General Electric Company

Scott Michael Elam

Kenneth Damon Black

Gregory Allan Crum

Prashant Kantappa Patil

A turbine diffuser is disclosed. The turbine diffuser includes a diffuser segment having a forward end and an aft end with a flange disposed at the aft end of the diffuser segment. The diffuser segment is joinable to an adjacent diffuser segment via the flange, which includes a seal retainer that is securedly connectable in a radial direction with a seal.

Method, system and apparatus for turbine diffuser sealing

An apparatus to support a rotor of a turbine engine disposed upon a support surface is disclosed. The apparatus includes a housing, a rotor support bearing disposed within the housing, and a support leg in operable communication with the housing and in direct structural connection with the support surface.

Growing community of inventors

Simpsonville, SC, United States of America

Scott Michael Elam