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Freeform Deposition Method for Coolant Channel CloseoutA 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.
Document ID
20180002477
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Gradl, Paul R.
Reynolds, David Christopher
Walker, Bryant H.
Date Acquired
April 20, 2018
Publication Date
December 5, 2017
Subject Category
Mechanical Engineering
Spacecraft Propulsion And Power
Report/Patent Number
Patent Number: US-Patent-9,835,114
Patent Application Number: US-Patent-Appl-SN-15/615,539
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,835,114
Patent Application
US-Patent-Appl-SN-15/615,539
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