EP0612567A2 - Chambre d'égalisation de pression comprenant un insert - Google Patents

Chambre d'égalisation de pression comprenant un insert Download PDF

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Publication number
EP0612567A2
EP0612567A2 EP94102122A EP94102122A EP0612567A2 EP 0612567 A2 EP0612567 A2 EP 0612567A2 EP 94102122 A EP94102122 A EP 94102122A EP 94102122 A EP94102122 A EP 94102122A EP 0612567 A2 EP0612567 A2 EP 0612567A2
Authority
EP
European Patent Office
Prior art keywords
burner head
head according
channel
channels
nozzle
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.)
Granted
Application number
EP94102122A
Other languages
German (de)
English (en)
Other versions
EP0612567A3 (fr
EP0612567B1 (fr
Inventor
Franz Künzli
Erwin Hühne
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.)
FRANZ KUENZLI AG
HUEHNE, ERWIN DIETER
Original Assignee
Franz Kuenzli AG
UTP Schweissmaterial GmbH and Co KG
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 Franz Kuenzli AG, UTP Schweissmaterial GmbH and Co KG filed Critical Franz Kuenzli AG
Publication of EP0612567A2 publication Critical patent/EP0612567A2/fr
Publication of EP0612567A3 publication Critical patent/EP0612567A3/fr
Application granted granted Critical
Publication of EP0612567B1 publication Critical patent/EP0612567B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/16—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed
    • B05B7/20—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed by flame or combustion
    • B05B7/201—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed by flame or combustion downstream of the nozzle

Definitions

  • the invention relates to a burner head for burner assemblies, with a single or multiple injector gas mixing system for the internal and / or external mixing of various combustion components, in particular fuel gases, auxiliary combustion gases and possibly liquid fuels, formed by an intermediate piece in the supply channels for the combustion components of a device connection surface up to a nozzle connection side are present, and a nozzle, which consists of a central part with channels and at least one union part, whereby for mixing at least two fuel components, the circumferentially distributed first channels assigned to a first fuel component open into first injector nozzle bores, which in turn lead to a , are connected by an annular gap between the central part and the coupling part, radial injector gap, and wherein the circumferentially distributed second channels assigned to the second combustion component are also in the radial injector gap flow out.
  • various combustion components in particular fuel gases, auxiliary combustion gases and possibly liquid fuels
  • Such a burner head is used, for example, in welding, cutting, flame or heating burners, in flame spraying devices or high-speed flame spray guns for spraying wire, rod and / or powdered spraying filler materials, as well as in high flame pressure guns, for producing synthetic diamond layers on substrate surfaces from a hydrocarbon - High speed oxygen flame with high flame pressure.
  • the burner head consists of an intermediate piece with supply channels and distributor grooves, which are connected to the supply channels, and a nozzle, which is formed from a central part with channels and a union part.
  • the fuel components are fed into the intermediate piece by means of individual, separate lines which open into the respective distributor grooves.
  • an annular gap is enclosed, which serves as a channel for a fuel component and opens into a radial injector gap, the other fuel component is also guided into the radial injector gap through nozzle channels designed as bores in the central part.
  • the distributor grooves guide the respective combustion component into the group of circumferentially distributed supply channels provided in the intermediate piece.
  • the combustion component which usually flows in at high pressure and high speed, is not distributed evenly into all the supply ducts belonging to the respective group, but rather that the combustion component in the supply ducts closest to the gas supply is led to the nozzle with higher pressure , than in the more distant supply channels.
  • This asymmetrical pressure distribution has the very disadvantageous consequence that the burner flame is not rotationally symmetrical and deviates in its flame direction from the central axis of the burner head.
  • the invention is therefore based on the object of providing a burner head which eliminates the disadvantages outlined above and which therefore produces a flame which is formed rotationally symmetrically around the burner head axis.
  • This object is achieved in that, circumferentially distributed in the intermediate piece, radial-axial pressure compensation chambers are connected on the one hand to the individual fuel component supply lines and on the other hand to the associated supply channels of the intermediate piece.
  • the radial-axial pressure compensation chambers change the flow direction of the combustion components in such a way that the more or less direct axial flow through the combustion component is prevented.
  • the cap part of the burner head according to the invention is provided with circumferentially distributed nozzle channels aligned in the installed position and completely covers the central part, towards the front side of the burner head pointing towards the flame, except for an optionally available spray additive guide channel: because with one
  • the central part of the nozzle is very hot due to the flame formation on the end face of the same, especially if, as in high-speed flame spraying, a burner chamber with an expansion nozzle is additionally attached to the end face of the burner head. Insulated cooling for the central part of the nozzle would be structurally very complex and extremely difficult because of its poor accessibility.
  • the preferred arrangement according to the invention of the central part and the union part of the nozzle shields the central part from the flame by the union part.
  • This measure in itself has the consequence that the thermal load on the central part is significantly reduced.
  • the heat generated on the end face of the burner head is dissipated inside the coupling part and thus to the outside of the nozzle, which is easily accessible to a cooling device.
  • a burner head according to the prior art which, due to the formation of the one burner component channel as an annular gap between the central part and the union part, only very few contact surfaces between these two parts, and therefore a poor heat transfer from the central part to the union part of the nozzle has eliminated in an incredibly simple manner.
  • the radial-axial pressure compensation chambers are annular. It may make sense for the individual radial-axial pressure compensation chambers of the individual burner components to be arranged on circles concentric with the central axis of the burner head. This is particularly advantageous if the individual groups of supply channels assigned to the individual fuel components are also arranged in concentric circles in the intermediate piece.
  • the radial-axial pressure compensation can take place by means of baffles integrated in the radial-axial pressure compensation chambers, which means elements which change the direction of flow and which can advantageously consist of stainless steel or brass, but which can also be formed by one or more, interchangeable filter stages.
  • baffles integrated in the radial-axial pressure compensation chambers, which means elements which change the direction of flow and which can advantageously consist of stainless steel or brass, but which can also be formed by one or more, interchangeable filter stages.
  • baffles are also designed to be annular or rotationally symmetrical.
  • the radial-axial pressure compensation chambers can also be provided with gas-permeable, porous material, which is smooth Flow through the combustion components from the distributor grooves into the nearest supply ducts is also prevented, thus ensuring the radial-axial pressure equalization.
  • the radial-axial pressure compensation chambers can be partially or completely filled with this material.
  • the gas-permeable, porous material can be a ceramic foam or a ceramic molded part; An open-pore sintered metal is advantageous for this purpose.
  • the outer fuel component guides which open into the radial injector gap, as an annular gap, but as individual, circumferentially distributed fuel component channels, the spaces between which are thermal bridges between the central part and the Form the union part.
  • This increases the heat transfer speed considerably, reduces the thermal load on the central part through better heat dissipation and prevents tensions between the central part and the union part caused by temperature differences.
  • It is structurally very simple to manufacture these fuel component channels by circumferentially distributed grooves in the central part or in the union part. The remaining, raised gaps then serve as a thermal bridge. This also has the additional advantage that an interference fit is made between the central part and the union part.
  • the throw-over part is expediently surrounded by a cooling space which holds a heat-dissipating medium, it being possible for the heat-dissipating medium to be cooling water.
  • downstream combustion chamber, the transition cone and the expansion nozzle are also surrounded by a cooling jacket, in which cooling channels are located, which are connected to the cooling space around the coupling part of the nozzle. Efficient cooling of the entire front area of the burner head is thus achieved in a simple manner with a single cooling circuit.
  • a liquid fuel component which is fed to the burner head according to the invention does not have to be an individual component, but it can advantageously also consist of a gasoline which has already been gasified and / or a liquid fuel which has already been mixed with oxygen.
  • the intermediate piece has on its device connection surface separate, gas-tightly sealed distributor grooves, into each of which a group of supply channels open.
  • These distributor grooves connect the individual fuel component supply lines to the associated supply channels of the intermediate piece or to the associated radial-axial pressure compensation chambers.
  • a spray additive guide channel is surrounded in the intermediate piece by a coaxial channel and in the central part by a coaxial ring channel, the latter opening into an annular channel which coaxially surrounds the spray additive guide channel in the coupling part: through this Channels surrounding the spray additive guide channel, the spray additive material jet emerging from the spray additive guide channel can be enveloped with a gas coaxially emerging from the end face of the burner head.
  • This gas can be a reaction gas;
  • a cooling gas which may be inert, for example, for low-melting spray additives.
  • a pressure compensation annular space is preferably arranged at least between the coaxial ring channel of the central part and the ring channel of the coupling part.
  • gas distribution bores which can be arranged between the coaxial channel of the intermediate piece and the coaxial ring channel of the central part.
  • the coaxial channels are preferably fed via an envelope gas feed line, which is connected to the coaxial channel of the intermediate piece by means of an envelope gas channel and a distributor annulus which serves for the uniform distribution of the envelope gas.
  • the coaxial channel of the intermediate piece, the coaxial ring channel of the central part and the ring channel of the coupling part are preferably flowed through with water vapor, in particular superheated water vapor.
  • water vapor in particular superheated water vapor.
  • the water vapor or the superheated water vapor which is thus fed to the flame as an additional medium, can improve the combustion, so that better energy utilization and clean, residue-free combustion result.
  • FIG. 1 shows the view of a device connection surface 6 with two fuel component feed lines 40 and a spray additive feed 41.
  • two combustion components for example oxygen and acetylene
  • a spray additive for example a metal powder
  • the fuel components flowing into the burner head through the fuel component supply lines 40 must now be passed on to the nozzle, distributed individually over the circumference, in this exemplary embodiment on circles concentric with the spray additive feed 41.
  • the combustion component flows into the distributor grooves 39, which are sealed off from one another and to the outside by O-rings inserted into the sealing grooves 46.
  • FIG. 3 illustrates the solutions to the object of the invention using this special exemplary embodiment, with two fuel components and a spray additive.
  • the section of FIG. 3 runs according to AA of FIG. 1.
  • the sealing grooves 46 for receiving O-rings are clearly recognizable.
  • the other fuel component is conducted from the fuel component feed line 40 ′′ via the distributor groove 39 ′′ to the circumferentially distributed feed ducts 3 and 4 in the intermediate piece 1, which, as seen from the central axis 23, lie further inside.
  • the fuel component supply lines 40 lie only at one point on the circumference of the combustion head, but the supply ducts 2, 3, 4, 5 are evenly distributed over its circumference.
  • the combustion components from the distributor grooves 39 are first routed into rotationally symmetrical radial-axial pressure compensation chambers 19, 20 arranged concentrically around the central axis 23, where they are by means of Baffles 24, 25 are distributed equally in their dynamic pressure and in terms of quantity over the entire circumference; only then are the fuel components passed on to the supply ducts 2, 3, 4, 5.
  • the supply channels 2, 3, 4, 5 open on the nozzle connection side 7 into the respective channels 10, 11, 17, 18 of the nozzle 8, which is fastened to the intermediate piece 1 by means of a union nut 44.
  • the radially inner channels 10, 11 open into injector nozzle bores 13, 14 with a reduced cross section, as a result of which the speed of the combustion component, here for example oxygen, is extremely increased.
  • the radially outer channels 17, 18 arranged between the central part 9 and the coupling part 12 are passed on to an annular gap 15, which becomes a radial injector gap 16 due to the simultaneous opening of the injector nozzle bores 13, 14.
  • acetylene which for safety reasons can only be brought into the feed line at a low pressure, is conducted into the radial injector gap 16. There it is entrained by the high-speed oxygen jet from the injector nozzle bores 13, 14 into the alternately axially and focusing nozzle channels 28, 29. The resulting fuel gas mixture emerges from the end face 30 of the burner head and is then ignited.
  • the central part 9 of the nozzle 8 is spaced from the end face 30 of the burner head, so that its thermal load is kept within limits; the heat is dissipated from the end face 30 of the burner head within the cap 12.
  • This embodiment of a burner head according to the invention can be used for flame spraying, which is why a spray additive guide channel 38 is fitted along the central axis 23.
  • Figure 4 shows the alternating axial and focussing design of the nozzle channels 28 and 29 in section BB according to Figure 3. Furthermore, it can be clearly seen here that the radially outer channels 17, 18 are formed by circumferentially distributed grooves in the central part 9, whereby an interference fit between the coupling part 12 and the remaining thermal bridges 31 of the central part 9. It is immediately clear that the heat balance between the central part 9 and the throwing part 12 is substantially improved compared to a channel 17, 18 designed as an annular gap.
  • FIG. 5 shows a view of a device connection surface 6 of another embodiment of the burner head according to the invention, with four different fuel component supply lines 40 and a spray additive guide channel 38.
  • FIG. 6 shows the intermediate piece 1 in the section AA according to FIG. 5.
  • FIG. 5 accordingly also forms a view in the direction B of FIG. 6.
  • the spray additive guide channel 38 is also fitted here along the central axis 23.
  • FIG. 7, which shows a view in the direction C of FIG. 6, clarifies that the four different combustion components on the nozzle connection side 7 are now guided in supply channel groups 2, 3, 4, 5 which are distributed around the circumference on concentric circles.
  • FIG. 8 shows how an embodiment of the burner head according to the invention with intermediate piece 1, central part 9 and coupling part 12 is integrated into a burner gun.
  • the nozzle channels 28, 29 guiding the fuel component mixture open at the end face of the burner head 30 into a combustion chamber 33, which is continued via a transition cone 34 in an expansion nozzle 35.
  • the spray additive guide channel 38 also opens into the combustion chamber 33.
  • the device connection surface 6 of the intermediate piece 1 is connected by means of screws 48 to a connection piece 45, in which there are cooling water connections 42, as well as two fuel component supply lines 40 and a spray additive supply 41.
  • the fuel components are conducted from the fuel component supply lines 40 via the distributor grooves 39 to the radial-axial pressure compensation chambers 19, 20 with their baffles 24, 25, from where they pass through the supply ducts 2, 3, 4 , 5 are led to the nozzle 8.
  • the cooling of the nozzle 8 takes place via a cooling water circuit;
  • the cooling space 32 surrounding the coupling part 12 is connected to the cooling water connections 42.
  • the combustion chamber 33, the transition cone 34 and the expansion nozzle 35 are cooled in the cooling jacket 36 by the cooling channels 37 connected to the cooling chamber 32, and thus in the same cooling water circuit.
  • the cooling channels 37 are formed by annular gaps between the cooling jacket 36 and the expansion nozzle wall 49 on the one hand, and between the cooling jacket 36 and the outer screw sleeve 47 on the other hand.
  • the entire burner gun can be mounted by means of a mounting plate 50 attached to the burner head holder 43.
  • FIG. 10 shows a section of a burner head according to the invention, with which the spray additive jet can be provided with an enveloping gas coaxially surrounding it when it emerges from the end face 30 of the burner head:
  • Nitrogen, argon, carbon dioxide or dry, oil-free compressed air, in special cases also oxygen or forming gas, as well as water vapor or superheated water vapor at a pressure which is greater than or equal to the combustion chamber pressure during the combustion are introduced into the envelope gas channel 54, from where they enter the Distributor annulus 55 pass for the purpose of uniform distribution around the spray additive guide channel 38, from there through the coaxial channel 56, the pressure compensation annular space 57, the coaxial ring channel 59 and the through holes of the centering ring 60 into the pressure compensation ring m 61 to be guided in order to finally flow out in a coaxially uniform manner through the annular channel 62 on the burner head face 30 in the form of a tube.
  • FIG. 11 a view in direction A according to FIG. 10, shows the ring channel 62, which is arranged coaxially around the spray additive guide channel 38 and from which the envelope gas emerges on the end of the burner head.
  • FIG. 12 shows, like FIG. 8, a section through a burner gun with a burner head according to the invention, the burner head corresponding to an embodiment as in FIG. 10 and the burner gun modified from the embodiment from FIG. 8:
  • the spray additive guide channel 38 is in the intermediate piece 1 , in the central part 9 and in the coupling part 12, as in FIG. 10, surrounded by a coaxial channel 56, a pressure compensation ring space 57, gas distributor bores 58, a coaxial ring channel 59, a centering ring 60 with through-bores, a pressure compensation ring space 61 and a ring channel 62.
  • a cooling gas in this illustrated embodiment a cooling gas
  • the embodiment shown is particularly suitable for high-speed (HVOF) flame spraying of low-melting, reactive injection additives that react strongly with oxygen in the melt-plastic and / or molten state:
  • HVOF high-speed flame spraying of low-melting, reactive injection additives that react strongly with oxygen in the melt-plastic and / or molten state:
  • the temperature becomes enveloped by enveloping the spray additive jet with a cooling gas applied to the envelope gas connection 52 to which the spray additive particles are heated is lowered;
  • the thermal load on the spray additive particles is further reduced due to the comparatively short design of the expansion nozzle 35. Due to the short design of the expansion nozzle 35, the expansion nozzle wall 49, the cooling jacket 36 and the outer screw sleeve 47 are also shorter.
  • FIG. 13 a view in the direction A according to FIG. 12, additionally shows the sheath gas connection 52 compared to FIG. 9, in this embodiment identified as a cooling gas connection.
  • the present invention thus provides a burner head which produces a flame which is formed rotationally symmetrically about the axis of the burner head and which, according to various embodiments, is advantageously suitable for flame spraying, in particular for high-speed flame spraying of high-melting as well as reactive, deep-melting materials, the invention not being applicable limited to the embodiments shown here.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Gas Burners (AREA)
  • Measuring Pulse, Heart Rate, Blood Pressure Or Blood Flow (AREA)
  • External Artificial Organs (AREA)
  • Earth Drilling (AREA)
  • Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
EP94102122A 1993-02-26 1994-02-11 Chambre d'égalisation de pression comprenant un insert Expired - Lifetime EP0612567B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4305896A DE4305896A1 (de) 1993-02-26 1993-02-26 Druckausgleichskammer mit Einsatzelement
DE4305896 1993-02-26

Publications (3)

Publication Number Publication Date
EP0612567A2 true EP0612567A2 (fr) 1994-08-31
EP0612567A3 EP0612567A3 (fr) 1995-08-02
EP0612567B1 EP0612567B1 (fr) 1998-04-29

Family

ID=6481356

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94102122A Expired - Lifetime EP0612567B1 (fr) 1993-02-26 1994-02-11 Chambre d'égalisation de pression comprenant un insert

Country Status (6)

Country Link
US (1) US5513801A (fr)
EP (1) EP0612567B1 (fr)
AT (1) ATE165533T1 (fr)
DE (2) DE4305896A1 (fr)
DK (1) DK0612567T3 (fr)
ES (1) ES2118989T3 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0825273A1 (fr) * 1996-08-20 1998-02-25 The BOC Group plc Revêtement de substrats avec des céramiques à haute température

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6076748A (en) * 1998-05-04 2000-06-20 Resch; Darrel R. Odor control atomizer utilizing ozone and water
ATE501095T1 (de) * 2001-05-30 2011-03-15 Prysmian Spa Verfahren und brenner zum herstellen einer glasvorform für optische fasern durch abscheidung aus der dampfphase
DE10357440B4 (de) * 2003-02-05 2006-02-09 Hühne, Erwin Dieter Niedertemperatur-Hochgeschwindigkeits-Flammspritzsystem zum Vorbereiten von Oberflächen und/oder zum thermischen Spritzen von pulverförmigen Spritzzusatzwerkstoffen
US20050145270A1 (en) * 2003-12-31 2005-07-07 Ray R. K. Pressure washer with injector
CN101363626B (zh) 2007-08-06 2015-05-20 国际壳牌研究有限公司 制造燃烧器前脸的方法
CN101363623B (zh) * 2007-08-06 2010-12-08 国际壳牌研究有限公司 燃烧器

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BE435836A (fr) *
US2397165A (en) * 1943-10-25 1946-03-26 Metallizing Engineering Co Inc Gun construction for gas blast spraying heat-fusible materials
FR996422A (fr) * 1949-02-07 1951-12-19 Schori Metallising Process Ltd Procédé pour le revêtement des surfaces
DE1135263B (de) * 1958-03-27 1962-08-23 Metallgesellschaft Ag Duesenkopf fuer Flammspritzpistolen
DE3033579A1 (de) * 1980-09-06 1982-03-25 Castolin S.A., 1025 St. Sulpice, Vaud Rueckzuendsicheres auftragsgeraet
US4384677A (en) * 1980-12-23 1983-05-24 Eutectic Corporation Nozzle construction for a gas torch
US4836447A (en) * 1988-01-15 1989-06-06 Browning James A Duct-stabilized flame-spray method and apparatus
DE8909503U1 (de) * 1989-08-08 1989-09-28 UTP Schweißmaterial GmbH & Co KG, 7812 Bad Krozingen Hochgeschwindigkeitsflammspritzpistole
FR2642990A1 (fr) * 1989-02-10 1990-08-17 Castolin Sa Dispositif pour projeter a la flamme des materiaux pulverulents
US5230470A (en) * 1991-06-19 1993-07-27 Alberta Research Council Flame spray applicator system

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US2367316A (en) * 1937-02-27 1945-01-16 Linde Air Prod Co Blowpipe and nozzle therefor
US2392593A (en) * 1944-02-02 1946-01-08 Alexander Milburn Company Torch tip
FR1084684A (fr) * 1953-06-10 1955-01-21 Metallisation Soc Nouv Chalumeau ou pistolet métalliseur
DE1003004B (de) * 1954-10-09 1957-02-21 Metallgesellschaft Ag Spritzpistole fuer schmelzfluessiges Material mit Draht- oder Pulverzufuehrung
US2920001A (en) * 1955-07-11 1960-01-05 Union Carbide Corp Jet flame spraying method and apparatus
SU626313A1 (ru) * 1976-01-20 1978-09-30 Предприятие П/Я А-1944 Газокислородный резак
US4136827A (en) * 1977-02-28 1979-01-30 Mushenko Nikolai Y Oxygen-fuel cutting torch
US4375954A (en) * 1979-12-26 1983-03-08 Roger Trudel Oil and gas combination nozzle
US4361285A (en) * 1980-06-03 1982-11-30 Fluid Kinetics, Inc. Mixing nozzle
US4363443A (en) * 1980-09-26 1982-12-14 Eutectic Corporation Gas-torch construction
FR2602309B1 (fr) * 1986-07-30 1988-11-10 Soudure Autogene Francaise Buse de coupe siderurgique a double couronne de chauffe

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE435836A (fr) *
US2397165A (en) * 1943-10-25 1946-03-26 Metallizing Engineering Co Inc Gun construction for gas blast spraying heat-fusible materials
FR996422A (fr) * 1949-02-07 1951-12-19 Schori Metallising Process Ltd Procédé pour le revêtement des surfaces
DE1135263B (de) * 1958-03-27 1962-08-23 Metallgesellschaft Ag Duesenkopf fuer Flammspritzpistolen
DE3033579A1 (de) * 1980-09-06 1982-03-25 Castolin S.A., 1025 St. Sulpice, Vaud Rueckzuendsicheres auftragsgeraet
US4384677A (en) * 1980-12-23 1983-05-24 Eutectic Corporation Nozzle construction for a gas torch
US4836447A (en) * 1988-01-15 1989-06-06 Browning James A Duct-stabilized flame-spray method and apparatus
FR2642990A1 (fr) * 1989-02-10 1990-08-17 Castolin Sa Dispositif pour projeter a la flamme des materiaux pulverulents
DE8909503U1 (de) * 1989-08-08 1989-09-28 UTP Schweißmaterial GmbH & Co KG, 7812 Bad Krozingen Hochgeschwindigkeitsflammspritzpistole
US5230470A (en) * 1991-06-19 1993-07-27 Alberta Research Council Flame spray applicator system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0825273A1 (fr) * 1996-08-20 1998-02-25 The BOC Group plc Revêtement de substrats avec des céramiques à haute température

Also Published As

Publication number Publication date
US5513801A (en) 1996-05-07
DE4305896A1 (de) 1994-09-01
EP0612567A3 (fr) 1995-08-02
ES2118989T3 (es) 1998-10-01
EP0612567B1 (fr) 1998-04-29
DE59405819D1 (de) 1998-06-04
DK0612567T3 (da) 1999-02-15
ATE165533T1 (de) 1998-05-15

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