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US 8,282,343 B2Granted
Vane
AssigneeROLLS-ROYCE plc
InventorRobert J. Smith
Life of this patent
Estimating the term…
Abstract
A vane for a gas turbine engine includes a cap arrangement having a cap insert and a cap adapted to receive the insert. The cap insert has a wall defining a through passage from top to bottom of the cap insert for receiving a cable or the like therethrough. The wall has a slot with a convoluted profile.
Claims13
A vane for a gas turbine engine comprising:
- a cap arrangement including:
- a cap insert;
- and
- a cap adapted to receive the insert,
- the cap insert having a wall defining a through passage from a top to a bottom of the cap insert for receiving a cable therethrough, and
- the wall defining a slot with a convoluted profile.
3 more elements
Dependencies are inferred from the claim text.