High pressure turbine inlet duct and engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9228488
APP PUB NO 20140190164A1
SERIAL NO

13925091

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Abstract

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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.

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Patent Owner(s)

Patent OwnerAddress
GE GLOBAL SOURCING LLC901 MAIN AVENUE NORWALK CT 06851

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Atz, Charles B New Castle, US 5 45
Bhide, Shirish Troy, US 3 17
Dowell, John Grove City, US 11 107
Jayakar, Vijayaselvan Bangalore, IN 13 82
Larson, Trent A Rochester, US 3 17
Phaneuf, Edward Madison Heights, US 3 17
Piotrowski, Cain Canton, US 2 4
Shitole, Pratap Subhash Bangalore, IN 4 19
Warale, Abhijeet Auburn Hills, US 2 14

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