CN2070219U - Composite structure conductive jet - Google Patents

Composite structure conductive jet Download PDF

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Publication number
CN2070219U
CN2070219U CN 90216975 CN90216975U CN2070219U CN 2070219 U CN2070219 U CN 2070219U CN 90216975 CN90216975 CN 90216975 CN 90216975 U CN90216975 U CN 90216975U CN 2070219 U CN2070219 U CN 2070219U
Authority
CN
China
Prior art keywords
hole
cover mouth
utility
model
welding
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.)
Pending
Application number
CN 90216975
Other languages
Chinese (zh)
Inventor
骆建华
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.)
Renqiu Hebei Innovation Welding Gun Factory
Aerospace Industry Survey And Design Research Institute Ministry Of Aeronautics And Astronautics Industry
Original Assignee
Renqiu Hebei Innovation Welding Gun Factory
Aerospace Industry Survey And Design Research Institute Ministry Of Aeronautics And Astronautics Industry
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 Renqiu Hebei Innovation Welding Gun Factory, Aerospace Industry Survey And Design Research Institute Ministry Of Aeronautics And Astronautics Industry filed Critical Renqiu Hebei Innovation Welding Gun Factory
Priority to CN 90216975 priority Critical patent/CN2070219U/en
Publication of CN2070219U publication Critical patent/CN2070219U/en
Pending legal-status Critical Current

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Abstract

The utility model provides a composite structure conductive jet, which is used for gas metal arc welding. The utility model comprises a red copper body, wherein, the back end of the red copper body is provided with screw threads; the red copper body is provided with a feeding hole for welding wires; the front end of the body is assembled with a sheath jet which can be often replaced, and. the sheath jet is provided with a through hole. The sheath jet of the utility model is made by adopting powder alloy materials of which the electrical conductivity and the abrasion resistance are favorable; the service life is enhance by 7 times to 10 times; the process of welding is stable, which is important for automatic welding. The utility model has the advantages of convenient use, and the utility model is economical and reliable.

Description

The composite construction ignition tip
The utility model relates to the composite construction ignition tip that a kind of gas metal-arc welding is used, and it comprises that the rear end of a red copper is threaded and have a welding wire to send the body in hole to, at the cover mouth that can often change of a band of the front end assembling through hole of body.
The ignition tip that existing gas metal-arc welding is used; integral body all uses red copper or chromium-bronze alloy material to make; because anti-wear performance is relatively poor; the little bore portion of ignition tip front end very easily weares and teares; (the red copper tip that Beijing innovation soldering set factory produces be exactly use at present a kind of widely) causes in the welding process and contacts the conductive site variation, the welding performance variation in the welding wire and ignition tip hole.Thereby also need often change ignition tip, the promptly time-consuming material that takes again.
The purpose of this utility model is to overcome weak point in the above-mentioned prior art and a kind of composite construction ignition tip is provided.Adopt that electric conductivity is good, the anti-wear performance powder alloy material superior far beyond red copper made Xiao Taozui, be set in red copper ignition tip front position again and make the composite construction ignition tip.Be 7~10 times of red copper ignition tip service life, because wear-resisting, welding wire contact conductive site remains at the front end of ignition tip, thereby welding process is stable.This is particularly important to automatic welding.
The drawing of accompanying drawing is described as follows:
Fig. 1: (1) body, (2) cover mouth
Fig. 2: (1) body, (2) cover mouth
Fig. 3: (1) body, (2) cover mouth
Shown in 1,2,3, the ignition tip body is to use red copper or chromium-bronze to make with reference to the accompanying drawings, and the cover mouth then is the tungsten copper powder alloy material, and sends hole perforation and coaxial to a through hole and with the welding wire of body.
The purpose of this utility model can reach by following measure, and is shown in Figure 1, at the front end of body a shrinkage pool arranged, and the cover mouth is embedded in this shrinkage pool of body, takes interference fit to make it unlikely under the high-temperature condition in welding process and deviates from.
The purpose of this utility model can also reach by following measure, and is shown in Figure 3, at the body front end one threaded cylindrical protrusions arranged, and cover mouth rear end has a shrinkage pool, and screw thread is arranged in the hole, makes it to be connected with body.
The purpose of this utility model can also reach by following measure, and is shown in Figure 2, at the body front end one shrinkage pool arranged, and screw thread is arranged in the hole, is connected with the threaded cylindrical protrusions in cover mouth rear end.
The utility model is described in further detail below in conjunction with (accompanying drawing) embodiment:
Make the ignition tip body with red copper or chromium-bronze material, front end has a cylindrical shrinkage pool, to send the hole to coaxial with welding wire, re-use the anti-wear performance tungsten copper powder alloy material superior and make the cylindrical shroud mouth than materials such as red coppers, take the molybdenum filament cutting to make through hole in the central, the grip mouth is set in the body shrinkage pool then, interference fit, make cover mouth through hole and welding wire send hole perforation and coaxial with it to, constitute the composite construction ignition tip.
The utility model compared with prior art has following advantage:
Cover mouth anti-wear performance is much better than red copper, and replaceable, and the life-span can be improved 7~10 times, and main is the front end that welding wire contact conductive site remains at ignition tip, thereby welding process is stable. This is particularly important to automatic welding.

Claims (5)

1. composite construction ignition tip that gas metal-arc welding is used comprises that the rear end of a red copper is threaded and have a welding wire to send the body in hole to, it is characterized in that: at the cover mouth that can often change of a band of the front end assembling through hole of body.
2. cover mouth according to claim 1 is characterized in that: the cover mouth is to have a through hole, and through hole is sent hole perforation and coaxial to the welding wire of body.
3. cover mouth according to claim 1 is characterized in that: the cover mouth is embedded in the shrinkage pool of body front end, takes interference fit.
4. cover mouth according to claim 1 is characterized in that: cover mouth rear end has a shrinkage pool, and screw thread is arranged in the hole, is connected with the threaded cylindrical protrusions of body front end.
5. cover mouth according to claim 1 is characterized in that: the threaded cylindrical protrusions in cover mouth rear end is connected with the threaded shrinkage pool of body front end.
CN 90216975 1990-08-03 1990-08-03 Composite structure conductive jet Pending CN2070219U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 90216975 CN2070219U (en) 1990-08-03 1990-08-03 Composite structure conductive jet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 90216975 CN2070219U (en) 1990-08-03 1990-08-03 Composite structure conductive jet

Publications (1)

Publication Number Publication Date
CN2070219U true CN2070219U (en) 1991-01-30

Family

ID=4896045

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 90216975 Pending CN2070219U (en) 1990-08-03 1990-08-03 Composite structure conductive jet

Country Status (1)

Country Link
CN (1) CN2070219U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105328312A (en) * 2014-08-06 2016-02-17 张建生 Current contact nozzle
CN107186322A (en) * 2017-06-29 2017-09-22 沈阳工业大学 Partly split the hollow tungsten electrode coaxial wire feed inert gas-shielded arc welding welding gun of formula
CN107309532A (en) * 2017-08-15 2017-11-03 徐绍华 Carbon dioxide gas arc welding alloy conductive mouth and preparation method thereof

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105328312A (en) * 2014-08-06 2016-02-17 张建生 Current contact nozzle
CN107186322A (en) * 2017-06-29 2017-09-22 沈阳工业大学 Partly split the hollow tungsten electrode coaxial wire feed inert gas-shielded arc welding welding gun of formula
CN107186322B (en) * 2017-06-29 2022-12-06 沈阳工业大学 Half-split hollow tungsten electrode coaxial wire feeding inert gas shielded welding gun
CN107309532A (en) * 2017-08-15 2017-11-03 徐绍华 Carbon dioxide gas arc welding alloy conductive mouth and preparation method thereof

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
AD01 Patent right deemed abandoned
C20 Patent right or utility model deemed to be abandoned or is abandoned