Invention Publication
- Patent Title: GAS TURBINE ENGINE COMPONENTS WITH FOAM FILLER FOR IMPACT RESISTANCE
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Application No.: US17557027Application Date: 2021-12-20
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Publication No.: US20230193763A1Publication Date: 2023-06-22
- Inventor: Michael J. Whittle, JR. , Stephen Harris
- Applicant: Rolls-Royce plc , Rolls-Royce High Temperature Composites Inc.
- Applicant Address: GB CA London
- Assignee: Rolls-Royce plc,Rolls-Royce High Temperature Composites Inc.
- Current Assignee: Rolls-Royce plc,Rolls-Royce High Temperature Composites Inc.
- Current Assignee Address: GB CA London
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D5/28 ; F01D5/14
Abstract:
An airfoil assembly for a gas turbine engine includes an airfoil extending radially relative to a central reference axis. A spar is located within the airfoil and spaced from the airfoil at all radial locations along the airfoil such that a gap is maintained between the airfoil and the spar. A foam is located between the airfoil and the spar.
Public/Granted literature
- US11746660B2 Gas turbine engine components with foam filler for impact resistance Public/Granted day:2023-09-05
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