Split-zone flow metering T-tube

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United States of America Patent

PATENT NO 10808617
APP PUB NO 20170342904A1
SERIAL NO

15134653

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Abstract

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A gas turbine engine according to an example of the present disclosure includes a fan situated at an inlet of a bypass passage. The fan has a fan diameter, Dfan. A low pressure turbine section is configured to drive the fan and a first compressor section. The low pressure turbine section has a greater number of stages than the first compressor section. The low pressure turbine section has a maximum rotor diameter, Dturb. A ratio of the maximum rotor diameter Dturb divided by the fan diameter Dfan is less than 0.6.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Baltas, Constantine Avon, US 17 261
Farah, Jorge I Hartford, US 47 490
Parekh, Kalpendu J Colchester, US 14 101

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