CN207141428U - A kind of adjustable aircraft cloth hole Moulage device of multimode - Google Patents
A kind of adjustable aircraft cloth hole Moulage device of multimode Download PDFInfo
- Publication number
- CN207141428U CN207141428U CN201721113632.4U CN201721113632U CN207141428U CN 207141428 U CN207141428 U CN 207141428U CN 201721113632 U CN201721113632 U CN 201721113632U CN 207141428 U CN207141428 U CN 207141428U
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- China
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- die body
- cloth hole
- pedestal
- connecting rod
- collar
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- Withdrawn - After Issue
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Abstract
A kind of adjustable aircraft cloth hole Moulage device of multimode, including：Baffle plate, pedestal, the collar, stamping head, ink feeding system and bar-link drive.During use, the connecting rod for driving N number of uniform intervals on circumferencial direction to arrange by bar-link drive is protruding, afterwards along propelled longitudinally pedestal, under the guide effect along sheet material of baffle plate, collar opposite base rotates, the stamping head that each outwardly directed connecting rod head end is fixed is rolled by cross stamp in plate surface, so as to form the printing of the equal cloth hole mark of spacing.The cloth hole mark position of printing is accurate, requires low to the technical merit of operator, improves aircraft workpiece maintenance effect and quality.
Description
Technical field
It the utility model is related to aircraft maintenance tool field, and in particular to a kind of adjustable aircraft cloth hole stamp dress of multimode
Put.
Background technology
During aircraft maintenance, after typically using excision for the crackle on body covering, perforation, heavy corrosion region
The mode for installing sticking patch additional places under repair.Sticking patch is connected with body covering, after needing the cloth hole drillings such as spacing line-spacing as requested
The connection of the fasteners such as rivet, high locked bolts is installed.
Above-mentioned cloth hole technique, using measurer range estimation manual drawing, to the level of skill of worker and is sentenced typically using worker
Disconnected power requires high, and the possibility for human factor error occur is big.In addition it is above-mentioned when batch machining repairs workpiece and part
Mode easily causes the workpiece random error increase of processing, and part specification and uniformity are deteriorated, gently then influence maintenance effect and
Workpiece quality, it is heavy then workpiece is produced form error, stress deformation etc. has a strong impact on aircraft navigation safety.
Utility model content
The utility model is in order to overcome the shortcomings of above technology, there is provided one kind improve maintenance convenience and operating efficiency,
The adjustable aircraft cloth hole Moulage device of the high multimode of cloth hole precision simultaneously.
Technical scheme is used by the utility model overcomes its technical problem：
A kind of adjustable aircraft cloth hole Moulage device of multimode, including：
Baffle plate, is vertically arranged at sheet material outboard end, and the outer face of the baffle plate medial surface and sheet material is slidably matched；
Pedestal, it is arranged at baffle plate upper end；
The collar, it is rotatablely installed by bearing in pedestal, along the circumferential direction uniform intervals are provided with some lead to the collar
Xiang Kong, connecting rod vertical sliding are plugged in pilot hole；
Stamping head, the top of connecting rod is installed on, the cross stamp of outwardly convex is provided with the stamping head upper surface；
Ink feeding system, it is arranged in stamping head, for ink to be transferred into cross stamp；And
Bar-link drive, be arranged in the collar, for drive the connecting rod that N number of uniform intervals on circumferencial direction are set to
Overhang until cross stamp is in contact with sheet material upper surface.
Above-mentioned bar-link drive include rotating be arranged in the collar and the cylindrical die body with collar same axis and
The knob I of die body outboard end is arranged at, along the circumferential direction uniform intervals are provided with some grooves to the die body, and each two is adjacent
Die body outer surface between groove forms die body outer rim, and the connecting rod lower end is provided with bulb, and spring I is set on connecting rod, institute
The upper end of spring I to be stated to be in contact with collar medial surface, its lower end is in contact with die body outer surface, when spring I is in free state,
In bulb insertion groove.
Above-mentioned ink feeding system includes the slot being arranged in stamping head and the fibre for storing ink being plugged in slot
Felt is tieed up, the fibrofelt is in contact with cross stamp.
In order to facilitate adjustment position, in addition to horizontally disposed locating retainer, the upper locating retainer is along length side
There is slide opening I to horizontally disposed respectively and be vertically provided with slide opening II, between the upper end edge longitudinal direction of the baffle plate
Every being provided with some screwed holes II, the pedestal is secured by bolts in the front end of retainer, and baffle plate is plugged in slide opening II, rotation
Button II is combined in screwed hole II after passing through slide opening I.
In order to improve operation ease, in addition to the horizontal handle for being fixed on pedestal outboard end.
For the ease of assembling, said base is made up of semicircular semicircular ring I and semicircular semicircular ring II, the semicircle
The medial extremity of ring II is provided with the cylinder bayonet lock of projection, and the medial extremity of semicircular ring I is provided with the bayonet lock corresponding with cylinder bayonet lock
Groove, counter sink is provided with the semicircular ring I, screwed hole I is provided with the semicircular ring II, semicircular ring II passes through cylinder bayonet lock
The pedestal for forming annular in bayonet lock groove with semicircular ring I is fastened on, screw is combined in screwed hole I after passing through counter sink.
In order to improve guidance quality, above-mentioned baffle plate lower end is horizontally disposed gib head, and the gib head connects with the baseplane of sheet material
Touch.
In order to improve the scope of application, above-mentioned die body has N number of, and N is the natural number more than or equal to 2, and each die body is same vertically
Axle is set, and the groove number that along the circumferential direction uniform intervals are set on each die body is different, and screw rod is coaxially connected with die body,
Knob III is rotatablely equipped with the pedestal, the knob III screws with screw rod to be connected, and spring II is set on screw rod, its front end
It is in contact with die body, its rear end is in contact with knob III.
In order to improve comfortableness, above-mentioned handle outer sheath is equipped with handle sleeve made of elastomeric material.
Further, above-mentioned cross stamp is made of high osmosis elastomeric material.
The beneficial effects of the utility model are：In use, driven by bar-link drive N number of uniform on circumferencial direction
Spaced apart connecting rod is protruding, and afterwards along propelled longitudinally pedestal, under the guide effect along sheet material of baffle plate, the collar is relative
Pedestal is rotated, and the stamping head that each outwardly directed connecting rod head end is fixed is rolled by cross stamp in plate surface, so as to shape
The printing of the cloth hole mark equal into spacing.The cloth hole mark position of printing is accurate, requires low to the technical merit of operator, carries
High aircraft workpiece maintenance effect and quality.
Brief description of the drawings
Fig. 1 is dimensional structure diagram of the present utility model；
Fig. 2 is stereochemical structure exploded perspective view of the present utility model；
In figure, the sheet material 8. of 1. knob, I 2. die body, 3. semicircular ring, I 4. semicircular ring, II 5. handle sleeve, 6. screw 7. is kept off
The cross stamp of 14. fibrofelt of plate 9. locating retainer, 10. slide opening, I 11. knob, II 12. connecting rod, 13. stamping head 15.
16. the collar 24. of 22. spring of spring I 17. bulb, 18. die body outer rim, 19. groove, 20. screw rod, 21. slot II 23. is led
To the knob III 32. of hole 25. bearing, 26. bayonet lock groove, 27. cylinder bayonet lock, 28. counter sink, 29. screwed hole, I 30. handle 31.
The gib head of II 33. screwed hole of slide opening II 34..
Embodiment
Below in conjunction with the accompanying drawings 1, accompanying drawing 2 is described further to the utility model.
A kind of adjustable aircraft cloth hole Moulage device of multimode, including：Baffle plate 8, it is vertically arranged at the outboard end of sheet material 7, baffle plate 8
The outer face of medial surface and sheet material 7 is slidably matched；Pedestal, it is arranged at the upper end of baffle plate 8；The collar 23, it is rotatablely installed by bearing 25
In pedestal, along the circumferential direction uniform intervals are provided with some pilot holes 24 to the collar 23, and the vertical sliding of connecting rod 12 is plugged in guiding
In hole 24；Stamping head 13, the top of connecting rod 12 is installed on, the cross stamp of outwardly convex is provided with the upper surface of stamping head 13
15；Ink feeding system, it is arranged in stamping head 13, for ink to be transferred into cross stamp 15；And bar-link drive, if
It is placed in the collar 23, for driving the connecting rod 12 that N number of uniform intervals on circumferencial direction are set protruding until cross stamp
15 are in contact with the upper surface of sheet material 7.In use, N number of uniform intervals on circumferencial direction are driven to arrange by bar-link drive
Connecting rod 12 it is protruding, afterwards along propelled longitudinally pedestal, under the guide effect along sheet material 7 of baffle plate 8, the collar 23 is with respect to base
Seat rotates, the stamping head 13 that each outwardly directed head end of connecting rod 12 is fixed by cross stamp 15 in the surface scrolls of sheet material 7, from
And form the printing of the equal cloth hole mark of spacing.The cloth hole mark position of printing is accurate, the technical merit requirement to operator
It is low, improve aircraft workpiece maintenance effect and quality.
Bar-link drive can be following structure, it include rotating be arranged in the collar 23 and with the same axis of the collar 23
The die body 2 of cylinder and be arranged at the knob I 1 of the outboard end of die body 2, die body 2 along the circumferential direction uniform intervals be provided with it is some
Groove 19, the outer surface of die body 2 between the adjacent groove 19 of each two form die body outer rim 18, and the lower end of connecting rod 12 is provided with bulb
17, spring I 16 is set on connecting rod 12, and the upper end of spring I 16 is in contact with the medial surface of the collar 23, its lower end and the appearance of die body 2
Face is in contact, and when spring I 16 is in free state, bulb 17 is inserted in groove 19.Die body 2 is revolved by turn knob I 1
Turn, so that each stamping head 13 that the bulb 17 of the corresponding lower end of connecting rod 12 is caught in groove 19, it is necessary to marking hole is right
In the bulb 17 of the lower end of connecting rod 12 be in contact with the die body outer rim 18 of die body 2, now connecting rod 12 is pushed outwards dynamic, spring I 16
Compression.Spring I 16 can be with the returning quickly of drive link 12.
Ink feeding system can be following structure, and it includes the slot 21 being arranged in stamping head 13 and is plugged in slot 21
In the fibrofelt 14 for storing ink, fibrofelt 14 is in contact with cross stamp 15, can be by fibrofelt when no ink
14 take out from slot 21, make to fill thereon after ink again insertable into slot 21, convenient to recycle.Above-mentioned cross stamp 15
It is made of high osmosis elastomeric material, therefore it can facilitate the ink absorption on fibrofelt 14.
Horizontally disposed locating retainer 9 can also be included, upper locating retainer 9 is distinguished in the horizontal direction along its length
It is provided with slide opening I 10 and is vertically provided with slide opening II 32, the upper end of baffle plate 8 is longitudinally spaced is provided with some spiral shells
Pit II 33, pedestal are secured by bolts in the front end of retainer 9, and baffle plate 8 is plugged in slide opening II 32, and knob II 11 is worn
It is combined on after crossing slide opening I 10 in screwed hole II 33.By the way that knob II 11 to be screwed to the dry screwed hole II 33 in different height
The purpose of regulation whole device height, the convenient sheet material 7 for being adapted to different-thickness specification can be realized.After knob II 11 are unclamped,
Locating retainer 9 can be slid laterally by the opposing flaps 8 of slide opening II 32, while knob II 11 is sliding in slide opening I 10
It is dynamic, the horizontal adjustment of stamping head 13 is realized, facilitates its regulation to the cloth hole mark position specified.Further increase operation just
Profit.
Further, in addition to level is fixed on the handle 30 of pedestal outboard end.The outer sheath of handle 30 is equipped with elastomeric material
Manufactured handle sleeve 5.By handle 30 propelled longitudinally pedestal can be made to improve the convenience that operator operates, rubber material when moving ahead
Handle sleeve 5 can improve gripping feel made of material, further improve the comfort level of operation.
Pedestal can be made up of semicircular semicircular ring I 3 and semicircular semicircular ring II 4, the medial extremity of semicircular ring II 4
The cylinder bayonet lock 27 of projection is provided with, the medial extremity of semicircular ring I 3 is provided with the bayonet lock groove 26 corresponding with cylinder bayonet lock 27, semicircle
Counter sink 28 is provided with ring I 3, screwed hole I 29 is provided with semicircular ring II 4, semicircular ring II 4 is detained by cylinder bayonet lock 27
Together in the pedestal for forming annular in bayonet lock groove 26 with semicircular ring I 3, screw 6 is combined on screwed hole I 29 after passing through counter sink 28
In.Because semicircular ring I 3 and semicircular ring II 4 are connected by cylinder bayonet lock 27 with bayonet lock groove 26, therefore semicircular ring I 3 can phase
Semicircular ring II 4 is overturn and opened, therefore is easy to the installation of internal part, the convenience of assembling is improved, passes through after installing
Tightening screw 6 can fix semicircular ring I 3 and the phase of semicircular ring II 4, and screw 6 is located in counter sink 28, overall appearance.
Preferably, the lower end of baffle plate 8 is horizontally disposed gib head 34, and gib head 34 is in contact with the baseplane of sheet material 7.Due to gib head
34 are hooked on the lower end of sheet material 7, therefore when baffle plate 8 is walked along the outward flange of sheet material 7, gib head 34 can play further guiding
Effect, make the traveling of whole device more stable.
Further, die body 2 can have N number of, and N is the natural number more than or equal to 2, and each die body 2 is coaxially disposed vertically,
The number of groove 19 that along the circumferential direction uniform intervals are set on each die body 2 is different, and screw rod 20 and die body 2 are coaxially connected,
Knob III 31 is rotatablely equipped with pedestal, knob III 31 is screwed with screw rod 20 and is connected, and spring II 22 is set on screw rod 20,
Its front end is in contact with die body 2, and its rear end is in contact with knob III 31.Being rotated by turn knob III 31 by screw rod 20 makes
Each transverse movement in the collar 23 of die body 2, so that different die bodys 2 drives each connecting rod 12, due on different die bodys 2
Spaced 19 numbers of groove are different, so that the number of the connecting rod 12 of driving is different, reach the cloth on sheet material 7 of stamping head 13
The spacing of hole mark printing realizes the adjustment of different size.When die body 2 is to medial motion, spring II 22 compresses, when reverse rotation
When rotating button III 31, spring II 22 promotes the returning quickly of die body 2.
Claims (10)
- A kind of 1. adjustable aircraft cloth hole Moulage device of multimode, it is characterised in that including：Baffle plate（8）, it is vertically arranged at sheet material（7）Outboard end, the baffle plate（8）Medial surface and sheet material（7）Outer face slide match somebody with somebody Close；Pedestal, it is arranged at baffle plate（8）Upper end；The collar（23）, pass through bearing（25）It is rotatablely installed in pedestal, the collar（23）Along the circumferential direction uniform intervals are set There are some pilot holes（24）, connecting rod（12）Vertical sliding is plugged in pilot hole（24）In；Stamping head（13）, it is installed on connecting rod（12）Top, the stamping head（13）The ten of outwardly convex are provided with upper surface Word stamp（15）；Ink feeding system, it is arranged at stamping head（13）In, for ink to be transferred into cross stamp（15）On；AndBar-link drive, it is arranged at the collar（23）In, for the connecting rod for driving N number of uniform intervals on circumferencial direction to set （12）It is protruding until cross stamp（15）With sheet material（7）Upper surface is in contact.
- 2. the adjustable aircraft cloth hole Moulage device of multimode according to claim 1, it is characterised in that：The connecting rod driving machine Structure is arranged at the collar including rotation（23）The interior and and collar（23）The cylindrical die body of same axis（2）And it is arranged at die body （2）The knob I of outboard end（1）, the die body（2）Along the circumferential direction uniform intervals are provided with some grooves（19）, each two phase Adjacent groove（19）Between die body（2）Outer surface forms die body outer rim（18）, the connecting rod（12）Lower end is provided with bulb （17）, spring I（16）It is set in connecting rod（12）On, the spring I（16）Upper end and the collar（23）Medial surface is in contact, its lower end With die body（2）Outer surface is in contact, when spring I（16）During in free state, bulb（17）Insert groove（19）In.
- 3. the adjustable aircraft cloth hole Moulage device of multimode according to claim 1, it is characterised in that：The ink feeding system bag Include and be arranged at stamping head（13）Interior slot（21）And it is plugged in slot（21）In the fibrofelt for storing ink（14）, institute State fibrofelt（14）With cross stamp（15）It is in contact.
- 4. the adjustable aircraft cloth hole Moulage device of multimode according to claim 1, it is characterised in that：Also include horizontally disposed Locating retainer（9）, the upper locating retainer（9）It is horizontally disposed respectively along its length to have slide opening I（10）With And vertically it is provided with slide opening II（32）, the baffle plate（8）Upper end longitudinally spaced be provided with some screwed holes II （33）, the pedestal is secured by bolts in retainer（9）Front end, baffle plate（8）It is plugged in slide opening II（32）In, knob II （11）Through slide opening I（10）After be combined on screwed hole II（33）In.
- 5. the adjustable aircraft cloth hole Moulage device of multimode according to claim 1, it is characterised in that：Also include horizontal fixed In the handle of pedestal outboard end（30）.
- 6. the adjustable aircraft cloth hole Moulage device of multimode according to claim 1, it is characterised in that：The pedestal is by semicircle The semicircular ring I of shape（3）And semicircular semicircular ring II（4）Form, the semicircular ring II（4）Medial extremity is provided with the cylinder of projection Bayonet lock（27）, the semicircular ring I（3）Medial extremity is provided with and cylinder bayonet lock（27）Corresponding bayonet lock groove（26）, the semicircle Ring I（3）On be provided with counter sink（28）, the semicircular ring II（4）On be provided with screwed hole I（29）, semicircular ring II（4）Pass through circle Post bayonet lock（27）It is fastened on bayonet lock groove（26）In with semicircular ring I（3）Form the pedestal of annular, screw（6）Through counter sink （28）After be combined on screwed hole I（29）In.
- 7. the adjustable aircraft cloth hole Moulage device of multimode as claimed in any of claims 1 to 6, it is characterised in that： The baffle plate（8）Lower end is horizontally disposed gib head（34）, the gib head（34）With sheet material（7）Baseplane be in contact.
- 8. the adjustable aircraft cloth hole Moulage device of multimode according to claim 2, it is characterised in that：The die body（2）There is N Individual, N is natural number more than or equal to 2, each die body（2）It is coaxially disposed vertically, each die body（2）On it is along the circumferential direction uniform Spaced groove（19）Number is different, screw rod（20）With die body（2）It is coaxially connected, it is rotatablely equipped with the pedestal Knob III（31）, the knob III（31）With screw rod（20）Screw connection, spring II（22）It is set in screw rod（20）On, its front end With die body（2）It is in contact, its rear end and knob III（31）It is in contact.
- 9. the adjustable aircraft cloth hole Moulage device of multimode according to claim 5, it is characterised in that：The handle（30）Outside Side is set with handle sleeve made of elastomeric material（5）.
- 10. the adjustable aircraft cloth hole Moulage device of multimode according to claim 1, it is characterised in that：The cross stamp （15）It is made of high osmosis elastomeric material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721113632.4U CN207141428U (en) | 2017-09-01 | 2017-09-01 | A kind of adjustable aircraft cloth hole Moulage device of multimode |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721113632.4U CN207141428U (en) | 2017-09-01 | 2017-09-01 | A kind of adjustable aircraft cloth hole Moulage device of multimode |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207141428U true CN207141428U (en) | 2018-03-27 |
Family
ID=61676963
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721113632.4U Withdrawn - After Issue CN207141428U (en) | 2017-09-01 | 2017-09-01 | A kind of adjustable aircraft cloth hole Moulage device of multimode |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207141428U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107585325A (en) * | 2017-09-01 | 2018-01-16 | 山东太古飞机工程有限公司 | A kind of adjustable aircraft cloth hole Moulage device of multimode |
-
2017
- 2017-09-01 CN CN201721113632.4U patent/CN207141428U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107585325A (en) * | 2017-09-01 | 2018-01-16 | 山东太古飞机工程有限公司 | A kind of adjustable aircraft cloth hole Moulage device of multimode |
| CN107585325B (en) * | 2017-09-01 | 2023-04-14 | 山东太古飞机工程有限公司 | Multi-mode adjustable airplane hole distribution die device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20180327 Effective date of abandoning: 20230414 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20180327 Effective date of abandoning: 20230414 |