CN102489617A - Metal tube seal process - Google Patents
Metal tube seal process Download PDFInfo
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- CN102489617A CN102489617A CN2011103964819A CN201110396481A CN102489617A CN 102489617 A CN102489617 A CN 102489617A CN 2011103964819 A CN2011103964819 A CN 2011103964819A CN 201110396481 A CN201110396481 A CN 201110396481A CN 102489617 A CN102489617 A CN 102489617A
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- metal tube
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- compressive plane
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Abstract
A metal tube seal process mainly resolves the problem that machining stainless steel tubes with large diameters wastes time and energy and is difficult to seal with the existing seal method of a metal pipe fitting port. The metal tube seal process is characterized by including the following process steps: a installing a metal tube (1) in clamping mode in an elastic clamping sleeve capable of rotating on a machine tool; b utilizing a no-cutting-edge tool (3) to extrude a port of the metal tube (1) in high rotation, extruding the port towards the center in the radial direction while moving outwards the no-cutting-edge tool (3) in the axial direction, forming a conical surface and then extruding the conical surface in the axial direction until the port of the metal tube (1) is completely sealed and integrated at a high temperature in melting mode; c utilizing a turning tool to machine the outer end face of the sealed port of the metal tube (1) to be flat. The metal tube seal process changes the previous machining method, achieves sealing the stainless steel tubes with large diameters, saves time and labor, and is simple in working procedures, low in cost, high in machining efficiency and flat and smooth in appearance.
Description
Technical field
The present invention relates to a kind of mouth-sealing method of metal tube port, be specifically related to a kind of metal tube sealing process.
Background technology
When producing five metals suspension member (hereinafter to be referred as suspension member),, need seal processing to the port of metal tube for serviceability and requirement such as attractive in appearance.The metal that the material of suspension member generally adopts copper, stainless steel, aluminium alloy, kirsite etc. to be difficult for getting rusty in order to improve working (machining) efficiency, generally is that the port to metal tube seals on instrument lathe.Utilize fricative heat between metal tube and the no angle of throat tool to make the port of metal tube softening; Extruding makes the port of metal tube distortion fuses into blind end at last to the center to the port of metal tube through no angle of throat tool simultaneously; For the soft metal (like copper, aluminium alloy, kirsite etc.) of minor diameter, this processing method obviously is feasible.When the customer requirements metal tube used the big slightly stainless steel material of pipe diameter, because stainless steel material hardness is higher, caliber was bigger simultaneously, directly advances cutter to seal to tube hub, wastes time and energy, and seals difficulty.
Summary of the invention
In order to overcome disadvantages of background technology, the present invention provides a kind of metal tube sealing process, wastes time and energy, seals the problem of difficulty when mainly having solved the big slightly stainless steel tube of the mouth-sealing method processing diameter of existing metal tube port; This metal tube sealing process has changed processing method in the past, has realized the big slightly stainless steel tube of diameter is sealed, and is time saving and energy saving; Operation is simple; Cost is low, and working (machining) efficiency is high, and flat appearance is smooth.
Technical scheme of the present invention is: this metal tube sealing process step is following:
In the elastic jacket that a. the metal tube clamping can be rotated on lathe;
B. adopt the no angle of throat tool that has front end compressive plane and side compressive plane; The metal tube that utilizes the front end compressive plane of no angle of throat tool to rotate at a high speed to metal tube center radial compression; Meanwhile move axially no angle of throat tool to the outer end of the port of metal tube; It is softening that fricative heat makes the port of metal tube between metal tube and the no angle of throat tool, and the port of metal tube forms taper seat to its center distortion gradually; Utilize the side compressive plane of no angle of throat tool to rely on the conical end of metal tube, slowly inwardly extruding, up to the port complete closed of metal tube and at high temperature fuse into one, taper seat is squeezed into the port plane;
C. utilize lathe tool that the outer face processing of metal tube closed port is smooth.
Described machine adopted instrument lathe.
Front end compressive plane on the described no angle of throat tool is an arc surface, and the side compressive plane is the plane.
The present invention has following beneficial effect: owing to take such scheme, utilize that fricative heat softens the port of metal tube between metal tube and the no angle of throat tool, the formation taper seat; Through the side compressive plane on the no angle of throat tool taper seat of metal tube being compressed axially the taper seat that makes metal tube simultaneously piles up and fuses into blind end at last; Adopt lathe that clamping of metal tube is accomplished and seal, realized the big slightly stainless steel tube of diameter is sealed, time saving and energy saving; Operation is simple; Cost is low, and working (machining) efficiency is high, and flat appearance is smooth.
Description of drawings
Accompanying drawing 1 is an initial manufacture view of the present invention.
Accompanying drawing 2, Fig. 3 are the machining state sketch mapes that the port closed of metal tube 1 of the present invention is shaped.
1-metal tube among the figure, 2-taper seat, 3-do not have the angle of throat tool, 4-front end compressive plane, 5-side compressive plane.
The specific embodiment
Below in conjunction with accompanying drawing the present invention is described further:
Combine Fig. 2, shown in Figure 3 by Fig. 1, this metal tube sealing process step is following:
In the elastic jacket that a. metal tube 1 clamping can be rotated on lathe;
B. adopt the no angle of throat tool 3 that has front end compressive plane 4 and side compressive plane 5; The metal tube 1 that utilizes the front end compressive plane 4 of no angle of throat tool 3 to rotate at a high speed to metal tube 1 center radial compression; Meanwhile move axially no angle of throat tool 3 to the outer end of the port of metal tube 1; It is softening that fricative heat makes the port of metal tube 1 between metal tube 1 and the no angle of throat tool 3, and the port of metal tube 1 forms taper seat 2 to its center distortion gradually; Utilize the side compressive plane 5 of no angle of throat tool 3 to rely on the conical end of metal tube 1, slowly inwardly extruding, up to the port complete closed of metal tube 1 and at high temperature fuse into one, taper seat 2 is squeezed into the port plane;
C. utilize lathe tool that the outer face processing of metal tube 1 closed port is smooth.
The material of the metal tube 1 of the present invention's processing generally is the higher metal of hardness, generally is stainless steel, ordinary carbon steel or other steel alloy.It is softening that fricative heat makes the port of metal tube 1 between this technology utilization metal tube 1 and the no angle of throat tool 3, forms taper seat, and the taper seat through the 5 pairs of metal tubes 1 of side compressive plane on the no angle of throat tool 3 compresses axially the taper seat accumulation that makes metal tube 1 and fuses into blind end at last simultaneously; Adopt lathe that No. 1 clampings of metal tube are accomplished and seal, realized the big slightly metal tube 1 of diameter is sealed, time saving and energy saving; Operation is simple; Cost is low, and working (machining) efficiency is high, and flat appearance is smooth.
Described machine adopted instrument lathe.Instrument lathe is simple in structure, and is easy to operate, and working (machining) efficiency is high.
Front end compressive plane 4 on the described no angle of throat tool 3 is an arc surface, and side compressive plane 5 is the plane.The arc length of front end compressive plane 4 is confirmed by the external diameter of metal tube 1 and the thickness of required blind end.The area of side compressive plane 5 is not less than the face area that seals of metal tube 1.
Claims (3)
1. metal tube sealing process, it is characterized in that: this processing step is following:
In the elastic jacket that a. metal tube (1) clamping can be rotated on lathe;
B. adopt the no angle of throat tool (3) that has front end compressive plane (4) and side compressive plane (5); The metal tube (1) that utilizes the front end compressive plane (4) of no angle of throat tool (3) to rotate at a high speed to metal tube (1) center radial compression; Meanwhile move axially no angle of throat tool (3) to the outer end of the port of metal tube (1); It is softening that fricative heat makes the port of metal tube (1) between metal tube (1) and the no angle of throat tool (3), and the port of metal tube (1) forms taper seat (2) to its center distortion gradually; Utilize the side compressive plane (5) of no angle of throat tool (3) to rely on the conical end of metal tube (1), slowly inwardly extruding, up to the port complete closed of metal tube (1) and at high temperature fuse into one, taper seat (2) is squeezed into the port plane;
C. utilize lathe tool that the outer face processing of metal tube (1) closed port is smooth.
2. metal tube sealing process according to claim 1 is characterized in that: described machine adopted instrument lathe.
3. metal tube sealing process according to claim 1 and 2 is characterized in that: the front end compressive plane (4) on the described no angle of throat tool (3) is an arc surface, and side compressive plane (5) is the plane.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN2011103964819A CN102489617A (en) | 2011-12-02 | 2011-12-02 | Metal tube seal process |
Applications Claiming Priority (1)
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CN2011103964819A CN102489617A (en) | 2011-12-02 | 2011-12-02 | Metal tube seal process |
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CN102489617A true CN102489617A (en) | 2012-06-13 |
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CN2011103964819A Pending CN102489617A (en) | 2011-12-02 | 2011-12-02 | Metal tube seal process |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103406761A (en) * | 2013-07-19 | 2013-11-27 | 首都航天机械公司 | TC4 titanium alloy pipe ball head heat flow forming method |
CN104923607A (en) * | 2015-04-23 | 2015-09-23 | 袁龙 | Planar groove forming technique, blade-free tool and hardware manufactured through planar groove forming technique |
CN107855427A (en) * | 2017-11-09 | 2018-03-30 | 中国航发贵州黎阳航空动力有限公司 | A kind of pipe end method for closing-in forming |
CN110091126A (en) * | 2019-04-13 | 2019-08-06 | 邓钜焕 | A kind of handlebar stem manufacturing process |
CN111354919A (en) * | 2020-04-01 | 2020-06-30 | 湖北亿纬动力有限公司 | Battery, liquid injection method of battery and battery module |
CN111774585A (en) * | 2020-07-29 | 2020-10-16 | 贵州航天精工制造有限公司 | Manufacturing method and cutter for tubular hemming part |
Citations (6)
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JPS59125220A (en) * | 1982-12-29 | 1984-07-19 | Showa Mfg Co Ltd | Closed end forming method of pipe |
EP0769337A1 (en) * | 1995-10-18 | 1997-04-23 | MAGNETI MARELLI CLIMATIZZAZIONE S.r.l. | A method of closing an end of a metal pipe |
EP0786295A1 (en) * | 1996-01-25 | 1997-07-30 | Reynolds Metals Company | Method for necking containers |
CN1282638A (en) * | 2000-09-07 | 2001-02-07 | 刘鸿恩 | High-strength multi-style integral shaping, enclosing and manufacture method of tubular body |
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2011
- 2011-12-02 CN CN2011103964819A patent/CN102489617A/en active Pending
Patent Citations (6)
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US2406059A (en) * | 1943-06-10 | 1946-08-20 | Linde Air Prod Co | Process of spinning hollow articles |
JPS59125220A (en) * | 1982-12-29 | 1984-07-19 | Showa Mfg Co Ltd | Closed end forming method of pipe |
EP0769337A1 (en) * | 1995-10-18 | 1997-04-23 | MAGNETI MARELLI CLIMATIZZAZIONE S.r.l. | A method of closing an end of a metal pipe |
EP0786295A1 (en) * | 1996-01-25 | 1997-07-30 | Reynolds Metals Company | Method for necking containers |
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Non-Patent Citations (3)
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103406761A (en) * | 2013-07-19 | 2013-11-27 | 首都航天机械公司 | TC4 titanium alloy pipe ball head heat flow forming method |
CN103406761B (en) * | 2013-07-19 | 2016-08-10 | 首都航天机械公司 | TC4 titanium alloy tube bulbec feverish sensation in the head spin-on process |
CN104923607A (en) * | 2015-04-23 | 2015-09-23 | 袁龙 | Planar groove forming technique, blade-free tool and hardware manufactured through planar groove forming technique |
CN107855427A (en) * | 2017-11-09 | 2018-03-30 | 中国航发贵州黎阳航空动力有限公司 | A kind of pipe end method for closing-in forming |
CN110091126A (en) * | 2019-04-13 | 2019-08-06 | 邓钜焕 | A kind of handlebar stem manufacturing process |
CN111354919A (en) * | 2020-04-01 | 2020-06-30 | 湖北亿纬动力有限公司 | Battery, liquid injection method of battery and battery module |
CN111774585A (en) * | 2020-07-29 | 2020-10-16 | 贵州航天精工制造有限公司 | Manufacturing method and cutter for tubular hemming part |
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Application publication date: 20120613 |