General Electric Company

Ge Avio S.r.l.

General Electric Deutschland Holding Gmbh

Lyle Douglas Dailey

Jeffrey Donald Clements

Aspi Rustom Wadia

Paul Hadley Vitt

Daniel Edward Mollmann

Matteo Renato Usseglio

Francesco Bertini

Christopher Ryan Johnson

Andreas Peters

Andrea Arnone

Filippo Rubechini

Matteo Giovanni

Daniel Mollmann

A turbine section for a gas turbine engine defines a radial direction and includes a low-pressure (LP) turbine that includes a first plurality of LP turbine blades that includes a first stage having first stage LP turbine blades that rotate in a first direction at a first speed, a second plurality of LP turbine blades that includes a plurality of stages of LP turbine blades disposed downstream of the first stage LP turbine blades that rotate in a second direction opposite the first direction at a second speed, a first LP turbine spool connected to the first plurality of LP turbine blades on an inner side of the first plurality of LP turbine blades in the radial direction, and a second LP turbine spool connected to the second plurality of LP turbine blades on an inner side of the second plurality of LP turbine blades in the radial direction.

Counter-rotating turbine

Growing community of inventors

Cincinnati, OH, United States of America

Lyle Douglas Dailey