CN205888881U - Aircraft part grinding device - Google Patents
Aircraft part grinding device Download PDFInfo
- Publication number
- CN205888881U CN205888881U CN201620884499.1U CN201620884499U CN205888881U CN 205888881 U CN205888881 U CN 205888881U CN 201620884499 U CN201620884499 U CN 201620884499U CN 205888881 U CN205888881 U CN 205888881U
- Authority
- CN
- China
- Prior art keywords
- clip arm
- feeding roller
- feed roller
- aircraft parts
- aircraft part
- 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.)
- Expired - Fee Related
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Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/10—Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working
Abstract
The utility model discloses an aircraft part grinding device, this grinding device includes the board, board feed roller and corresponding to the actuating mechanism that polishes of feed roller discharge gate, it places in this feed roller to wait the aircraft part of polishing, feed roller's front end is equipped with the automatically clamped mechanism that the formula is inhaled to magnetism, feed roller's end is equipped with the blevile of push who is used for promoting a station of aircraft part antedisplacement, the board is equipped with the fender bits board that album bits were fought and were erect in the discharge gate department corresponding to feed roller. The utility model discloses when using, the aircraft part of placing in feed roller is promoted a station forward by blevile of push for be located feed roller aircraft part foremost and is pushed away to feed roller's discharge gate, then the magnetism automatically clamped mechanism of inhaling the formula to carry out the centre gripping to this aircraft part automatically fixed, the actuating mechanism that polishes delivers to the station of polishing in step, makes the emery wheel and this aircraft part contact on the actuating mechanism of polishing, carries out the automation and polishes.
Description
Technical field
The utility model is related to grinding technology field, particularly to a kind of aircraft parts for aircraft parts of polishing
Sanding apparatus.
Background technology
Sanding apparatus are the instruments that using grinding tool, surface of the work is carried out with grinding, for the higher material of workhardness
With some fragile materials, such as hard steel, hard alloy, special steel, glass and granite etc..Carry out grinding using sanding apparatus
Quite varied, it is machine parts closely one of main method of processing.Aircraft parts as the critical component on aircraft, its
It is necessary to ensure that reliable in quality, the sanding apparatus of existing aircraft parts mostly adopt hand adjustment mode or semi-automatic in production and processing
Mode, the feeding of aircraft parts and the regulation of emery wheel are required for manually adjusting, and need again clamping to fly after having polished
Device part, seriously reduces grinding efficiency.
Utility model content
For solving the above problems, the utility model provides a kind of polishing of the aircraft parts for aircraft parts of polishing
Device, has the characteristics that grinding efficiency is high.
For achieving the above object, the technical scheme that the utility model is taken is:
A kind of aircraft parts sanding apparatus, including board, described board is provided with for disposing aircraft zero to be polished
The feeding roller of part and the polishing executing agency of the discharging opening corresponding to described feeding roller, described polishing executing agency is connected with
Feeder, wherein, the front end of described feeding roller is provided with magnetic-type automated exchanged cutter mechanism, and the end of described feeding roller sets
There is the material-pulling device for promoting aircraft parts one station of reach to be polished, described polishing executing agency includes abrasive wheel chuck
And variable-frequency motor, the output shaft of described variable-frequency motor is connected with described abrasive wheel chuck, described abrasive wheel chuck be fixedly arranged at the front end with sand
Wheel, described automated exchanged cutter mechanism includes upper clip arm and lower clip arm, described upper clip arm and the described lower folder that can separate up and down and fasten
Arm is adapted with the external peripheral surface of described feeding roller after fastening, the front end of described feeding roller be provided with described upper clip arm and
The annular through groove that lower clip arm matches.
Preferably, the fixing end of the fixing end of described upper clip arm and described lower clip arm is all actively set in one vertically sliding
On bar and bi-directional drive screw mandrel, one end of described bi-directional drive screw mandrel is connected with the motor shaft of a stepper motor.
Preferably, described upper clip arm and described lower clip arm are composite structure, towards described polishing execution machine
The side of structure is magnet steel layer, is being rubber layer towards the side of described feeding roller end, described magnet steel layer connects electricity, in energising
When add magnetic, demagnetization during power-off.
Preferably, described board is provided with crumb loading bucket and the gear bits erect in the discharge outlet corresponding to described feeding roller
Plate, described crumb loading bucket and described shred holding up plate are just to setting.
The utility model has the advantages that the utility model passes through to put before and after aircraft parts to be polished
In cylindric feeding roller, and automatically advanced, eliminated manually feeding.Magnetic-type automated exchanged cutter mechanism exists
Aircraft parts foremost proceed to and fasten during the discharging opening of feeding roller, and upper clip arm and lower clip arm are in the drive of bi-directional drive screw mandrel
Dynamic lower fastening, sinks to the magnetic that the annular through groove being opened in feeding roller front end carries out strength to the aircraft parts proceeding to discharging opening
Absorption, clamping stable convenient, the grinding efficiency of aircraft parts can be greatly improved.
Brief description
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation of automated exchanged cutter mechanism described in the utility model；
Fig. 3 is the enlarged diagram of ii part in Fig. 1.
In figure: 1- board, 2- feeding roller, 3- abrasive wheel chuck, 4- variable-frequency motor, 5- automated exchanged cutter mechanism, 6- shred holding up plate,
On 7- crumb loading bucket, 8- guide rod cylinder, 9- pusher disk, 10- emery wheel, 21- annular through groove, 41- output shaft, 42- feeder, 51-
Jig arm, 52- lower clip arm, 53- upright sliding bar, 54- bi-directional drive screw mandrel, 55- stepper motor, 56- limited block, 521- magnet steel layer,
522- rubber layer.
Specific embodiment
In order that the purpose of this utility model and advantage become more apparent, below in conjunction with example, the utility model is carried out
Further describe.It should be appreciated that instantiation described herein, only in order to explain the utility model, is not used to limit
Determine the utility model.
As shown in Figure 1 to Figure 3, a kind of aircraft parts sanding apparatus, including board 1, this board 1 is provided with for disposing
The feeding roller 2 of aircraft parts to be polished and the polishing executing agency of the discharging opening corresponding to feeding roller 2.This polishing executes
Mechanism is connected with feeder 42.After aircraft parts are in place, executing agency of polishing is delivered to polishing station by feeder 42
Aircraft parts in place are polished.Wherein, as a kind of improvement of the present utility model, the front end of feeding roller 2 is provided with
Magnetic-type automated exchanged cutter mechanism 5.The end of feeding roller 2 is provided with for promoting aircraft parts one station of reach to be polished
Material-pulling device.Material-pulling device is a guide rod cylinder 8, and the guide rod end of this guide rod cylinder 8 is provided with pusher disk 9.In guide rod cylinder 8
Guide rod when stretching out, pusher disk 9 enters from the end of feeding roller 2, carries out to being placed in aircraft parts to be polished therein
Promote.Polishing executing agency includes abrasive wheel chuck 3 and variable-frequency motor 4, and variable-frequency motor 4 is slidably disposed within machine by feeder 42
On the guide rail of platform 1, this feeder 42 is feeding trolley.The output shaft 41 of variable-frequency motor 4 is connected with abrasive wheel chuck 3.Emery wheel presss from both sides
3 be fixedly arranged at the front end with emery wheel 10.According to different operating mode needs, the rotational frequency of adjustable variable-frequency motor 4 is so that emery wheel presss from both sides
3 with different rotational speed.Automated exchanged cutter mechanism 5 includes structure identical upper clip arm 51 and lower clip arm 52, upper clip arm 51 He
Lower clip arm 52 is adapted with the external peripheral surface of feeding roller 2 after fastening.The front end of feeding roller 2 be provided with upper clip arm 51 and
The annular through groove 21 that lower clip arm 52 matches, the width of annular through groove 21 is slightly larger than the width of upper clip arm 51.When upper clip arm 51 He
After lower clip arm 52 fastens, it fastens one annular retaining ring of formation and sinks in annular through groove 21, and follow-up aircraft parts are entered
Row stops.For neatly adjusting separation and fastening, the fixing end of upper clip arm 51 and the lower clip arm 52 of upper clip arm 51 and lower clip arm 52
Fixing end be all actively set on a upright sliding bar 53 and bi-directional drive screw mandrel 54.One end of this bi-directional drive screw mandrel 54
It is connected with the motor shaft of a stepper motor 55, the end of the other end is provided with limited block 56.When the motor shaft of stepper motor 55 is suitable
When hour hands rotate, bi-directional drive screw mandrel 54 rotates and upper clip arm 51 is moved downward along upright sliding bar 53, and lower clip arm 52 is upwards
Move along upright sliding bar 53, make upper clip arm 51 and lower clip arm 52 be buckled into annular retaining ring.When the motor shaft of stepper motor 55 is inverse
When hour hands rotate, bi-directional drive screw mandrel 54 rotates and upper clip arm 51 is moved up along upright sliding bar 53, and lower clip arm 52 is downward
Move along upright sliding bar 53, so that upper clip arm 51 and lower clip arm 52 is separated.
Further, in preferred embodiment of the present utility model, for more stable and convenient ground clamping aircraft parts, on
Jig arm 51 and lower clip arm 52 are composite structure, and it is being magnet steel layer 521 towards the side of polishing executing agency.In court
It is rubber layer 522 to the side of the end of feeding roller 2, magnet steel layer 521 connects electricity, it adds magnetic in energising, demagnetization during power-off.When
In feeding roller 2 forefront when aircraft parts of polishing proceed to the discharging opening of feeding roller 2, upper clip arm 51 and lower clip arm 52
Fasten and form annular retaining ring.Now, upper clip arm 51 and lower clip arm 52 energising plus magnetic, because aircraft parts are connect with magnet steel layer 521
Touch, therefore under strong magnetic-adsorption.Aircraft parts are firmly fixed, and then abrasive wheel chuck 3 is sent into and enters polishing station, to flight
Device part is polished.For avoiding the scrap iron from splashing producing of polishing, board 1 is provided with the discharge outlet corresponding to feeding roller 2
, just to setting, the iron filings that polishing produces fly out in shred holding up plate 6 for crumb loading bucket 7 and the shred holding up plate 6 erect, this crumb loading bucket 7 and shred holding up plate 6
Stop under enter crumb loading bucket 7.
The above is only preferred embodiment of the present utility model.It should be pointed out that the common skill for the art
For art personnel, on the premise of without departing from the utility model principle, some improvements and modifications can also be made, these improve and
Retouching also should be regarded as protection domain of the present utility model.
Claims (4)
1. a kind of aircraft parts sanding apparatus, including board, described board is provided with for disposing aircraft parts to be polished
Feeding roller and corresponding to described feeding roller discharging opening polishing executing agency；Described polishing executing agency is connected with and send
Enter device it is characterised in that the front end of described feeding roller is provided with magnetic-type automated exchanged cutter mechanism, the end of described feeding roller
End is provided with the material-pulling device for promoting aircraft parts one station of reach to be polished；Described polishing executing agency includes emery wheel
Chuck and variable-frequency motor, the output shaft of described variable-frequency motor is connected with described abrasive wheel chuck, and the front end of described abrasive wheel chuck is fixed
There is emery wheel；Described automated exchanged cutter mechanism includes upper clip arm and the lower clip arm that can separate up and down and fasten, described upper clip arm and described
Lower clip arm is adapted with the external peripheral surface of described feeding roller after fastening, and the front end of described feeding roller is provided with and described upper folder
The annular through groove that arm and lower clip arm match.
2. a kind of aircraft parts sanding apparatus according to claim 1 are it is characterised in that the fixing end of described upper clip arm
All actively it is set on a upright sliding bar and bi-directional drive screw mandrel with the fixing end of described lower clip arm, described bi-directional drive silk
One end of bar is connected with the motor shaft of a stepper motor.
3. a kind of aircraft parts sanding apparatus according to claim 1 it is characterised in that described upper clip arm and described under
Jig arm is composite structure, is being magnet steel layer towards the side of described polishing executing agency, towards described feeding rolling
The side of cylinder end is rubber layer, and described magnet steel layer connects electricity, adds magnetic in energising, demagnetization during power-off.
4. a kind of aircraft parts sanding apparatus according to claim 1 are it is characterised in that described board is corresponding to institute
The discharge outlet stating feeding roller is provided with crumb loading bucket and the shred holding up plate erect, and described crumb loading bucket and described shred holding up plate are just to setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620884499.1U CN205888881U (en) | 2016-08-11 | 2016-08-11 | Aircraft part grinding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620884499.1U CN205888881U (en) | 2016-08-11 | 2016-08-11 | Aircraft part grinding device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205888881U true CN205888881U (en) | 2017-01-18 |
Family
ID=57779017
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620884499.1U Expired - Fee Related CN205888881U (en) | 2016-08-11 | 2016-08-11 | Aircraft part grinding device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205888881U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107971932A (en) * | 2017-12-07 | 2018-05-01 | 郭斌 | The collection apparatus of iron filings after a kind of accessory polishing for vehicle complete vehicle manufacture |
| CN111730452A (en) * | 2020-06-22 | 2020-10-02 | 赣县洪顺工艺厂 | Resin base holds in palm polishing device for resin toy processing |
-
2016
- 2016-08-11 CN CN201620884499.1U patent/CN205888881U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107971932A (en) * | 2017-12-07 | 2018-05-01 | 郭斌 | The collection apparatus of iron filings after a kind of accessory polishing for vehicle complete vehicle manufacture |
| CN111730452A (en) * | 2020-06-22 | 2020-10-02 | 赣县洪顺工艺厂 | Resin base holds in palm polishing device for resin toy processing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170118 Termination date: 20170811 |