Seal assembly for a static structure of a gas turbine engine

Ensemble joint pour une structure statique d'un moteur a turbine a gaz

Abstract

A static structure of a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, an outer platform, an inner platform, an airfoil that extends between the outer platform and the inner platform, a service tube disposed at least partially through the airfoil, and a seal assembly that seals between the service tube and one of the outer platform and the inner platform.

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