CN205763325U - A kind of porous punching composite die - Google Patents

A kind of porous punching composite die Download PDF

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Publication number
CN205763325U
CN205763325U CN201620460839.8U CN201620460839U CN205763325U CN 205763325 U CN205763325 U CN 205763325U CN 201620460839 U CN201620460839 U CN 201620460839U CN 205763325 U CN205763325 U CN 205763325U
Authority
CN
China
Prior art keywords
plate
lower mold
composite die
fuselage
fixed plate
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
CN201620460839.8U
Other languages
Chinese (zh)
Inventor
丁键
钱艳红
李军
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.)
JIANGSU JINSANLI MACHINERY MANUFACTURING Co Ltd
Original Assignee
JIANGSU JINSANLI MACHINERY MANUFACTURING 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 JIANGSU JINSANLI MACHINERY MANUFACTURING Co Ltd filed Critical JIANGSU JINSANLI MACHINERY MANUFACTURING Co Ltd
Priority to CN201620460839.8U priority Critical patent/CN205763325U/en
Application granted granted Critical
Publication of CN205763325U publication Critical patent/CN205763325U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of porous punching composite die, including frame, described upper rack is provided with upper die component, and the lower mold assemblies matched by guide pillar with described upper die component;Described upper die component includes fuselage upper junction plate, the lower end of described fuselage upper junction plate is fixed with composite die top board, described composite die top board lower end is provided with upper mould fixed plate, being provided with shearing top cutter and drift on described upper mould fixed plate, described shearing top cutter is connected through described upper mould fixed plate and described composite die top board are fixing;Described lower mold assemblies includes that fuselage lower connecting plate, the upper end of described fuselage lower connecting plate are provided with composite die base plate, and described composite die base plate upper end is provided with lower mold fixed plate;The shearing bottom knife matched with described shearing top cutter, and the lower mold matched with described drift it is provided with inside described lower mold fixed plate.Use this novel mould, improve production efficiency, and improve the machining accuracy of workpiece.

Description

A kind of porous punching composite die
Technical field
This utility model relates to a kind of porous punching composite die.
Background technology
Traditional workpiece porous to be realized is rushed, and manufacturing procedure is: first according to the overall dimensions oxygen-acetylene cutting of workpiece, Then workpiece is carried out single hole punching, because workpiece requires processing porous, so punching to divide a few procedure ability complete Become, and cannot be accurately positioned on mould, therefore cannot ensure the precision of pitch-row.
Utility model content
This utility model purpose is that the defect existed for prior art provides a kind of porous punching composite die. This utility model for achieving the above object, adopts the following technical scheme that a kind of porous punching composite die, including Frame, described upper rack is provided with upper die component, and is matched down with described upper die component by guide pillar Membrane module;Wherein, described upper die component includes that fuselage upper junction plate, the upper end of described fuselage upper junction plate pass through Cylinder piston rod is connected with oil cylinder, and the lower end of described fuselage upper junction plate is fixed with composite die top board, described multiple Mould top board lower end is provided with upper mould fixed plate, and described upper mould fixed plate is provided with shearing top cutter and punching Head, wherein, described shearing top cutter is connected through described upper mould fixed plate and described composite die top board are fixing; Described lower mold assemblies includes fuselage lower connecting plate, the lower end of described fuselage lower connecting plate be arranged in described frame T-slot plate fixing connect, the upper end of described fuselage lower connecting plate is provided with composite die base plate, described compound Die bottom plate upper end is provided with lower mold fixed plate;It is provided with inside described lower mold fixed plate and described shearing top cutter The shearing bottom knife matched, and the lower mold matched with described drift;Front side and the inner side of described lower mold are equal It is provided with positioner;Described lower mold fixed plate upper end is additionally provided with stripper, is provided with in the middle of described stripper Discharging packing ring.
The beneficial effects of the utility model: use this novel mould, not only change conventional workpiece porous and rush work The drawback that sequence is loaded down with trivial details, improves production efficiency, and improves the machining accuracy of workpiece, saved production cost.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
Shown in Fig. 1, relating to a kind of porous punching composite die, including frame 1, described frame 1 top is arranged There are upper die component, and the lower mold assemblies matched by guide pillar 18 with described upper die component;Wherein, described Upper die component includes fuselage upper junction plate 12, and cylinder piston rod 16 is passed through in the upper end of described fuselage upper junction plate 12 Being connected with oil cylinder 11, the lower end of described fuselage upper junction plate 12 is fixed with composite die top board 13, described multiple Mould top board 13 lower end is provided with upper mould fixed plate 14, and described upper mould fixed plate 14 is provided with in shearing Blade 15 and drift 17, wherein, described shearing top cutter 15 is multiple with described through described upper mould fixed plate 14 Mould top board 13 is fixing to be connected;Described lower mold assemblies includes fuselage lower connecting plate 21, connects under described fuselage The lower end of plate 21 is fixing with the T-slot plate 28 being arranged in described frame 1 to be connected, described fuselage lower connecting plate The upper end of 21 is provided with composite die base plate 22, and described composite die base plate 22 upper end is provided with lower mold fixed plate 23;The shearing bottom knife matched with described shearing top cutter 15 it is provided with inside described lower mold fixed plate 23 24, and the lower mold 29 matched with described drift 17;Front side and the inner side of described lower mold 29 are provided with Positioner 27;Described lower mold fixed plate 23 upper end is additionally provided with in the middle of stripper 25, described stripper 25 It is provided with discharging packing ring 26.
Using said structure, as long as ordering batten according to the width dimensions of workpiece, batten being sent directly into compound die In tool, owing on front side of lower mold and inner side is provided with positioner, after position shifted onto by workpiece, the standard being workpiece is long Degree, thus realize multiple piercing and disposably complete with cutting off.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all at this Within the spirit of utility model and principle, any modification, equivalent substitution and improvement etc. made, should be included in Within protection domain of the present utility model.

Claims (1)

1. a porous punching composite die, it is characterised in that include that frame, described upper rack are provided with Upper die component, and the lower mold assemblies matched with described upper die component by guide pillar;Wherein, described upper module Part includes fuselage upper junction plate, and the upper end of described fuselage upper junction plate is connected with oil cylinder by cylinder piston rod, institute The lower end stating fuselage upper junction plate is fixed with composite die top board, and described composite die top board lower end is provided with upper mold Fixed plate, described upper mould fixed plate is provided with shearing top cutter and drift, and wherein, described shearing top cutter is worn Cross that described upper mould fixed plate and described composite die top board are fixing to be connected;Described lower mold assemblies includes connecting under fuselage Plate, the lower end of described fuselage lower connecting plate is fixing with the T-slot plate being arranged in described frame to be connected, described machine The upper end of body lower connecting plate is provided with composite die base plate, and described composite die base plate upper end is provided with lower mold and fixes Plate;The shearing bottom knife matched with described shearing top cutter, Yi Jiyu it is provided with inside described lower mold fixed plate The lower mold that described drift matches;Front side and the inner side of described lower mold are provided with positioner;Wherein, described Lower mold fixed plate upper end is additionally provided with stripper, is provided with discharging packing ring in the middle of described stripper.
CN201620460839.8U 2016-05-19 2016-05-19 A kind of porous punching composite die Expired - Fee Related CN205763325U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620460839.8U CN205763325U (en) 2016-05-19 2016-05-19 A kind of porous punching composite die

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620460839.8U CN205763325U (en) 2016-05-19 2016-05-19 A kind of porous punching composite die

Publications (1)

Publication Number Publication Date
CN205763325U true CN205763325U (en) 2016-12-07

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620460839.8U Expired - Fee Related CN205763325U (en) 2016-05-19 2016-05-19 A kind of porous punching composite die

Country Status (1)

Country Link
CN (1) CN205763325U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108747397A (en) * 2018-06-15 2018-11-06 江苏金三力机械制造有限公司 A kind of steel arch-shelf connecting plate automatic shearing rushes production line and its production method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108747397A (en) * 2018-06-15 2018-11-06 江苏金三力机械制造有限公司 A kind of steel arch-shelf connecting plate automatic shearing rushes production line and its production method

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

Granted publication date: 20161207