WO2025099554A1 - Deposition nozzle for coating a surface of a piece - Google Patents

Deposition nozzle for coating a surface of a piece Download PDF

Info

Publication number
WO2025099554A1
WO2025099554A1 PCT/IB2024/060874 IB2024060874W WO2025099554A1 WO 2025099554 A1 WO2025099554 A1 WO 2025099554A1 IB 2024060874 W IB2024060874 W IB 2024060874W WO 2025099554 A1 WO2025099554 A1 WO 2025099554A1
Authority
WO
WIPO (PCT)
Prior art keywords
nozzle
deposition
nozzle body
powder feeding
recess
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
PCT/IB2024/060874
Other languages
French (fr)
Inventor
Fabiano Carminati
Francesco Andrea BRESCIANI
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.)
Brembo SpA
Original Assignee
Brembo SpA
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 Brembo SpA filed Critical Brembo SpA
Publication of WO2025099554A1 publication Critical patent/WO2025099554A1/en
Anticipated expiration legal-status Critical
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/16Spraying 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
    • B05B7/22Spraying 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 electrically, magnetically or electromagnetically, e.g. by arc
    • B05B7/228Spraying 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 electrically, magnetically or electromagnetically, e.g. by arc using electromagnetic radiation, e.g. laser
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
    • B22F12/50Means for feeding of material, e.g. heads
    • B22F12/53Nozzles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • B23K26/1462Nozzles; Features related to nozzles
    • B23K26/1464Supply to, or discharge from, nozzles of media, e.g. gas, powder, wire
    • B23K26/1476Features inside the nozzle for feeding the fluid stream through the nozzle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y30/00Apparatus for additive manufacturing; Details thereof or accessories therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D65/00Parts or details
    • F16D65/02Braking members; Mounting thereof
    • F16D65/12Discs; Drums for disc brakes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D2202/00Metallic substrate
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D2401/00Form of the coating product, e.g. solution, water dispersion, powders or the like
    • B05D2401/30Form of the coating product, e.g. solution, water dispersion, powders or the like the coating being applied in other forms than involving eliminable solvent, diluent or dispersant
    • B05D2401/32Form of the coating product, e.g. solution, water dispersion, powders or the like the coating being applied in other forms than involving eliminable solvent, diluent or dispersant applied as powders
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
    • B05D3/06Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/25Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/006Vehicles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/34Laser welding for purposes other than joining
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y10/00Processes of additive manufacturing

Definitions

  • the present invention relates to a deposition nozzle for coating a surface of a piece, and to an assembly comprising said deposition nozzle and said piece, e . g . , a braking band of a disc brake disc .
  • the brake caliper is generally arranged straddling the outer peripheral margin of a brake disc, adapted to rotate about a rotation axis (A-A) defining an axial direction (X- X) .
  • a radial direction (R-R) substantially orthogonal to said axial direction (X-X)
  • a circumferential direction (C-C) orthogonal to both said axial direction (X-X) and said radial direction (R-R) , as well as a tangential direction ( T-T ) locally, or rather punctually, i . e . , in an intersection point of an axial and a radial direction, orthogonal to both said axial direction (X-X ) and said radial direction (R-R) .
  • discs for a disc brake comprise a bell adapted to associate the disc with a hub of a vehicle , from which an annular portion extends , referred to as a braking band, intended to cooperate with brake pads of a caliper .
  • the braking band is obtained by two facing plates connected to each other by means of connection elements , e . g . , in the form of pins or fins .
  • connection elements e . g .
  • the outer surfaces of the two plates define opposite braking surfaces
  • the inner surfaces together with the pins or fins , delimit ventilation channels for cooling the disc, which channels are crossed by air according to a centrifugal direction during the rotary motion of the disc itself .
  • Said braking band is intended to cooperate with disc brake calipers adapted to apply a braking action to the vehicle by applying, by means of the aforesaid pads , friction to the opposite surfaces of the two plates , referred to as braking surfaces .
  • the metal powder is thus applied in layers to the base material with which it melts without creating pinholes or cracks .
  • the metal powder generates a high-strength welding j oint with the surface .
  • a metal layer that can be subj ected to mechanical machining is formed .
  • the laser cladding process not only ensures less particulate matter, but also less wear of the braking band .
  • Example of laser cladding technologies are : LMD (Laser Metal Deposition) , EHLA (Extreme High-speed Laser Material Deposition) .
  • WO2023152014A1 discloses a laser deposition welding method for producing coating layers on opposite surfaces of a component .
  • an additive material in particular an additive powder material
  • a processing traj ectory in particular a spiral-shaped processing traj ectory
  • the additive material and the component are heated along the processing traj ectory by means of a laser beam so that the additive material connects to the component upon impacting against the surface of the component , and coating layers are simultaneously produced on the opposite surfaces of the component .
  • WO2021156317A1 discloses a material depositing unit comprising a radiating unit, a powder discharging device , having seven powder discharging units , and a powder dividing unit, having seven powder channels , where the individual powder channels are connected to the individual powder channels by means of an interchangeable connection element, where all the powder discharging units have an interchangeable powder discharging element, where the powder discharging element is elongated in shape and is arranged at least partially inside the corresponding powder discharging unit . [0018 ] .
  • WO2023116983A1 discloses an apparatus for coating a piece ; said apparatus has the following components : a laser device for generating a laser beam with a laser focus ; a noz zle for feeding powder; and an advancement actuator system for advancing the laser device and the powder noz zle .
  • the laser device is designed to thermally treat the powder material provided by a powder nozzle to coat a surface of a piece and/or thermally treat this surface .
  • the equipment further comprises :
  • US2006065650A1 discloses a compact coaxial noz zle useful in laser welding operations in which the piece to be welded has a narrow or confined geometry .
  • the nozzle is generally conical in shape and ends with a relatively small tip .
  • the noz zle includes a central opening for laser discharge .
  • the conical shape allows the movement of the nozzle in narrow areas .
  • the nozzle includes a cooling j acket to provide coolant to the noz zle .
  • the nozzle also includes a powder mixing chamber which provides good mixing of the powder filling material with a coaxial discharge about the laser .
  • the noz zle provides for the passage of inert gas from an upper inlet, through passages , out of an annular discharge .
  • the annular discharge is also arranged coaxially about the central laser .
  • annular discharge provides the inert gas mixing to minimize turbulent flow problems associated with limiting plates .
  • US2009095214A1 discloses a laser device for applying a coating to a part comprising a laser which can generate laser light, which is adapted to heat the coating and the part .
  • Said device has a main body which defines a laser light channel adapted to transmit the laser light to the part, a coating channel adapted to transmit the coating to the part, and a vacuum channel and nozzle having an outlet .
  • the nozzle comprises a dispensing port at one end of the laser light channel , a coating port at one end of the coating channel , and a vacuum port at one end of the vacuum channel , where the vacuum port is positioned adj acent to the dispensing port .
  • the vacuum port creates a vacuum, pulling the coating toward the piece .
  • the powder supply device has a plurality of powder supply lines extending through a second end of the nozzle head, which is opposite to the first nozzle head, in the direction toward the cavity to direct the powder from a powder reservoir into the cavity .
  • WO9520458A1 discloses a laser metal powder coating apparatus which includes a removable conical nozzle having a central opening through which the laser beam and the metal powder exit from the apparatus .
  • the opening extends up to the front surface of the noz zle which is close to the piece .
  • the axial passages in the tapered nozzle wall extend backward from the front surface and are arranged in a series centered about the opening .
  • the inert gas flows through these axial passages to cool the noz zle and form an oxidation screen in the liquid metal pool .
  • the metal powder for the coating is dispensed to a conical passage at the inlets thereof and exits through the opening .
  • a recess is made in the nozzle to reduce the inclination angle at which the gun needs to be tilted when coating the undercut zone, e.g., an undercut between bell and braking band.
  • FIG. 1 depicts an axonometric view of an assembly comprising a piece , in this case a brake disc comprising a ventilated braking band connected in one piece to a bell , or portion for the connection of the brake disc with a support, or hub, of a vehicle , and a deposition noz zle placed close to the bell and oriented so as to treat the connection channel between the braking surface , or surface to be treated, of the braking band and the bell ;
  • FIG. - figure 2 shows a side view of the assembly in figure 1 , in which the deposition nozzle is viewed from the side and the recess thereof is highlighted;
  • FIG. 3 diagrammatically depicts a side view of the cladding process performed with the deposition nozzle of the present invention while performing a treatment on a surface to be treated of a piece ;
  • FIG. 4 shows a side view of the assembly in figure 1 , in which the deposition nozzle is shown frontally;
  • FIG. 5 depicts an axonometric view sectioned on a plane passing through the axial A-A and radial R-R directions of the brake disc passing through the nozzle axis L-L of the assembly in figure 1 ;
  • FIG. 6 depicts an axonometric view of the deposition nozzle of the present invention
  • FIG. 7 to 9 depict top, side , and bottom views of the deposition nozzle in figure 6 ;
  • FIG. 10 shows an axonometric view sectioned according to the plane passing through the nozzle axis and defined by letters A-A in figure 9 of the deposition noz zle in figure 6 ;
  • FIG. 11 shows an axonometric view sectioned according to the plane passing through the nozzle axis and defined by letters B-B in figure 9 of the deposition noz zle in figure 6 ;
  • FIG. 12 shows an axonometric view sectioned according to the plane passing through the nozzle axis and defined by letters C-C in figure 9 of the deposition noz zle in figure 6 ;
  • FIG. 13 shows a very diagrammatic side view of a disc surface treatment system
  • figure 14 shows a deposition nozzle and piece-to-be- treated assembly according to the prior art ;
  • f igure 15 shows a deposition nozzle and piece-to-be- treated assembly according to the invention .
  • Said deposition nozzle 1 comprises a radiation conduit 5 connectable to a laser device 6 to generate a focused laser beam 7 through a laser focusing device 8 , said focused laser beam 7 being directed along a predetermined direction defining a nozzle axis L-L.
  • Said deposition nozzle 1 comprises a nozzle body 9; said nozzle body 9 is initially axisymmetric in shape with respect to said nozzle axis L-L.
  • Said nozzle body 9 has an elongated shape toward a nozzle radiation mouth 10.
  • Said deposition nozzle 1 further comprises a plurality of powder feeding conduits 11 having extension along powder feeding directions D-D converging toward said nozzle axis L-L.
  • said nozzle body 9 comprises a nozzle recess 13, which makes said nozzle body 9 dissymmetric.
  • Said nozzle recess 13 affects an arc extending about said nozzle axis L-L by less than 180 DEG, preferably between 140 DEG and 160 DEG.
  • Said nozzle recess 13 tapers the elongated shape of the nozzle body 9 locally narrowing the nozzle body 9 toward said nozzle radiation mouth 10.
  • said nozzle recess 13 is given by the intersection between a ball and said nozzle body 9 when still axisymmetric.
  • said nozzle recess 13 is obtained by the subtraction of a ball portion from said nozzle body 9 when still axisymmetric.
  • said nozzle body 9 comprises a first proximal cylindrical nozzle portion 14 , a first intermediate conical portion 15 , a second intermediate cylindrical portion 16, and a second distal conical portion 17 .
  • said noz zle recess 13 af fects said first intermediate conical portion 15, said second intermediate cylindrical portion 16, and said second distal conical portion 17 .
  • said nozzle body 9 comprises a first proximal cylindrical noz zle portion 14 distally connected to a first intermediate conical portion 15 distally connected to a second intermediate cylindrical portion 16 distally connected to a second distal conical portion 17 .
  • Said noz zle recess 13 affects said first intermediate conical portion 15, said second intermediate cylindrical portion 16 , and said second distal conical portion 17 .
  • said powder feeding conduits 11 converge in a single point of intersection 12 of the powder feeding directions , placed on said noz zle axis L- L .
  • said plurality of powder feeding conduits 11 is distributed so as to have the powder feeding conduits 11 equally spaced apart from each other and mutually converging .
  • said radiation conduit 5 has cylinder-shaped radiation conduit walls 18 .
  • said radiation conduit 5 delimits a passage in the shape of a right cylinder.
  • said nozzle radiation 10 is delimited by a circumference-shaped periphery.
  • said nozzle radiation mouth 10 is orthogonal to said nozzle axis L-L.
  • said powder feeding conduits 11 are distributed in said nozzle body 9 in an arc extending about said nozzle axis L-L with a width of less than 200 DEG.
  • said powder feeding conduits 11 delimit a cylindrical passage with rectilinear extension along a straight powder feeding direction D-D.
  • the present invention also relates to a deposition nozzle 1 and piece-to-be-treated assembly, comprising
  • a laser beam e.g., surrounded by a shielding gas, is focused into the deposition nozzle 1.
  • the process powder 20 is fed into the powder feeding conduits 11.
  • the deposition nozzle is cooled with fluid, e.g., water.
  • the laser beam 19 is directed along a direction defined by the nozzle axis L-L and focuses on a point, in which point the melting and thus the process activation occur, which point is preferably close to or coinciding with the intersection point of the powder feeding directions D-D.
  • the surface to be treated 2 of the piece 3 is heated, e.g., melts, and creates a bonding zone, to which the cladding layer obtained by activating the powder with the laser, e.g., by melting the powder at least partially, is bonded ( Figure 3) .
  • the nozzle body 9, by virtue of the nozzle recess 13, is very close to the bell 22 and allows having a very small angle 23, for example between 13 DEG and 20 DEG, between the direction given by the extension of the nozzle axis L-L and the normal to the surface to be treated 2, e.g., the axial direction A-A of the brake disc 21 even when the laser beam 19 is directed to the connection portion between the braking band 3 and the bell 22, i.e., the undercut given by the connection channel.
  • a very small angle 23 for example between 13 DEG and 20 DEG

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Optics & Photonics (AREA)
  • Materials Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • General Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Electromagnetism (AREA)
  • Nozzles (AREA)
  • Laser Beam Processing (AREA)

Abstract

Deposition nozzle for coating a surface of a piece The present invention relates to a deposition nozzle (1) for coating a surface (2) of a piece (3) by means of the heat treatment of additive material, in particular powder material (4), and/or for thermally treating the surface (2) of said piece (3), comprising - a radiation conduit (5) connectable to a laser device (6) to generate a focused laser beam (7) through a laser focusing device (8), said focused laser beam (7) being directed along a predetermined direction defining a nozzle axis (L-L); wherein - said deposition nozzle (1) comprises a nozzle body (9); said nozzle body (9) is initially axisymmetric-in shape with respect to said nozzle axis (L-L); - said nozzle body (9) has an elongated shape toward a nozzle radiation mouth (10); - said deposition nozzle (1) further comprises a plurality of powder feeding conduits (11) having extension along powder feeding directions (D-D) converging toward said nozzle axis (L-L); and wherein - said nozzle body (9) comprises a nozzle recess (13) which makes said nozzle body (9) dissymmetric; - said nozzle recess (13) affects an arc extending about said nozzle axis (L-L) by less than 180 DEG, preferably between 140 DEG and 160 DEG; - said nozzle recess (13) tapers the elongated shape of the nozzle body (9) locally narrowing the nozzle body (9) toward said nozzle radiation mouth (10); - said plurality of powder feeding conduits (11) being arranged entirely in the part of nozzle body (9) not affected by said nozzle recess (13).

Description

Deposition nozzle for coating a surface of a piece DESCRIPTION
[0001 ] . Field of the invention
[0002 ] . The present invention relates to a deposition nozzle for coating a surface of a piece, and to an assembly comprising said deposition nozzle and said piece, e . g . , a braking band of a disc brake disc .
[0003] . Background art
[0004 ] . In a disc brake , the brake caliper is generally arranged straddling the outer peripheral margin of a brake disc, adapted to rotate about a rotation axis (A-A) defining an axial direction (X- X) . In a disc brake , there are defined a radial direction (R-R) substantially orthogonal to said axial direction (X-X) , and a circumferential direction (C-C) , orthogonal to both said axial direction (X-X) and said radial direction (R-R) , as well as a tangential direction ( T-T ) locally, or rather punctually, i . e . , in an intersection point of an axial and a radial direction, orthogonal to both said axial direction (X-X ) and said radial direction (R-R) .
[0005 ] . As is known, discs for a disc brake comprise a bell adapted to associate the disc with a hub of a vehicle , from which an annular portion extends , referred to as a braking band, intended to cooperate with brake pads of a caliper . In the case of discs of ventilated type , the braking band is obtained by two facing plates connected to each other by means of connection elements , e . g . , in the form of pins or fins . The outer surfaces of the two plates define opposite braking surfaces , while the inner surfaces , together with the pins or fins , delimit ventilation channels for cooling the disc, which channels are crossed by air according to a centrifugal direction during the rotary motion of the disc itself .
[0006] . Said braking band is intended to cooperate with disc brake calipers adapted to apply a braking action to the vehicle by applying, by means of the aforesaid pads , friction to the opposite surfaces of the two plates , referred to as braking surfaces .
[0007 ] . It is known that during the operation of the brakes , the friction between the pads of brake calipers and the braking surfaces of the braking band generates particulate matter .
[0008 ] . In particular, the automotive braking systems generate the aforementioned particulate matter, resulting in damage to health . Based on these assumptions , the Euro 7 exhaust gas standard (European Community standard) introduces restrictions to the amount of the allowed emitted particulate matter .
[0009] . Currently, to solve this drawback, it is known to coat the braking band of the disc by means of laser cladding technology : the powder to be coated is conveyed directly into the focus of the laser beam, where it melts in contact with air and reaches the molten surface of the brake disc . Argon, as an inert shielding gas , also passes through the noz zle so that the melting zone is substantially surrounded by this shielding gas .
[0010 ] . The metal powder is thus applied in layers to the base material with which it melts without creating pinholes or cracks .
[0011 ] . At this stage, the metal powder generates a high-strength welding j oint with the surface . After cooling, a metal layer that can be subj ected to mechanical machining is formed .
[0012 ] . The special feature of this technique is that several identical or even di fferent metal layers can be purposefully superimposed .
[0013] . The laser cladding process not only ensures less particulate matter, but also less wear of the braking band .
[0014 ] . Example of laser cladding technologies are : LMD (Laser Metal Deposition) , EHLA (Extreme High-speed Laser Material Deposition) .
[0015 ] . Examples of devices for applying these technologies to surfaces are disclosed in the following documents .
[0016] . WO2023152014A1 discloses a laser deposition welding method for producing coating layers on opposite surfaces of a component . In particular, on each surface , an additive material , in particular an additive powder material , is directed onto each surface along a processing traj ectory, in particular a spiral-shaped processing traj ectory, where the additive material and the component are heated along the processing traj ectory by means of a laser beam so that the additive material connects to the component upon impacting against the surface of the component , and coating layers are simultaneously produced on the opposite surfaces of the component .
[0017 ] . WO2021156317A1 discloses a material depositing unit comprising a radiating unit, a powder discharging device , having seven powder discharging units , and a powder dividing unit, having seven powder channels , where the individual powder channels are connected to the individual powder channels by means of an interchangeable connection element, where all the powder discharging units have an interchangeable powder discharging element, where the powder discharging element is elongated in shape and is arranged at least partially inside the corresponding powder discharging unit . [0018 ] . WO2023116983A1 discloses an apparatus for coating a piece ; said apparatus has the following components : a laser device for generating a laser beam with a laser focus ; a noz zle for feeding powder; and an advancement actuator system for advancing the laser device and the powder noz zle .
[0019] . The laser device is designed to thermally treat the powder material provided by a powder nozzle to coat a surface of a piece and/or thermally treat this surface .
[0020 ] . The equipment further comprises :
[0021 ] . - a measuring device for detecting the coordinates of a point on a surface to be coated;
[0022 ] . - an adj ustment device for adj usting the laser focus and the powder nozzle with respect to each other .
[0023] . US2006065650A1 discloses a compact coaxial noz zle useful in laser welding operations in which the piece to be welded has a narrow or confined geometry .
[0024 ] . The nozzle is generally conical in shape and ends with a relatively small tip .
[0025 ] . The noz zle includes a central opening for laser discharge . [0026] . The conical shape allows the movement of the nozzle in narrow areas .
[0027 ] . The nozzle includes a cooling j acket to provide coolant to the noz zle .
[0028 ] . The nozzle also includes a powder mixing chamber which provides good mixing of the powder filling material with a coaxial discharge about the laser .
[0029] . Finally, the noz zle provides for the passage of inert gas from an upper inlet, through passages , out of an annular discharge .
[0030 ] . The annular discharge is also arranged coaxially about the central laser .
[0031 ] . Moreover, the annular discharge provides the inert gas mixing to minimize turbulent flow problems associated with limiting plates .
[0032 ] . US2009095214A1 discloses a laser device for applying a coating to a part comprising a laser which can generate laser light, which is adapted to heat the coating and the part . Said device has a main body which defines a laser light channel adapted to transmit the laser light to the part, a coating channel adapted to transmit the coating to the part, and a vacuum channel and nozzle having an outlet .
[0033] . The nozzle comprises a dispensing port at one end of the laser light channel , a coating port at one end of the coating channel , and a vacuum port at one end of the vacuum channel , where the vacuum port is positioned adj acent to the dispensing port . In operation, the vacuum port creates a vacuum, pulling the coating toward the piece .
[0034 ] . US2015298258A1 discloses a powder supply device for a laser powder welding device . [0035 ] . The powder supply device has a noz zle head which tapers along a longitudinal axis of the powder supply device in the direction of a first end . A cavity which tapers toward the first end of the nozzle head is arranged radially about the longitudinal axis inside the nozzle head . The cavity leads to an annular opening at the first end for the discharge of a powder .
[0036] . The powder supply device has a plurality of powder supply lines extending through a second end of the nozzle head, which is opposite to the first nozzle head, in the direction toward the cavity to direct the powder from a powder reservoir into the cavity .
[0037 ] . WO9520458A1 discloses a laser metal powder coating apparatus which includes a removable conical nozzle having a central opening through which the laser beam and the metal powder exit from the apparatus .
[0038 ] . The opening extends up to the front surface of the noz zle which is close to the piece .
[0039] . The axial passages in the tapered nozzle wall extend backward from the front surface and are arranged in a series centered about the opening .
[0040 ] . The inert gas flows through these axial passages to cool the noz zle and form an oxidation screen in the liquid metal pool .
[0041 ] . Water is circulated through a water j acket between the openings to cool the apparatus .
[0042 ] . The metal powder for the coating is dispensed to a conical passage at the inlets thereof and exits through the opening .
[0043] . However, these known solutions do not allow solving a particular need, as will be explained below.
[0044] . By holding the nozzle in a vertical position (laser beam perpendicular to the piece to be treated, e.g., to the braking band) , it is not possible to coat the undercuts, e.g., the undercut between the braking band and the brake disc bell, or portions of the braking band close to the brake disc bell, such as the groove (or gully) at the junction between the bell and the disc braking band present in some discs, for example (see Figure 14 regarding a solution of the prior art) .
[0045] . This problem arises because of the size of the nozzle body itself, which abuts against the disc bell when held in a vertical position. It is necessary to tilt the nozzle at an extreme inclination angle in order to direct the laser into the undercut to also coat these portions of the disc.
[0046] . The technologies used today exhibit a reduction in efficiency and quality of the coating made in the undercut portion between bell and disc braking band when made by tilting the nozzle as previously described.
[0047] . The main problems identifiable from this solution in Figure 14 are:
[0048] . - loss of efficiency and quality due to the need to tilt, or tilt at a high angle, the process powder distribution unit to process specific parts or components during the laser cladding operation;
[0049] . - inability to process specific parts or components using laser cladding techniques due to the geometry of the part or component to be processed;
[0050] . - longer overall processing cycle time.
[0051] . Solut ion
[0052] . It is the object of the present invention to provide a deposition nozzle which also allows processing zones close to the undercuts to be treated with greater precision and speed.
[0053] . This and other objects and advantages are achieved by a deposition nozzle according to claim 1 as well as by a deposition nozzle and piece-to-be-treated assembly according to claim 10.
[0054] . Some advantageous embodiments are the subject of the dependent claims.
[0055] . From the discussion of this solution, it was found that the suggested solution allows obtaining a reduction of the gun nozzle section and in particular a non-axisymmetric nozzle.
[0056] . In particular, a recess is made in the nozzle to reduce the inclination angle at which the gun needs to be tilted when coating the undercut zone, e.g., an undercut between bell and braking band.
[0057] . Unlike the currently known nozzles (free from recess) , which must be tilted at inclination angles between 25 and 35 degrees, as a function of the specific geometry of the bell (cylindrical or with a "C"-shaped section, as depicted in the accompanying Figures 1, 2 and 4, 5) and the degree of precision chosen to coat the critical zones, in order to reach the undercut/grooves between the bell and braking band of the brake disc, by virtue of the suggested solution the inclination angle of the noz zle can be reduced between 13 and 20 degrees with respect to the direction orthogonal to the flat surface to be treated .
[0058 ] . By virtue of the suggested solution, it is possible to obtain several advantages , including :
[0059] . - improving the ef ficiency and overall quality of a layer deposited by laser cladding techniques in operations which would otherwise need to tilt the process powder distribution unit to be performed;
[0060 ] . - improving the ef ficiency and overall quality of a layer deposited by laser cladding techniques in operations that would otherwise require to tilt the process powder distribution unit at an extreme angle to be performed thus reducing the required angle ;
[0061 ] . - allowing the possibility to process parts or components which would otherwise be impossible to process with a standard process powder distribution unit .
[0062 ] . By virtue of the suggested solution, the technology is applicable :
[0063] . in brake discs which could hinder the use of laser cladding techniques ;
[0064 ] . - in zones close to the bell for the connection with the brake disc hub near the inner diameter of the friction ring ( car on the outside ) ;
[0065 ] . - in zones close to the bell for the connection with the brake disc hub with undercut ( e . g . , application on commercial vehicles ) .
[0066] . Figures [0067 ] . Further features and advantages of the device , the disc brake, and the vehicle will become apparent from the following description of preferred embodiments thereof , given by way of nonlimiting indication, with reference to the accompanying drawings , in which :
[0068 ] . - figure 1 depicts an axonometric view of an assembly comprising a piece , in this case a brake disc comprising a ventilated braking band connected in one piece to a bell , or portion for the connection of the brake disc with a support, or hub, of a vehicle , and a deposition noz zle placed close to the bell and oriented so as to treat the connection channel between the braking surface , or surface to be treated, of the braking band and the bell ; [0069] . - figure 2 shows a side view of the assembly in figure 1 , in which the deposition nozzle is viewed from the side and the recess thereof is highlighted;
[0070 ] . - figure 3 diagrammatically depicts a side view of the cladding process performed with the deposition nozzle of the present invention while performing a treatment on a surface to be treated of a piece ;
[0071 ] . - figure 4 shows a side view of the assembly in figure 1 , in which the deposition nozzle is shown frontally;
[0072 ] . - figure 5 depicts an axonometric view sectioned on a plane passing through the axial A-A and radial R-R directions of the brake disc passing through the nozzle axis L-L of the assembly in figure 1 ;
[0073] . - figure 6 depicts an axonometric view of the deposition nozzle of the present invention;
[0074 ] . - figures 7 to 9 depict top, side , and bottom views of the deposition nozzle in figure 6 ;
[0075 ] . - figure 10 shows an axonometric view sectioned according to the plane passing through the nozzle axis and defined by letters A-A in figure 9 of the deposition noz zle in figure 6 ;
[0076] . - figure 11 shows an axonometric view sectioned according to the plane passing through the nozzle axis and defined by letters B-B in figure 9 of the deposition noz zle in figure 6 ;
[0077 ] . - figure 12 shows an axonometric view sectioned according to the plane passing through the nozzle axis and defined by letters C-C in figure 9 of the deposition noz zle in figure 6 ;
[0078 ] . - figure 13 shows a very diagrammatic side view of a disc surface treatment system;
[0079] . figure 14 shows a deposition nozzle and piece-to-be- treated assembly according to the prior art ;
[0080 ] . f igure 15 shows a deposition nozzle and piece-to-be- treated assembly according to the invention .
[0081 ] . Description of some preferred embodiments
[0082 ] . According to a general embodiment, a deposition noz zle 1 for coating a surface 2 of a piece 3 by means of the heat treatment of additive material , in particular powder material 4 , and/or for thermally treating the surface 2 of said piece 3 .
[0083] . Said deposition nozzle 1 comprises a radiation conduit 5 connectable to a laser device 6 to generate a focused laser beam 7 through a laser focusing device 8 , said focused laser beam 7 being directed along a predetermined direction defining a nozzle axis L-L.
[0084] . Said deposition nozzle 1 comprises a nozzle body 9; said nozzle body 9 is initially axisymmetric in shape with respect to said nozzle axis L-L.
[0085] . Said nozzle body 9 has an elongated shape toward a nozzle radiation mouth 10.
[0086] . Said deposition nozzle 1 further comprises a plurality of powder feeding conduits 11 having extension along powder feeding directions D-D converging toward said nozzle axis L-L.
[0087] . Advantageously, said nozzle body 9 comprises a nozzle recess 13, which makes said nozzle body 9 dissymmetric.
[0088] . Said nozzle recess 13 affects an arc extending about said nozzle axis L-L by less than 180 DEG, preferably between 140 DEG and 160 DEG.
[0089] . Said nozzle recess 13 tapers the elongated shape of the nozzle body 9 locally narrowing the nozzle body 9 toward said nozzle radiation mouth 10.
[0090] . Said plurality of powder feeding conduits 11 being arranged entirely in the part of nozzle body 9 not affected by said nozzle recess 13.
[0091] . According to a constructional variant, said nozzle recess 13 is given by the intersection between a ball and said nozzle body 9 when still axisymmetric.
[0092] . According to a constructional variant, said nozzle recess 13 is obtained by the subtraction of a ball portion from said nozzle body 9 when still axisymmetric. [0093] . According to a constructional variant, said nozzle body 9 comprises a first proximal cylindrical nozzle portion 14 , a first intermediate conical portion 15 , a second intermediate cylindrical portion 16, and a second distal conical portion 17 .
[0094 ] . According to a constructional variant, said noz zle recess 13 af fects said first intermediate conical portion 15, said second intermediate cylindrical portion 16, and said second distal conical portion 17 .
[0095 ] . According to a constructional variant, said nozzle body 9 comprises a first proximal cylindrical noz zle portion 14 distally connected to a first intermediate conical portion 15 distally connected to a second intermediate cylindrical portion 16 distally connected to a second distal conical portion 17 .
[0096] . Said noz zle recess 13 affects said first intermediate conical portion 15, said second intermediate cylindrical portion 16 , and said second distal conical portion 17 .
[0097 ] . According to a constructional variant , said powder feeding conduits 11 converge in a single point of intersection 12 of the powder feeding directions , placed on said noz zle axis L- L .
[0098 ] . According to a constructional variant , said plurality of powder feeding conduits 11 is distributed so as to have the powder feeding conduits 11 equally spaced apart from each other and mutually converging .
[0099] . According to a constructional variant, said radiation conduit 5 has cylinder-shaped radiation conduit walls 18 .
[00100 ] . According to a constructional variant, said radiation conduit 5 delimits a passage in the shape of a right cylinder.
[00101] . According to a constructional variant, said nozzle radiation 10 is delimited by a circumference-shaped periphery.
[00102] . According to a constructional variant, said nozzle radiation mouth 10 is orthogonal to said nozzle axis L-L.
[00103] . According to a constructional variant, said powder feeding conduits 11 are distributed in said nozzle body 9 in an arc extending about said nozzle axis L-L with a width of less than 200 DEG.
[00104] . According to a constructional variant, said powder feeding conduits 11 delimit a cylindrical passage with rectilinear extension along a straight powder feeding direction D-D.
[00105] . The present invention also relates to a deposition nozzle 1 and piece-to-be-treated assembly, comprising
[00106] . - a feeding nozzle 1 according to any one of the previous embodiments described;
[00107] . - and where said piece 3 is a braking band of a disc brake disc .
[00108] . A treatment process possible with this deposition nozzle is described below.
[00109] . For example, there is described the laser cladding process on a surface to be treated 2 of a braking band 3 of a brake disc 21 for a disc brake, where the treatment is taken close to the bell 22 or portion for the connection of the brake disc to the vehicle hub (see figures 1, 2, 4, 5 and 15) .
[00110] . A laser beam, e.g., surrounded by a shielding gas, is focused into the deposition nozzle 1. The process powder 20 is fed into the powder feeding conduits 11. Usually the deposition nozzle is cooled with fluid, e.g., water.
[00111] . As mentioned, the laser beam 19 is directed along a direction defined by the nozzle axis L-L and focuses on a point, in which point the melting and thus the process activation occur, which point is preferably close to or coinciding with the intersection point of the powder feeding directions D-D. At this point, the surface to be treated 2 of the piece 3 is heated, e.g., melts, and creates a bonding zone, to which the cladding layer obtained by activating the powder with the laser, e.g., by melting the powder at least partially, is bonded (Figure 3) .
[00112] . The nozzle body 9, by virtue of the nozzle recess 13, is very close to the bell 22 and allows having a very small angle 23, for example between 13 DEG and 20 DEG, between the direction given by the extension of the nozzle axis L-L and the normal to the surface to be treated 2, e.g., the axial direction A-A of the brake disc 21 even when the laser beam 19 is directed to the connection portion between the braking band 3 and the bell 22, i.e., the undercut given by the connection channel. [00113] . LIST OF REFERENCE SIGNS
1 deposition nozzle
2 surface to be treated
3 piece, e . g . , braking band of a disc brake disc
4 powder material
5 radiation conduit
6 laser device
7 focused laser beam
8 laser focusing device
9 nozzle body
10 nozzle radiation mouth
11 powder feeding conduits
12 single point of intersection of the powder feeding directions
13 nozzle recess
14 first proximal cylindrical noz zle portion
15 first intermediate conical portion
16 second intermediate cylindrical portion
17 second distal conical portion
18 radiation conduit walls
X-X rotation axis
A-A axial direction
R-R radial direction
C-C circumferential direction
T-T tangential direction
L-L nozzle axis
D-D powder feeding direction
ANG arc of extension of the recess about the nozzle axis

Claims

1. A deposition nozzle (1) for coating a surface (2) of a piece (3) by means of the heat treatment of additive material, in particular powder material (4) , and/or for thermally treating the surface (2) of said piece (3) , comprising
- a radiation conduit (5) connectable to a laser device (6) to generate a focused laser beam (7) through a laser focusing device (8) , said focused laser beam (7) being directed along a predetermined direction defining a nozzle axis (L-L) ; wherein said deposition nozzle (1) comprises a nozzle body (9) ; said nozzle body (9) is initially axisymmetric-in shape with respect to said nozzle axis (L-L) ; said nozzle body (9) has an elongated shape toward a nozzle radiation mouth (10) ;
- said deposition nozzle (1) further comprises a plurality of powder feeding conduits (11) having extension along powder feeding directions (D-D) converging toward said nozzle axis (L-L) ; characterized in that
- said nozzle body (9) comprises a nozzle recess (13) which makes said nozzle body (9) dissymmetric;
- said nozzle recess (13) affects an arc (ANG) extending about said nozzle axis (L-L) by less than 180 DEG, preferably between 140 DEG and 160 DEG;
- said nozzle recess (13) tapers the elongated shape of the nozzle body (9) locally narrowing the nozzle body (9) toward said nozzle radiation mouth (10) ; said plurality of powder feeding conduits (11) being arranged entirely in the part of nozzle body (9) not affected by said nozzle recess (13) .
2. A deposition nozzle (1) according to claim 1, wherein said nozzle recess (13) is given by the intersection between a ball and said nozzle body (9) when still axisymmetric; or wherein said nozzle recess (13) is obtained by the subtraction of a ball portion from said nozzle body (9) when still axisymmetric.
3. A deposition nozzle (1) according to claim 1 or 2, wherein said nozzle body (9) comprises a first proximal cylindrical nozzle portion (14) , a first intermediate conical portion (15) , a second intermediate cylindrical portion (16) , and a second distal conical portion ( 17 ) ; and wherein said nozzle recess (13) affects said first intermediate conical portion (15) , said second intermediate cylindrical portion (16) , and said second distal conical portion (17) ; or wherein said nozzle body (9) comprises a first proximal cylindrical nozzle portion (14) distally connected to a first intermediate conical portion (15) distally connected to a second intermediate cylindrical portion (16) distally connected to a second distal conical portion (17) ; and wherein said nozzle recess (13) affects said first intermediate conical portion (15) , said second intermediate cylindrical portion (16) , and said second distal conical portion (17) .
4. A deposition nozzle (1) according to any one of the preceding claims, wherein said powder feeding conduits (11) converge in a single point of intersection (12) of the powder feeding directions, placed on said nozzle axis (L-L) and/or wherein said plurality of powder feeding conduits (11) is distributed so as to have the powder feeding conduits (11) equally spaced apart from each other and mutually converging.
5. A deposition nozzle (1) according to any one of the preceding claims, wherein said radiation conduit (5) has cylinder-shaped radiation conduit walls ( 18 ) .
6. A deposition nozzle (1) according to the preceding claim, wherein said radiation conduit (5) delimits a passage in the shape of a right cylinder.
7. A deposition nozzle (1) according to any one of the preceding claims, wherein said nozzle radiation mouth (10) is delimited by a circumferenceshaped periphery; and/or wherein said nozzle radiation mouth (10) is orthogonal to said nozzle axis (L-L) .
8. A deposition nozzle (1) according to any one of the preceding claims, wherein said powder feeding conduits (11) are distributed in said nozzle body (9) in an arc extending about said nozzle axis (L-L) with a width of less than 200 DEG.
9. A deposition nozzle (1) according to any one of the preceding claims, wherein said powder feeding conduits (11) delimit a cylindrical passage with rectilinear extension along a straight powder feeding direction (D- D) .
10. A deposition nozzle (1) and piece-to-be-treated assembly, comprising
- a feeding nozzle (1) according to any one of the preceding claims; and wherein said piece (3) is a braking band of a disc brake disc.
PCT/IB2024/060874 2023-11-07 2024-11-04 Deposition nozzle for coating a surface of a piece Pending WO2025099554A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT102023000023418A IT202300023418A1 (en) 2023-11-07 2023-11-07 DEPOSIT NOZZLE FOR COATING A SURFACE OF A WORKPIECE
IT102023000023418 2023-11-07

Publications (1)

Publication Number Publication Date
WO2025099554A1 true WO2025099554A1 (en) 2025-05-15

Family

ID=89897247

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2024/060874 Pending WO2025099554A1 (en) 2023-11-07 2024-11-04 Deposition nozzle for coating a surface of a piece

Country Status (2)

Country Link
IT (1) IT202300023418A1 (en)
WO (1) WO2025099554A1 (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5389822B2 (en) * 2008-01-08 2014-01-15 レール・リキード−ソシエテ・アノニム・プール・レテュード・エ・レクスプロワタシオン・デ・プロセデ・ジョルジュ・クロード Laser welding using a nozzle that can stabilize the keyhole
EP3045294A1 (en) * 2015-01-16 2016-07-20 Rolls-Royce Corporation Compact axially translational powder deposition head, system comprising the head and method using the head
US20180050421A1 (en) * 2016-08-18 2018-02-22 Caterpillar Inc. Hybrid Laser Cladding System
WO2023161088A1 (en) * 2022-02-22 2023-08-31 Trumpf Laser- Und Systemtechnik Gmbh Laser deposition welding process for producing a coating layer on a component

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5477026A (en) 1994-01-27 1995-12-19 Chromalloy Gas Turbine Corporation Laser/powdered metal cladding nozzle
US7259353B2 (en) 2004-09-30 2007-08-21 Honeywell International, Inc. Compact coaxial nozzle for laser cladding
GB2465950B (en) 2007-10-10 2012-10-03 Ronald Peter Whitfield Laser cladding device with an improved nozzle
EP2712697A1 (en) 2012-10-01 2014-04-02 Siemens Aktiengesellschaft Powder feeding device for a laser powder application welding device
DE102020103175A1 (en) 2020-02-07 2021-08-12 Trumpf Laser- Und Systemtechnik Gmbh Material separation unit for powder deposition welding
DE102021214891A1 (en) 2021-12-22 2023-06-22 HPL Technologies GmbH Device for coating a workpiece
EP4476021A1 (en) 2022-02-11 2024-12-18 Trumpf Laser- und Systemtechnik GmbH Laser deposition welding method for producing coating layers on opposing surfaces of a component

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5389822B2 (en) * 2008-01-08 2014-01-15 レール・リキード−ソシエテ・アノニム・プール・レテュード・エ・レクスプロワタシオン・デ・プロセデ・ジョルジュ・クロード Laser welding using a nozzle that can stabilize the keyhole
EP3045294A1 (en) * 2015-01-16 2016-07-20 Rolls-Royce Corporation Compact axially translational powder deposition head, system comprising the head and method using the head
US20180050421A1 (en) * 2016-08-18 2018-02-22 Caterpillar Inc. Hybrid Laser Cladding System
WO2023161088A1 (en) * 2022-02-22 2023-08-31 Trumpf Laser- Und Systemtechnik Gmbh Laser deposition welding process for producing a coating layer on a component

Also Published As

Publication number Publication date
IT202300023418A1 (en) 2025-05-07

Similar Documents

Publication Publication Date Title
KR100333314B1 (en) Laser / Powder Coating Nozzle
US6696664B2 (en) Powder feed nozzle for laser welding
CN101024881B (en) Nozzles for Laser Net Shaping
US20230146425A1 (en) Material deposition unit for powder build-up welding
CN101291772B (en) Powder delivery nozzle
JPH06503040A (en) Nozzle for surface treatment of metal workpieces
CN104736289B (en) Laser processing head and ring nozzle for laser processing head
CN115379918A (en) Device and method for producing and reprocessing a layer applied by laser cladding
CN101909807A (en) Laser welding method using a nozzle capable of stabilizing pores
WO2025099554A1 (en) Deposition nozzle for coating a surface of a piece
CN112703078A (en) Coaxial powder nozzle tip module for workpiece surface treatment
CN114929426B (en) Material conveying device
US20250381619A1 (en) Jet nozzle having a powder unit and process-gas unit
CA3286211A1 (en) Jet nozzle having a powder unit and a process-gas unit
US20250353110A1 (en) Jet nozzle having a powder section and an advance section
US20250353111A1 (en) Jet nozzle having a light channel with an oblong cross-sectional area
US20250339924A1 (en) Jet nozzle with opposing injector guides
JP2026509076A (en) Injection nozzle with cooling system
AU2006284512B2 (en) Powder delivery nozzle
CN216039822U (en) Coaxial powder nozzle tip module for workpiece surface treatment
CN120603672A (en) Jet nozzle having an absorption section for absorbing reflected radiation
JP2002144062A (en) Laser beam machining head
JPH0116314B2 (en)

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 24805915

Country of ref document: EP

Kind code of ref document: A1