AIRCRAFT

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20250092823A1
SERIAL NO

18969412

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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An aircraft comprises a machine body which encloses a turbofan gas turbine engine. The turbofan gas turbine engine includes a heat exchanger module, fan assembly, compressor module, turbine module, and exhaust module. The heat exchanger module communicates with the fan assembly by an inlet duct. The heat exchanger module includes first heat transfer elements that transfer heat energy from a first fluid within the transfer elements to an airflow passing over a surface of the transfer elements before entry of the airflow into a fan assembly inlet. The first fluid contained within transfer elements has a temperature, and the airflow passing over the transfer element surface has a temperature. The turbofan gas turbine engine further includes at least one second heat transfer element, with the or each second heat transfer element transfers heat energy from the first fluid to a second fluid.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE PLCKINGS PLACE 90 YORK WAY LONDON N1 9FX

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
BINNINGTON, Thomas S Bristol, GB 15 18
BLACKER, Daniel Bristol, GB 11 12
JONES, David A Bristol, GB 117 1881
WONG, Natalie C Bristol, GB 20 21

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