Improved leakage control in a gas turbine engine

Details Improved leakage control in a gas turbine engine Improved leakage control in a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/00 (2006.01) F01D 11/00 (2006.01)

Patent

CA 2543670

A gas turbine engine expansion joint comprises first and second members (28) having confronting faces (46) defining a gap (29) therebetween. At room temperature, the gap (29) varies in accordance with the temperature distribution profile of the first and second members (28) during normal engine operation.

L'invention concerne un joint de dilatation de moteur de turbine à gaz comprenant un premier élément et un second élément présentant des faces opposées définissant un espace entre elles. A température ambiante, cet espace varie selon le profil de distribution de température du premier élément et du second élément, lors du fonctionnement normal du moteur.

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