CN106739445A - A kind of printing positioning instrument of aircraft V-type label - Google Patents
A kind of printing positioning instrument of aircraft V-type label Download PDFInfo
- Publication number
- CN106739445A CN106739445A CN201710038799.7A CN201710038799A CN106739445A CN 106739445 A CN106739445 A CN 106739445A CN 201710038799 A CN201710038799 A CN 201710038799A CN 106739445 A CN106739445 A CN 106739445A
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- China
- Prior art keywords
- type
- clamping bar
- aircraft
- support shaft
- printing
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41F—PRINTING MACHINES OR PRESSES
- B41F15/00—Screen printers
- B41F15/14—Details
- B41F15/16—Printing tables
- B41F15/18—Supports for workpieces
- B41F15/30—Supports for workpieces for articles with curved surfaces
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Labeling Devices (AREA)
- Clamps And Clips (AREA)
Abstract
A kind of printing the invention discloses aircraft V-type label positions instrument, it is provided with framework, clamping bar, positive stop strip, pressing plate, aircraft V-type label is installed in above clamping bar, the leg of frame of left and right two of framework is respectively equipped with stopper slot, clamping bar is installed on framework by the support shaft at two ends, a plurality of clamping bar horizontal distribution and it is parallel to each other, two positive stop strip is pressed on above clamping bar, aircraft V-type label is gripped between two positive stop strips, the frame facet that pressing plate is fixed on, pressing plate medial surface pushes down the end face that support shaft stretches out outside, simple structure of the present invention, printing efficiency is high, and realize batch printing.
Description
Technical field
The present invention relates to a kind of printing equipment, the printing positioning instrument of more particularly to a kind of aircraft V-type label.
Technical background
When being screen printed onto printing, by certain pressure make ink by the eyelet of half tone be transferred to stock (paper,
Ceramics etc.) on, image or word are formed, operation is carried out by generally only there need to be a table plane, but to special shape
Surface when printed, due to the operational characteristic of silk-screen printing, simply put or it is not strict to position restriction all
Presswork cannot be carried out, is typically to be supported with foam below part for the way of such part.But B787 aircrafts seat
Position label is V-type label, when being printed to two face because positioning is inaccurate, place the reasons such as shakiness, causes operation difficult
Degree is big, and scrappage is high, and being completed for printing after one side the ink such as needs could be printed to another side after drying, and has a strong impact on work
Make efficiency.
The content of the invention
The technical problems to be solved by the invention, are just to provide a kind of printing positioning instrument of aircraft V-type label, its structure
Simply, printing efficiency is high, and realizes batch printing.
Above-mentioned technical problem is solved, the technical solution adopted by the present invention is as follows：
A kind of printing positioning instrument of aircraft V-type label, the aircraft V-type label is the strip sheet metal component of V-type, V-type
Two end edges are provided with the flange of bending inwards, it is characterized in that, printing positioning instrument includes：
One framework, is rectangle structure；
A plurality of clamping bar, is provided with the first V-type surface, the V-type that the first V-type surface is formed with the inner surface of aircraft V-type label
Face is corresponding, and aircraft V-type label is installed in above clamping bar and flange withstands the bottom surface of clamping bar；
The clamping bar is respectively fixed at two ends with the support shaft extended along the length direction of clamping bar, the wherein support of one end
Axle is provided with the two of the second V-type surface, the positive and negative handstand of V-type on the V-type on the second V-type surface and the first V-type surface, and two V-type surfaces
The corresponding V-type side difference of bar is parallel, wherein a support shaft stretches out frame facet, standing screw is provided with the side；
The leg of frame of left and right two of the framework is respectively equipped with stopper slot corresponding with support shaft size, wherein on a leg of frame
Stopper slot be provided with horizontal bottom, be provided with the support shaft on the second V-type surface and coordinate with the stopper slot, the horizontal bottom of the stopper slot
All the time fitted with a wherein V-type side on the second V-type surface；
A plurality of clamping bar horizontal distribution and it is parallel to each other；
Two positive stop strips, are pressed on above clamping bar, and vertical with clamping bar, and aircraft V-type is gripped between two positive stop strips
Label, front and rear two leg of frame of framework has mounting groove corresponding with positive stop strip, and positive stop strip two ends are respectively embedded into mounting groove；
One pressing plate, is provided with mounting hole corresponding with standing screw, the framework where standing screw is installed on by mounting hole
Side, the outer end of standing screw is screwed with clamp nut, and pressing plate medial surface pushes down the end face that support shaft stretches out outside.
The clamping bar is the strip sheet metal component of V-type.
Described support shaft one end is provided with fixed block, and fixed-block-architecture (FBA) is corresponding to the V-structure that the inner surface of clamping bar is constituted,
Fixed block is embedded in the two ends of clamping bar, and is provided with screw and is fixed, so as to support shaft is fixed on into clamping bar two ends.
The clamp nut is wing nut.
The frame size is corresponding to the web plate size used by silk-screen printing.
Compared with prior art, the invention has the advantages that：
1st, aircraft V-type label is installed on clamping bar, clamping bar is carried out by framework it is spacing, then by two positive stop strips
Moving left and right for aircraft V-type label is limited, the positioning to aircraft V-type label is realized, it is seen that simple structure of the present invention.
2nd, after a face to aircraft V-type label is completed for printing, positive stop strip is unclamped, unclamps clamp nut, rotate clamping
Bar so that unprinted the facing up of aircraft V-type label, and printed, realize and the surface of aircraft V-type label is connected
Continuous printing, and no longer need to wait the ink could be printed to another side after drying, improve printing efficiency.
3rd, multiple aircraft V-type labels can be inserted on a clamping bar, and a plurality of clamping bar is installed on framework, can be with
These aircraft V-type labels are printed simultaneously, realizes batch printing, also improve efficiency.
Brief description of the drawings
Fig. 1 is schematic perspective view of the invention；
Fig. 2 is the schematic perspective view of aircraft V-type label；
Fig. 3 is the schematic perspective view of framework of the invention；
Fig. 4 is the schematic perspective view of clamping bar of the invention and the assembling structure of support shaft；
Fig. 5 is the schematic perspective view that aircraft V-type label is installed in the assembling structure shown in Fig. 4；
Fig. 6 is a schematic side view of the assembling structure shown in Fig. 4, the knot on the first V-type surface of display and the second V-type surface
Structure relation.
Reference implication in figure：
1- frameworks；2- positive stop strips；3- aircraft V-type labels；4- clamping bars；5- pressing plates；6- clamp nuts；7- standing screws；
8- stopper slots；9- flange；10- mounting grooves；11- horizontal bottoms；The first V-types of 12- surface；13- support shafts；14- the second V-type tables
Face；15- fixed blocks.
Specific embodiment
The present invention is further described with reference to embodiment.
As shown in Figure 1 and Figure 2, the present invention is provided with framework 1, seven clamping bar 4, two positive stop strip 2, pressing plate 7, it is necessary to print
Aircraft V-type label 3 be the strip sheet metal component of V-type, two end edges of V-type are provided with the flange 9 of bending inwards.
The rectangle structure that framework 1 is spliced by four block length square plates, its size is big with web plate used by silk-screen printing
It is small corresponding；Clamping bar 4 is the strip sheet metal component of V-type, and its surface is the first V-type surface 12, the first V-type surface 12 and aircraft V-type
The V-type face that the inner surface of label 3 is formed is corresponding, and aircraft V-type label 3 is installed in clamping bar 4 above and flange 9 withstands clamping bar 4
Bottom surface, such aircraft V-type label 3 is just installed in above clamping bar 4, can be with 3 aircraft V-type marks of clamp above a clamping bar
Board.Aircraft V-type label 3 is snapped in from the side of clamping bar 4.
Clamping bar 4 is respectively fixed at two ends with the support shaft 13 extended along the length direction of clamping bar, the wherein support of one end
Axle 13 is provided with the second V-type surface 14, as shown in fig. 6, the positive and negative handstand of V-type on the V-type on the second V-type surface and the first V-type surface, and
Two corresponding V-type side difference on two V-type surfaces are parallel, and the support shaft of the other end is cylinder；Wherein a support shaft 13 is stretched out
Frame facet 1, standing screw 7 is provided with the side.The fixed form of support shaft 13 is：Fixation is provided with the one end of support shaft 13
Block 15, the structure of fixed block 15 is corresponding to the V-structure that the inner surface of clamping bar 4 is constituted, and the two of the insertion clamping of fixed block 15 bar 4
Hold, and be provided with screw and be fixed, so as to support shaft 13 is fixed on into the two ends of clamping bar 4.
The leg of frame of left and right two of framework is respectively equipped with stopper slot 8 corresponding with the size of support shaft 13, wherein on a leg of frame
Stopper slot 8 be provided with horizontal bottom 11, be provided with the support shaft on the second V-type surface 14 and coordinate with the stopper slot, the water of the stopper slot
Planar base surface 11 is fitted with a wherein V-type side on the second V-type surface 14 all the time.Due to the V-type and the first V-type on the second V-type surface 14
The V-type on surface 12 is mutually stood upside down, and two V-type sides difference of two V-types is parallel, therefore when the horizontal bottom 11 and second of stopper slot
When a wherein V-type side on V-type surface 14 is fitted, the one side of the V-type of clamping bar 4 will be upward and in horizontality, so that aircraft V
The one side of type label 3 also can will thus print upward and in horizontality to the face upward of aircraft V-type label 3
Brush.Seven horizontal distributions of clamping bar 4 and it is parallel to each other, clamping bar face upward is convenient to aircraft V-type mark in same level
Board 3 carries out batch printing.
Positive stop strip 2 is pressed on above clamping bar 4, and vertical with clamping bar 4, and aircraft V-type mark is gripped between two positive stop strips 2
Board 3, the front and rear two block frames side of framework 1 has mounting groove 10 corresponding with positive stop strip 2, and the two ends of positive stop strip 2 are respectively embedded into
Mounting groove 10, two positive stop strips 2 limit moving left and right for aircraft V-type label 3.
Pressing plate 5 is provided with and the corresponding mounting hole of standing screw 7, the framework 1 where being installed on standing screw 7 by mounting hole
Side, the outer end of standing screw 7 is screwed with clamp nut 6, and the clamp nut 6 is wing nut, and convenient use person directly uses hand
It is adjusted, the medial surface of pressing plate 5 pushes down the end face that support shaft 13 stretches out outside, and clamping bar 4 is pressed on framework 1, prevents
During mobile printing positioning instrument, clamping bar 4 is shifted over.
When using, first aircraft V-type label 3 is installed on clamping bar 4, then clamping bar 4 is placed in the stopper slot 8 of framework 1
On, and the horizontal bottom 11 of stopper slot fits with a wherein V-type side on the second V-type surface 14 so that the one of aircraft V-type label 3
Face up and in horizontality, after seven clamping bars 4 are all installed, then aircraft V-type label 3 is limited by two positive stop strips 2
Move left and right, tighten clamp nut 6, complete positioning work, 3 face upward of aircraft V-type label is printed；The face is printed
After having brushed, positive stop strip 2 is unclamped, unclamp clamp nut 6, rotate clamping bar 4 so that the V-type of horizontal bottom 11 and second of stopper slot
Another V-type side laminating on surface 14, presses upper limit bar 2 again, tightens clamp nut 6, and the another side to aircraft V-type label 3 enters
Row printing, finally completes to this batch of printing work of aircraft V-type label 3.
Claims (5)
1. the printing of a kind of aircraft V-type label positions instrument, and the aircraft V-type label is the strip sheet metal component of V-type, the two of V-type
End edge is provided with the flange of bending inwards, it is characterised in that the printing positioning instrument includes：
One framework, is rectangle structure；
A plurality of clamping bar, is provided with the first V-type surface, and the first V-type surface is formed with the inner surface of the aircraft V-type label
V-type face is corresponding, and the aircraft V-type label is installed in above clamping bar and the flange withstands the bottom surface of the clamping bar；
The clamping bar is respectively fixed at two ends with the support shaft extended along the length direction of the clamping bar, and wherein one end is described
Support shaft is provided with the second V-type surface, the positive and negative handstand of V-type on the V-type on the second V-type surface and the first V-type surface, and two
Two corresponding V-type side difference on V-type surface are parallel, wherein support shaft described in stretches out the frame facet, in the side
It is provided with standing screw；
The leg of frame of left and right two of the framework is respectively equipped with stopper slot corresponding with the support shaft size, wherein on a leg of frame
The stopper slot be provided with horizontal bottom, be provided with the support shaft on the second V-type surface and coordinate with the stopper slot, the stopper slot
The horizontal bottom is fitted with a wherein V-type side on the second V-type surface all the time；
A plurality of clamping bar horizontal distribution and it is parallel to each other；
Two positive stop strips, are pressed on above the clamping bar, and vertical with the clamping bar, are gripped between two positive stop strips described
Aircraft V-type label, front and rear two leg of frame of the framework has mounting groove corresponding with the positive stop strip, the positive stop strip
Two ends are respectively embedded into the mounting groove；
One pressing plate, is provided with mounting hole corresponding with the standing screw, and the standing screw institute is installed on by the mounting hole
Frame facet, the outer end of the standing screw is screwed with clamp nut, and the pressing plate medial surface pushes down the support shaft extension
Go out the end face in outside.
It is 2. according to claim 1 to print positioning instrument, it is characterised in that：The clamping bar is the strip sheet metal component of V-type.
It is 3. according to claim 2 to print positioning instrument, it is characterised in that：Described support shaft one end is provided with fixed block, institute
It is corresponding to the V-structure that the inner surface of the clamping bar is constituted to state fixed-block-architecture (FBA), and the fixed block is embedded in the clamping bar
Two ends, and be provided with screw and be fixed, so as to the support shaft is fixed on into the clamping bar two ends.
4. the printing according to claim 1 or 3 positions instrument, it is characterised in that：The clamp nut is wing nut.
It is 5. according to claim 4 to print positioning instrument, it is characterised in that：Used by the frame size and silk-screen printing
Web plate size is corresponding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710038799.7A CN106739445B (en) | 2017-01-19 | 2017-01-19 | Printing positioning tool for V-shaped label of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710038799.7A CN106739445B (en) | 2017-01-19 | 2017-01-19 | Printing positioning tool for V-shaped label of airplane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106739445A true CN106739445A (en) | 2017-05-31 |
| CN106739445B CN106739445B (en) | 2022-09-23 |
Family
ID=58944046
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710038799.7A Active CN106739445B (en) | 2017-01-19 | 2017-01-19 | Printing positioning tool for V-shaped label of airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106739445B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108214965A (en) * | 2018-02-08 | 2018-06-29 | 常熟市创新陶瓷有限公司 | The clamp for machining and processing method of high powered water pump axis impeller locating platform |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003231237A (en) * | 2002-02-08 | 2003-08-19 | Yamato Koei Seisakusho:Kk | Printing apparatus for curved surface or the like |
| CN201856438U (en) * | 2010-10-27 | 2011-06-08 | 东莞市创智涂装设备工程有限公司 | Progressive printing machine |
| CN204235993U (en) * | 2014-10-24 | 2015-04-01 | 宁波如强模塑有限公司 | A kind of special silk of router cover |
| CN205552362U (en) * | 2016-04-13 | 2016-09-07 | 山东英特力新材料有限公司 | A frock that is used for accurate group of multilayer combined material frame right |
| CN206426629U (en) * | 2017-01-19 | 2017-08-22 | 广州飞机维修工程有限公司 | A kind of printing positioning instrument of aircraft V-type label |
-
2017
- 2017-01-19 CN CN201710038799.7A patent/CN106739445B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003231237A (en) * | 2002-02-08 | 2003-08-19 | Yamato Koei Seisakusho:Kk | Printing apparatus for curved surface or the like |
| CN201856438U (en) * | 2010-10-27 | 2011-06-08 | 东莞市创智涂装设备工程有限公司 | Progressive printing machine |
| CN204235993U (en) * | 2014-10-24 | 2015-04-01 | 宁波如强模塑有限公司 | A kind of special silk of router cover |
| CN205552362U (en) * | 2016-04-13 | 2016-09-07 | 山东英特力新材料有限公司 | A frock that is used for accurate group of multilayer combined material frame right |
| CN206426629U (en) * | 2017-01-19 | 2017-08-22 | 广州飞机维修工程有限公司 | A kind of printing positioning instrument of aircraft V-type label |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108214965A (en) * | 2018-02-08 | 2018-06-29 | 常熟市创新陶瓷有限公司 | The clamp for machining and processing method of high powered water pump axis impeller locating platform |
| CN108214965B (en) * | 2018-02-08 | 2024-03-12 | 常熟市创新陶瓷有限公司 | Machining clamp and machining method for high-power water pump shaft impeller positioning platform |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106739445B (en) | 2022-09-23 |
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