Flow control device for a three stream turbofan engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9506423
APP PUB NO 20150121841A1
SERIAL NO

14206232

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Abstract

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A gas turbine engine includes a core engine, a first bypass passage disposed about the core engine and a second bypass passage disposed about the first bypass passage. A flow control is disposed within the second bypass for controlling bypass airflow through the second bypass. The flow control translates axially between an open position and a closed position to vary and control airflow through the second bypass passage.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bush, Robert H Glastonbury, US 9 65
Izquierdo, Felix Boynton Beach, US 10 28
McAlice, Timothy J Jupiter, US 14 81

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