Method for the manufacture of a component for high thermal loads, a component producible by this method and an aircraft engine provided with the component
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United States of America Patent
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Mar 7, 2017
Grant Date -
Feb 21, 2013
app pub date -
Aug 17, 2012
filing date -
Aug 17, 2011
priority date (Note) -
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Abstract
A method for manufacturing a thermally deformable component for high thermal loads, includes: providing a first area of the component with a first metallic material by a generative laser process, or making the first area of the first metallic material; providing a second area of the component with a second metallic material by a generative laser process, or making the second area of the second metallic material; where at least one of the metallic materials is deposited by the generative laser process, and a ratio of a linear expansion coefficient α1 of the first metallic material and of a linear expansion coefficient α2 of the second metallic material is as:
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