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公开(公告)号:US10179362B2
公开(公告)日:2019-01-15
申请号:US15214747
申请日:2016-07-20
Applicant: United Technologies Corporation
Inventor: Thomas N Slavens , James T Auxier
Abstract: A core for use in casting an internal cooling circuit within a gas turbine engine component, the core including a core body with an outer skin in which a core body additively manufacturing binder is locally eliminated. A method of manufacturing a core for casting a component, including casting a core body for at least partially forming an internal passage architecture of a component; and forming an outer skin on the core body in which a core body binder is locally eliminated.