NASA NTRS · 20180002477
Freeform Deposition Method for Coolant Channel Closeout
Abstract
A method is provided for fabricating a coolant channel closeout jacket on a structure having coolant channels formed in an outer surface thereof. A line of tangency relative to the outer surface is defined for each point on the outer surface. Linear rows of a metal feedstock are directed towards and deposited on the outer surface of the structure as a beam of weld energy is directed to the metal feedstock so-deposited. A first angle between the metal feedstock so-directed and the line of tangency is maintained in a range of 20-90.degree.. The beam is directed towards a portion of the linear rows such that less than 30% of the cross-sectional area of the beam impinges on a currently-deposited one of the linear rows. A second angle between the beam and the line of tangency is maintained in a range of 5-65 degrees.
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Gradl, Paul R., Reynolds, David Christopher, Walker, Bryant H.. 2017-12-05. Freeform Deposition Method for Coolant Channel Closeout. https://ntrs.nasa.gov/citations/20180002477
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