EP0465941B1 - Plasmabrenner für übertragenen Lichtbogen - Google Patents

Plasmabrenner für übertragenen Lichtbogen Download PDF

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Publication number
EP0465941B1
EP0465941B1 EP91110640A EP91110640A EP0465941B1 EP 0465941 B1 EP0465941 B1 EP 0465941B1 EP 91110640 A EP91110640 A EP 91110640A EP 91110640 A EP91110640 A EP 91110640A EP 0465941 B1 EP0465941 B1 EP 0465941B1
Authority
EP
European Patent Office
Prior art keywords
plasma torch
end piece
nozzle end
nozzle
torch according
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 - Lifetime
Application number
EP91110640A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP0465941A2 (de
EP0465941A3 (en
Inventor
Herbert Dipl.-Ing. Klein
Heinrich-Otto Dipl.-Ing. Rossner
Ulrich Dipl.-Ing. Scheffler
Gebhard Dipl.-Ing. Tomalla
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.)
Fried Krupp AG Hoesch Krupp
Original Assignee
Fried Krupp AG Hoesch Krupp
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 Fried Krupp AG Hoesch Krupp filed Critical Fried Krupp AG Hoesch Krupp
Publication of EP0465941A2 publication Critical patent/EP0465941A2/de
Publication of EP0465941A3 publication Critical patent/EP0465941A3/de
Application granted granted Critical
Publication of EP0465941B1 publication Critical patent/EP0465941B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00—Generating plasma; Handling plasma
    • H05H1/24—Generating plasma
    • H05H1/26—Plasma torches
    • H05H1/32—Plasma torches using an arc
    • H05H1/34—Details, e.g. electrodes, nozzles
    • H05H1/3431—Coaxial cylindrical electrodes
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00—Generating plasma; Handling plasma
    • H05H1/24—Generating plasma
    • H05H1/26—Plasma torches
    • H05H1/32—Plasma torches using an arc
    • H05H1/34—Details, e.g. electrodes, nozzles
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00—Generating plasma; Handling plasma
    • H05H1/24—Generating plasma
    • H05H1/26—Plasma torches
    • H05H1/28—Cooling arrangements

Definitions

  • the invention relates to a plasma torch for transmitted arc with a central electrode, a concentric nozzle end piece, wherein an annular gap for the passage of plasma gas is present between the electrode and the nozzle end piece, and a concentric burner jacket with outer, middle and inner wall, between the nozzle end piece and an annular channel is present in the burner jacket, the inner wall of which is partially formed by an insulating tube that electrically separates both parts.
  • Parasitic arches not only significantly impair the stability of the arc column and thus the efficiency and economy of a plasma torch or a system operated with plasma torches, they generally even lead to the complete destruction of plasma torches.
  • the insulation provided in the end face of the nozzle be laid in an end groove.
  • a plasma torch has also been carried out.
  • the end groove is formed on the one hand by the outer wall of a nozzle nozzle or end piece and on the other hand by a burner jacket, the burner jacket having on its front side a flange pointing towards the axis of the burner, which offers the insulation piece lying behind a certain heat protection.
  • this burner is in an atmosphere with electrically conductive particles, e.g. B. operated metal or steel dusts, the electrically conductive dusts can precipitate on the cooled insulating piece, so that an electrical bridge from the nozzle neck to the burner jacket form and parasitic arcs can now flow over the outer end edge of the burner jacket.
  • the invention is based, which Risk of the formation of parasitic arcs, in particular when operating with alternating current, is further restricted, ie with greater success.
  • the annular channel between the nozzle end piece and the burner jacket is withdrawn at least up to the level of the coolant inlet and outlet of the burner jacket and has a line connection at its rear end with a source of a pressurized gaseous medium. Due to its length, the coaxial ring channel already represents a factor that increases operational safety and service life, due to the lack of mechanical connections on which electrically conductive vapors or dusts could be deposited, which could lead to bridges between the nozzle connection piece and the nozzle casing.
  • the line connection to a source of a pressurized gaseous medium is equivalent to blowing a gaseous pressure medium into the ring channel.
  • Blowing the ring channel with gas represents a further step in the direction of increasing operational safety and increasing the service life.
  • the mouth or outlet area of the ring channel is additionally cooled by the gas. Any electrically conductive vapors or dusts that occur are prevented from entering the ring channel.
  • blowback plasma arc curls are prevented and melt and slag splashes that want to penetrate into the ring channel are rejected and cooled.
  • oxidation-promoting gases are shielded, which are sucked in from the environment via the plasma arc and have a strong wear-promoting effect on refractory metals that are located outside the plasma gas area.
  • oxidation-prone burner components do not exist outside the plasma gas range and the process leaves the If oxidizing gases are used in the ring channel, this also converts metallic vapors that reach the effective area of the ring gas jacket to poorly conductive metal oxides.
  • the cooling effect of the additional gas flowing through the ring channel results in a longer service life for coatings or coatings present in the mouth area of the ring channel.
  • the radiation of the plasma arc is reduced by the gas ring jacket flowing out of the ring channel, which is also referred to as enveloping gas, and thus above all the vessel delivery is spared.
  • the length of the ring channel which extends up to the height of the coolant inlet and outlet of the burner jacket, results in a large homogenization of the gas flow at the outlet from the ring gap up to its mouth.
  • the plasma torch is advantageously also suitable for transporting or carrying solid substances in powder or grain form with the additional gas.
  • the entire plasma arc circumference and a certain distance in the direction of the plasma arc axis can be used for melting or vaporization of the solid matter in the plasma torch according to the invention.
  • the homogenization of the gas flow through the ring channel can be further improved in that the line connection has a tangential component at the rear end of the ring channel.
  • the line connection has a tangential component at the rear end of the ring channel.
  • each tangential component can be provided.
  • the at least partially tangential direction of insertion into the ring channel and the leveling that can be achieved with it is particularly important in the case of the conveyance of solids.
  • the electrode and the nozzle end piece require only a low coolant throughput, it is advantageous to assign a separate cooling circuit to the burner jacket, so that the coolant throughput required can be adapted to the respective degree of stress.
  • the nozzle jacket is connected to the jacket tube of the burner jacket via a simple threaded connection, possibly via a connecting part. It is therefore easy to remove and thus enables the electrode and the nozzle or the nozzle end piece to be quickly replaced for other applications, which can also be easily assembled or exchanged by means of threaded connections.
  • the annular channel is advantageously conically converging in the arc direction in its mouth region.
  • the insulating tube electrically separating the nozzle end piece and the burner jacket is adjacent to the outside of the nozzle end piece. It is also used to form the conical inner surface in the mouth region of the ring channel.
  • the surfaces of the conical mouth region of the ring channel can preferably have a coating of insulation material, in particular ceramic, which makes it possible to also convey electrically conductive solids through the ring channel and to feed them to the arc.
  • insulation material in particular ceramic
  • the insulating tube surrounding the electrode lance is further set back into the ring channel up to the line connection.
  • the clear diameter of the outer edge of the ring channel at the mouth is preferably smaller than the outer diameter of the inner wall of the ring channel before the conical course begins.
  • the nozzle end piece is advantageously mechanically connected to the electrode via an annular body made of insulation material and combined with it to form a structural unit.
  • This annular body has passages running parallel to the main axis of the plasma torch, through which the main plasma gas can reach the annular gap between the electrode and the nozzle end piece.
  • a common coolant circuit is provided for the latter.
  • displacement bodies can be arranged in the ring channel.
  • spacers or supporting bodies are advantageously inserted into the ring channel.
  • These support bodies are shaped as aerodynamically as possible, viewed in the longitudinal axis of the burner, arranged offset from one another and advantageously fastened to the insulating tube assigned to the electrode and the nozzle end piece.
  • the support body can be designed as a hollow and solid body and run axially parallel or helical and thus contribute to the promotion and management of additives in the Afford ring channel.
  • Hollow bodies parallel to the axis can preferably be extended as a nozzle-shaped ceramic tube beyond the end face of the nozzle end piece in order, for example, to supply powder locally and in a directed manner to the plasma arc.
  • the plasma torch essentially consists of an electrode lance and a torch jacket.
  • the electrode lance again consists essentially of an electrode 10 and a nozzle nozzle or nozzle end piece 11 and the parts holding them.
  • the electrode 10 has a weakly conical end surface and the nozzle nozzle 11 has a weakly conical inner surface and a more conical outer surface.
  • the electrode 10 is fastened with its outer wall via a substantially sleeve-shaped connecting piece 12 to the current tube 13, a tube connected to the main voltage source, a threaded connection or pairing in each case between the electrode 10 and the connecting element 12 and between this and the current tube 13 consists.
  • the inner wall of the electrode 10 is slidably guided on an inner tube 14 fastened in the rear end of the plasma torch. Between the flow pipe 13 and the inner pipe 14 there is a plastic center pipe 15 for separating the partial circuits of the coolant for the electrode. In its lower area, the center tube 15 also serves to deflect the coolant flow.
  • the inner wall of the nozzle end piece 11 is connected via a threaded connection to an annular body 16 made of insulation material, preferably ceramic, and this in turn is connected to the connecting piece 12 via a threaded connection.
  • the connecting piece 12 (cf. FIGS. 4 and 5) has upper and lower radial passages 17, 18 and parallel to it, distributed uniformly on its circumference Passages 19 extending through the burner axis.
  • the passages 26 point downward into the annular gap 27 between the electrode 10 and the nozzle end piece 11.
  • a plastic tube 28 Arranged around the flow tube 13 is a plastic tube 28 which has passages 29 running parallel to the axis of the burner, which pass into an annular cavity 31 in the lower region of the tube 28, which creates a connection to the passages 19 of the connecting piece 16.
  • the tube 28 At its upper end, the tube 28 is provided with a flange 32 which has radial passages 33 which are connected to the axially parallel passages 29.
  • the plastic tube 28 is surrounded by a steel tube 34 with a flange 35.
  • the outside diameter of the steel tube 34 corresponds to the outside diameter of the nozzle end piece 11.
  • An insulation tube 36 is arranged on the outside of the steel tube 34 and has a flange 37 at its upper end.
  • a transition surface 38 is provided between the cylindrical outer surface of the insulation tube 36 and the underside of the flange 37.
  • Another lower ceramic tube 39 lies with its inner surface on the outer surfaces of the steel tube 34 and the nozzle end piece 11 and is detachably connected to the upper insulation tube 36 via a screw or thread connection. At its lower end, the outer surface of the lower ceramic tube 39 is continuously transferred into the conical outer surface of the nozzle end piece 11.
  • An auxiliary electrode 42 is guided through the inner tube 14 of the electrode lance and is centered in a known manner by spacers. At its upper end, the auxiliary electrode 42 has a current connection 44 for the ignition current. In its upper region, the auxiliary electrode 42 is electrically separated from the inner tube 14 and the other parts of the electrode lance by a plastic disk 45.
  • the plastic disk 45 has one or more radial passages 46 for supplying ignition gas, which can continue to flow through the annular channel formed by the ignition electrode 42 and the inner tube 14.
  • the electrode 10 and the nozzle end piece 11 are cooled by a common, combined coolant circuit. From the coolant inlet 48, the coolant passes through the annular channel 49 formed by the inner tube 14 and the middle tube 15, is deflected at the bottom of the middle tube 15, flows through the radial passages 18, is deflected by the deflection part 24 and flows through the passages 17 and through the flow tube 13 and the center tube 15 formed ring channel 50 to the coolant outlet 51st
  • a housing part 54 is centered on the outside of the flange 37 and mechanically firmly connected to the flange 32 of the plastic tube 28.
  • the housing part 54 has a connection for a tangential feed line 55, which is connected to a compressed gas source 56 for envelope gas.
  • the housing part 54 On its inside, the housing part 54 has a downward cylindrical flange 57 (cf. FIG. 3).
  • a so-called pipe connector 58 is fastened under the housing part 54 and has a coolant inlet and outlet 61, 62.
  • An outer jacket tube 63 is in turn attached to the pipe connector 58 via its flange 64.
  • a connector 65 is releasably attached.
  • An upper central tube 66, an inner tube 72 and a lower central and separating tube 67 are detachably fastened to an internal thread of the intermediate piece 65 and a nozzle jacket 68 together with the inner wall 69 are detachably fastened to an external thread of the intermediate piece 65.
  • the intermediate piece 65 has passages 71 for the cooling medium of the burner jacket which are aligned parallel to the axis of the burner.
  • the upper middle wall 66 is guided with the upper part of its outer surface in a pressure-tight sliding manner on an inner surface of the pipe connector 58.
  • the inner wall of the nozzle jacket 68 is slidably guided on the inner tube 72.
  • the upper end of the inner tube 72 of the burner jacket 73 is guided in a pressure-tight manner on the cylindrical flange 57 of the housing 54.
  • the entire outer surface of the burner jacket 73 is made free of gaps and steps and thus creates good conditions for sealing in the vessel leadthrough, good uniformity of the cooling and also for preventing parasitic arcing.
  • annular channel 75 is formed, which runs for most of its length parallel to the main axis of the burner and has a conical shape 76 in the area in front of the end face of the nozzle end piece 11 .
  • the conical course 76 of the ring channel 75 in the mouth area is formed by the outer surface of the nozzle end piece 11 and a conical inner surface of the nozzle jacket 68. Both conical surfaces have a coating 77 or 78 made of ceramic.
  • the inside diameter of the nozzle jacket 68 on its end face is smaller than the outer diameter of the nozzle end piece 11, so that the end face of the cooled nozzle jacket 68 for the ceramic tube 39 provides heat protection against the hot atmosphere surrounding the plasma torch or the burner arc.
  • spacer or support bodies 80 are attached to the insulation tube 36 comprising the electrode lance, which extend as far as the inner tube 72 of the torch jacket.
  • displacement body 81 (FIG. 3) can also be attached to the insulation tube 36.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Plasma Technology (AREA)
  • Arc Welding In General (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Macromolecular Compounds Obtained By Forming Nitrogen-Containing Linkages In General (AREA)
  • Developing Agents For Electrophotography (AREA)
  • Discharge Heating (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Manufacture, Treatment Of Glass Fibers (AREA)
EP91110640A 1990-07-11 1991-06-27 Plasmabrenner für übertragenen Lichtbogen Expired - Lifetime EP0465941B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4022111 1990-07-11
DE4022111A DE4022111A1 (de) 1990-07-11 1990-07-11 Plasmabrenner fuer uebertragenen lichtbogen

Publications (3)

Publication Number Publication Date
EP0465941A2 EP0465941A2 (de) 1992-01-15
EP0465941A3 EP0465941A3 (en) 1992-07-01
EP0465941B1 true EP0465941B1 (de) 1997-04-23

Family

ID=6410097

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91110640A Expired - Lifetime EP0465941B1 (de) 1990-07-11 1991-06-27 Plasmabrenner für übertragenen Lichtbogen

Country Status (11)

Country Link
US (1) US5206481A (ja)
EP (1) EP0465941B1 (ja)
JP (1) JPH04229995A (ja)
KR (1) KR100203089B1 (ja)
AT (1) ATE152314T1 (ja)
CA (1) CA2045844A1 (ja)
DE (2) DE4022111A1 (ja)
ES (1) ES2100184T3 (ja)
FI (1) FI103250B1 (ja)
NO (1) NO912474L (ja)
ZA (1) ZA915358B (ja)

Families Citing this family (25)

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Publication number Priority date Publication date Assignee Title
DE4034731A1 (de) * 1990-10-30 1992-05-07 Mannesmann Ag Plasmabrenner zum schmelzen und warmhalten von in gefaessen zu behandelnden materialien
GB9108891D0 (en) * 1991-04-25 1991-06-12 Tetronics Research & Dev Co Li Silica production
US5455401A (en) * 1994-10-12 1995-10-03 Aerojet General Corporation Plasma torch electrode
DE4440323A1 (de) * 1994-11-11 1996-05-15 Sulzer Metco Ag Düse für einen Brennerkopf eines Plasmaspritzgeräts
US5660743A (en) * 1995-06-05 1997-08-26 The Esab Group, Inc. Plasma arc torch having water injection nozzle assembly
FR2735939B1 (fr) * 1995-06-20 1997-09-26 Aerospatiale Dispositif de refroidissement externe d'une torche a plasma
CA2482911C (en) * 2002-04-19 2012-08-07 Thermal Dynamics Corporation Plasma arc torch electrode
JP2005118816A (ja) * 2003-10-16 2005-05-12 Koike Sanso Kogyo Co Ltd プラズマトーチ用のノズル
KR100886872B1 (ko) 2007-06-22 2009-03-06 홍용철 플라즈마 버너
US8257455B2 (en) * 2007-07-30 2012-09-04 Korea Institute Of Machinery & Materials Plasma burner and diesel particulate filter trap
TWI352368B (en) * 2007-09-21 2011-11-11 Ind Tech Res Inst Plasma head and plasma-discharging device using th
IT1392379B1 (it) * 2008-12-24 2012-03-02 Cebora Spa Torcia al plasma ad elevate prestazioni.
DE102009009451A1 (de) * 2009-02-13 2010-08-19 Siemens Aktiengesellschaft Schaltgeräteanordnung mit einer Schaltstrecke
DE102009031857C5 (de) * 2009-07-03 2017-05-11 Kjellberg Finsterwalde Plasma Und Maschinen Gmbh Düse für einen flüssigkeitsgekühlten Plasmabrenner sowie Plasmabrennerkopf mit derselben
CA2765449C (en) 2009-07-03 2014-10-21 Kjellberg Finsterwalde Plasma Und Maschinen Gmbh Nozzle for a liquid-cooled plasma torch and plasma torch head having the same
ITBO20120375A1 (it) * 2012-07-11 2014-01-12 Tec Mo S R L Dispositivo a torcia al plasma raffreddato
DE102012213453A1 (de) * 2012-07-31 2014-02-06 Siemens Aktiengesellschaft Brenner für das Wolfram-Inertgas-Schweißen
DE102013103508A1 (de) * 2013-04-09 2014-10-09 PLASMEQ GmbH Plasmabrenner
US8698036B1 (en) * 2013-07-25 2014-04-15 Hypertherm, Inc. Devices for gas cooling plasma arc torches and related systems and methods
WO2016023112A1 (en) * 2014-08-11 2016-02-18 Best Theratronics Ltd. System and method for metallic isotope separation by a combined thermal-vacuum distillation process
DE102014219275A1 (de) * 2014-09-24 2016-03-24 Siemens Aktiengesellschaft Zündung von Flammen eines elektropositiven Metalls durch Plasmatisierung des Reaktionsgases
US10129969B2 (en) * 2016-04-11 2018-11-13 Hypertherm, Inc. Arc cutting system, including coolant tubes and other consumables, and related operational methods
GB2568106B (en) * 2017-11-07 2022-09-21 Tetronics Tech Limited Plasma Torch Assembly
CN110056893A (zh) * 2019-05-21 2019-07-26 成都高鑫焊割科技有限公司 一种有害气体焚烧裂解处理器
CZ309391B6 (cs) * 2021-09-24 2022-11-09 Thermacut, K.S. Směrovací dílec pro plazmový hořák, sestava a plazmový hořák

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Also Published As

Publication number Publication date
ES2100184T3 (es) 1997-06-16
EP0465941A2 (de) 1992-01-15
JPH04229995A (ja) 1992-08-19
FI913024A (fi) 1992-01-12
FI103250B (fi) 1999-05-14
EP0465941A3 (en) 1992-07-01
FI913024A0 (fi) 1991-06-20
CA2045844A1 (en) 1992-01-12
KR920003820A (ko) 1992-02-29
NO912474L (no) 1992-01-13
ATE152314T1 (de) 1997-05-15
NO912474D0 (no) 1991-06-25
DE4022111A1 (de) 1992-01-23
US5206481A (en) 1993-04-27
KR100203089B1 (ko) 1999-06-15
ZA915358B (en) 1992-04-29
FI103250B1 (fi) 1999-05-14
DE59108674D1 (de) 1997-05-28

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