Pressure equalization in a dual flow path exhaust of a hypersonic propulsion system

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United States of America Patent

PATENT NO 11339744
SERIAL NO

16785052

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Abstract

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A dual flow path exhaust assembly for use with a combined turbofan and ramjet engine includes a turbofan engine exhaust duct, a ramjet engine exhaust duct, a combined outlet, and door configured to move between an open position and a closed position to selectively isolate the turbofan engine exhaust duct from the combined outlet.

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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
Metzger, Nicholas Fishers, US 2 1
Pesyna, Kenneth M Carmel, US 35 244
Roesler, Timothy Plainfield, US 2 1
Taylor, Todd S Bargersville, US 9 66

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