Propelling nozzle for a turbofan engine on a supersonic aircraft

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United States of America Patent

PATENT NO 11448162
APP PUB NO 20210079870A1
SERIAL NO

16954053

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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The invention relates to a propelling nozzle for a turbofan engine on a supersonic aircraft, the propelling nozzle including: a propelling nozzle wall, a duct, which is radially outwardly bounded by the propelling nozzle wall, and a central body arranged in the duct. According to the invention, the central body is connected to the propelling nozzle wall via at least one brace.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE DEUTSCHLAND LTD & CO KGESCHENWEG 11 BLANKENFELDE-MAHLOW 15827

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Schillinger, Thomas Berlin, DE 6 48
Todorovic, Predrag Berlin, DE 62 370

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