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公开(公告)号:US20190323359A1
公开(公告)日:2019-10-24
申请号:US16378800
申请日:2019-04-09
Applicant: ROLLS-ROYCE plc
Inventor: Peter T. IRELAND , Nicholas Russell GREEN , Eduardo ROMERO , Gladys C. NGETICH
Abstract: Disclosed herein is a method of manufacturing a double walled section of an aerofoil (701) of a gas turbine engine (10), the method comprising: forming a plurality of columns (402) on an outer surface of a first structure; forming a plurality of columns (402) on a surface of each of a plurality of parts of a second structure; and forming a double walled section of an aerofoil (701) by attaching the ends of columns (402) on each part of the second structure to the ends of columns (402) on the first structure such that the first structure is an inner wall (401) of the section of the aerofoil (701) and the second structure is an outer wall (501) of the section of the aerofoil (701).