CN106739445B - Printing positioning tool for V-shaped label of airplane - Google Patents
Printing positioning tool for V-shaped label of airplane Download PDFInfo
- Publication number
- CN106739445B CN106739445B CN201710038799.7A CN201710038799A CN106739445B CN 106739445 B CN106739445 B CN 106739445B CN 201710038799 A CN201710038799 A CN 201710038799A CN 106739445 B CN106739445 B CN 106739445B
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- shaped
- frame
- strips
- clamping
- positioning tool
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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
The invention discloses a printing positioning tool for an airplane V-shaped label, which is provided with a frame, clamping strips, limiting strips and a pressing plate, wherein the airplane V-shaped label is clamped on the clamping strips, the left frame edge and the right frame edge of the frame are respectively provided with a limiting groove, the clamping strips are arranged on the frame through supporting shafts at two ends, a plurality of clamping strips are horizontally distributed and are parallel to each other, two limiting strips are pressed on the clamping strips, the airplane V-shaped label is tightly clamped between the two limiting strips, the pressing plate is fixed on the side surface of the frame, and the inner side surface of the pressing plate presses the end surface of the supporting shaft extending out of the outer side.
Description
Technical Field
The invention relates to a printing tool, in particular to a printing positioning tool for a V-shaped label of an airplane.
Technical Field
In the process of printing, the printing ink is transferred to a printing stock (paper, ceramic and the like) through holes of a screen plate by certain pressure to form images or characters, generally, only one workbench plane is needed for operation, but when the surface with a special shape is printed, due to the process characteristics of the screen printing, the printing operation cannot be performed simply or strictly on the position limitation, and the parts are generally supported by foam below the parts. However, the B787 aircraft seat number label is a V-shaped label, and when two surfaces of the label are printed, due to the reasons of inaccurate positioning, unstable placement and the like, the operation difficulty is high, the rejection rate is high, and after one surface is printed, the other surface can be printed only after ink is dried, so that the working efficiency is seriously affected.
Disclosure of Invention
The invention aims to solve the technical problem of providing a printing positioning tool for a V-shaped label of an airplane, which has a simple structure and high printing efficiency and realizes batch printing.
To solve the technical problems, the technical scheme adopted by the invention is as follows:
the utility model provides a printing positioning tool of aircraft V type sign, aircraft V type sign is the rectangular sheet metal component of V type, and the both ends limit of V type is equipped with the turn-ups of bending inwards, and characterized by prints positioning tool and includes:
a frame with a rectangular structure;
the aircraft V-shaped sign is clamped on the clamping strips, and the flanges prop against the bottom surfaces of the clamping strips;
two ends of the clamping strip are respectively fixed with a support shaft extending along the length direction of the clamping strip, wherein the support shaft at one end is provided with a second V-shaped surface, the V shape of the second V-shaped surface is inverted with the V shape of the first V-shaped surface, two corresponding V-shaped edges of the two V-shaped surfaces are respectively parallel, one support shaft extends out of the side surface of the frame, and the side surface is provided with a fixing screw rod;
the left frame side and the right frame side of the frame are respectively provided with a limiting groove corresponding to the size of the supporting shaft, the limiting groove on one frame side is provided with a horizontal bottom surface, the supporting shaft with a second V-shaped surface is matched with the limiting groove, and the horizontal bottom surface of the limiting groove is always attached to one V-shaped side of the second V-shaped surface;
the clamping strips are horizontally distributed and are mutually parallel;
the two limiting strips are pressed on the clamping strips and are perpendicular to the clamping strips, the V-shaped airplane label is tightly clamped between the two limiting strips, mounting grooves corresponding to the limiting strips are respectively formed in the front frame edge and the rear frame edge of the frame, and two ends of the limiting strips are respectively embedded into the mounting grooves;
and the pressing plate is provided with a mounting hole corresponding to the fixing screw rod and is mounted on the side face of the frame where the fixing screw rod is located through the mounting hole, the outer end of the fixing screw rod is screwed with a compression nut, and the inner side face of the pressing plate presses the end face of the support shaft extending out of the outer side.
The clamping strip is a V-shaped long sheet metal part.
One end of the supporting shaft is provided with a fixing block, the structure of the fixing block corresponds to a V-shaped structure formed by the inner surfaces of the clamping strips, the fixing blocks are embedded into the two ends of the clamping strips and are fixed by screws, and therefore the supporting shaft is fixed at the two ends of the clamping strips.
The compression nut is a butterfly nut.
The size of the frame corresponds to the size of a screen plate used for screen printing.
Compared with the prior art, the invention has the following beneficial effects:
1. the V-shaped label of the airplane is clamped on the clamping strip, the clamping strip is limited through the frame, and the left and right movement of the V-shaped label of the airplane is limited through the two limiting strips, so that the V-shaped label of the airplane is positioned, and the structure of the V-shaped label of the airplane is simple.
2. After printing of one face of aircraft V type sign is accomplished, loosen spacing, loosen gland nut, rotate clamping strip for the face of aircraft V type sign that does not print faces up, and print, realized carrying out continuous printing to the surface of aircraft V type sign, and no longer need wait that printing ink dries the back just can print the another side, improved printing efficiency.
3. A plurality of aircraft V type signs can embolia on a clamping strip, and many clamping strips are installed on the frame, can print these aircraft V type signs simultaneously, have realized printing in batches, have also improved efficiency.
Drawings
FIG. 1 is a schematic perspective view of the present invention;
FIG. 2 is a schematic perspective view of an aircraft V-tag;
FIG. 3 is a schematic perspective view of the frame of the present invention;
FIG. 4 is a perspective view showing an assembling structure of the clip holding strip and the supporting shaft according to the present invention;
FIG. 5 is a perspective view of the aircraft V-tag card in the assembled configuration shown in FIG. 4;
FIG. 6 is a schematic side view of the mounting structure shown in FIG. 4, showing the structural relationship of the first V-shaped surface and the second V-shaped surface.
The reference numerals in the drawings mean:
1-a frame; 2-a limit strip; 3-airplane V-shaped signs; 4, clamping strips are installed; 5, pressing a plate; 6, pressing a nut; 7-fixing the screw rod; 8-a limiting groove; 9-flanging; 10-mounting grooves; 11-horizontal bottom surface; 12-a first V-shaped surface; 13-supporting the shaft; 14-a second V-shaped surface; and 15, fixing blocks.
Detailed Description
The invention is further described below with reference to examples.
As shown in figures 1 and 2, the invention is provided with a frame 1, seven clamping strips 4, two limiting strips 2 and a pressing plate 7, a V-shaped airplane tag 3 to be printed is a V-shaped strip sheet metal part, and two inward-bent flanges 9 are arranged at two end edges of the V shape.
The frame 1 is a rectangular structure formed by splicing four rectangular plates, and the size of the rectangular structure corresponds to that of a screen plate used for screen printing; the clamping strip 4 is a V-shaped strip sheet metal part, the surface of the clamping strip is a first V-shaped surface 12, the first V-shaped surface 12 corresponds to a V-shaped surface formed by the inner surface of the airplane V-shaped label 3, the airplane V-shaped label 3 is clamped on the clamping strip 4, the turned edge 9 props against the bottom surface of the clamping strip 4, and therefore the airplane V-shaped label 3 is clamped on the clamping strip 4, and 3 airplane V-shaped labels can be clamped on one clamping strip. The airplane V-shaped label 3 is clamped into the side surface of the clamping strip 4.
Supporting shafts 13 extending along the length direction of the clamping strip are respectively fixed at two ends of the clamping strip 4, wherein the supporting shaft 13 at one end is provided with a second V-shaped surface 14, as shown in fig. 6, the V shape of the second V-shaped surface is inverted from the V shape of the first V-shaped surface, the two corresponding V-shaped edges of the two V-shaped surfaces are respectively parallel, and the supporting shaft at the other end is cylindrical; one of the support shafts 13 extends out of the side 1 of the frame, on which side the fixing screw 7 is arranged. The fixing mode of the supporting shaft 13 is as follows: the fixing block 15 is arranged at one end of the supporting shaft 13, the structure of the fixing block 15 corresponds to the V-shaped structure formed by the inner surfaces of the clamping strips 4, the fixing block 15 is embedded into the two ends of the clamping strips 4 and is fixed by screws, and therefore the supporting shaft 13 is fixed at the two ends of the clamping strips 4.
The left frame side and the right frame side of the frame are respectively provided with a limiting groove 8 corresponding to the size of the supporting shaft 13, the limiting groove 8 on one frame side is provided with a horizontal bottom surface 11, the supporting shaft provided with a second V-shaped surface 14 is matched with the limiting groove, and the horizontal bottom surface 11 of the limiting groove is always attached to one V-shaped side of the second V-shaped surface 14. Because the V shape of the second V-shaped surface 14 and the V shape of the first V-shaped surface 12 are inverted from each other, and the two V-shaped sides of the two V-shapes are parallel to each other, when the horizontal bottom surface 11 of the limiting groove is attached to one of the V-shaped sides of the second V-shaped surface 14, the V-shaped side of the clamping strip 4 faces upward and is in a horizontal state, and thus the plane V-shaped sign 3 also faces upward and is in a horizontal state, so that the upward side of the plane V-shaped sign 3 can be printed. Seven clamping strips 4 horizontal distribution and parallel to each other, the face that the clamping strip was up all is at same horizontal plane, conveniently prints in batches aircraft V type sign 3.
The pressing plate 5 is provided with a mounting hole corresponding to the fixing screw 7 and is mounted on the side face of the frame 1 where the fixing screw 7 is located through the mounting hole, the outer end of the fixing screw 7 is screwed with the compression nut 6, the compression nut 6 is a butterfly nut, a user can directly adjust the fixing screw by hand, the inner side face of the pressing plate 5 presses the end face of the supporting shaft 13 extending out of the outer side, the clamping strip 4 is pressed on the frame 1, and the clamping strip 4 is prevented from shifting when the printing positioning tool is moved.
When the airplane V-shaped sign is used, the airplane V-shaped sign 3 is clamped on the clamping strips 4, the clamping strips 4 are arranged on the limiting grooves 8 of the frame 1, the horizontal bottom surfaces 11 of the limiting grooves are attached to one V-shaped edge of the second V-shaped surface 14, one surface of the airplane V-shaped sign 3 faces upwards and is in a horizontal state, after the seven clamping strips 4 are installed, the left and right movement of the airplane V-shaped sign 3 is limited through the two limiting strips 2, the compression nut 6 is screwed tightly, the positioning work is completed, and the upward surface of the airplane V-shaped sign 3 is printed; after the plane is printed, the limiting strip 2 is loosened, the compression nut 6 is loosened, the clamping strip 4 is rotated, the horizontal bottom surface 11 of the limiting groove is attached to the other V-shaped edge of the second V-shaped surface 14, the limiting strip 2 is pressed again, the compression nut 6 is screwed, the other plane of the airplane V-shaped label 3 is printed, and finally the printing work of the batch of airplane V-shaped labels 3 is completed.
Claims (5)
1. The utility model provides a printing positioning tool of aircraft V type sign, aircraft V type sign is the rectangular sheet metal component of V type, and the both ends limit of V type is equipped with the turn-ups of bending inwards, its characterized in that, printing positioning tool includes:
a frame with a rectangular structure;
the aircraft V-shaped sign is clamped on the clamping strips, and the flanges prop against the bottom surfaces of the clamping strips;
supporting shafts extending along the length direction of the clamping strip are fixed at two ends of the clamping strip respectively, a second V-shaped surface is arranged on the supporting shaft at one end, the V shape of the second V-shaped surface is inverted from the V shape of the first V-shaped surface, two corresponding V-shaped edges of the two V-shaped surfaces are parallel respectively, one supporting shaft extends out of the side face of the frame, and a fixing screw rod is arranged on the side face;
the left frame side and the right frame side of the frame are respectively provided with a limiting groove corresponding to the size of the supporting shaft, the limiting groove on one frame side is provided with a horizontal bottom surface, the supporting shaft provided with the second V-shaped surface is matched with the limiting groove, and the horizontal bottom surface of the limiting groove is always attached to one V-shaped side of the second V-shaped surface;
the clamping strips are horizontally distributed and are mutually parallel;
the two limiting strips are pressed on the clamping strip and are perpendicular to the clamping strip, the V-shaped airplane label is tightly clamped between the two limiting strips, mounting grooves corresponding to the limiting strips are formed in the front frame edge and the rear frame edge of the frame respectively, and two ends of the limiting strips are embedded into the mounting grooves respectively;
and the pressing plate is provided with a mounting hole corresponding to the fixing screw rod, the pressing plate is mounted on the side face of the frame where the fixing screw rod is located through the mounting hole, a compression nut is screwed at the outer end of the fixing screw rod, and the inner side face of the pressing plate presses the end face of the support shaft extending out of the outer side.
2. The print positioning tool of claim 1, wherein: the clamping strip is a V-shaped long sheet metal part.
3. The print positioning tool of claim 2, wherein: one end of the supporting shaft is provided with a fixing block, the structure of the fixing block corresponds to a V-shaped structure formed by the inner surfaces of the clamping strips, the fixing blocks are embedded into the two ends of the clamping strips and fixed by screws, and therefore the supporting shaft is fixed at the two ends of the clamping strips.
4. The print positioning tool of claim 1 or 3, wherein: the compression nut is a butterfly nut.
5. The print positioning tool of claim 4, wherein: the size of the frame corresponds to the size of a screen plate used for screen printing.
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 CN106739445A (en) | 2017-05-31 |
| CN106739445B true CN106739445B (en) | 2022-09-23 |
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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 |
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| CN (1) | CN106739445B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
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 |
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| Publication number | Publication date |
|---|---|
| CN106739445A (en) | 2017-05-31 |
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