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US 2006/0222487 A1Published application
Vane for a gas turbine engine
AssigneeROLLS-ROYCE plc
InventorAndy Au
Life of this patent
Estimating the term…
Abstract
A vane (110, 210) for a gas turbine engine includes an aerofoil part (112, 212) and a sealing part (114, 214) at one end of the aerofoil part. The sealing part defines a cavity (122, 222) and an opening (130, 230) to the cavity.
Claims25
A vane for a gas turbine engine, characterised in that the vane (110, 240) includes an aerofoil part (112, 212) and a sealing part (114, 214) at one end of the aerofoil part, the sealing part defining a cavity (122, 222) and an opening (130, 230) to the cavity.
Dependencies are inferred from the claim text.