CN202052904U - All-metallic blocking nut automatic point pressing machine - Google Patents
All-metallic blocking nut automatic point pressing machine Download PDFInfo
- Publication number
- CN202052904U CN202052904U CN2011200095338U CN201120009533U CN202052904U CN 202052904 U CN202052904 U CN 202052904U CN 2011200095338 U CN2011200095338 U CN 2011200095338U CN 201120009533 U CN201120009533 U CN 201120009533U CN 202052904 U CN202052904 U CN 202052904U
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- CN
- China
- Prior art keywords
- locking nut
- pressure point
- hydraulic system
- blanking
- point pressing
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- Expired - Fee Related
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Abstract
An all-metallic blocking nut automatic point pressing machine comprises a frame rack, a hydraulic system, a stamping device, a feed trough, a feeding barrel, blanking channels, a control box, an electrical control box and a power motor and is characterized in that the hydraulic system is fixed on the front side of the frame rack and connected with the stamping device through a conduit, the stamping device is arranged on the center of the frame rack and contacted with the feed trough made of two solid steel plates parallel to each other and perpendicular to the horizontal plane, and the blanking channels are connected to the top ends of the feed trough and respectively fixed in front of the feeding barrel. The all-metallic blocking nut automatic point pressing machine, being novel and practical, is scientific and reasonable in design, low in manufacturing cost, saving in electricity and manpower. Moreover, the all-metallic blocking nut automatic point pressing machine greatly improves product quality and working efficiency, and is applicable for point pressing all-metallic blocking nuts of various specifications.
Description
Technical field
The utility model relates to the metalworking machinery field, be specifically a kind of on the metal nuts surface automatic hydraulic machinery of pressure point.
Background technology
At present, in known all-metal locking nut pressure point equipment, all be each nut to be placed on punching press under the forging equipment by manual, because this manual forging equipment danger is high, floor space is big, quality is unstable, production capacity is low, operate with a people but also get a machine, therefore operating efficiency is lower, has directly influenced the economic well-being of workers and staff of enterprise.
Summary of the invention
In order to overcome above-mentioned deficiency, the utility model provides a kind of all-metal locking nut automatic pressure point machine, it is placed on nut to be processed in the metal blowing bucket of this machine top setting, nut drops in the vertical forging and pressing groove by the gravity effect, then drive operation by hydraulic system by horizontally disposed stamping die, stamp out node in the metal nuts end, do industry thereby finish, because hydraulic system need not manual operations have been stopped potential safety hazard by the electric control box automation, and this machine power consumption is low, constant product quality, the high easy operating of production capacity, can a people see several machines simultaneously, saving power labour, thereby improved economic benefit, so just overcome above-mentioned drawback, efficiently solved a difficult problem.
The utility model solves technical scheme that its technical problem adopts: the automatic pressure point machine of all-metal locking nut, it comprises: fuselage cradle, hydraulic system, decompressor, blanking groove, the blowing bucket, blanking is led the way, control case, electric control box, power motor, it is characterized in that: described hydraulic system is fixedly set in the front side of fuselage cradle, and be connected with decompressor by conduit, the middle part that described decompressor is located at the fuselage machine contacts with blanking groove, described blanking groove is made up of two hard matter steel plates, the two setting parallel to each other, and it is vertical respectively at horizontal plane, described blanking groove top is connected with blanking respectively and leads the way, described blanking is led the way and is fixedly set in the front of blowing bucket respectively, the described case of controlling is located at the fuselage cradle left side, and by lead respectively with hydraulic system, decompressor and power motor, electric control box is connected, described power motor is fixed at the fuselage cradle right side, be connected with electric control box by conduit, described electric power control cabinet places the rear side of fuselage cradle, fix with fuselage cradle, be used to control the electrical control of entire machine.
The beneficial effects of the utility model are: design science is reasonable, and cost of manufacture is low, and Nover practical has been saved electric power, manpower, has improved product quality and operating efficiency greatly, is fit to the processing of all size all-metal locking nut pressure point and uses.
Description of drawings
Fig. 1 is the utility model structural representation
Fig. 2 is the utility model backsight structural representation
Among the figure, 1. fuselage cradle, 2. hydraulic system, 3. decompressor, 4. blanking groove, 5. blowing bucket, 6. blanking is led the way, and 7. controls case, 8. electric control box, 9. power motor, 10. conduit.
The specific embodiment
In example, described hydraulic system (2) is fixedly set in the front side of fuselage cradle (1), and be connected with decompressor (3) by conduit (10), the middle part that described decompressor (3) is located at fuselage cradle (1) contacts with blanking groove (4), described blanking groove (4) is made up of two hard matter steel plates, the two setting parallel to each other, and it is vertical respectively at horizontal plane, described blanking groove (4) top is connected with blanking lead the way (6) respectively, described blanking lead the way (6) be fixedly set in the front of blowing bucket (5) respectively, the described case (7) of controlling is located at fuselage cradle (1) left side, and by conduit (10) respectively with hydraulic system (2), decompressor (3) and power motor (9), electric control box (8) is connected, described power motor (9) is fixed at fuselage cradle (1) right side, be connected with electric control box (8), described electric power control cabinet (8) places the rear side of fuselage cradle (1), fixes with fuselage cradle (1), is used to control the electrical control of entire machine.
Claims (6)
1. the automatic pressure point machine of all-metal locking nut, it comprises: case, electric control box, power motor are led the way, are controlled in fuselage cradle, hydraulic system, decompressor, blanking groove, blowing bucket, blanking, it is characterized in that: described hydraulic system is fixedly set in the front side of fuselage cradle, and is connected with decompressor by conduit.
2. the automatic pressure point machine of all-metal locking nut according to claim 1, it is characterized in that: the middle part that described decompressor is located at the fuselage machine contacts with blanking groove, described blanking groove is made up of two hard matter steel plates, the two setting parallel to each other, and vertical respectively at horizontal plane.
3. the automatic pressure point machine of all-metal locking nut according to claim 1, it is characterized in that: the blanking groove top is connected with blanking respectively and leads the way, and described blanking is led the way and is fixedly set in the front of blowing bucket respectively.
4. the automatic pressure point machine of all-metal locking nut according to claim 1 is characterized in that: control case and be located at the fuselage cradle left side, and be connected with hydraulic system, decompressor and power motor, electric control box respectively by lead.
5. the automatic pressure point machine of all-metal locking nut according to claim 1, it is characterized in that: power motor is fixed at the fuselage cradle right side, is connected with electric control box by conduit.
6. the automatic pressure point machine of all-metal locking nut according to claim 1, it is characterized in that: described electric power control cabinet places the rear side of fuselage cradle, fixes with fuselage cradle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011200095338U CN202052904U (en) | 2011-01-13 | 2011-01-13 | All-metallic blocking nut automatic point pressing machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011200095338U CN202052904U (en) | 2011-01-13 | 2011-01-13 | All-metallic blocking nut automatic point pressing machine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202052904U true CN202052904U (en) | 2011-11-30 |
Family
ID=45012891
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2011200095338U Expired - Fee Related CN202052904U (en) | 2011-01-13 | 2011-01-13 | All-metallic blocking nut automatic point pressing machine |
Country Status (1)
Country | Link |
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CN (1) | CN202052904U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106001349A (en) * | 2016-07-07 | 2016-10-12 | 浙江鼎盛汽车紧固件有限公司 | Nut locking point press-fit machine |
CN107350380A (en) * | 2017-07-24 | 2017-11-17 | 浙江群展精密紧固件股份有限公司 | A kind of pressure point formula locking nut processing unit (plant) |
-
2011
- 2011-01-13 CN CN2011200095338U patent/CN202052904U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106001349A (en) * | 2016-07-07 | 2016-10-12 | 浙江鼎盛汽车紧固件有限公司 | Nut locking point press-fit machine |
CN107350380A (en) * | 2017-07-24 | 2017-11-17 | 浙江群展精密紧固件股份有限公司 | A kind of pressure point formula locking nut processing unit (plant) |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20111130 Termination date: 20130113 |
|
CF01 | Termination of patent right due to non-payment of annual fee |