includes the fixed frock of motor and the fixed frock of aircraft nose that move about in installation station and butt joint station through drive arrangement, the fixed frock fixed mounting of motor is in the frame, the fixed frock of aircraft nose passes through adjusting device and frame fixed, the fixed frock of motor and aircraft nose passes through the flange butt joint after adjusting motor and aircraft nose for the axiality through laser sensor and adjusting device when being located the butt joint station simultaneously.
2. The automatic coaxiality debugging apparatus according to claim 1, wherein: adjusting device includes guiding mechanism and displacement mechanism, displacement mechanism is including fixing the linear motion subassembly in the symmetry of frame, be fixed with the mounting panel on the slider of linear motion subassembly, install guiding mechanism on the mounting panel, the last fixed frock of aircraft nose of installing of guiding mechanism.
3. The automatic coaxiality debugging apparatus according to claim 1, wherein: the motor fixing tool and the machine head fixing tool are the same in structure.
4. The automatic coaxiality debugging apparatus according to claim 1, wherein: the motor fixing tool and the machine head fixing tool comprise bottom plates driven by a driving device, displacement slide rails are symmetrically arranged on the bottom plates, connecting plates are fixedly arranged on sliders of the displacement slide rails, the bottom plates and the connecting plates respectively comprise three straight edges and an arc-shaped edge, bayonets are arranged on the arc-shaped edge of the bottom plate and the straight edge opposite to the arc-shaped edge, and the bayonets when the bottom plates are positioned at a motor mounting station and a machine head mounting station are fixed through clamping blocks driven by the driving device; the positioning device comprises a connecting plate, positioning blocks, a driving device and an ejector rod, wherein the two straight edges of the connecting plate, which are connected with an arc edge, are fixedly provided with limiting blocks, the limiting blocks are provided with limiting grooves, the straight edges of the connecting plate, which are opposite to the arc edge, are fixedly provided with positioning plates, the positioning plates are provided with positioning holes, the positioning blocks are sequentially arranged on the periphery of the connecting plate and are fixed through a support, one positioning block is driven by the driving device, the ejector rod is driven by the driving device and can be inserted into the positioning holes, the positioning blocks are matched with the limiting grooves, when the positioning blocks are positioned at a motor installation station and a machine head installation station, ba; when the connecting plate is positioned at the motor installation station and the machine head installation station, the connecting plate is fixed by a positioning block fixed through a support and a positioning block driven by a driving device through opposite positions and matching with a limiting groove, and the ejector rod is inserted into the positioning hole through the driving device.
5. The automatic coaxiality debugging apparatus according to claim 1, wherein: the bottom plate is provided with symmetrical balance supports between the displacement slide rails, a plurality of guide rods are arranged between the balance supports, a stop block is arranged between the guide rods, springs are arranged on the guide rods between the balance supports and the stop block, and the stop block is fixedly connected with the connecting plate.
6. The automatic coaxiality debugging apparatus according to claim 1, wherein: the adjusting mechanism is a six-axis platform.
7. The automatic coaxiality debugging apparatus according to claim 1, wherein: the machine head installation tool and the motor installation tool are respectively fixed on the working installation plate, the working installation plate is provided with an installation hole and a bearing, and a driving shaft of the driving device is fixedly connected with the bottom plate.
8. The automatic coaxiality debugging apparatus according to claim 1, wherein: the motor fixing tool is characterized in that a dovetail groove is fixedly arranged on the upper end face of a connecting plate of the motor fixing tool, and a motor installation front plate and a motor installation rear plate are arranged on the dovetail groove.
9. The automatic coaxiality debugging apparatus according to claim 1, wherein: and a fixed baffle is fixedly arranged on the upper end face of the connecting plate of the machine head fixing tool.
10. The automatic coaxiality debugging apparatus according to claim 1, wherein: the driving device is a driving motor; and/or a cylinder; and/or the telescopic rod of the cylinder drives the linear slide rail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922386401.6U CN211262143U (en) | 2019-12-26 | 2019-12-26 | Automatic coaxiality debugging equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922386401.6U CN211262143U (en) | 2019-12-26 | 2019-12-26 | Automatic coaxiality debugging equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211262143U true CN211262143U (en) | 2020-08-14 |
Family
ID=71990862
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922386401.6U Active CN211262143U (en) | 2019-12-26 | 2019-12-26 | Automatic coaxiality debugging equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211262143U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114485487A (en) * | 2022-01-10 | 2022-05-13 | 圣邦集团有限公司 | Automatic laser detection device and detection method for coaxiality of winch |
-
2019
- 2019-12-26 CN CN201922386401.6U patent/CN211262143U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114485487A (en) * | 2022-01-10 | 2022-05-13 | 圣邦集团有限公司 | Automatic laser detection device and detection method for coaxiality of winch |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102901450B (en) | Measuring device and shaft body detection equipment | |
| CN103128485B (en) | Four-head numerical control corner assembling production line | |
| CN211262143U (en) | Automatic coaxiality debugging equipment | |
| US9989583B2 (en) | Cross-bar unit for a test apparatus for circuit boards, and test apparatus containing the former | |
| CN111076683A (en) | Automatic coaxiality debugging equipment | |
| CN212609085U (en) | Main end beam assembling device of single-beam crane | |
| CN103331521B (en) | Laser multichannel processing film engraving equipment and processing method of solar film panel | |
| CN113458627A (en) | Light path dimming method of laser cutting equipment | |
| CN111458810B (en) | Optical fiber clamping and coupling positioning device for COC packaging | |
| CN211236338U (en) | Coupling device of PWDM wavelength division multiplexer | |
| CN218723879U (en) | Municipal administration bridge expansion joint detection device | |
| CN212779107U (en) | Size detection device of fuel cell stack | |
| CN215064386U (en) | Clutch flatness detection device | |
| CN114199131A (en) | Cylindrical part measuring device and measuring method capable of achieving accurate position adjustment | |
| CN110411382B (en) | Device and method for detecting flatness of front shell of optical full-detection mobile phone | |
| CN215064383U (en) | Servo motor main shaft maintenance test platform | |
| CN218847636U (en) | Cylinder cover positioning platform and air flue test bed | |
| CN216746429U (en) | Chromatic aberration detection device | |
| CN217425045U (en) | Special regulation frock of industrial camera is used in fatigue test | |
| CN211978664U (en) | Airplane spare and accessory part identification and detection platform | |
| CN117870579A (en) | Coaxiality detection device and main cylinder replacement system of radial forging machine | |
| CN212169807U (en) | Positioning device for numerical control flat head automatic length control machine | |
| CN2754078Y (en) | Operating table for chrominance, brightness, colour temperature and contrast ratio measurement | |
| CN211717402U (en) | Mobile measuring device for detecting straightness of working edge of knife edge-shaped ruler | |
| CN216859523U (en) | Assembly tool for top wing door of car body |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |