Fuel delivery system for delivering hydrogen fuel to a fuel injection system in a complex cycle gas turbine engine

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United States of America

PATENT NO 12006871
SERIAL NO

17476311

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Abstract

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A complex cycle gas turbine engine for an aircraft with hydrogen fuel supply. The gas turbine engine comprises, in fluid flow series, a core gas turbine and a recuperator for heating hydrogen fuel prior to combustion by turbine exhaust products.

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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
Palmer, Chloe J Derby, GB 24 42
Whurr, John R Derby, GB 7 68

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