CN208098805U - A kind of self-action laser cleaner for airplane component cleaning - Google Patents
A kind of self-action laser cleaner for airplane component cleaning Download PDFInfo
- Publication number
- CN208098805U CN208098805U CN201820284337.3U CN201820284337U CN208098805U CN 208098805 U CN208098805 U CN 208098805U CN 201820284337 U CN201820284337 U CN 201820284337U CN 208098805 U CN208098805 U CN 208098805U
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- laser
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- support plate
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Abstract
The utility model provides a kind of self-action laser cleaner for airplane component cleaning, base including opening, support plate is connected on base, rectangular opening is offered in support plate, support plate is equipped with two locating pieces being located on the outside of rectangular opening, rotation is equipped with two the first parallel screw rods between two locating pieces, is threadedly engaged the sliding seat being slidably matched with support plate on two first screw rods；Rotation is equipped with rotating disk on sliding seat, and rotation seat and vertical hydraulic cylinder are connected in rotating disk, and rotation is equipped with the laser cleaning head connecting with laser generator by optical fiber on rotation seat, and the end of laser cleaning head is connect with the piston rod rotation of vertical hydraulic cylinder；Rotating disk, which protrudes into base, is connected with the first driving motor, and the driving mechanism for driving the first driving motor and sliding seat synchronizing moving is equipped in base, is additionally provided with positioning tool in support plate.Position and the swing of laser cleaning head, spot size of the control laser on illuminated irradiation object are automatically controlled, so that regulating time is short, fast response time.
Description
Technical field
The utility model relates to airplane component cleaning equipment technical fields, and in particular to one kind is clear for airplane component
The self-action laser cleaner washed.
Background technique
There is several components, airplane component or aircraft outer surface in aircraft in order to corrosion-resistant characteristic,
The surface or aircraft outer surface of airplane component carry out spray painting processing, thus avoid being corroded, but aircraft is in the flight time
Interval just needs depainting to be safeguarded in 5 years or so, overhaul, thus guarantee the reliability of aircraft, the depainting agent method used now
The health for not only polluting environment, damaging operator, and somewhat expensive, the airplane component after can't guaranteeing depainting can also be just
The case where being often used, airplane component be easy to cause to be scrapped, in order to overcome this cleaning way there are the drawbacks of, using laser
Cleaning device cleans the paint on airplane component, is only just able to satisfy cleaning requirement in the case where expending electric energy,
Have the effect of environmental protection, and the size of airplane component is protected, the airplane component after guaranteeing cleaning still conforms to
Use regulation, moreover it is possible to speed cleaning efficiency.
After the mechanism of laser cleaning is mainly based upon body surface pollutant absorption laser energy, or vaporization volatilization or wink
Between expanded by heating and overcome surface to disengage it from body surface to the adsorption capacity of particle, and then achieve the purpose that cleaning.At present compared with
The most commonly used is laser dry cleaning process, directly adopt the direct radiation decontamination of pulse laser, and the laser cleaning of laser dry cleaning process is used to set
Back-up is hand-held, and the volume of portion of the handle is big, heavy, for a long time using be easy to causeing fatigue.The laser of the prior art is clear
Cleaning device is when in use by manually carrying out movement to laser cleaning head, rotating to change laser on airplane component and generate
Spot size and position, to adjust cleaning area and speed, but caused by the status that manual type is adjusted plus
The shortcomings that long between working hour, inefficiency.
Utility model content
For the deficiency in the presence of the prior art, the utility model provide it is a kind of for airplane component cleaning from
Dynamic formula laser cleaner, the laser cleaner for solving the prior art are beaten in adjusting laser when derusting on airplane component
The spot size of generation and position, be adjusted using manual type cause long processing time, inefficiency the problem of.
To achieve the above object, the utility model uses the following technical solution：One kind is cleaned for airplane component
Self-action laser cleaner, the base including opening, base is to be connected with support plate, base on rectangular parallelepiped structure and base
Laser generator is inside installed, offers rectangular opening in the support plate along its length, support plate is equipped with and is located at
Two locating pieces on the outside of the short side of rectangular opening, rotation is equipped with two the first parallel screw rods between two locating pieces, and two pieces the
The sliding seat being slidably matched with support plate is threadedly engaged on one screw rod；Rotation is equipped with the " T " shape knot in section on the sliding seat
The rotating disk of structure, interval is connected with rotation seat and vertical hydraulic cylinder in rotating disk, and wherein rotation is equipped on rotation seat and laser is sent out
The laser cleaning head that raw device is connected by optical fiber, the end of laser cleaning head is connect with the piston rod rotation of vertical hydraulic cylinder；Institute
The first driving motor is protruded into base and be connected in the lower end for stating rotating disk, is equipped in base and drives the movement of the first driving motor
Driving mechanism, driving mechanism include the mounting plate, sliding stand and erecting bed being successively fixed in base, and wherein erecting bed is equipped with
Second driving motor is equipped with rotatable second screw rod, slides and set on the sliding stand between mounting plate and the second driving motor
There is the movable plate with the cooperation of the second wire rod thread, the first driving motor is mounted vertically on movable plate；The sliding stand and installation
It is connected with driving pulley on the second screw rod between platform, is equipped with the passive belt ipsilateral with driving pulley on two first screw rods
Wheel is connected by belt between driving pulley and two passive belt wheels；Go out light positioned at laser cleaning head in the support plate
Hole side is equipped with positioning tool.
In use, will be positioned on positioning tool by airplane component, the laser that laser generator generates passes through
Optical fiber is transferred to be adjusted in laser cleaning head after beat on airplane component, thus on airplane component paint carry out
Radiation cleaning, when the second driving motor rotates forward, the second screw rod rotates and driving pulley is driven to rotate, and passive belt wheel is in belt
Transmission is lower and driving pulley keeps rotating synchronously, so that two first screw rods, the second screw rod rotate synchronously, wherein two first
Bar driving sliding seat moves backward, meanwhile, the second screw rod driving movable plate moves backward, so that the sliding seat made and movable plate are same
Moved further allows the laser cleaning head on sliding seat to move backward, so that the hot spot beaten on airplane component be become larger；Control moves
The first driving motor reciprocating rotation on movable plate, so that the position of horizontal direction of the laser cleaning head on airplane component occurs
Variation；The piston rod for controlling vertical hydraulic cylinder moves up and down, so that laser cleaning head changes in the position of vertical direction, from
And laser cleaning head is cleaned to the entire plane of airplane component.When the size of hot spot to be changed, control second is driven
Dynamic motor reversal is located proximate to airplane component by laser cleaning head, is swashed by whole device by what is projected in laser cleaning head
Light is beaten on airplane component and is moved on airplane component, thus realize the surface clean of entire airplane component,
Guarantee the size constancy of entire airplane component.
Compared with the prior art, the utility model has the advantages that：
1, using the position and swing for automatically controlling laser cleaning head, to control hot spot of the laser on airplane component
Size, so that regulating time is short, fast response time, and the frequency cleaned is consistent, and can be avoided repeated washing
Process not only increases cleaning efficiency, also guarantees that the body surface after cleaning is of the required size；
2, two first screw rods and the synchronization of the second screw rod are driven simultaneously by the second driving motor and is rotate in same direction, so that
Sliding seat and sliding stand synchronizing moving, thus guarantee that the first driving motor can move simultaneously with rotating disk, so that rotating disk
Bearing capacity reduces, and guarantees the smooth movement of sliding seat on the supporting plate, allows the laser cleaning head of installation on the rotating pan can be fast
Speed response is moved forward and backward, and beats the spot size on airplane component to control laser；
3, by the reciprocating rotation of the first driving motor rotating disk is rotated on sliding seat, changes laser cleaning head
Horizontally rotate position, the hot spot that the laser projected from laser cleaning head is beaten on airplane component moves in the horizontal direction；Together
When moved up and down on rotation seat by vertical Driven by Hydraulic Cylinder laser cleaning head so that laser beats the light on airplane component
Spot is mobile in vertical direction, to realize that laser facula forms plane motion, cleans to whole surface, and according to rule
Carrying out cleaning can be avoided the process of repeated washing, and automation control cleaning frequency can guarantee the outer dimension of airplane component
It is consistent.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the overlooking structure diagram of the utility model；
Fig. 3 is partial enlargement structural representation at A in Fig. 1；
In figure, base 1, support plate 2, rectangular opening 201, locating piece 3, the first screw rod 4, sliding seat 5, rotating disk 6, rotation seat
7, vertical hydraulic cylinder 8, laser cleaning head 9, the first driving motor 10, driving mechanism 11, mounting plate 111, sliding stand 112, installation
Platform 113, the second driving motor 114, the second screw rod 115, movable plate 116, driving pulley 12, passive belt wheel 13, belt 14, positioning
Tooling 15, limit plate 151, limit square bar 152, mounting groove 1520, adjustment hole 1521, pushing plate 153, compressed spring 154, transverse direction
Hydraulic cylinder 155, cushion block 156, gag lever post 157, laser generator 100, optical fiber 200.
Specific embodiment
The utility model is described further with reference to the accompanying drawing.
As shown in FIG. 1 to 3, a kind of self-action laser cleaning for airplane component cleaning described in the utility model
Device, the base 1 including opening, base 1 are to be connected with support plate 2 on rectangular parallelepiped structure and base 1, are equipped in base 1 sharp
Optical generator 100, rectangular opening 201 is offered in support plate 2 along its length, and support plate 2 is equipped with and is located at rectangular opening
Two locating pieces 3 on the outside of 201 short side, rotation is equipped with two the first parallel screw rods 4 between two locating pieces 3, and two pieces the
The sliding seat 5 being slidably matched with support plate 2 is threadedly engaged on one screw rod 4, by the rotation of two first screw rods 4, driving is slided
The dynamic transverse shifting in support plate 2 of seat 5.Rotation is equipped with the rotating disk 6 of the " T " shape structure in section on sliding seat 5, in rotating disk 6
Interval is connected with rotation seat 7 and vertical hydraulic cylinder 8, and wherein rotation is equipped with and passes through optical fiber with laser generator 100 on rotation seat 7
The laser cleaning head 9 of 200 connections, the end of laser cleaning head 9 are connect with the piston rod rotation of vertical hydraulic cylinder 8, and laser occurs
The laser that device 100 generates is transferred in laser cleaning head 9 by optical fiber 200, and the hot spot road of S-shaped is formed in laser cleaning head 9
Diameter, and project and beaten on airplane component from the light hole on laser cleaning head 9, existed by the piston rod of vertical hydraulic cylinder 8
It is moved back and forth on vertical direction, to drive laser cleaning head 9 to swing up and down on rotation seat 7, so that laser facula is in aircraft
It is vertically movable on components.
In order to enable laser cleaning head 9 to be rotated in the horizontal direction, laser facula water on airplane component is allowed
Translation is dynamic, and the lower end of rotating disk 6 is protruded into base 1 to and is connected with the first driving motor 10, is equipped in base 1 and drives first to drive
The mobile driving mechanism 11 of dynamic motor 10, driving mechanism 11 include mounting plate 111, the sliding stand 112 being successively fixed in base 1
And erecting bed 113, wherein erecting bed 113 is equipped with the second driving motor 114, between mounting plate 111 and the second driving motor 114
Equipped with rotatable second screw rod 115, sliding is equipped with the movable plate 116 being threadedly engaged with the second screw rod 115 on sliding stand 112,
First driving motor 10 is mounted vertically on movable plate 116, after the first driving motor 10 drives the rotation of the second screw rod 115, is made
It obtains movable plate 116 to move on sliding stand 112, so that the first driving motor 10 be allowed to be supported on movable plate 116, avoids sliding seat
5 bear the weight of the first driving motor 10, guarantee the smooth sliding in support plate 2 of sliding seat 5.In order to guarantee the first driving motor
10 is synchronous with mobile holding of the sliding seat 5 in support plate 2, while being driven by the second driving motor 114, in sliding stand
It is connected with driving pulley 12 on the second screw rod 115 between 112 and erecting bed 113, is equipped on two first screw rods 4 and active
The ipsilateral passive belt wheel 13 of belt wheel 12 is connected by belt 14 between driving pulley 12 and two passive belt wheels 13, when actively
After belt wheel 12 follows the second screw rod 115 to rotate, passive belt wheel 13 is driven to rotate synchronously, so that two first screw rods 4 and second
Screw rod 115 keeps synchronous and rotates in same direction, so that holding is synchronous when sliding seat 5 and mobile movable plate 116, guarantees the first driving electricity
The stable connection of machine 10 and rotating disk 6.
It is equipped with positioning tool 15 positioned at the light hole side of laser cleaning head 9 in support plate 2, convenient for wanting zero, aircraft
Part is positioned, to cooperate the movement routine of the laser projected in laser cleaning head 9 not repeat.Positioning tool 15 includes
It is vertically fixed in limit plate 151 in support plate 2, sliding is equipped with two groups of parallel limit square bars 152 on limit plate 151, and every group
The quantity for limiting square bar 152 is 4, and limit square bar 152 stretches out 151 side of limit plate and is connected with pushing plate 153, pushing plate 153
Outside is equipped with pushing mechanism, and limit square bar 152 does not extend out and offers mounting groove 1520 on the position of 151 side of limit plate, installs
4 adjustment holes 1521 are offered on the bottom surface of slot 1520, and adjustable gag lever post 157 is equipped in each adjustment hole 1521,
Middle adjustment hole 1521 is to be threadedly engaged with gag lever post 157, according to the width for the airplane component to be positioned to gag lever post 157
It is adjusted, gag lever post 157 is allowed reliably to catch on airplane component edge, remaining not applicable gag lever post 157 is withdrawn into installation
In slot 1520, avoid generating interference.Pushing mechanism includes the cushion block 156 being fixed in support plate 2, is equipped with cross on cushion block 156
To hydraulic cylinder 155, the piston-rod end and pushing plate 153 of hydraulic cylinder are affixed, control the reciprocal of the piston rod of transverse hydraulic cylinder 155
It is mobile, so that pushing plate 153 will limit the drive of square bar 152 and slide on limit plate 151, so that airplane component reliably be pressed
Tightly positioned on the side of limit plate 151.
In order to save the power source of transverse hydraulic cylinder 155, moreover it is possible to the pressure for protecting the airplane component being compacted to bear
In the pressure-bearing limit, between pushing plate 153 and limit plate 151 be equipped with several compressed springs 154, the one of compressed spring 154
End is fixed in pushing plate 153, and the other end of compressed spring 154 is fixed on limit plate 151, after airplane component positioning,
Pushing plate 153 is pushed open by the tensile force of compressed spring 154, so that airplane component is compacted, it at this time can be by lateral liquid
Cylinder pressure 155 is closed, and only supports pushing plate 153 when needing to remove airplane component, so that compressed spring 154 is compressed,
To allow airplane component to be removed.
When the components that cannot be removed on to aircraft clean, positioning tool can be removed, will directly be swashed
Laser facula in light cleaning head 9 is projected and is cleaned on aircraft, so that the scope of application of whole device is more extensive,
It can be suitably used for the cleaning of entire aircraft appearance.
In the explanation of the utility model, it should be noted that term " first ", " second " etc. be merely for convenience of description and
Understand, not to the quantity of technical characteristic, using being sequentially defined.
Finally, it is stated that above embodiments are merely intended for describing the technical solutions of the present application, but not for limiting the present application, although ginseng
The utility model is described in detail according to preferred embodiment, those skilled in the art should understand that, it can be to this
The technical solution of utility model is modified or replaced equivalently, without departing from the objective and model of technical solutions of the utility model
It encloses, should all cover in the scope of the claims of the utility model.
Claims (5)
1. a kind of self-action laser cleaner for airplane component cleaning, the base including opening, base is cuboid
It is connected with support plate in structure and base, laser generator is installed in base, it is characterised in that：Along its length in the support plate
Degree direction offers rectangular opening, and support plate is equipped with two locating pieces being located on the outside of the short side of rectangular opening, two positioning
Rotation is equipped with two the first parallel screw rods between block, is threadedly engaged the cunning being slidably matched with support plate on two first screw rods
Dynamic seat；
Rotation is equipped with the rotating disk of the " T " shape structure in section on the sliding seat, and interval is connected with rotation seat and erects in rotating disk
To hydraulic cylinder, wherein rotation is equipped with the laser cleaning head connecting with laser generator by optical fiber, laser cleaning head on rotation seat
End connect with the piston rod rotation of vertical hydraulic cylinder；
The first driving motor is protruded into base and be connected in the lower end of the rotating disk, is equipped in base and drives the first driving motor
Mobile driving mechanism, driving mechanism include the mounting plate, sliding stand and erecting bed being successively fixed in base, wherein erecting bed
It is equipped with the second driving motor, rotatable second screw rod is equipped between mounting plate and the second driving motor, on the sliding stand
Sliding is equipped with the movable plate cooperated with the second wire rod thread, and the first driving motor is mounted vertically on movable plate；
It is connected with driving pulley on the second screw rod between the sliding stand and erecting bed, is equipped on two first screw rods and master
Movable belt pulley ipsilateral passive belt wheel is connected by belt between driving pulley and two passive belt wheels；
Positioning tool is equipped with positioned at the light hole side of laser cleaning head in the support plate.
2. a kind of self-action laser cleaner for airplane component cleaning according to claim 1, feature exist
In：The positioning tool includes vertical affixed limit plate on the supporting plate, and sliding is equipped with two groups of parallel limits on limit plate
Square bar, limit square bar stretch out limit plate side and are connected with pushing plate, pushing mechanism are equipped on the outside of pushing plate, limit square bar does not extend out
Mounting groove is offered on the position of limit plate side, offers multiple adjustment holes on the bottom surface of mounting groove, in each adjustment hole
Equipped with adjustable gag lever post.
3. a kind of self-action laser cleaner for airplane component cleaning according to claim 2, feature exist
In：The adjustment hole is to be threadedly engaged with gag lever post.
4. a kind of self-action laser cleaner for airplane component cleaning according to claim 2 or 3, feature
It is：The pushing mechanism includes affixed cushion block on the supporting plate, and transverse hydraulic cylinder, the piston of hydraulic cylinder are equipped on cushion block
Bar end and pushing plate are affixed.
5. a kind of self-action laser cleaner for airplane component cleaning according to claim 4, feature exist
In：Several compressed springs are equipped between the pushing plate and limit plate, one end of compressed spring is fixed in pushing plate, compresses bullet
The other end of spring is fixed on limit plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820284337.3U CN208098805U (en) | 2018-02-28 | 2018-02-28 | A kind of self-action laser cleaner for airplane component cleaning |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820284337.3U CN208098805U (en) | 2018-02-28 | 2018-02-28 | A kind of self-action laser cleaner for airplane component cleaning |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208098805U true CN208098805U (en) | 2018-11-16 |
Family
ID=64124951
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820284337.3U Expired - Fee Related CN208098805U (en) | 2018-02-28 | 2018-02-28 | A kind of self-action laser cleaner for airplane component cleaning |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208098805U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108202052A (en) * | 2018-02-28 | 2018-06-26 | 彭州启光科技有限公司 | A kind of self-action laser cleaner for airplane component cleaning |
| CN113751432A (en) * | 2021-09-17 | 2021-12-07 | 宁波翔明激光科技有限公司 | Laser cleaning head of integrated lens cleanliness detection device |
-
2018
- 2018-02-28 CN CN201820284337.3U patent/CN208098805U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108202052A (en) * | 2018-02-28 | 2018-06-26 | 彭州启光科技有限公司 | A kind of self-action laser cleaner for airplane component cleaning |
| CN113751432A (en) * | 2021-09-17 | 2021-12-07 | 宁波翔明激光科技有限公司 | Laser cleaning head of integrated lens cleanliness detection device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181116 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |