CN201342455Y - Necking device for wind pipe - Google Patents

Necking device for wind pipe Download PDF

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Publication number
CN201342455Y
CN201342455Y CNU2009200383111U CN200920038311U CN201342455Y CN 201342455 Y CN201342455 Y CN 201342455Y CN U2009200383111 U CNU2009200383111 U CN U2009200383111U CN 200920038311 U CN200920038311 U CN 200920038311U CN 201342455 Y CN201342455 Y CN 201342455Y
Authority
CN
China
Prior art keywords
compression
cylinder
airduct
opening
chuck
Prior art date
Application number
CNU2009200383111U
Other languages
Chinese (zh)
Inventor
宗绪惠
Original Assignee
昆山六丰机械工业有限公司
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 昆山六丰机械工业有限公司 filed Critical 昆山六丰机械工业有限公司
Priority to CNU2009200383111U priority Critical patent/CN201342455Y/en
Application granted granted Critical
Publication of CN201342455Y publication Critical patent/CN201342455Y/en

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Abstract

A necking device for a wind pipe is provided. A tail seat can do feed motion corresponding to the machine body; a compression jig is fixedly arranged at the tail of a head seat; the chuck of the wind pipe is fixedly arranged at the head of a tail seat; the clamping opening of the chuck of the wind pipe is matched with the outer diameter of the wind pipe;the compression opening of the compression jig is opposite to the clamping opening of the chuck of the wind pipe; the compression opening is in the shape of a chamfered opening with a big outer part and a small inner part; the minimum inner diameter of the compression opening is less than the outer diameter of the wind pipe;while the maximum inner diameter of the compression opening is not less than the outer diameter of the wind pipe; a cylinder is arranged on the tail seat; a cylinder control switch is arranged on the machine body to control the cylinder; and the cylinder piston is fixedly connected with the tail seat. The operation of the cylinder is controlled by the cylinder control switch; the cylinder controls the feeding of the tail seat; the chuck of the wind pipe is placed at the opening of the wind pipe of the clamping opening, inserted in the compression opening of the compression jig and drawn out from the compression opening of the compression jig along with feeding of the tail seat; roasting is not needed in use and compression deformation is adopted without manual interference, thereby reducing human resource cost and processing time; due to the fixed compression opening size, the size of the necked opening of the wind pipe is ensured to be consistent.

Description

Air pipe reducing device
Technical field
The utility model relates to a kind of airduct processing unit (plant), especially a kind of air pipe reducing device.
Background technology
Air-cooled is the principal mode of mold cools down, so every mold all needs to make a large amount of airducts.Now general way is: after making the complete primary school airduct, dwindle wind gathering, adopt the method that hits with a hammer when the airduct mouth toasted to make its reducing for making the airduct mouth, after the making again to the abrasive machine polishing of airduct mouth finished surface.This way Production Time is long, efficient is low, cuts not of uniform size the causing of airduct mouth after dwindling, and is difficult to reach designing requirement and instructions for use, and therefore the Personal Skills to the producer requires height.
Summary of the invention
In order to overcome above-mentioned defective, the utility model provides a kind of air pipe reducing device, and this air pipe reducing device can be done efficient reducing to airduct, and the size of the airduct mouth after the reducing is consistent.
The utility model for the technical scheme that solves its technical problem and adopt is:
A kind of air pipe reducing device, comprise fuselage, headstock and tailstock, to use direction to be benchmark, headstock is located at fuselage head, tailstock is located at afterbody, described tailstock fuselage is relatively done feed motion, also comprise the compression tool, the airduct chuck, cylinder gauge tap and cylinder, described compression tool is fixedly arranged on the headstock afterbody, described airduct chuck is fixedly arranged on the tailstock head, the folder mouth and the airduct external diameter of described airduct chuck are supporting, the compression port of described compression tool is corresponding with the Jia Kou position of described airduct chuck, the compression port of described compression tool is the little chamfering mouth of outer imperial palace, the minimum diameter of this compression port is less than the airduct external diameter, and the maximum inner diameter of this compression port is not less than the airduct external diameter, described tailstock is provided with cylinder, described fuselage is provided with the cylinder gauge tap, the cylinder gauge tap is controlled described cylinder, the steam-cylinder piston tailstock that is connected, like this by the work of cylinder gauge tap control cylinder, the feeding of cylinder control tailstock, the airduct chuck will place the airduct mouth of the airduct of folder mouth to insert the compression port of compression tool and the compression port of extracting the compression tool with the feeding of tailstock.
Described headstock comprises main shaft and spindle motor, the described main shaft compression tool that is connected, and spindle motor control main shaft rotates, and the rotation of compression tool can make after the reducing of airduct mouth more smooth.
The compression port wall material of described compression tool is a wolfram steel.
The invention has the beneficial effects as follows: by the work of cylinder gauge tap control cylinder, the feeding of cylinder control tailstock, the airduct chuck will place the airduct mouth of the airduct of folder mouth to insert the compression port of compression tool and the compression port of extracting the compression tool with the feeding of tailstock, need not baking during use and adopt the compression of compression tool to need not manual intervention, thereby human cost and process time have been reduced, again because the compression port fixed size of compression tool has guaranteed that the airduct mouth size after the reducing is consistent.
Description of drawings
Fig. 1 is a schematic diagram of the present invention;
Fig. 2 is a compression tool schematic diagram of the present invention;
Fig. 3 is an airduct chuck schematic diagram of the present invention.
The specific embodiment
Embodiment: a kind of air pipe reducing device, comprise fuselage 11, headstock 12 and tailstock 13, to use direction to be benchmark, headstock 12 is located at fuselage 11 heads, tailstock 13 is located at fuselage 11 afterbodys, described tailstock 13 fuselage 11 is relatively done feed motion, also comprise compression tool 1, airduct chuck 2, cylinder gauge tap 3 and cylinder 4, described compression tool 1 is fixedly arranged on headstock 12 afterbodys, described airduct chuck 2 is fixedly arranged on tailstock 13 heads, the folder mouth 20 of described airduct chuck 2 is supporting with the airduct external diameter, the compression port 10 of described compression tool 1 is corresponding with folder mouth 20 positions of described airduct chuck, the compression port 10 of described compression tool 1 is the little chamfering mouth of outer imperial palace, the minimum diameter of this compression port 10 is less than the airduct external diameter, and the maximum inner diameter of this compression port 10 is not less than the airduct external diameter, described tailstock 13 is provided with cylinder 4, described fuselage 11 is provided with cylinder gauge tap 3, the described cylinder 4 of cylinder gauge tap 3 controls, the cylinder 4 pistons tailstock 13 that is connected, like this by 4 work of cylinder gauge tap 3 control cylinders, the feeding of cylinder 4 control tailstocks 13, airduct chuck 2 will place the airduct mouth of the airduct of folder mouth 20 to insert the compression port 10 of compression tool 1 and the compression port 10 of extracting compression tool 1 with the feeding of tailstock 13.
Described headstock 12 comprises main shaft and spindle motor, the described main shaft compression tool 1 that is connected, and spindle motor control main shaft rotates, and the rotation of compression tool can make after the reducing of airduct mouth more smooth.
The compression port wall material of described compression tool 1 is a wolfram steel.
During use, airduct one end is placed the folder mouth 20 of airduct chuck 2, open cylinder gauge tap 3, cylinder 4 promotes tailstock 13 forward, airduct chuck 2 will place the airduct mouth of the airduct of folder mouth 20 to insert the compression port 10 of compression tool 1 forward with tailstock 13, by compression tool 1 distortion of airduct mouth is dwindled, close cylinder gauge tap 3, cylinder 4 drags tailstock 13 and returns, the compression port 10 that airduct chuck 2 will place the airduct mouth of the airduct of folder mouth 20 to extract compression tool 1 with tailstock 13 backward, this moment, air pipe reducing was finished.
By 4 work of cylinder gauge tap 3 control cylinders, the feeding of cylinder 4 control tailstocks 13, airduct chuck 2 will place the airduct mouth of the airduct of folder mouth 20 to insert the compression port 10 of compression tool 1 and the compression port 10 of extracting compression tool 1 with the feeding of tailstock 13, need not baking during use and adopt compression tool 1, compression to need not manual intervention, thereby human cost and process time have been reduced, again because compression port 10 fixed size of compression tool 1 have guaranteed that the airduct mouth size after the reducing is consistent.

Claims (3)

1. air pipe reducing device, comprise fuselage (11), headstock (12) and tailstock (13), to use direction to be benchmark, headstock is located at fuselage head, tailstock is located at afterbody, described tailstock fuselage is relatively done feed motion, it is characterized in that: also comprise compression tool (1), airduct chuck (2), cylinder gauge tap (3) and cylinder (4), described compression tool is fixedly arranged on the headstock afterbody, described airduct chuck is fixedly arranged on the tailstock head, the folder mouth (20) of described airduct chuck is supporting with the airduct external diameter, the compression port of described compression tool (10) is corresponding with the Jia Kou position of described airduct chuck, the compression port of described compression tool is the little chamfering mouth of outer imperial palace, and the minimum diameter of this compression port is less than the airduct external diameter, and the maximum inner diameter of this compression port is not less than the airduct external diameter, described tailstock is provided with cylinder, described fuselage is provided with the cylinder gauge tap, and the cylinder gauge tap is controlled described cylinder, the steam-cylinder piston tailstock that is connected.
2. air pipe reducing device according to claim 1 is characterized in that: described headstock comprises main shaft and spindle motor, the described main shaft compression tool that is connected, and spindle motor control main shaft rotates.
3. air pipe reducing device according to claim 1 is characterized in that: the compression port wall material of described compression tool is a wolfram steel.
CNU2009200383111U 2009-01-13 2009-01-13 Necking device for wind pipe CN201342455Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2009200383111U CN201342455Y (en) 2009-01-13 2009-01-13 Necking device for wind pipe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2009200383111U CN201342455Y (en) 2009-01-13 2009-01-13 Necking device for wind pipe

Publications (1)

Publication Number Publication Date
CN201342455Y true CN201342455Y (en) 2009-11-11

Family

ID=41274040

Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2009200383111U CN201342455Y (en) 2009-01-13 2009-01-13 Necking device for wind pipe

Country Status (1)

Country Link
CN (1) CN201342455Y (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104741466A (en) * 2015-04-07 2015-07-01 江苏仓环铜业股份有限公司 Processing equipment for horn mouth of metal tube
CN105773167A (en) * 2016-03-30 2016-07-20 黄建财 Automatic pipe-end machining system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104741466A (en) * 2015-04-07 2015-07-01 江苏仓环铜业股份有限公司 Processing equipment for horn mouth of metal tube
CN105773167A (en) * 2016-03-30 2016-07-20 黄建财 Automatic pipe-end machining system

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
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Granted publication date: 20091111

Termination date: 20180113