The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 06, 2015

Filed:

May. 19, 2011
Applicants:

Juergen Steinwandel, Uhldingen-Muehlhofen, DE;

Domenico Furfari, Hamburg, DE;

Nikolaus Ohrloff, Buxtehude, DE;

Claudio Dalle Donne, Munich, DE;

Inventors:

Juergen Steinwandel, Uhldingen-Muehlhofen, DE;

Domenico Furfari, Hamburg, DE;

Nikolaus Ohrloff, Buxtehude, DE;

Claudio Dalle Donne, Munich, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B23K 26/00 (2014.01); C21D 10/00 (2006.01); B64F 5/00 (2006.01);
U.S. Cl.
CPC ...
C21D 10/005 (2013.01); B64F 5/0081 (2013.01); C21D 10/00 (2013.01);
Abstract

The present invention provides a method for preventing the forming of cracks and slowing the crack propagation in metallic airplane structural parts by laser shock peening with the following steps: Providing an airplane structural part having a crack; irradiating a first surface area of the airplane structural part close to the crack with a first pulsed laser beam having a first wavelength and a first pulsation frequency, wherein energy of the first laser beam is absorbed by the airplane structural part and a shock wave runs through the airplane structural part, which creates compressive prestressings in the airplane structural part.


Find Patent Forward Citations

Loading…