General Electric Company

Trent A Larson

John Patrick Dowell

Vijayaselvan Jayakar

Charles B Atz

Pratap Subhash Shitole

Shirish Bhide

Abhijeet Warale

Gary Szuch

Jayesh Jain

Edward Phaneuf

Aravind Kalavara

Amit Kawatkar

Scott Snyder

Cain Piotrowski

An exhaust casing for use with a turbocharger includes a hollow body that has two mutually opposed large walls, which extend along first and second major dimensions of the hollow body and are spaced apart by a minor dimension of the hollow body, the hollow body defining a plenum and an inlet nozzle opening into the plenum along the minor dimension of the hollow body. The casing further includes an outlet nozzle opening from the plenum along one of the major dimensions of the hollow body.

Multi-stage turbocharged engine

A charge air cooler cover includes a nozzle configured for connection to an outlet of a compressor for receiving charge air, a tray configured for connection to an inlet of a charge air cooler, and a plenum leading from the nozzle to a plurality of passages defined by a plurality of ribs. The plurality of passages connects the plenum to the tray. The ribs and the tray are arranged to achieve substantially uniform charge air velocity across the inlet of the charge air cooler, in at least one mode of operation.

Charge air cooler cover and turbocharger bracket

A duct for connection between an exhaust manifold and a high-pressure turbine inlet include a cylindrical duct body defining a longitudinal axis. A frustoconical outlet nozzle connected at one end of the duct body and extending at about eighty-five degrees from the longitudinal axis. The duct further includes an inlet bell connected at the other end of the duct body and extending at about fifty degrees from the longitudinal axis.

High pressure turbine inlet duct and engine

Growing community of inventors

Rochester, MI, United States of America

Trent A Larson