CN203155789U - Novel turret punch press - Google Patents

Novel turret punch press Download PDF

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Publication number
CN203155789U
CN203155789U CN 201320090997 CN201320090997U CN203155789U CN 203155789 U CN203155789 U CN 203155789U CN 201320090997 CN201320090997 CN 201320090997 CN 201320090997 U CN201320090997 U CN 201320090997U CN 203155789 U CN203155789 U CN 203155789U
Authority
CN
China
Prior art keywords
wheel disc
turret
reduced
punch press
fuselage
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.)
Expired - Fee Related
Application number
CN 201320090997
Other languages
Chinese (zh)
Inventor
范永明
陈星军
丁明波
李成忠
陶洪涛
李方
王德敬
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
QINGDAO SHENGTONG MECHANICAL TECHNOLOGY Co Ltd
Original Assignee
QINGDAO SHENGTONG MECHANICAL TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by QINGDAO SHENGTONG MECHANICAL TECHNOLOGY Co Ltd filed Critical QINGDAO SHENGTONG MECHANICAL TECHNOLOGY Co Ltd
Priority to CN 201320090997 priority Critical patent/CN203155789U/en
Application granted granted Critical
Publication of CN203155789U publication Critical patent/CN203155789U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

A novel turret punch press comprises a machine body, an upper wheel disk, a lower wheel disk, a servo motor and a driving shaft. The thickness of a turret of the novel turret punch press is small, the overall strength of the turret is guaranteed, meanwhile, the weight of the turret is reduced, the load of the machine body is reduced, and the problem that the machining precision is reduced due to deformation of a throat of the machine body is solved. The weight of the turret is reduced, the turret can be driven by a chain transmission mechanism, and the transmission mechanism is simple in structure, convenient to install and easy to maintain, so that manufacturing and usage costs of the whole turret punch press are reduced. The guiding precision of the up-and-down movement of a stamping die is improved by a fixed sleeve installed on an installation hole, and the inner diameter of the fixed sleeve is smaller than the hole diameter of the corresponding installation hole, so that the bottom of the stamping die is not in contact with a rotating disk, the friction between the stamping die and the rotating disk is transferred to the friction between the stamping die and the fixed sleeve, the abrasion of the rotating disk is avoided, and the service life of the whole turret punch press is prolonged; and the fixed sleeve can be changed directly, so that the maintenance cost is further reduced.

Description

Novel rotating tower punch
Technical field
The utility model relates to a kind of novel rotating tower punch.
Background technology
The wheel disc of existing rotating tower punch, thickness is bigger, thereby the weight of rotating disk is bigger, makes the fuselage of C type bear very big load, and the aditus laryngis of fuselage is deformed, and influences the machining accuracy of punch press.And in order to drive the bigger rotating disk of weight, also need the bigger transmission mechanism of inertia, the transmission mechanism complex structure is difficult for installing, and is difficult in maintenance, increased the manufacturing cost and use cost of equipment integral body.
The utility model content
The utility model is big at the thickness of rotating tower punch wheel disc, weight is big, fuselage bears big load, deforms easily, influences machining accuracy, need mate big inertia transmission mechanism with it, complex structure is difficult for installing, and is difficult in maintenance, shortcomings such as manufacturing cost and use cost height have designed a kind of novel rotating tower punch.
This novel rotating tower punch, comprise fuselage, last wheel disc, following wheel disc, servomotor, driving shaft, last wheel disc, following wheel disc is respectively by last connecting axle, following connecting axle is installed on the fuselage, the thickness of last wheel disc is M, the thickness of following wheel disc is N, on last connecting axle and the following connecting axle driven sprocket is installed all, servomotor is installed on the fuselage, the main shaft of servomotor is connected with driving shaft is coaxial, driving shaft vertically is installed on the pedestal that arranges on the fuselage, the top of driving shaft and bottom all are equipped with drive sprocket, two drive sprockets connect by chain with corresponding driven sprocket respectively, the same circumference of last wheel disc card is provided with a plurality of installing holes, and fixed cover all is installed on the opening on installing hole top, and diel all is installed in the fixed cover, the bottom of diel is positioned at installing hole, the internal diameter of fixed cover all is provided with slug hole less than the aperture of the installing hole of correspondence on the following wheel disc card corresponding with installing hole, and die holder all is installed on the opening of slug hole.
Preferably, M and N are more than or equal to 40mm, smaller or equal to 55mm.
The beneficial effects of the utility model are: the thickness of novel rotating tower punch capstan head is less, when having guaranteed the capstan head bulk strength, has reduced the weight of capstan head, has alleviated the load of fuselage, has avoided because the problem that the machining accuracy that the distortion of fuselage aditus laryngis causes reduces.Because the weight of capstan head reduces, use chain drive can drive capstan head, transmission mechanism is simple in structure, and is easy for installation, is easy to safeguard, reduced the manufacturing cost and use cost of rotating tower punch integral body.The fixed cover of installing on the installing hole has improved the guiding accuracy that diel moves up and down, the internal diameter of fixed cover is less than the aperture of the installing hole of correspondence, the bottom of diel is not contacted with rotating disk, with diel not and the friction transfer between the rotating disk to the friction between diel and the fixed cover, the wearing and tearing of rotating disk have been avoided, improved the service life of rotating tower punch integral body, and fixed cover can change directly, further reduce maintenance cost.
Description of drawings
Accompanying drawing 1 is the perspective view of novel rotating tower punch.
The specific embodiment
This novel rotating tower punch, as shown in Figure 1, comprise fuselage 1, last wheel disc 2, following wheel disc 3, servomotor 4, driving shaft 5, last wheel disc 2, following wheel disc 3 are installed on the fuselage 1 by last connecting axle 6, following connecting axle 7 respectively, the thickness of last wheel disc 2 is M, the thickness of following wheel disc 3 is N, and M and N are more than or equal to 40mm, smaller or equal to 55mm.
On last connecting axle 6 and the following connecting axle 7 driven sprocket 8 is installed all, servomotor 4 is installed on the fuselage 1, the main shaft of servomotor 4 and 5 coaxial connections of driving shaft, driving shaft 5 vertically is installed on the pedestal 9 that arranges on the fuselage 1, the top of driving shaft 5 and bottom all are equipped with 10, two drive sprockets 10 of drive sprocket and connect by chain with corresponding driven sprocket 8 respectively.
The same circumference of last wheel disc 2 cards is provided with a plurality of installing holes 12, on the opening on installing hole 12 tops fixed cover 13 is installed all, diel 11 all is installed in the fixed cover 13, the bottom of diel 11 is positioned at installing hole 12, the internal diameter of fixed cover 13 is less than the aperture of the installing hole 12 of correspondence, all be provided with slug hole 14 on following wheel disc 3 cards corresponding with installing hole 12, die holder 15 all is installed on the opening of slug hole 14.

Claims (2)

1. novel rotating tower punch, it is characterized in that, comprise fuselage (1), last wheel disc (2), following wheel disc (3), servomotor (4), driving shaft (5), last wheel disc (2), following wheel disc (3) is respectively by last connecting axle (6), following connecting axle (7) is installed on the fuselage (1), the thickness of last wheel disc (2) is M, the thickness of following wheel disc (3) is N, on last connecting axle (6) and the following connecting axle (7) driven sprocket (8) is installed all, servomotor (4) is installed on the fuselage (1), the main shaft of servomotor (4) and coaxial connection of driving shaft (5), driving shaft (5) vertically is installed in fuselage (1) and goes up on the pedestal (9) that arranges, the top of driving shaft (5) and bottom all are equipped with drive sprocket (10), two drive sprockets (10) connect by chain with corresponding driven sprocket (8) respectively, the same circumference of last wheel disc (2) card is provided with a plurality of installing holes (12), on the opening on installing hole (12) top fixed cover (13) is installed all, diel (11) all is installed in the fixed cover (13), the bottom of diel (11) is positioned at installing hole (12), the internal diameter of fixed cover (13) is less than the aperture of the installing hole (12) of correspondence, all be provided with slug hole (14) on following wheel disc (3) card corresponding with installing hole (12), die holder (15) all is installed on the opening of slug hole (14).
2. according to the described novel rotating tower punch of claim 1, it is characterized in that M and N are more than or equal to 40mm, smaller or equal to 55mm.
CN 201320090997 2013-02-27 2013-02-27 Novel turret punch press Expired - Fee Related CN203155789U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201320090997 CN203155789U (en) 2013-02-27 2013-02-27 Novel turret punch press

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201320090997 CN203155789U (en) 2013-02-27 2013-02-27 Novel turret punch press

Publications (1)

Publication Number Publication Date
CN203155789U true CN203155789U (en) 2013-08-28

Family

ID=49017013

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201320090997 Expired - Fee Related CN203155789U (en) 2013-02-27 2013-02-27 Novel turret punch press

Country Status (1)

Country Link
CN (1) CN203155789U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104399787A (en) * 2014-11-14 2015-03-11 扬州固诚机床有限公司 Bending machine platform mechanism
CN105107913A (en) * 2015-09-19 2015-12-02 青岛盛通机械科技有限公司 Transmission direct-connected type autorotation die
CN106238544A (en) * 2016-08-30 2016-12-21 洛阳润信机械制造有限公司 A kind of punch press

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104399787A (en) * 2014-11-14 2015-03-11 扬州固诚机床有限公司 Bending machine platform mechanism
CN105107913A (en) * 2015-09-19 2015-12-02 青岛盛通机械科技有限公司 Transmission direct-connected type autorotation die
CN106238544A (en) * 2016-08-30 2016-12-21 洛阳润信机械制造有限公司 A kind of punch press

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C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130828

Termination date: 20140227