IP Library Granted Patent US 7,525,065
Granted Patent B2
US 7,525,065 · App. 11/130,677 · Granted Apr 28, 2009

Laser-assisted coating removal method

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Quick Facts
Patent No.
US 7,525,065
App. No.
11/130,677
Granted
Apr 28, 2009
Kind
B2
Abstract

Stripping is accomplished with a pulsed laser beam that targets the material and area to be stripped. The wavelength laser beam may be selected or adjusted to the absorption behavior of the material to be stripped without damaging the underlying base material. A control unit may operably adjust an optical system to guide the laser beam over the surface to be treated. a coating. This makes it possible to improve the surface stripping process.

Claims (20)

1. A method for removing a surface coating of a terminal surface area on an aircraft structural component surface using a laser beam, the method comprising the steps of:

positioning and aligning the laser beam on the area to be cleaned;

pulsing the laser beam;

removing the surface coating from the terminal surface area by repeating the steps of positioning and pulsing such that the terminal surface area is electrically conductive over the entire terminal surface area and a sharp transition is defined between the terminal surface area and the surface coating remaining on the aircraft structural component; and

making an electrical ground connection at the terminal surface area of the aircraft structural component, wherein the step of removing is limited to contour edges of a terminal shoe, and the step of making fastens the terminal shoe over the terminal surface area such that the contour edges of the terminal shoe are aligned with the sharp transition.

2. The method of claim 1 , further comprising the step of:

applying an Nd: YAG laser for generating the laser beam.

3. The method of claim 1 , further comprising the step of:

applying a TEA CO 2 laser for generating the laser beam.

4. The method of claim 1 , further comprising the step of:

evaporating the surface coating.

5. The method of claim 4 , further comprising the step of:

performing a suction cleaning of the evaporated surface coating.

6. The method of claim 1 , further comprising the step of:

adjusting a wavelength of the laser beam to an absorption behavior of the surface coating.

7. The method of claim 6 , further comprising: confining the effect of the laser beam to the surface coating.

8. The method of claim 6 , wherein the step of adjusting the wavelength includes selecting the wavelength of the laser beam to substantially reflect from a surface disposed beneath the surface coating.

9. The method of claim 8 , wherein the surface coating is a layer selected from the following group consisting of an anodizing layer, a primer layer, and a top coat layer; wherein the anodizing layer is based on chromic acid or sulfuric acid; and wherein the top coat layer is based on at least one of polyurethane, epoxide or powdered lacquer.

10. The method of claim 9 , further comprising: confining the effect of the laser beam to the surface coating.

11. The method of claim 1 , wherein the step of pulsing limits a length of each pulse to a range from 100 to not greater than 150 nanoseconds, and the steps of positioning and pulsing are repeated such that 15 square millimeters of the surface coating are removed per second in the step of removing.

Assignments (2)
CHANGE OF NAME Recorded May 31, 2011
From: AIRBUS DEUTSCHLAND GMBH
To: AIRBUS OPERATIONS GMBH
Reel/Frame 026360/0849 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 15, 2005
From: ENGLER, HARALD; BERNHARD HOENEMANN, LOTHER; DOERR, TILLMANN
To: AIRBUS DEUTSCHLAND GMBH
Reel/Frame 016540/0872 →