Reverse flow gas turbine engine with radially outward turbine

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United States of America Patent

PATENT NO 10378438
APP PUB NO 20170306841A1
SERIAL NO

15134089

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Abstract

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A gas turbine engine includes a propulsor, a compressor comprising a compressor rotor, and a turbine comprising a turbine rotor fixedly mechanically coupled to the compressor rotor. The propulsor and the compressor are arranged in axial flow series. The turbine rotor is radially outward of the compressor rotor, and the direction of fluid flow through the turbine is generally opposite the direction of gas flow through the propulsor and the compressor.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC2059 S TIBBS AVE INDIANAPOLIS IN 46241

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Skertic, Richard Joseph Carmel, US 25 72

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