GAS TURBINE ENGINE COMPONENT WITH EMBEDDED DATA
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United States of America Patent
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Issued Date -
Oct 29, 2015
app pub date -
Apr 28, 2014
filing date -
Apr 28, 2014
priority date (Note) -
Abandoned
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Abstract
A component for a gas turbine engine is disclosed. The component includes at least a first portion and a second portion, and a data representing matrix. The second portion includes a second portion surface. The data representing matrix is formed directly on the second portion surface and includes a plurality of contrasting cells arranged in a geometric pattern representing information about the component including test data, a serial number, and a part number. The plurality of contrasting cells includes a plurality of first cells and a plurality of second cells that contrast from the plurality of first cells.
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