Surfacing of additively manufactured components and corresponding manufactured components of a turbomachine
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United States of America Patent
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Jan 9, 2018
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N/A
app pub date -
Sep 1, 2015
filing date -
Sep 8, 2014
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Abstract
The present invention relates to a method for manufacturing components, in particular components of turbomachines, such as aircraft engines, wherein an additive method is used at least partially for the manufacture of the component (1), wherein at least one surface region (3) of the additively manufactured portion of the component (1) is provided with a smoothing layer (2), which is deposited by vapor deposition. In addition, the invention relates to a correspondingly manufactured component of a turbomachine.
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