US20170218505A1 - System and Method for Low Thermal Shock-Fast Cooling of Thermal Barrier Coating - Google Patents

System and Method for Low Thermal Shock-Fast Cooling of Thermal Barrier Coating Download PDF

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Publication number
US20170218505A1
US20170218505A1 US15/014,232 US201615014232A US2017218505A1 US 20170218505 A1 US20170218505 A1 US 20170218505A1 US 201615014232 A US201615014232 A US 201615014232A US 2017218505 A1 US2017218505 A1 US 2017218505A1
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recited
chamber
arcuate wall
workpiece
cool down
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US15/014,232
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Shayan Ahmadian
Hoyt Y. Chang
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RTX Corp
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United Technologies Corp
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Priority to US15/014,232 priority Critical patent/US20170218505A1/en
Assigned to UNITED TECHNOLOGIES CORPORATION reassignment UNITED TECHNOLOGIES CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: AHMADIAN, SHAYAN, CHANG, HOYT Y
Priority to EP17154312.7A priority patent/EP3284844B1/en
Publication of US20170218505A1 publication Critical patent/US20170218505A1/en
Priority to US16/884,602 priority patent/US10995402B2/en
Assigned to RAYTHEON TECHNOLOGIES CORPORATION reassignment RAYTHEON TECHNOLOGIES CORPORATION CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: UNITED TECHNOLOGIES CORPORATION
Assigned to RAYTHEON TECHNOLOGIES CORPORATION reassignment RAYTHEON TECHNOLOGIES CORPORATION CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Assignors: UNITED TECHNOLOGIES CORPORATION
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/58After-treatment
    • C23C14/5806Thermal treatment
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/24Vacuum evaporation
    • C23C14/28Vacuum evaporation by wave energy or particle radiation
    • C23C14/30Vacuum evaporation by wave energy or particle radiation by electron bombardment

Definitions

  • the present disclosure relates to a system for thermal barrier coatings (TBCs), and more particularly, to thermal control therein.
  • TBCs thermal barrier coatings
  • Thermal barrier coatings are multilayer materials that are typically applied to hot sections of an engine to reduce the surface temperature experienced by workpieces.
  • TBCs often include (1) a substrate, which may be an engine workpiece—typically a gamma-gamma prime superalloy (2) an aluminum rich bond coat (3) thermally grown oxide (TGO) that reduce further oxidation of bond coat by blocking oxygen (4) a low thermal conductivity ceramic top coat.
  • a substrate typically an engine workpiece—typically a gamma-gamma prime superalloy
  • TGO thermally grown oxide
  • EB-PVD electron beam-physical vapor deposition
  • a columnar top coat microstructure develops on the surface of the workpieces in near vacuum at elevated temperatures.
  • EB-PVD is a form of physical vapor deposition in which an ingot of material is bombarded with an electron beam given off by a charged tungsten filament under high vacuum. The electron beam causes atoms from the ingot to transform into the gaseous phase. These atoms then condense into solid form, coating the workpiece in the vacuum chamber, and within a line of sight, with a thin layer of the material.
  • a coating system can include a reflective cool down chamber with at least one arcuate wall and an infrared lamp directed at the arcuate wall.
  • a further embodiment of the present disclosure may include wherein the at least one arcuate wall includes an interior surface with a high index of reflection.
  • a further embodiment of the present disclosure may include wherein the at least one arcuate wall includes an interior surface with a mirror finish.
  • a further embodiment of the present disclosure may include, wherein the infrared lamp is located on a movable door that permits intake of a workpiece holder.
  • a further embodiment of the present disclosure may include, wherein the infrared lamp is located on a movable door that permits egress of a workpiece holder.
  • a further embodiment of the present disclosure may include a diffusion lens mounted to the infrared lamp.
  • a further embodiment of the present disclosure may include a diffusion chamber adjacent to the reflective cool down chamber.
  • a further embodiment of the present disclosure may include, wherein the diffusion chamber is an electron beam physical vapor deposition (EB PVD).
  • EB PVD electron beam physical vapor deposition
  • a method coating a workpiece according to one disclosed non-limiting embodiment of the present disclosure can include moving a workpiece holder from a deposition chamber a reflective cool down chamber with at least one arcuate wall; and directing infrared energy from an infrared lamp at the arcuate wall to reduce a temperature gradient of a workpiece.
  • a further embodiment of the present disclosure may include directing the infrared energy for 3-10 seconds.
  • a further embodiment of the present disclosure may include diffusing the infrared energy.
  • a further embodiment of the present disclosure may include locating the infrared lamp on a door of the reflective cool down chamber.
  • a further embodiment of the present disclosure may include, wherein the diffusion chamber is an electron beam physical vapor deposition (EB PVD).
  • EB PVD electron beam physical vapor deposition
  • a further embodiment of the present disclosure may include operating the infrared energy for a time in response to a thermal mass of the workpiece.
  • FIG. 1 is a partial schematic view of a deposition system
  • FIG. 2 is a schematic view a reflective cool down chamber.
  • FIG. 3 is a schematic view of the reflective cool down chamber operation.
  • FIG. 1 schematically illustrates an example system 20 for depositing coating on workpieces 22 in the interior 24 of a deposition chamber 26 .
  • the system 20 passes the workpiece 22 downstream along a workpiece flowpath sequentially through a first load lock chamber 28 forming an in-feed chamber, a preheat chamber 30 , the deposition chamber 26 , a cool down chamber 34 , and a second load lock chamber 36 .
  • Each of a multiple of workpieces 22 may be conveyed through the system on a workpiece holder 40 of which, depending upon implementation, may support a single workpiece or multiple workpieces.
  • the workpiece holder 40 may be manipulated by a sting mechanism 42 .
  • a loading station 50 and an unloading station 52 are provided. These may include robots (e.g., six-axis industrial robots) to transfer fixture workpieces from and to conveyors, pallets, and the like.
  • the sting mechanism 42 is withdrawn back through the preheat chamber 30 into the first load lock chamber 28 , such that the workpieces may be removed from the deposition chamber 26 .
  • the exemplary deposition chamber 26 is configured for electron beam physical vapor deposition (EB-PVD).
  • EB electron beam
  • at least one electron beam (EB) gun 60 is positioned to direct its beam to one or more deposition material ingots 70 , 72 .
  • the ingots may be ceramics of different composition for forming distinct layers in a thermal barrier coating, erosion coating, abradable coating, or abrasive coating.
  • Zirconia-based ingot examples include, but are not limited to, an yttria-stabilized zirconia (YSZ) such as 7YSZ, a gadolinia-stabilized zirconia, or an YSZ of different yttria content or dopant.
  • YSZ yttria-stabilized zirconia
  • 7YSZ a gadolinia-stabilized zirconia
  • YSZ yttria-stabilized zirconia
  • the reflective cool down chamber 34 provides a reflective chamber that includes an arcuate wall 100 and one or more infrared lamps 102 that have diffusing lenses 104 such that the reflective cool down chamber 34 forms an ovid-like shape.
  • the infrared lamps 102 may, for example, be located on a movable door 108 that permits entry and/or egress of the workpiece holder 40 .
  • the exact size and shape may be optimized such that the workpieces are cooled down slowly and uniformly.
  • An interior surface 106 of the arcuate wall 100 provides a high index of reflection, e.g., mirror polish aluminum, stainless steel, etc.
  • the cooling workpiece dissipates heat primarily through radiation and the reflective arcuate wall 100 of the reflective cool down chamber 34 reflects radiation back to the workpieces, thereby reducing the cooling rate.
  • the infrared lamps 102 may be located on movable doors 108 that permit intake and egress of the workpiece holder 40 .
  • the infrared lamps 102 increase heat to make up for heat loss to the interior surface 106 of the arcuate wall 100 and also reduce the cooling rate.
  • the orientation of the infrared lamps 102 is configured to uniformly distribute heat to the workpieces. Thus, temperature gradients in the workpiece are significantly reduced.
  • the diffusing lenses 104 facilitate diffusion of the radiation in a suitably wide cone to permit uniform heating.
  • the reflective cool down chamber 34 and infrared lamps 102 may be used in conjunction with various existing coaters.
  • the infrared lamps 102 can be turned on and off quickly, unlike a heating oven that requires a relatively long time to heat up and cool down.
  • the reflective cool down chamber 34 is adjacent to the deposition chamber 26 such that after the coating process is complete (step 206 ), the door 108 opens (step 202 ) such that the workpieces, which are supported by workpiece holder 40 , are moved from the deposition chamber 26 to the reflective cool down chamber 34 (step 204 ).
  • the movable doors 108 are then closed and the infrared lamps 102 are activated (step 206 ).
  • the infrared lamps 102 may be activated for about 3-10 seconds such that the infrared energy is provided in response to a thermal mass of the workpiece.
  • the workpieces are then cooled within the reflective cool down chamber 34 at a suitable rate, to prevent spallation.

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Physical Vapour Deposition (AREA)

Abstract

A coating system including a reflective cool down chamber with at least one arcuate wall; and an infrared lamp directed at the arcuate wall.

Description

    BACKGROUND
  • The present disclosure relates to a system for thermal barrier coatings (TBCs), and more particularly, to thermal control therein.
  • Thermal barrier coatings (TBCs) are multilayer materials that are typically applied to hot sections of an engine to reduce the surface temperature experienced by workpieces. TBCs often include (1) a substrate, which may be an engine workpiece—typically a gamma-gamma prime superalloy (2) an aluminum rich bond coat (3) thermally grown oxide (TGO) that reduce further oxidation of bond coat by blocking oxygen (4) a low thermal conductivity ceramic top coat.
  • One of the fabrication methods for top coat is electron beam-physical vapor deposition (EB-PVD) in which a columnar top coat microstructure develops on the surface of the workpieces in near vacuum at elevated temperatures. EB-PVD is a form of physical vapor deposition in which an ingot of material is bombarded with an electron beam given off by a charged tungsten filament under high vacuum. The electron beam causes atoms from the ingot to transform into the gaseous phase. These atoms then condense into solid form, coating the workpiece in the vacuum chamber, and within a line of sight, with a thin layer of the material.
  • To reduce the thermal shock between the ceramic top coat and the metallic bond coat post top coating, workpieces are slowly cooled down to room temperature in a preheated oven. The aforementioned method of cool down may be time consuming and not cost effective.
  • SUMMARY
  • A coating system according to one disclosed non-limiting embodiment of the present disclosure can include a reflective cool down chamber with at least one arcuate wall and an infrared lamp directed at the arcuate wall.
  • A further embodiment of the present disclosure may include wherein the at least one arcuate wall includes an interior surface with a high index of reflection.
  • A further embodiment of the present disclosure may include wherein the at least one arcuate wall includes an interior surface with a mirror finish.
  • A further embodiment of the present disclosure may include, wherein the infrared lamp is located on a movable door that permits intake of a workpiece holder.
  • A further embodiment of the present disclosure may include, wherein the infrared lamp is located on a movable door that permits egress of a workpiece holder.
  • A further embodiment of the present disclosure may include a diffusion lens mounted to the infrared lamp.
  • A further embodiment of the present disclosure may include a diffusion chamber adjacent to the reflective cool down chamber.
  • A further embodiment of the present disclosure may include, wherein the diffusion chamber is an electron beam physical vapor deposition (EB PVD).
  • A method coating a workpiece according to one disclosed non-limiting embodiment of the present disclosure can include moving a workpiece holder from a deposition chamber a reflective cool down chamber with at least one arcuate wall; and directing infrared energy from an infrared lamp at the arcuate wall to reduce a temperature gradient of a workpiece.
  • A further embodiment of the present disclosure may include directing the infrared energy for 3-10 seconds.
  • A further embodiment of the present disclosure may include diffusing the infrared energy.
  • A further embodiment of the present disclosure may include locating the infrared lamp on a door of the reflective cool down chamber.
  • A further embodiment of the present disclosure may include, wherein the diffusion chamber is an electron beam physical vapor deposition (EB PVD).
  • A further embodiment of the present disclosure may include operating the infrared energy for a time in response to a thermal mass of the workpiece.
  • The foregoing features and elements may be combined in various combinations without exclusivity, unless expressly indicated otherwise. These features and elements as well as the operation thereof will become more apparent in light of the following description and the accompanying drawings. It should be understood, however, the following description and drawings are intended to be exemplary in nature and non-limiting.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Various features will become apparent to those skilled in the art from the following detailed description of the disclosed non-limiting embodiment. The drawings that accompany the detailed description can be briefly described as follows:
  • FIG. 1 is a partial schematic view of a deposition system; and
  • FIG. 2 is a schematic view a reflective cool down chamber.
  • FIG. 3 is a schematic view of the reflective cool down chamber operation.
  • DETAILED DESCRIPTION
  • FIG. 1 schematically illustrates an example system 20 for depositing coating on workpieces 22 in the interior 24 of a deposition chamber 26. The system 20 passes the workpiece 22 downstream along a workpiece flowpath sequentially through a first load lock chamber 28 forming an in-feed chamber, a preheat chamber 30, the deposition chamber 26, a cool down chamber 34, and a second load lock chamber 36.
  • Each of a multiple of workpieces 22 may be conveyed through the system on a workpiece holder 40 of which, depending upon implementation, may support a single workpiece or multiple workpieces. In the deposition chamber 26, the workpiece holder 40 may be manipulated by a sting mechanism 42. In one embodiment, a loading station 50 and an unloading station 52 are provided. These may include robots (e.g., six-axis industrial robots) to transfer fixture workpieces from and to conveyors, pallets, and the like.
  • After deposition is complete, the sting mechanism 42 is withdrawn back through the preheat chamber 30 into the first load lock chamber 28, such that the workpieces may be removed from the deposition chamber 26.
  • The exemplary deposition chamber 26 is configured for electron beam physical vapor deposition (EB-PVD). In this example, at least one electron beam (EB) gun 60 is positioned to direct its beam to one or more deposition material ingots 70, 72. In this example, there are two ingots 70, 72 of different materials. The ingots may be ceramics of different composition for forming distinct layers in a thermal barrier coating, erosion coating, abradable coating, or abrasive coating. For example, Zirconia-based ingot examples include, but are not limited to, an yttria-stabilized zirconia (YSZ) such as 7YSZ, a gadolinia-stabilized zirconia, or an YSZ of different yttria content or dopant.
  • With reference to FIG. 2, in one exemplary implementation, the reflective cool down chamber 34 provides a reflective chamber that includes an arcuate wall 100 and one or more infrared lamps 102 that have diffusing lenses 104 such that the reflective cool down chamber 34 forms an ovid-like shape. The infrared lamps 102 may, for example, be located on a movable door 108 that permits entry and/or egress of the workpiece holder 40. The exact size and shape may be optimized such that the workpieces are cooled down slowly and uniformly. An interior surface 106 of the arcuate wall 100 provides a high index of reflection, e.g., mirror polish aluminum, stainless steel, etc. The cooling workpiece dissipates heat primarily through radiation and the reflective arcuate wall 100 of the reflective cool down chamber 34 reflects radiation back to the workpieces, thereby reducing the cooling rate.
  • The infrared lamps 102 may be located on movable doors 108 that permit intake and egress of the workpiece holder 40. The infrared lamps 102 increase heat to make up for heat loss to the interior surface 106 of the arcuate wall 100 and also reduce the cooling rate. The orientation of the infrared lamps 102 is configured to uniformly distribute heat to the workpieces. Thus, temperature gradients in the workpiece are significantly reduced.
  • The diffusing lenses 104 facilitate diffusion of the radiation in a suitably wide cone to permit uniform heating. The reflective cool down chamber 34 and infrared lamps 102 may be used in conjunction with various existing coaters. The infrared lamps 102 can be turned on and off quickly, unlike a heating oven that requires a relatively long time to heat up and cool down.
  • With reference to FIG. 3, the reflective cool down chamber 34 is adjacent to the deposition chamber 26 such that after the coating process is complete (step 206), the door 108 opens (step 202) such that the workpieces, which are supported by workpiece holder 40, are moved from the deposition chamber 26 to the reflective cool down chamber 34 (step 204). The movable doors 108 are then closed and the infrared lamps 102 are activated (step 206). In one example, the infrared lamps 102 may be activated for about 3-10 seconds such that the infrared energy is provided in response to a thermal mass of the workpiece. The workpieces are then cooled within the reflective cool down chamber 34 at a suitable rate, to prevent spallation.
  • The use of the terms “a,” “an,” “the,” and similar references in the context of description (especially in the context of the following claims) are to be construed to cover both the singular and the plural, unless otherwise indicated herein or specifically contradicted by context. The modifier “about” used in connection with a quantity is inclusive of the stated value and has the meaning dictated by the context (e.g., it includes the degree of error associated with measurement of the particular quantity). All ranges disclosed herein are inclusive of the endpoints, and the endpoints are independently combinable with each other.
  • Although the different non-limiting embodiments have specific illustrated components, the embodiments of this invention are not limited to those particular combinations. It is possible to use some of the components or features from any of the non-limiting embodiments in combination with features or components from any of the other non-limiting embodiments.
  • It should be appreciated that like reference numerals identify corresponding or similar elements throughout the several drawings. It should also be appreciated that although a workpiece component arrangement is disclosed in the illustrated embodiment, other arrangements will benefit herefrom.
  • Although particular step sequences are shown, described, and claimed, it should be understood that steps may be performed in any order, separated or combined unless otherwise indicated and will still benefit from the present disclosure.
  • The foregoing description is exemplary rather than defined by the limitations within. Various non-limiting embodiments are disclosed herein, however, one of ordinary skill in the art would recognize that various modifications and variations in light of the above teachings will fall within the scope of the appended claims. It is therefore to be understood that within the scope of the appended claims, the disclosure may be practiced other than as specifically described. For that reason the appended claims should be studied to determine true scope and content.

Claims (13)

What is claimed:
1. A coating system, comprising:
a reflective cool down chamber with at least one arcuate wall; and
an infrared lamp directed at the arcuate wall.
2. The system as recited in claim 1, wherein the at least one arcuate wall includes an interior surface with a high index of reflection.
3. The system as recited in claim 1, wherein the at least one arcuate wall includes an interior surface with a mirror finish.
4. The system as recited in claim 1, wherein the infrared lamp is located on a movable door that permits intake of a workpiece holder.
5. The system as recited in claim 1, wherein the infrared lamp is located on a movable door that permits egress of a workpiece holder.
6. The system as recited in claim 1, further comprising a diffusion lens mounted to the infrared lamp.
7. The system as recited in claim 1, further comprising a diffusion chamber adjacent to the reflective cool down chamber.
8. A method coating a workpiece, comprising:
moving a workpiece holder from a deposition chamber a reflective cool down chamber with at least one arcuate wall; and
directing infrared energy from an infrared lamp at the arcuate wall to reduce a temperature gradient of a workpiece.
9. The method as recited in claim 8, further comprising directing the infrared energy for 3-10 seconds.
10. The method as recited in claim 8, further comprising diffusing the infrared energy.
11. The method as recited in claim 8, further comprising locating the infrared lamp on a door of the reflective cool down chamber.
12. The method as recited in claim 8, wherein the diffusion chamber is an electron beam physical vapor deposition (EB-PVD).
13. The method as recited in claim 8, further comprising operating the infrared energy for a time in response to a thermal mass of the workpiece.
US15/014,232 2016-02-03 2016-02-03 System and Method for Low Thermal Shock-Fast Cooling of Thermal Barrier Coating Abandoned US20170218505A1 (en)

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US15/014,232 US20170218505A1 (en) 2016-02-03 2016-02-03 System and Method for Low Thermal Shock-Fast Cooling of Thermal Barrier Coating
EP17154312.7A EP3284844B1 (en) 2016-02-03 2017-02-02 System and method for low thermal shock-fast cooling of thermal barrier coating
US16/884,602 US10995402B2 (en) 2016-02-03 2020-05-27 System and method for low thermal shock-fast cooling of thermal barrier coating

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Publication number Priority date Publication date Assignee Title
US4575608A (en) * 1983-10-05 1986-03-11 Lennart Wictorin Method and apparatus for spot heating a body, particularly for brazing hard solder gold alloys
US5099586A (en) * 1989-09-08 1992-03-31 W. R. Grace & Co.-Conn. Reflector assembly for heating a substrate
US5882415A (en) * 1995-10-05 1999-03-16 Von Ardenne Anlagentechnik Gmbh Electron-beam continuous process vaporization installation for thermally high stressed substrata
US20060002112A1 (en) * 2004-07-01 2006-01-05 Osram Sylvania Inc. Incandescent reflector heat lamp with uniform irradiance
US20070259173A1 (en) * 2006-05-05 2007-11-08 Sulzer Metco Ag Method for the manufacture of a coating

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US20200318231A1 (en) 2020-10-08
EP3284844A1 (en) 2018-02-21
EP3284844B1 (en) 2020-04-01
US10995402B2 (en) 2021-05-04

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