Nova Patents
EP1197635A3

Gas turbine engine airfoil cooling

Abstract

Cooling air bled from the compressor section of a gas turbine engine is used to first cool the leading edge portion of the turbine blades and is then used to cool other portions of the turbine blades e.g. by film cooling.

EP1197635A3, drawing sheet 1
Sheet 1 of 1

Term

Term ended

Projected expiry passed 23 August 2021, 5.1 years ago.

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