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US5484980A Expired / Lapsed US ⏱️ 0.0 years remaining

Apparatus and method for smoothing and densifying a coating on a workpiece

Assignee: General Electric Co
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Filing: 1993-02-26
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Granted: 1996-01-16
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Expires: 2013-02-26
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Abstract

Abstract An apparatus for smoothing and densifying or increasing the density of a coating on a workpiece includes a laser for generating a laser beam and a cylindrical lens for focusing the laser beam into a line of light on the coating surface. A manipulator is provided for moving one of the workpiece or the laser and the light line generated thereby relative to one another to cause the light line to scan across the coating to remove any rough portions and provide a smoother surface with a higher density depending upon the nature of the coating material. In one embodiment of the present invention, a mechanism is provided to oscillate the laser light line to homogenize adverse effects caused by any hot spots along the line.

Inventors

  • 👤 Vanon D. Pratt
  • 👤 Eric J. Whitney
  • 👤 Wilbur D. Scheidt

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 03:56
CPC Classifications
B; B23; B23K; B23K26/00; B23K26/08; B23K26/082; B23K26/34; B23K2101/00; B23K2101/34; B23K2103/00; B23K2103/08

Claims Analysis

Total Claims: 18
Claim 1
Independent Claim 93 words
An apparatus for smoothing and densifying a coating on a workpiece, comprising: a laser for generating a laser beam; a cylindrical lens for focusing said laser beam into a line of light on the coating surface; means for moving said line of light and the workpiece relative to one another to cause said line of light to scan across the coating to remove rough portions and provide a smooth glaze surface; and a beam spinner disposed in an optical path between said laser and said cylindrical lens for oscillating said line of light.
Claim 2
Independent Claim 93 words
An apparatus for smoothing and densifying a coating on a workpiece, comprising: a laser for generating a laser beam; a cylindrical lens for focusing said laser beam into a line of light on the coating surface; means for moving said line of light and the workpiece relative to one another to cause said line of light to scan across the coating to remove rough portions and provide a smooth glaze surface; and a beam spinner disposed in an optical path between said laser and said cylindrical lens for oscillating said line of light.
Claim 3
Dependent Claim 35 words
The apparatus of claim 1, wherein said cylindrical lens has a focal length to focus said line of light in a predetermined length extending substantially perpendicular to a scanning direction of said line of light.
Claim 4
Dependent Claim 55 words
The apparatus of claim 2, wherein said laser beam has a predetermined energy density and said cylindrical lens focal length focuses said line of light at a predetermined width to provide a spot power density along said predetermined length of said light line to cause smoothing and densification of the coating in a single scan.
Claim 5
Dependent Claim 32 words
The apparatus of claim 3, wherein said laser is a CO 2 laser having an energy density of about 3500 w/cm 2 -11,000 w/cm 2 and said predetermined width is about 0.030".
Claim 6
Dependent Claim 19 words
The apparatus of claim 3, wherein the coating is a thermal barrier coating on a gas turbine engine component.
Claim 7
Dependent Claim 47 words
The apparatus of claim 5, wherein said line of light has a predetermined spot power density to cause an upper portion of said thermal barrier coating to melt and resolidify in a denser layer with a surface roughness of less than about 100 μin. R a .
Claim 8
Dependent Claim 26 words
The apparatus of claim 1, wherein said line of light is oscillated at a frequency substantially faster than a scanning speed of said line of light.
Claim 9
Dependent Claim 33 words
The apparatus of claim 1, wherein said beam spinner is driven by a variable drive motor to permit adjustment of an oscillation speed relative to a scanning speed of said line of light.
Claim 10
Dependent Claim 46 words
The apparatus of claim 1, wherein said line of light has a predetermined spot power density and is oscillated at a speed relative to a scanning speed of said line of light to provide a surface roughness of less than about 50 μin. R a .
Claim 11
Independent Claim 108 words
A method for making a coated workpiece, comprising the steps of: (a) depositing a coating of material on a workpiece; (b) forming a line of laser light; (c) scanning the line of laser light at a scanning speed across the coating to cause smoothing and increased density of at least an upper portion of the coating to form a glaze within a heat affected zone (d) selecting a laser spot power density; and (e) oscillating the line of laser light at a speed relative the scanning speed to homogenize the heat affected zone and to provide a surface roughness of less than about 100 μin. R a .
Claim 12
Independent Claim 108 words
A method for making a coated workpiece, comprising the steps of: (a) depositing a coating of material on a workpiece; (b) forming a line of laser light; (c) scanning the line of laser light at a scanning speed across the coating to cause smoothing and increased density of at least an upper portion of the coating to form a glaze within a heat affected zone (d) selecting a laser spot power density; and (e) oscillating the line of laser light at a speed relative the scanning speed to homogenize the heat affected zone and to provide a surface roughness of less than about 100 μin. R a .
Claim 13
Dependent Claim 27 words
The method of claim 10, wherein the line of laser light is oscillated at a speed substantially faster than a scanning speed of the line of light.
Claim 14
Dependent Claim 29 words
The method of claim 10, further comprising the step of controlling an oscillation speed of the line of light relative to a scanning speed of the line of light.
Claim 15
Dependent Claim 20 words
The method of claim 10, wherein the coating is a thermal barrier coating deposited on a gas turbine engine component.
Claim 16
Independent Claim 92 words
A method to reduce the surface roughness of a thermal barrier coating on a gas turbine engine component, comprising the steps of: (a) applying a line of laser light substantially perpendicular to the thermal barrier coating; and (b) scanning said lute of laser light across the gas turbine engine component such that said line of laser light glazes an upper portion of said ceramic coating, causing said upper portion to melt and then to densify upon resolidification, wherein said upper portion has a resulting surface roughness of less than about 100 μin.
Claim 17
Independent Claim 92 words
A method to reduce the surface roughness of a thermal barrier coating on a gas turbine engine component, comprising the steps of: (a) applying a line of laser light substantially perpendicular to the thermal barrier coating; and (b) scanning said lute of laser light across the gas turbine engine component such that said line of laser light glazes an upper portion of said ceramic coating, causing said upper portion to melt and then to densify upon resolidification, wherein said upper portion has a resulting surface roughness of less than about 100 μin.
Claim 18
Dependent Claim 43 words
The method of claim 14 further comprising the step of oscillating said line of light to homogenize any adverse effects caused by hot spots along the line of said laser light and to provide increased smoothing and uniform thickness of said upper portion.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1999-01-15 1999-07-17 2000-01-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2003-01-15 2003-07-17 2004-01-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2007-01-15 2007-07-17 2008-01-16 $7700.00 Window Closed / Lapsed

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