CN220330776U - State shaft polishing assembly device for aero-engine detection - Google Patents
State shaft polishing assembly device for aero-engine detection Download PDFInfo
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- CN220330776U CN220330776U CN202321948083.8U CN202321948083U CN220330776U CN 220330776 U CN220330776 U CN 220330776U CN 202321948083 U CN202321948083 U CN 202321948083U CN 220330776 U CN220330776 U CN 220330776U
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- polishing
- fixedly connected
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- aeroengine
- plate
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- 238000005498 polishing Methods 0.000 title claims abstract description 59
- 238000001514 detection method Methods 0.000 title abstract description 17
- 239000000428 dust Substances 0.000 claims abstract description 26
- 230000007246 mechanism Effects 0.000 claims abstract description 13
- 238000003908 quality control method Methods 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 5
- 238000010521 absorption reaction Methods 0.000 claims description 4
- 241000883990 Flabellum Species 0.000 claims description 2
- 230000017525 heat dissipation Effects 0.000 claims description 2
- 230000008859 change Effects 0.000 abstract description 11
- 238000000034 method Methods 0.000 abstract description 9
- 230000008569 process Effects 0.000 abstract description 7
- 230000003749 cleanliness Effects 0.000 abstract description 3
- 238000007599 discharging Methods 0.000 abstract description 3
- 230000000903 blocking effect Effects 0.000 abstract description 2
- 238000007517 polishing process Methods 0.000 description 7
- 230000009471 action Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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- Constituent Portions Of Griding Lathes, Driving, Sensing And Control (AREA)
Abstract
The utility model provides a state shaft polishing assembly device for aero-engine detection, which belongs to the technical field of aero-engine detection and comprises the following components: the utility model provides a platform, the fixedly connected with electronic box of platform, the internally mounted of electronic box has the motor, through the cooperation use of dust catcher and fan blade sways, make the staff can absorb the piece through the dust catcher, the piece that has avoided producing in polishing the in-process appears blocking easily when discharging from the discharge gate, the problem of polishing the process can be influenced for a long time, thereby the cleanliness of this aeroengine detects with the status axle assembly device that polishes, through polishing mechanism's use, make the device change the size through the status axle, the casing size that has avoided current equipment to polish is fixed, can't change according to the change of status axle, the status axle size that leads to the device to polish is single problem relatively, thereby the variety of this aeroengine detects with status axle assembly device that polishes has been promoted.
Description
Technical Field
The utility model belongs to the technical field of aero-engine detection, and particularly relates to a state shaft polishing assembly device for aero-engine detection.
Background
The aeroengine is a highly complex and precise thermodynamic machine, is used as the heart of an airplane, is not only the power of the airplane in flight, but also an important driving force for promoting the development of aviation industry, each important transformation in human aviation history is closely and indispensible with the technical progress of the aeroengine, the heart aeroengine used as the airplane needs to be detected and checked more carefully before being used so as to ensure that the aeroengine can run safely, the state shaft is an indispensable same part in the detection process of the aeroengine, and the state shaft needs to be polished and polished before being used so as to ensure that the smoothness of the surface of the state shaft cannot influence the final detection result.
The utility model with the retrieval authorized bulletin number of CN214323012U relates to the technical field of aeroengine detection, and discloses a state shaft polishing assembly device for aeroengine detection, which comprises a base, the top fixedly connected with electric putter of base, the top fixedly connected with push pedal of electric putter, the top fixedly connected with fixture of push pedal, the top fixedly connected with protection box of base, the inner wall fixedly connected with fixed column of protection box. This aeroengine detects with state axle assembly quality control device that polishes has reached aeroengine and has detected with state axle assembly quality control device centre gripping steady purpose, has solved the unstable problem of state axle assembly quality control device centre gripping for general aeroengine detects with state axle, makes people can fix the state axle body through simple structure and polish, need not worry polishing in-process polishing device power too big can cause damage and harm to staff and state axle body, and simple structure easy to operate has satisfied people's demand.
The technical scheme is characterized in that the clamping device is structurally matched with the clamping device for the state shaft for detecting the aeroengine, the clamping device is stable in clamping, the problem that the clamping device for detecting the state shaft for detecting the aeroengine is unstable is solved, people can fix and polish the state shaft body through a simple structure, damage and harm to workers and the state shaft body caused by overlarge power of the polishing device in the polishing process are avoided, the structure is simple and easy to operate, the requirements of people are met, the situation that the chips generated in the polishing process are easy to block when discharged from a discharge port is achieved, the polishing process can be influenced for a long time, the polishing shell is fixed in size and cannot be changed according to the change of the state shaft, and the polishing state shaft size of the device is single, so that the device has limitation.
Disclosure of Invention
The utility model aims to provide a state shaft polishing assembly device for aeroengine detection, which aims to solve the problems that in the prior art, common chips generated in the polishing process are easy to block when discharged from a discharge hole, the polishing process can be influenced for a long time, the size of a shell for polishing is fixed at present, the shell cannot be changed according to the change of a state shaft, and the dimension of the state shaft which can be polished by the device is single, so that the device has limitation.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
the utility model provides an aeroengine detects with state axle assembly quality control device that polishes, belongs to aeroengine and detects technical field, includes: the electric motor is arranged at the top of the installation shell, and swing blades are movably connected with the surface of the electric motor.
As a preferable scheme of the utility model, a control panel is arranged on the surface of the fence, and the control panel is electrically connected with the polishing mechanism, the dust collector and the motor.
As a preferable scheme of the utility model, the polishing mechanism comprises a first electric telescopic rod, a mounting plate, a second electric telescopic rod, a polishing plate and polishing paper, wherein the first electric telescopic rod is mounted on the surface of the platform, the mounting plate is fixedly connected to the top of the platform, the second electric telescopic rod is mounted on the surface of the mounting plate, the polishing plate is fixedly connected to one end of the second electric telescopic rod, and the polishing paper is arranged on the surface of the polishing plate.
As a preferable scheme of the utility model, the clamping mechanism comprises a connecting plate, side plates, fixing bolts, a guide rod and a clamping plate, wherein the connecting plate is fixedly connected to the output end of the motor, the side plates are fixedly connected to two sides of the surface of the connecting plate, the fixing bolts are movably connected to the center of the side plates, the clamping plate is fixedly connected to one end of the fixing bolts, and the guide rod is movably connected to the surface of the clamping plate.
As a preferable scheme of the utility model, the guide rod penetrates through two ends of the clamping plate, and the two ends of the guide rod are fixedly connected with the side plates.
As a preferable scheme of the utility model, one side of the clamping plate is semicircular, and the surface of the clamping plate is provided with an anti-slip gasket.
As a preferable scheme of the utility model, a plurality of heat dissipation holes are uniformly formed in the surface of the electric box, and the supporting legs are fixedly connected to the four corners of the bottom of the platform.
Compared with the prior art, the utility model has the beneficial effects that:
this scheme is through the cooperation use of dust catcher and fan blade sways, make the staff absorb the piece through the dust catcher, the piece that has avoided producing in the process of polishing appears blocking easily when discharging from the discharge gate, the problem of polishing the process can be influenced for a long time, thereby promoted the cleanliness of this aeroengine detection with the state axle assembly device that polishes, through grinding machanism's use, make the device change the size through the state axle, the casing size that has avoided current equipment to polish usefulness is fixed, can't change according to the change of state axle, the state axle size that leads to the device to polish is single problem relatively, thereby the variety of this aeroengine detection with the state axle assembly device that polishes has been promoted.
Drawings
The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model.
In the drawings:
FIG. 1 is a first schematic view of the overall structure of the present utility model;
FIG. 2 is a second schematic diagram of the overall structure of the present utility model;
FIG. 3 is a schematic view of a structural clamping mechanism according to the present utility model;
FIG. 4 is a schematic view of a grinding mechanism in accordance with the present utility model;
figure 5 is a schematic view of a dust extraction assembly in accordance with the present utility model.
In the figure: 1. a platform; 2. support legs; 3. a fence; 4. a control panel; 5. a polishing mechanism; 6. a clamping mechanism; 7. a dust collector; 8. a dust collection pipe; 9. an electric box; 10. a motor; 11. an electric motor; 12. a mounting shell; 13. a wobble blade; 501. a first electric telescopic rod; 502. a mounting plate; 503. a second electric telescopic rod; 504. polishing the plate; 505. polishing paper; 601. a connecting plate; 602. a side plate; 603. a fixing bolt; 604. a guide rod; 605. and a clamping plate.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Examples
Referring to fig. 1-5, the technical scheme provided in this embodiment is as follows:
the utility model provides an aeroengine detects with state axle assembly device that polishes, aims at solving the common piece that produces in the process of polishing among the prior art and appears the circumstances that blocks up easily when discharging from the discharge gate, probably influences the process of polishing for a long time, and the casing size that polishes at present is fixed, can't change according to the change of state axle, leads to the device state axle size that polishes more singleness to make the device have the problem of limitation.
An aeroengine detects with state axle assembly quality control device that polishes includes: platform 1, the fixedly connected with electric box 9 of platform 1, the internally mounted of electric box 9 has motor 10, motor 10's output shaft runs through platform 1, and motor 10's output shaft fixedly connected with fixture 6, the surface mounting of platform 1 has grinding machanism 5, the fixed surface of platform 1 has rail 3, dust catcher 7 is installed to one side of rail 3, the surface of dust catcher 7 is provided with dust absorption pipe 8, the one end swing joint of dust absorption pipe 8 has installation shell 12, electric motor 11 is installed at the top of installation shell 12, electric motor 11's surface swing joint has the flabellum 13.
In the specific embodiment of the utility model, through the cooperation of the dust collector 7 and the swing fan blades 13, workers can absorb scraps through the dust collector 7, the problem that scraps generated in the polishing process are easy to block when discharged from a discharge hole and the polishing process can be influenced for a long time is avoided, so that the cleanliness of the state shaft polishing assembly device for detecting the aeroengine is improved, the size of the device can be changed through the state shaft through the use of the polishing mechanism 5, the problem that the size of a shell for polishing of the current equipment is fixed and cannot be changed according to the change of the state shaft, and the problem that the size of the state shaft which can be polished by the device is single is solved, and the diversity of the state shaft polishing assembly device for detecting the aeroengine is improved.
Specifically, the surface mounting of rail 3 has control panel 4, and control panel 4 and grinding machanism 5, dust catcher 7 and motor 10 all electric connection.
In the specific embodiment of the utility model, the control panel 4 is used to enable a user to control equipment through the control panel 4, so that the operation is simple, and the easiness of the state shaft polishing assembly device for the aero-engine detection is improved.
Specifically, the polishing mechanism 5 includes a first electric telescopic rod 501, a mounting plate 502, a second electric telescopic rod 503, a polishing plate 504 and polishing paper 505, the first electric telescopic rod 501 is mounted on the surface of the platform 1, the mounting plate 502 is fixedly connected to the top of the platform 1, the second electric telescopic rod 503 is mounted on the surface of the mounting plate 502, the polishing plate 504 is fixedly connected to one end of the second electric telescopic rod 503, and the polishing paper 505 is disposed on the surface of the polishing plate 504.
In the specific embodiment of the utility model, through the cooperation of the first electric telescopic rod 501 and the second electric telescopic rod 503, a user can adjust the distance between the polishing plates 504 according to the size of the state shaft, and the height of the polishing paper 505 can be adjusted through the first electric telescopic rod 501, so that the device polishes the state shaft more comprehensively, and the adjustability of the state shaft polishing assembly device for the aeroengine detection is improved.
Specifically, the clamping mechanism 6 includes a connecting plate 601, a side plate 602, a fixing bolt 603, a guide rod 604 and a clamping plate 605, the connecting plate 601 is fixedly connected to the output end of the motor 10, the side plate 602 is fixedly connected to two sides of the surface of the connecting plate 601, the fixing bolt 603 is movably connected to the center of the side plate 602, the clamping plate 605 is fixedly connected to one end of the fixing bolt 603, and the guide rod 604 is movably connected to the surface of the clamping plate 605.
In the specific embodiment of the utility model, through the cooperation of the fixing bolt 603 and the clamping plate 605, the device can clamp and fix the status shaft, so that the status shaft cannot deviate when rotating under the action of the motor 10, and the stability of the status shaft polishing and assembling device for detecting the aeroengine is improved.
Specifically, the guide rods 604 penetrate through two ends of the clamping plate 605, and two ends of the guide rods 604 are fixedly connected with the side plates 602.
In the specific embodiment of the utility model, the clamping plate 605 is not deviated when moving through the use of the guide rod 604, so that the accuracy of the state shaft polishing assembly device for detecting the aero-engine is improved.
Specifically, one side of the clamping plate 605 is semicircular, and an anti-slip gasket is arranged on the surface of the clamping plate 605.
In the specific embodiment of the utility model, the state shaft is more stable when clamped and polished in the clamping plate 605 through the use of the clamping plate 605, and cannot move, so that the stability of the state shaft polishing and assembling device for the aeroengine detection is improved.
Specifically, a plurality of louvres have evenly been seted up on the surface of electronic box 9, and the bottom four corners fixedly connected with supporting leg 2 of platform 1.
In the specific embodiment of the utility model, the motor 10 can be prevented from being damaged due to overheating through the use of the radiating holes on the surface of the electric box 9, and the equipment is more stable in the use process through the use of the supporting legs 2, so that the practicability of the state shaft polishing and assembling device for the aeroengine detection is improved.
Working principle: before the use, the state shaft part to be polished is placed on the surface of the connecting plate 601 and is placed between the clamping plates 605, then the clamping plates 605 are moved to the center position on the surface of the guide rod 604 by screwing the fixing bolts 603 until the state shaft is fixed at the center position of the connecting plate 601, then the motor 10 is started through the control panel 4, the motor 10 drives the connecting plate 601 to start rotating, so that the state shaft and the connecting plate 601 are driven to synchronously rotate, then the second electric telescopic rod 503 is started through the control panel 4 to adjust the polishing paper 505 to be in contact with the surface of the state shaft, so that the state shaft is polished, the polishing plate 504 and the polishing paper 505 on the top of the second electric telescopic rod 503 can be driven to stretch according to the starting of the first electric telescopic rod 501, the polishing position is changed, the polishing effect can be started by avoiding excessive influence of dust and scraps during polishing, the dust collector 7 can be started, the dust collector 7 begins to inwards swing left and right under the action of the electric motor 11 during the dust collection, the dust collection range can be enlarged, and the dust collection effect is better.
Finally, it should be noted that: the foregoing description is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present utility model has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.
Claims (7)
1. The utility model provides an aeroengine detects with state axle assembly quality control device that polishes which characterized in that includes: platform (1), fixedly connected with electric box (9) of platform (1), the internally mounted of electric box (9) has motor (10), the output shaft of motor (10) runs through platform (1), just the output shaft fixedly connected with fixture (6) of motor (10), the surface mounting of platform (1) has grinding machanism (5), the fixed surface of platform (1) is connected with rail (3), dust catcher (7) are installed to one side of rail (3), the surface of dust catcher (7) is provided with dust absorption pipe (8), the one end swing joint of dust absorption pipe (8) has installation shell (12), electric motor (11) are installed at the top of installation shell (12), the surface swing joint of electric motor (11) has sways flabellum (13).
2. The state shaft grinding and assembling device for detecting an aeroengine according to claim 1, wherein: the surface mounting of rail (3) has control panel (4), control panel (4) with grinding machanism (5), dust catcher (7) with motor (10) all electric connection.
3. The state shaft grinding and assembling device for detecting an aeroengine according to claim 1, wherein: the polishing mechanism (5) comprises a first electric telescopic rod (501), a mounting plate (502), a second electric telescopic rod (503), a polishing plate (504) and polishing paper (505), wherein the first electric telescopic rod (501) is mounted on the surface of the platform (1), the mounting plate (502) is fixedly connected to the top of the platform (1), the second electric telescopic rod (503) is mounted on the surface of the mounting plate (502), the polishing plate (504) is fixedly connected to one end of the second electric telescopic rod (503), and the polishing paper (505) is arranged on the surface of the polishing plate (504).
4. The state shaft grinding and assembling device for detecting an aeroengine according to claim 1, wherein: the clamping mechanism (6) comprises a connecting plate (601), side plates (602), fixing bolts (603), guide rods (604) and clamping plates (605), wherein the connecting plate (601) is fixedly connected to the output end of the motor (10), the side plates (602) are fixedly connected to two sides of the surface of the connecting plate (601), the fixing bolts (603) are movably connected to the centers of the side plates (602), the clamping plates (605) are fixedly connected to one ends of the fixing bolts (603), and the guide rods (604) are movably connected to the surface of the clamping plates (605).
5. The state shaft grinding and assembling device for detecting an aeroengine according to claim 4, wherein: the guide rods (604) penetrate through two ends of the clamping plate (605), and two ends of the guide rods (604) are fixedly connected with the side plates (602).
6. The state shaft grinding and assembling device for detecting an aeroengine according to claim 4, wherein: one side of the clamping plate (605) is semicircular, and an anti-slip gasket is arranged on the surface of the clamping plate (605).
7. The state shaft grinding and assembling device for detecting an aeroengine according to claim 1, wherein: a plurality of heat dissipation holes are uniformly formed in the surface of the electric box (9), and supporting legs (2) are fixedly connected to four corners of the bottom of the platform (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321948083.8U CN220330776U (en) | 2023-07-24 | 2023-07-24 | State shaft polishing assembly device for aero-engine detection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321948083.8U CN220330776U (en) | 2023-07-24 | 2023-07-24 | State shaft polishing assembly device for aero-engine detection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220330776U true CN220330776U (en) | 2024-01-12 |
Family
ID=89461452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321948083.8U Active CN220330776U (en) | 2023-07-24 | 2023-07-24 | State shaft polishing assembly device for aero-engine detection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220330776U (en) |
-
2023
- 2023-07-24 CN CN202321948083.8U patent/CN220330776U/en active Active
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