Ge Avio S.r.l.

Alberto Buonvino

Daniele Coutandin

Luca Giacobone

Francesco Bertini

Ernesto Sozio

Cosimo Bianchini

Riccardo Da Soghe

An airfoil assembly defining a primary airflow path for a turbine engine comprising a platform, an airfoil extending from the platform and into at least a portion of the primary airflow path, a secondary airflow path comprising air from the primary airflow path, and a deflector provided within the secondary airflow path.

Turbine engine component with a set of deflectors

A turbine engine having counter-rotating rotors comprising a first rotor, rotating in a first rotational direction, defining a first rotor set of blades axially spaced to define a gap, and a second rotor, rotating in a second rotational direction counter the first rotational direction. The second rotor further including a second set of blades received within the gap of the first rotor. A plurality of fluid passages is formed in the first rotor with an outlet facing the gap.

Method and apparatus for cooling a portion of a counter-rotating turbine engine

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Turin, Italy

Alberto Buonvino