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US 2014/0193249 A1Published application
Electrical conductor paths
AssigneeROLLS-ROYCE plc
InventorsDavid V. ROBERTS, Alison Jane McMILLAN, Stephen John BOOTH
Life of this patent
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Abstract
A component, for example an aerofoil vane or other gas path structure in a gas turbine machine such as a gas turbine engine, in which an insulated electrical conductor path is embedded structurally integrally, and in which electromagnetic shielding, for the embedded electrical conductor path is provided structurally integrally.
Claims14
An aircraft component comprising:
- an insulated electrical conductor path that is embedded structurally integrally, wherein electromagnetic shielding for the embedded electrical conductor path is provided structurally integrally to suppress electromagnetic effects between the embedded electrical conductor path and other electrical conductor paths in the aircraft.
Dependencies are inferred from the claim text.