Method for detecting cracks in an aircraft or gas turbine component

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United States of America Patent

PATENT NO 9719774
APP PUB NO 20120297600A1
SERIAL NO

13479316

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Abstract

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A method for detecting cracks in an aircraft or gas turbine component includes ascertaining geometric data about the component using an optical measurement method, analyzing the geometric data, using an electronic evaluation device, so as to automatically recognize and/or classify at least one of cracks and other damage and storing a position of the at least one of cracks and other damage.

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Patent Owner(s)

Patent OwnerAddress
LUFTHANSA TECHNIK AGWEG BEIM JAEGER 193 HAMBURG 22335

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Ernst, Michael Pinneberg, DE 24 385
Ullrich, Thiemo Hamburg, DE 3 41

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