CN109127879A - A kind of aircraft solution component continuous punching device - Google Patents
A kind of aircraft solution component continuous punching device Download PDFInfo
- Publication number
- CN109127879A CN109127879A CN201810976695.5A CN201810976695A CN109127879A CN 109127879 A CN109127879 A CN 109127879A CN 201810976695 A CN201810976695 A CN 201810976695A CN 109127879 A CN109127879 A CN 109127879A
- Authority
- CN
- China
- Prior art keywords
- upper housing
- solution component
- continuous punching
- piston
- lower case
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D28/00—Shaping by press-cutting; Perforating
- B21D28/24—Perforating, i.e. punching holes
- B21D28/34—Perforating tools; Die holders
Abstract
The invention discloses a kind of aircraft solution component continuous punching devices, including upper housing, lower case, attachment base, pedestal, punch mechanism, displacement mechanism, driving mechanism and fixed mechanism, it is connected between the upper housing and lower case by attachment base, the pedestal is fixed on the bottom of lower case, the punch mechanism and driving structure are arranged in upper housing, and institute's displacement mechanism and fixed mechanism are arranged in lower case.This continuous punching device is using cylinder as power mechanism, and continuous punching by the mobile realization of workbench to solution component has movement speed very fast, generates the biggish feature of punching press strength；Platform is worked at the same time equipped with fixed mechanism, drives firm block to consolidate component is solved by screw rod, the operation is stable, the punching efficiency of plate is substantially increased, realization is worked continuously, and labour is saved, high degree of automation, and can adapt to the limitation to made by electricity usage of some special occasions.
Description
Technical field
The present invention relates to aircraft package technique fields, particularly relate to a kind of aircraft solution component continuous punching device.
Background technique
During transport is re-assemblied to strange land after rolling over solution to aircraft, need in all kinds of connecting elements or type
Installation fastener is after carrying out cloth hole and drilling molding on material to complete reinstalling for folding solution component.To all kinds of connecting elements or
If perhaps for slot using brill or Milling Machining, heavy workload, working efficiency is low, and dangerous for profile aperture.Using punching
Mould processing, can be improved productivity, and stable product quality, highly-safe.
But there are some defects, only one punching head of existing piercing die, a punching presses for piercing die in the prior art
A hole can only be rushed, if needing repetitive operation one after another to rush at punching press continuously multiple holes on connection member or profile
Hole acts the punch forming that could complete multiple holes, and when carrying out the punching press of continuous aperture, metal material easily deforms, punching
The position in hole is inaccurate, causes the ratio of briquetting in hole lower, causes defect ware, wastes material, and then increase cost.
Summary of the invention
In view of the above deficiencies, the present invention provides a kind of aircraft solution component continuous punching devices.
The present invention is achieved by the following technical solutions: a kind of aircraft solution component continuous punching device, including upper housing,
Lower case, attachment base, pedestal, punch mechanism, displacement mechanism, driving mechanism and fixed mechanism, the upper housing and lower case it
Between connected by attachment base, the pedestal is fixed on the bottom of lower case, and the punch mechanism and driving structure are arranged in upper casing
In vivo, institute's displacement mechanism and fixed mechanism are arranged in lower case；The punch mechanism include upper connecting rod, lower link, spring,
Formed punch, drilling rod, piston rod, air inlet, air outlet valve, cylinder and piston, the inner wall of the upper end connection upper housing of the upper connecting rod, under
End is separately connected piston rod and lower link；The upper end of the lower link connects piston rod, and lower end connects formed punch；The piston rod
Free end connects piston, and the piston is mounted in cylinder, and the side of upper housing is arranged in the cylinder；The casing wall of the cylinder
On be provided with air outlet valve, the air outlet valve connects air inlet；The lower end of the formed punch is provided with spring, and the lower end of the spring connects
Stacks, the drilling rod are pierced by from attachment base；The driving mechanism include motor, connecting shaft, driving wheel, driven wheel, connecting rod,
Axle sleeve and driving gear, the motor are fixed in upper housing, and the power output end of motor, the master is arranged in the connecting shaft
Driving wheel is fixedly connected with connecting shaft；The connecting shaft is installed in upper housing again by axle sleeve, and the upper end is provided with nibbles with driving wheel
The driven wheel of conjunction, lower end are provided with driving gear.
Institute's displacement mechanism includes that workbench, a pair of of fixture block and rack gear, the pair of fixture block are separately positioned on lower case
On the inner wall of two sides, card slot is provided on the pair of fixture block, the workbench is slidably connected by card slot and a pair of of fixture block, described
Rack gear is arranged on the table, engages with driving gear.
The fixed mechanism includes a pair of of lead screw and a pair of of feed screw nut, wherein and the lead screw is mounted on feed screw nut,
The lead screw spiral shell is arranged on workbench by link block.
The upper and lower ends of the piston are provided with sealing ring, and the piston is connect by sealing ring with cylinder slide.
The driving wheel and driven wheel are bevel type gear.
The diameter of the spring is greater than drill pipe diameter.
The link block is flexibly connected with workbench.
The usefulness of the invention is that this continuous punching device passes through the movement of workbench using cylinder as power mechanism
It realizes the continuous punching to solution component, has movement speed very fast, generate the biggish feature of punching press strength；It works at the same time and is set on platform
There is fixed mechanism, drives firm block to consolidate component is solved by screw rod, the operation is stable substantially increases the punching efficiency of plate,
Realization is worked continuously, and saves labour, high degree of automation, and can adapt to some special occasions to made by electricity usage
Limitation.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention.
Fig. 2 is the structural schematic diagram of punch mechanism of the present invention.
Fig. 3 is the structural schematic diagram of displacement mechanism of the present invention.
Fig. 4 is the structural schematic diagram of driving mechanism of the present invention.
Fig. 5 is the structural schematic diagram of fixed mechanism of the present invention.
Fig. 6 is the attachment structure schematic diagram of inventive piston and cylinder.
Fig. 7 is the attachment structure schematic diagram of link block of the present invention and workbench.
In figure, 1, upper housing, 2, lower case, 3, attachment base, 4, pedestal, 5, punch mechanism, 6, displacement mechanism, 7, driving machine
Structure, 8, fixed mechanism, 9, upper connecting rod, 10, lower link, 11, spring, 12, formed punch, 13, drilling rod, 14, piston rod, 15, air inlet,
16, air outlet valve, 17, cylinder, 18, piston, 19, motor, 20, connecting shaft, 21, driving wheel, 22, driven wheel, 23, connecting rod, 24,
Axle sleeve, 25, driving gear, 26, workbench, 27, fixture block, 28, rack gear, 29, card slot, 30, lead screw, 31, feed screw nut, 32, company
Connect block, 33, sealing ring.
Specific embodiment
What the invention is realized by the following technical scheme:
A kind of aircraft solution component continuous punching device, including upper housing 1, lower case 2, attachment base 3, pedestal 4, punch mechanism
5, displacement mechanism 6, driving mechanism 7 and fixed mechanism 8 are connected between the upper housing 1 and lower case 2 by attachment base 3, described
Pedestal 4 is fixed on the bottom of lower case 2, and the punch mechanism 5 and driving structure 7 are arranged in upper housing 1, institute's displacement mechanism
6 and fixed mechanism 8 be arranged in lower case 2；The punch mechanism 5 include upper connecting rod 9, lower link 10, spring 11, formed punch 12,
The upper end of drilling rod 13, piston rod 14, air inlet 15, air outlet valve 16, cylinder 17 and piston 18, the upper connecting rod 9 connects upper housing 1
Inner wall, lower end is separately connected piston rod 14 and lower link 10；The upper end of the lower link 10 connects piston rod 14, lower end connection
Formed punch 12；The free end of the piston rod 14 connects piston 18, and the piston 18 is mounted in cylinder 17, and the cylinder 17 is arranged
In the side of upper housing 1；Air outlet valve 16 is provided on the casing wall of the cylinder 17, the air outlet valve 16 connects air inlet 15；Institute
The lower end for stating formed punch 12 is provided with spring 11, the lower end jointed rod 13 of the spring 11, and the drilling rod 13 is worn from attachment base 3
Out；The driving mechanism 7 includes motor 19, connecting shaft 20, driving wheel 21, driven wheel 22, connecting rod 23, axle sleeve 24 and sliding tooth
Wheel 25, the motor 19 is fixed in upper housing 1, and the power output end of motor 19, the active is arranged in the connecting shaft 20
Wheel 21 is fixedly connected with connecting shaft 20；The connecting shaft 20 is installed in upper housing 1 again by axle sleeve 24, and the upper end is provided with and master
The driven wheel 22 that driving wheel 21 engages, lower end are provided with driving gear 25.
Institute's displacement mechanism 6 includes that workbench 26, a pair of of fixture block 27 and rack gear 28, the pair of fixture block 27 are separately positioned on
On the two sides inner wall of lower case 2, card slot 29 is provided on the pair of fixture block 27, the workbench 26 passes through card slot 29 and a pair
Fixture block 27 is slidably connected, and the rack gear 28 is arranged on workbench 26, engages with driving gear 28.
The fixed mechanism 8 includes a pair of of lead screw 30 and a pair of of feed screw nut 31, wherein the lead screw 30 is mounted on lead screw
On nut 31, the feed screw nut 31 is arranged on workbench 26 by link block 32.
The upper and lower ends of the piston 18 are provided with sealing ring 33, and the piston 18 is sliding by sealing ring 33 and cylinder 17
Dynamic connection.
The driving wheel 21 and driven wheel 22 are bevel type gear.
The diameter of the spring 11 is greater than 13 diameter of drilling rod.
The link block 32 is flexibly connected with workbench 26.
Working principle: firstly, destructing is moved on workbench 26, rotating threaded shaft 30, solution component is fixed on workbench
On 26, then solution component, is moved to the suitable position of punching, and locked movable block 32 by mobile link block 32；Air inlet 15 connects
Air pump is connect, air pump is opened, gas enters from air inlet 15, and piston 18 is pushed to travel forward, and piston 18 drives piston rod 14, lower company
Bar 10 pushes formed punch 12, and formed punch 12 moves down, and pushes drilling rod 13, and drilling rod 13 drills out suitable hole on solution component, can lead to
Cross the size of replacement 13 adjustment aperture of drilling rod；When needing continuous drilling, motor 19 is opened, motor 19 passes through driving wheel 21 and driven
The rotation of 22 drive connection bars 23 is taken turns, connecting rod 23 drives the engagement force of driving gear 25 and rack gear 28 to drive workbench 16 to Forward
Dynamic, operator can adjust the distance of adjacent holes by the speed of change motor 19.This continuous punching device is using cylinder as power
Mechanism, the continuous punching by the mobile realization of workbench to solution component, has movement speed very fast, it is larger to generate punching press strength
The characteristics of；Platform is worked at the same time equipped with fixed mechanism, drives firm block to consolidate component is solved by screw rod, the operation is stable, significantly
The punching efficiency of plate is improved, realization is worked continuously, and saves labour, high degree of automation, and can adapt to some spies
Different occasion limitation to made by electricity usage.
For the ordinary skill in the art, introduction according to the present invention, do not depart from the principle of the present invention with
In the case where spirit, changes, modifications that embodiment is carried out, replacement and variant still fall within protection scope of the present invention it
It is interior.
Claims (7)
1. a kind of aircraft solution component continuous punching device, it is characterised in that: including upper housing, lower case, attachment base, pedestal, punching
Holes mechanism, displacement mechanism, driving mechanism and fixed mechanism are connected between the upper housing and lower case by attachment base, described
Pedestal is fixed on the bottom of lower case, and the punch mechanism and driving structure are arranged in upper housing, institute's displacement mechanism and solid
Determine mechanism to be arranged in lower case；The punch mechanism includes upper connecting rod, lower link, spring, formed punch, drilling rod, piston rod, air inlet
Mouth, air outlet valve, cylinder and piston, the inner wall of the upper end connection upper housing of the upper connecting rod, lower end is separately connected piston rod under
Connecting rod；The upper end of the lower link connects piston rod, and lower end connects formed punch；The free end of the piston rod connects piston, described
Piston is mounted in cylinder, and the side of upper housing is arranged in the cylinder；Air outlet valve is provided on the casing wall of the cylinder, it is described
Air outlet valve connects air inlet；The lower end of the formed punch is provided with spring, and the lower end jointed rod of the spring, the drilling rod is from even
Joint chair is pierced by；The driving mechanism includes motor, connecting shaft, driving wheel, driven wheel, connecting rod, axle sleeve and drives gear, described
Motor is fixed in upper housing, and the power output end of motor, the driving wheel and the fixed company of connecting shaft is arranged in the connecting shaft
It connects；The connecting shaft is installed in upper housing again by axle sleeve, and the upper end is provided with the driven wheel engaged with driving wheel, lower end setting
There is driving gear.
2. aircraft solution component continuous punching device according to claim 1, it is characterised in that: institute's displacement mechanism includes work
Make platform, a pair of of fixture block and rack gear, the pair of fixture block to be separately positioned on the two sides inner wall of lower case, on the pair of fixture block
It is provided with card slot, the workbench is slidably connected by card slot and a pair of of fixture block, and the rack gear is arranged on the table, with sliding tooth
Wheel engagement.
3. aircraft solution component continuous punching device according to claim 1, it is characterised in that: the fixed mechanism includes one
To lead screw and a pair of of feed screw nut, wherein the lead screw is mounted on feed screw nut, and work is arranged by link block in the lead screw spiral shell
Make on platform.
4. aircraft solution component continuous punching device according to claim 1, it is characterised in that: the upper and lower ends of the piston
It is provided with sealing ring, the piston is connect by sealing ring with cylinder slide.
5. aircraft solution component continuous punching device according to claim 1, it is characterised in that: the driving wheel and driven wheel
It is bevel type gear.
6. aircraft solution component continuous punching device according to claim 1, it is characterised in that: the diameter of the spring is greater than
Drill pipe diameter.
7. aircraft solution component continuous punching device according to claim 3, it is characterised in that: the link block and workbench
It is flexibly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810976695.5A CN109127879A (en) | 2018-08-25 | 2018-08-25 | A kind of aircraft solution component continuous punching device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810976695.5A CN109127879A (en) | 2018-08-25 | 2018-08-25 | A kind of aircraft solution component continuous punching device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109127879A true CN109127879A (en) | 2019-01-04 |
Family
ID=64828152
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810976695.5A Withdrawn CN109127879A (en) | 2018-08-25 | 2018-08-25 | A kind of aircraft solution component continuous punching device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109127879A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01278924A (en) * | 1988-04-27 | 1989-11-09 | Kyodo Printing Co Ltd | Punching equipment for sheet |
| CN101829723A (en) * | 2009-03-11 | 2010-09-15 | 吴远东 | Novel pneumatic punching machine |
| CN102233377A (en) * | 2011-03-02 | 2011-11-09 | 浙江博雷重型机床制造有限公司 | Numerical control punching machine tool |
| CN108405711A (en) * | 2018-04-10 | 2018-08-17 | 朱成林 | A kind of industry plank continuous punching device |
| CN207735415U (en) * | 2018-01-18 | 2018-08-17 | 广州雄志金属制品有限公司 | A kind of continuous punching die |
-
2018
- 2018-08-25 CN CN201810976695.5A patent/CN109127879A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01278924A (en) * | 1988-04-27 | 1989-11-09 | Kyodo Printing Co Ltd | Punching equipment for sheet |
| CN101829723A (en) * | 2009-03-11 | 2010-09-15 | 吴远东 | Novel pneumatic punching machine |
| CN102233377A (en) * | 2011-03-02 | 2011-11-09 | 浙江博雷重型机床制造有限公司 | Numerical control punching machine tool |
| CN207735415U (en) * | 2018-01-18 | 2018-08-17 | 广州雄志金属制品有限公司 | A kind of continuous punching die |
| CN108405711A (en) * | 2018-04-10 | 2018-08-17 | 朱成林 | A kind of industry plank continuous punching device |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190104 |