Abstract: Described is a ceramic core for producing cast component for a gas turbine engine, the core comprising: a first cavity forming member; a second member adjacent to or opposite the first cavity forming member; and a removable web which joins the first and second members.
Type:
Application
Filed:
January 25, 2018
Publication date:
August 2, 2018
Applicants:
ROLLS-ROYCE plc, ROSS CERAMICS LTD.
Inventors:
Aleksander M. CENDROWICZ, Graham J. BING, Stewart T. WELCH