CN205271983U - Dash some wares - Google Patents
Dash some wares Download PDFInfo
- Publication number
- CN205271983U CN205271983U CN201520979531.XU CN201520979531U CN205271983U CN 205271983 U CN205271983 U CN 205271983U CN 201520979531 U CN201520979531 U CN 201520979531U CN 205271983 U CN205271983 U CN 205271983U
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- electro
- magnet
- punching
- punching point
- structural body
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Abstract
The utility model provides a dash some wares, contains the structure body, dash the some round pin, first electro -magnet, the second electro -magnet, a battery, switch and delay timer, the front end of structure body is the positioning head that the area dashed some holes, coaxial inlaying there is first electro -magnet in the siphonozooid of structure body, second electro -magnet and strong some round pin, the iron core of second electro -magnet is the tail end that dashes the some round pin, opposite direction is twined with the coil that the second coil of adjacent second electro -magnet was organized in the first coil group of first electro -magnet, the front end that dashes the some round pin dashes to nod, it nods to fill is a conical body, it nods and dash to dash there is the step between the some round pin, the middle part that dashes the some round pin is equipped with reset spring and check ring, the moving distance who dashes the some round pin receives the preceding guiding hole of structure body spacing, the tail end that dashes the some round pin can insert second coil inter block and form the second electro -magnet.
Description
Technical field
The application relates to Aircraft tooling technology, and what specifically a kind of punching of ruling was put rushes a device.
Background technology
In Aircraft Production process, the line on tooling used needs punching to rush a little, and these punching point quantity are big, and status requirement is accurate. These punching points become for punching point device punching substantially, and the tradition punching point device structure that current transporation by plane industry uses is simple, and complicated operation, without self-locking, without automatic function. For this kind of situation, it is badly in need of being found and a kind of novel rushes a device, meet the demand that Aircraft tooling punching is rushed in point process.
Summary of the invention
The purpose of this utility model is to provide a kind of new-type rushes a device, can meet a punching point precision, again can be less take space, small and exquisite refining, band self-locking, can punching automatically.
A kind of punching point device, containing structural body, punching point pin, first electro-magnet, 2nd electro-magnet, battery, power switch and time delay unit, it is characterized in that described structural body is the pistol shape of a L-shaped, handle portion in structural body is provided with the installation chamber of battery, the front end of structural body is the positioning head that band rushes spot hole, the first electro-magnet coaxially it is inlaid with in the tubular body arranged inside of structural body, 2nd electro-magnet and punching point pin, the iron core of the 2nd electro-magnet is the tail end of punching point pin, first coil assembly of the first electro-magnet is contrary with the coil winding direction of the two coil group of the 2nd adjacent electro-magnet, the front end of punching point pin is that punching is nodded, it is a cone-shaped body that punching is nodded, punching is nodded and rushed has step between a pin, the middle part of punching point pin is provided with return spring and spring collar, the movement travel of punching point pin is subject to the leading spacing to hole of structural body, the tail end of punching point pin can insert and form the 2nd electro-magnet in two coil group.
During work, utilize positioning head to align tooling and need the scribing position rushing point, turn on the power switch, time delay unit works, time delay unit ensures that the first electro-magnet and the 2nd electro-magnet are energized a second, first electro-magnet attracts the 2nd electro-magnet to retreat by magnetic force, owing to the iron core of the 2nd electro-magnet is the tail end that punching point is sold, therefore punching point pin is retreated, return spring is compressed, time delay unit power-off after one second, the magnetic force of the first electro-magnet and the 2nd electro-magnet disappears, return spring recovers stretched condition, punching point pin and punching are nodded and launches forward, utilize return spring impulse force forward, punching is nodded and is got ready in the line of tooling.
The useful effect of the application is to make use of compression spring and electromagnetic principle, it is achieved that punching point function automatically, it is minimum that structure takies space, it is achieved that manufacture claim.
Below in conjunction with embodiment accompanying drawing, this application is described in further detail.
Accompanying drawing explanation
Fig. 1 rushes the structure signal of a device
Fig. 2 rushes a device and rushes dotted state signal
Fig. 3 rushes a device spring compressed state signal
Fig. 4 positioning head structure is illustrated
Fig. 5 rushes a circuit principle signal
Attached number description: 1 structural body, 2 punching point pin, 3 return springs, 4 spring collars, 5 the 2nd electro-magnet, 6 first electro-magnet; 7 power switches, 8 power-on button, 9 batteries, 10 positioning heads, 11 two coil groups, 12 first coil assembly, 13 passing hole, 14 leading holes of leading after hole, 15 inner chamber body, 16,17 punching nod, 18 steps, 19 handles, 20 locating slots, 21 line
Embodiment
FIGS 1��Fig. 5, the application rushes a device, containing structural body 1, punching point pin 2, first electro-magnet 6, 2nd electro-magnet 5, battery 9, power switch 7, power-on button 8 and time delay unit, it is characterized in that described structural body 1 is the pistol shape of a L-shaped, handle 19 part in structural body 1 is provided with the installation chamber of battery 9, coaxial groove chamber is had in the tubular body arranged inside of structural body 1, first electro-magnet 6, the coil assembly of the 2nd electro-magnet 5 and punching point pin 2, coaxially it is embedded in successively in the groove chamber of structural body 1, the front end of structural body 1 is the positioning head 10 that band rushes spot hole, the all fixing tail end being embedded in structural body 1 tubular body arranged inside of the iron core of the first electro-magnet 6 and the first coil assembly 12, the iron core of the 2nd electro-magnet 5 is the tail end of punching point pin 2, it it is movable structure, first coil assembly 12 of the first electro-magnet 6 is contrary with the coil winding direction of the two coil group 11 of the 2nd adjacent electro-magnet 5, the front end of punching point pin 2 is that punching nods 17, punching nod 17 center be provided with and rush spot hole, punching nod 17 front end by rushing spot hole rush a little, the tail end of punching point pin 2 can insert and form the 2nd electro-magnet 5 in two coil group 11, it 17 is a cone-shaped body that punching is nodded, punching is nodded has step 18 between 17 and punching point pin 2, the middle part of punching point pin 2 is provided with return spring 3 and spring collar 4, the movement travel of punching point pin 2 is subject to the leading spacing to hole 14 of structural body 1, leading nodding with punching to the front end cavity in hole 14 17 is mated, the leading rear end cavity to hole 14 mates with return spring 3 and spring collar 4, distance between spring collar 4 and step 18 is the maximum stroke of punching point pin 2 priming, in order to accurately location rushes a little, positioning head 10 is provided with rush the cross locating slot 20 centered by spot hole.
FIGS 3, Fig. 4, during work, the long and short dash line 21 that rushes on the corresponding tooling of the locating slot 20 of positioning head 10 is utilized to carry out rushing point location, power switch 7 is opened, press button 8, time delay unit works, time delay unit ensures that the first electro-magnet 5 and the 2nd electro-magnet 6 are energized a second, first electro-magnet 5 attracts the 2nd electro-magnet 6 to retreat by magnetic force, owing to the iron core of the 2nd electro-magnet 6 is the afterbody rushing some pin 2, punching point pin 2 is driven to retreat, return spring 3 is compressed, time delay unit power-off after one second, the magnetic force of the first electro-magnet 5 and the 2nd electro-magnet 6 disappears, spring 3 recovers stretched condition, oppositely suppress punching point pin 2 to launch forward, utilize spring 3 impulse force forward to intersect at the cross of the line 21 of tooling to get ready.
Claims (2)
1. a punching point device, containing structural body, punching point pin, first electro-magnet, 2nd electro-magnet, battery, power switch and time delay unit, it is characterized in that described structural body is the pistol shape of a L-shaped, handle portion in structural body is provided with the installation chamber of battery, the front end of structural body is the positioning head that band rushes spot hole, the first electro-magnet coaxially it is inlaid with in the tubular body arranged inside of structural body, 2nd electro-magnet and punching point pin, the iron core of the 2nd electro-magnet is the tail end of punching point pin, first coil assembly of the first electro-magnet is contrary with the coil winding direction of the two coil group of the 2nd adjacent electro-magnet, the front end of punching point pin is that punching is nodded, it is a cone-shaped body that punching is nodded, punching is nodded and rushed has step between a pin, the middle part of punching point pin is provided with return spring and spring collar, the movement travel of punching point pin is subject to the leading spacing to hole of structural body, the tail end of punching point pin can insert and form the 2nd electro-magnet in two coil group.
2. punching point device as claimed in claim 1, it is characterised in that described positioning head is provided with to rush the cross locating slot centered by spot hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520979531.XU CN205271983U (en) | 2015-11-30 | 2015-11-30 | Dash some wares |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520979531.XU CN205271983U (en) | 2015-11-30 | 2015-11-30 | Dash some wares |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205271983U true CN205271983U (en) | 2016-06-01 |
Family
ID=56056599
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520979531.XU Active CN205271983U (en) | 2015-11-30 | 2015-11-30 | Dash some wares |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205271983U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112518676A (en) * | 2020-09-30 | 2021-03-19 | 成都飞机工业（集团）有限责任公司 | Dot punching gun capable of adjusting control depth |
-
2015
- 2015-11-30 CN CN201520979531.XU patent/CN205271983U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112518676A (en) * | 2020-09-30 | 2021-03-19 | 成都飞机工业（集团）有限责任公司 | Dot punching gun capable of adjusting control depth |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: No. 710089 in Shaanxi province Xi'an city Yanliang District West Avenue Patentee after: AVIC Xi'an Aircraft Industry Group Co.,Ltd. Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee before: AVIC AIRCRAFT Corp. |
|
| CP03 | Change of name, title or address | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210624 Address after: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee after: AVIC AIRCRAFT Corp. Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee before: XI'AN AIRCRAFT BRANCH OF XI'AN AIRCRAFT INTERNATIONAL Corp. |
|
| TR01 | Transfer of patent right |