CN108421798A - A kind of aircraft skin laser cleaner - Google Patents
A kind of aircraft skin laser cleaner Download PDFInfo
- Publication number
- CN108421798A CN108421798A CN201810617202.9A CN201810617202A CN108421798A CN 108421798 A CN108421798 A CN 108421798A CN 201810617202 A CN201810617202 A CN 201810617202A CN 108421798 A CN108421798 A CN 108421798A
- Authority
- CN
- China
- Prior art keywords
- sliding
- guide
- traversing
- aircraft skin
- lead screw
- 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.)
- Pending
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 49
- 238000004140 cleaning Methods 0.000 claims abstract description 39
- 239000013307 optical fiber Substances 0.000 claims abstract description 6
- 238000000034 method Methods 0.000 abstract description 9
- 230000008569 process Effects 0.000 abstract description 7
- 239000003973 paint Substances 0.000 description 7
- 238000010586 diagram Methods 0.000 description 5
- 230000033001 locomotion Effects 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 238000005108 dry cleaning Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005202 decontamination Methods 0.000 description 1
- 230000003588 decontaminative effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000036541 health Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B13/00—Accessories or details of general applicability for machines or apparatus for cleaning
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B7/00—Cleaning by methods not provided for in a single other subclass or a single group in this subclass
- B08B7/0035—Cleaning by methods not provided for in a single other subclass or a single group in this subclass by radiant energy, e.g. UV, laser, light beam or the like
- B08B7/0042—Cleaning by methods not provided for in a single other subclass or a single group in this subclass by radiant energy, e.g. UV, laser, light beam or the like by laser
Abstract
The invention discloses a kind of aircraft skin laser cleaners, it is parallel and be fixed on the guide rail bracket on ground including two, the transverse-moving mechanism slided along guide rail bracket length direction is equipped between two guide rail brackets, transverse-moving mechanism is equipped with can be with respect to the vertical shift mechanism of its sliding, laser cleaning head is installed in vertical shift mechanism, laser cleaning head is connect by optical fiber with laser generator, it is slided on guide rail bracket by transverse-moving mechanism and vertical shift mechanism is driven to be moved on transverse-moving mechanism so that laser cleaning head can cover aircraft skin surface.It improves aircraft skin and expends the problem that the time is long, efficiency is low using laser cleaning process is held.
Description
Technical field
The present invention relates to aircraft washing plant fields, and in particular to a kind of aircraft skin laser cleaner.
Background technology
Aircraft just needs depainting to be safeguarded in 5 years or so at flight time interval, overhaul, to ensure the reliable of aircraft
Property, it needs the paint that will spray before on the surface to be removed aircraft skin, is convenient for subsequent maintenance or maintenance, now
The health that the depainting agent method used not only pollutes environment, damages operator, and somewhat expensive, in order to overcome this cleaning side
Formula there are the drawbacks of, the paint on airplane component is cleaned using laser cleaner, only expend electric energy feelings
Cleaning requirement can be met under condition, have the effect of environmental protection, and protect to the size of airplane component, after ensureing cleaning
Airplane component still conform to using 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 adsorption capacity of the surface to particle, disengage it from body surface, and then achieve the purpose that cleaning.At present compared with
The most commonly used is laser dry cleaning process, directly use the direct radiation decontamination of pulse laser, and the laser cleaning of laser dry cleaning process is used to set
Standby includes hand-held, and the volume of portion of the handle is big, heavy, for a long time using be easy to causeing fatigue.For aircraft external surface area
It is larger, compared by the way of man-hour manually hand-held laser cleaning and expends the time, inefficiency, and also use for a long time be easy to cause people
Work fatigue.
Invention content
For the deficiency in the presence of the prior art, the present invention provides a kind of aircraft skin laser cleaners, solve
Aircraft skin expends the problem that the time is long, efficiency is low using laser cleaning process is held.
To achieve the above object, present invention employs the following technical solutions：
A kind of aircraft skin laser cleaner, including two parallel and be fixed on the guide rail bracket on ground, two guide rails
The transverse-moving mechanism slided along guide rail bracket length direction is equipped between frame, transverse-moving mechanism is equipped with can be with respect to the vertical shift machine of its sliding
Structure is equipped with laser cleaning head in vertical shift mechanism, and laser cleaning head is connect by optical fiber with laser generator；Each guide rail bracket packet
Support plate and multiple support columns are included, multiple support columns are fixed on the lower surface of support plate and are evenly distributed with along support plate length direction,
It is connected with directive slide track in support plate, the first limiting plate, the second limiting plate, the first limit are respectively equipped in the both ends of directive slide track
Driving lead screw is equipped with by bearing rotation between plate and the second limiting plate, the end of lead screw is driven to pass through the second limiting plate and first
Motor connects, and first motor is installed on the supporting plate；The transverse-moving mechanism includes two guide pads and rectangular guide bar, wherein being oriented to
Block is slidably matched with directive slide track, and guide pad is fixed in driving lead screw threaded engagement, rectangular guide bar between two guide pads, square
The rectangular channel of perforation is offered on the side of shape guide rod, is equipped with across the traversing of rectangular channel by bearing between two guide pads
One end of lead screw, traversing lead screw is connected with traversing gear, and traversing motor, traversing electricity are equipped on the guide pad of traversing gear
It is connected on the output shaft of machine and the intermeshing driving gear of traversing gear；The vertical shift mechanism includes being slided with rectangular guide bar
The sliding seat of cooperation, sliding seat and traversing lead screw threaded engagement are connected with longitudinal direction on sliding seat on the side of rectangular channel homonymy
Guide rod offers the sliding groove penetrated through downwards on Der Laengslenker, is offered on two sides of Der Laengslenker and sliding groove connects
Logical slider bar hole；Sliding is equipped with the sliding shoe for installing laser cleaning head in sliding groove, is connected with and slides on sliding shoe
Multiple gag lever posts that hole is slidably matched；The driving mechanism that driving sliding shoe moves up and down is installed on sliding seat.
Whole device is installed on the ground in aircraft maintenance warehouse, is needing to carry out depainting processing to aircraft skin
When, it allows aircraft to be aligned among two guide rail brackets and is moved, allow aircraft completely between two guide rail brackets, sent out by laser
The laser that raw device generates is transferred to by optical fiber be adjusted in laser cleaning head after beat on aircraft surfaces, thus to aircraft table
The paint in face carries out radiation cleaning, so that the peeling paint on aircraft skin, and it is by dust catcher that the paint to fall off is grey
Dirt is collected；Driving lead screw is driven to turn on the first limiting plate and the second limiting plate by the first motor on two guide rail brackets
It is dynamic, so that transverse-moving mechanism slides on two guide rail brackets, and drive traversing lead screw to rotate by traversing motor so that vertical
Telephone-moving structure slides on rectangular guide bar, so that laser cleaning head can follow vertical shift mechanism to be moved up in two axial directions
It is dynamic so that laser cleaning head covers entire aircraft surfaces in moving process；And the driving mechanism driving in vertical shift mechanism is slided
Motion block moves up and down on Der Laengslenker, and the hot spot on aircraft surfaces is beaten to the laser projected in laser cleaning head to realize
Size beats the temperature value on aircraft skin when changing Investigation of Laser Delacquer-ing, rationally adjusts the surface of temperature effective protection aircraft skin
Finish.
Compared with the prior art, the present invention has the advantages that：
1, it drives transverse-moving mechanism to be slided on two guide rail brackets by first motor, and passes through traversing motor on transverse-moving mechanism
Driving vertical shift mechanism is slided on rectangular guide bar, so that laser cleaning head follows vertical shift mechanism to be moved up in two axis,
Enable the moving range of laser cleaning head to cover entire aircraft surfaces, avoids using man-hour manually hand-held laser cleaning head in aircraft
Mobile present situation is carried out on surface, improves cleaning efficiency, reduces the time of cleaning process consuming, hand labor intensity is allowed to drop
It is low；
2, it drives sliding shoe to be moved up and down on Der Laengslenker by driving mechanism in vertical shift mechanism, adjusts laser cleaning head
Spacing distance between aircraft skin is beaten temperature value and light-gathering on aircraft skin when adjusting Investigation of Laser Delacquer-ing, is being protected
Paint removal efficiency is improved while protecting aircraft skin surface smoothness.
Description of the drawings
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the side view of the present invention；
Fig. 3 be transverse-moving mechanism of the present invention, vertical shift mechanism overlooking structure diagram；
Fig. 4 is the structural schematic diagram of directive slide track of the present invention；
Fig. 5 is the structural schematic diagram of guide pad of the present invention；
Fig. 6 is the structural schematic diagram of sliding shoe of the present invention；
In figure, guide rail bracket 1, support column 102, supporting rod 1021, mounting plate 1022, directive slide track 103, is consolidated support plate 101
Fixed board 1031, sliding rail portion 1032, the first limiting plate 104, the second limiting plate 105, driving lead screw 106, first motor 2, cross sliding machine
Structure 3, guide pad 301, guide groove 3011, bearing hole 3012, threaded hole 3013, rectangular guide bar 302, rectangular channel 3021, traversing silk
Bar 303, traversing motor 305, driving gear 306, vertical shift mechanism 4, sliding seat 401, Der Laengslenker 402, is slided traversing gear 304
Dynamic slot 4021, slider bar hole 4022, sliding shoe 403, rack structure 4031, gag lever post 404, the second motor 405, vertical shift gear
406, laser generator 100, laser cleaning head 200, optical fiber 300.
Specific implementation mode
Following further describes the present invention with reference to the drawings.
As shown in Fig. 1~Fig. 6, a kind of aircraft skin laser cleaner of the present invention, including two parallel and solid
It is traversing due to being equipped with the transverse-moving mechanism 3 that is slided along 1 length direction of guide rail bracket between the guide rail bracket 1 on ground, two guide rail brackets 1
Mechanism 3 be equipped with can the opposite vertical shift mechanism 4 that it is slided, laser cleaning head 200, laser cleaning head are installed in vertical shift mechanism 4
200 are connect by optical fiber 300 with laser generator 100, are slided on guide rail bracket 1 by transverse-moving mechanism 3, and allow vertical shift mechanism 4
It is slided on transverse-moving mechanism 3 so that the moving range of laser cleaning head 200 can cover entire aircraft skin surface, and swash
Light generating apparatus, laser cleaning head 200 carry out disclosure in patent application before, herein no longer to their specific knot
Structure feature is defined, and mainly improves working strength and cleaning efficiency when current aircraft skin depainting.
Each guide rail bracket 1 includes support plate 101 and multiple support columns 102, and the quantity of support column 102 is at least 3, avoids
The case where 101 middle part of support plate deforms, and support column 102 includes supporting rod 1021 and is fixed under supporting rod 1021
Four corners of the mounting plate 1022 at end, mounting plate 1022 offer mounting hole, by mounting plate 1022 by support column 102
It is affixed on the ground, and support column 102 is directly fixed on the lower surface of support plate 101 and equal along 101 length direction of support plate
Cloth is connected with directive slide track 103 in support plate 101, the first limiting plate 104, second is respectively equipped in the both ends of directive slide track 103
Limiting plate 105 is equipped with driving lead screw 106 by bearing rotation between first limiting plate 104 and the second limiting plate 105, drives silk
The end of bar 106 is connect across the second limiting plate 105 with first motor 2, and first motor 2 is mounted in support plate 101.In order to make
Obtaining directive slide track 103 can also prevent from turning on one's side while being oriented to, and directive slide track 103 includes being fixed in support plate 101
Fixed plate 1031, is connected with the sliding rail portion 1032 of section structure in the shape of an " I " in fixed plate 1031, by fixed plate when processing
1031 are integrally formed making with sliding rail portion 1032, ensure whole intensity, are limited using the groove in sliding rail portion 1032, energy
Enough the case where effectively avoiding turning on one's side, improve stability and reliability of the transverse-moving mechanism 3 in sliding process.
Transverse-moving mechanism 3 includes two guide pads 301 and rectangular guide bar 302, and wherein guide pad 301 is slided with directive slide track 103
Dynamic cooperation, the rectangular in cross-section structure of guide pad 301 offer the section with sliding rail portion 1032 on the lower surface of guide pad 301
The guide groove 3011 that shape matches is offered for installation axle on the side of 302 side of rectangular guide bar on guide pad 301
The bearing hole 3012 held offers the threaded hole 3013 with driving 106 threaded engagement of lead screw on guide pad 301, when first motor 2
When driving lead screw 106 being driven to rotate so that guide pad 301 moves on directive slide track 103；And rectangular guide bar 302 is fixed in two
Between a guide pad 301, the rectangular channel 3021 of perforation is offered on the side of rectangular guide bar 302, is led between two guide pads 301
It crosses bearing and traversing lead screw 303 across rectangular channel 3021 is installed, bearing interference fit is mounted in bearing hole 3012 so that horizontal
Silk shifting rod 303 can on two guide pads 301 flexible rotating, be connected with traversing gear 304 in one end of traversing lead screw 303,
Traversing motor 305 is installed on the guide pad 301 of traversing gear 304, is connected on the output shaft of traversing motor 305 and cross
304 intermeshing driving gear 306 of gear is moved, drives traversing lead screw 303 to be rotated by traversing motor 305, to right
Movement of the vertical shift mechanism 4 on rectangular guide bar 302 is controlled.
Vertical shift mechanism 4 includes the sliding seat 401 being slidably matched with rectangular guide bar 302, sliding seat 401 and traversing lead screw 303
Threaded engagement sliding seat 401 is rectangular configuration, centre offer with 302 matched rectangular opening of rectangular guide bar, and in rectangle
The drive block with 303 threaded engagement of traversing lead screw is connected on the side in hole, so that direct band after the rotation of traversing lead screw 303
Dynamic sliding seat 401 is slided on rectangular guide bar 302；On sliding seat 401 with 302 rectangular channel of rectangular guide bar, 3021 homonymy
Side on be connected with Der Laengslenker 402, the sliding groove 4021 penetrated through downwards, Der Laengslenker 402 are offered on Der Laengslenker 402
Two sides on offer the slider bar hole 4022 being connected to sliding groove 4021；Sliding is equipped with for pacifying in sliding groove 4021
The sliding shoe 403 of laser cleaning head 200 is filled, the multiple limits being slidably matched with slider bar hole 4022 are connected on sliding shoe 403
Bar 404 passes through the cooperation in gag lever post 404 and slider bar hole 4022, the cooperation of sliding shoe 403 and sliding groove 4021 so that sliding
Block 403 can slide on Der Laengslenker 402, and laser cleaning head 200 is mounted on sliding shoe 403, can also be moved up and down,
To adjust the spacing distance between laser cleaning head 200 and aircraft skin, it is big that change laser beats the hot spot on aircraft skin
It is small, to adjust the temperature value on aircraft skin, ensure to improve paint removal efficiency while aircraft skin surface smoothness；It is sliding
The driving mechanism that driving sliding shoe 403 moves up and down is installed, in order to enable between sliding shoe 403 and driving mechanism on seat 401
Movement relation be it is adjustable, ensure laser adjusting have rule, the " T " shape structure in section of sliding shoe 403, sliding
On block 403 rack structure 4031 is equipped with close to the side of sliding seat 401；Driving mechanism includes being mounted on sliding seat 401
Second motor 405 is connected with 4031 intermeshing vertical shift gear 406 of rack structure on the output shaft of second motor 405, and
Two motors 405 allow sliding shoe 403 to be moved on Der Laengslenker 402, and energy by driving 406 forward or reverse of vertical shift gear
It is enough that turnning circle is adjusted according to displacement distance.
In the explanation of the present invention, it should be noted that term " first ", " second " etc. are merely for convenience of describing and manage
Solution, is not defined the usage quantity of particular technique feature, significance level or erection sequence, for the first electricity in the present invention
The control of machine 2, the second motor 405, traversing motor 305 is controlled using the PLC control cabinet of the prior art.
Finally illustrate, the above examples are only used to illustrate the technical scheme of the present invention and are not limiting, although with reference to compared with
Good embodiment describes the invention in detail, it will be understood by those of ordinary skill in the art that, it can be to the skill of the present invention
Art scheme is modified or replaced equivalently, and without departing from the objective and range of technical solution of the present invention, should all be covered at this
In the right of invention.
Claims (6)
1. a kind of aircraft skin laser cleaner, it is characterised in that：It is parallel and be fixed on the guide rail bracket on ground including two
(1), the transverse-moving mechanism (3) slided along guide rail bracket (1) length direction is equipped between two guide rail brackets (1), transverse-moving mechanism is set on (3)
Laser cleaning head (200), laser cleaning head can be equipped with respect to the vertical shift mechanism (4) of its sliding, in vertical shift mechanism (4) by having
(200) it is connect with laser generator (100) by optical fiber (300)；
Each guide rail bracket (1) includes support plate (101) and multiple support columns (102), and multiple support columns (102) are fixed in support plate
(101) on lower surface and uniformly distributed along support plate (101) length direction, directive slide track (103) is connected in support plate (101),
It is respectively equipped with the first limiting plate (104), the second limiting plate (105), the first limiting plate (104) in the both ends of directive slide track (103)
Driving lead screw (106) is equipped with by bearing rotation between the second limiting plate (105), the end of driving lead screw (106) passes through the
Two limiting plates (105) are connect with first motor (2), and first motor (2) is mounted in support plate (101)；
The transverse-moving mechanism (3) includes two guide pads (301) and rectangular guide bar (302), and wherein guide pad (301) is slided with guiding
Rail (103) is slidably matched, and guide pad (301) is fixed in two and leads with driving lead screw (106) threaded engagement, rectangular guide bar (302)
To the rectangular channel (3021) between block (301), offering perforation on the side of rectangular guide bar (302), two guide pads (301) it
Between the traversing lead screw (303) across rectangular channel (3021) is equipped with by bearing, one end of traversing lead screw (303) is connected with traversing
Gear (304) is equipped with traversing motor (305) on the guide pad (301) of traversing gear (304), traversing motor (305)
It is connected on output shaft and the intermeshing driving gear (306) of traversing gear (304)；
The vertical shift mechanism (4) includes the sliding seat (401) being slidably matched with rectangular guide bar (302), sliding seat (401) with it is traversing
Lead screw (303) threaded engagement is connected with Der Laengslenker (402) on sliding seat (401) on the side of rectangular channel (3021) homonymy,
The sliding groove (4021) penetrated through downwards is offered on Der Laengslenker (402), is offered on two sides of Der Laengslenker (402)
The slider bar hole (4022) being connected to sliding groove (4021)；Sliding is equipped with for installing laser cleaning head in sliding groove (4021)
(200) sliding shoe (403) is connected with the multiple gag lever posts being slidably matched with slider bar hole (4022) on sliding shoe (403)
(404)；The driving mechanism that driving sliding shoe (403) moves up and down is installed on sliding seat (401).
2. a kind of aircraft skin laser cleaner according to claim 1, it is characterised in that：The directive slide track
(103) include the fixed plate (1031) being fixed in support plate (101), it is in the shape of an " I " to be connected with section in fixed plate (1031)
The sliding rail portion (1032) of structure.
3. a kind of aircraft skin laser cleaner according to claim 2, it is characterised in that：The guide pad (301)
Rectangular in cross-section structure, offer on the lower surface of guide pad (301) and to match with the cross sectional shape of sliding rail portion (1032)
Guide groove (3011) offers on the side of rectangular guide bar (302) side the axis for installing bearing on guide pad (301)
Bearing bore (3012) offers the threaded hole (3013) with driving lead screw (106) threaded engagement on guide pad (301).
4. a kind of aircraft skin laser cleaner according to claim 2, it is characterised in that：The sliding shoe (403)
The " T " shape structure in section, be equipped with rack structure (4031) close to the side of sliding seat (401) on sliding shoe (403).
5. a kind of aircraft skin laser cleaner according to claim 3, it is characterised in that：The driving mechanism includes
The second motor (405) on sliding seat (401) is connected with rack structure on the output shaft of the second motor (405)
(4031) intermeshing vertical shift gear (406).
6. a kind of aircraft skin laser cleaner according to claim 4, it is characterised in that：The support column (102)
Including supporting rod (1021) and it is fixed in the mounting plate (1022) of supporting rod (1021) lower end, four corners of mounting plate (1022)
Place offers mounting hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810617202.9A CN108421798A (en) | 2018-06-15 | 2018-06-15 | A kind of aircraft skin laser cleaner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810617202.9A CN108421798A (en) | 2018-06-15 | 2018-06-15 | A kind of aircraft skin laser cleaner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108421798A true CN108421798A (en) | 2018-08-21 |
Family
ID=63164531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810617202.9A Pending CN108421798A (en) | 2018-06-15 | 2018-06-15 | A kind of aircraft skin laser cleaner |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108421798A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108372158A (en) * | 2018-02-28 | 2018-08-07 | 彭州启光科技有限公司 | A kind of laser cleaner for aircraft skin depainting |
| CN111729903A (en) * | 2020-07-20 | 2020-10-02 | 山东创瑞激光科技有限公司 | High-repetition-frequency pulse laser cleaning equipment for large-sized workpiece |
| CN112934857A (en) * | 2021-01-27 | 2021-06-11 | 南昌市彦畅机电科技有限公司 | Laser cleaning device for aircraft skin |
| CN113639647A (en) * | 2021-07-08 | 2021-11-12 | 中国重型机械研究院股份公司 | Skin laser measuring device based on take characteristic vision adapter |
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| BE885796A (en) * | 1979-10-25 | 1981-02-16 | Langen Robert | METHOD AND DEVICE FOR REMOVING METAL RUST |
| DE102010062082A1 (en) * | 2010-11-29 | 2012-05-31 | 4Jet Sales + Service Gmbh | Cleaning of surfaces in vacuum apparatus by means of laser |
| AU2013203887A1 (en) * | 2012-02-20 | 2013-09-05 | Adc Telecommunications, Inc. | Fiber optic connector, fiber optic connector and cable assembly, and methods for manufacturing |
| CN104438227A (en) * | 2013-09-16 | 2015-03-25 | 上海海固电器设备有限公司 | Airplane coated paint laser cleaning equipment |
| CN106238411A (en) * | 2016-07-28 | 2016-12-21 | 深圳吉阳智云科技有限公司 | A kind of liftable cleaning platform assembly and laser cleaning equipment thereof |
| CN206474891U (en) * | 2017-01-24 | 2017-09-08 | 中山德智自动化机械有限公司 | A kind of new type auto machine that screws |
| CN208555434U (en) * | 2018-06-15 | 2019-03-01 | 彭州启光科技有限公司 | A kind of aircraft skin laser cleaner |
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2018
- 2018-06-15 CN CN201810617202.9A patent/CN108421798A/en active Pending
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| Publication number | Priority date | Publication date | Assignee | Title |
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| BE885796A (en) * | 1979-10-25 | 1981-02-16 | Langen Robert | METHOD AND DEVICE FOR REMOVING METAL RUST |
| DE102010062082A1 (en) * | 2010-11-29 | 2012-05-31 | 4Jet Sales + Service Gmbh | Cleaning of surfaces in vacuum apparatus by means of laser |
| AU2013203887A1 (en) * | 2012-02-20 | 2013-09-05 | Adc Telecommunications, Inc. | Fiber optic connector, fiber optic connector and cable assembly, and methods for manufacturing |
| CN104438227A (en) * | 2013-09-16 | 2015-03-25 | 上海海固电器设备有限公司 | Airplane coated paint laser cleaning equipment |
| CN106238411A (en) * | 2016-07-28 | 2016-12-21 | 深圳吉阳智云科技有限公司 | A kind of liftable cleaning platform assembly and laser cleaning equipment thereof |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108372158A (en) * | 2018-02-28 | 2018-08-07 | 彭州启光科技有限公司 | A kind of laser cleaner for aircraft skin depainting |
| CN111729903A (en) * | 2020-07-20 | 2020-10-02 | 山东创瑞激光科技有限公司 | High-repetition-frequency pulse laser cleaning equipment for large-sized workpiece |
| CN111729903B (en) * | 2020-07-20 | 2021-08-03 | 山东创瑞激光科技有限公司 | High-repetition-frequency pulse laser cleaning equipment for large-sized workpiece |
| CN112934857A (en) * | 2021-01-27 | 2021-06-11 | 南昌市彦畅机电科技有限公司 | Laser cleaning device for aircraft skin |
| CN113639647A (en) * | 2021-07-08 | 2021-11-12 | 中国重型机械研究院股份公司 | Skin laser measuring device based on take characteristic vision adapter |
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Application publication date: 20180821 |