Selectively deoxygenated stored fuel system
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United States of America Patent
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Jan 9, 2018
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app pub date -
Jan 19, 2015
filing date -
Jan 23, 2014
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Abstract
A gas turbine engine includes a multi-stage fuel injection system including at least a first fuel injection stage and a second fuel injection stage, a first fuel reservoir fluidly connected to the first fuel injection stage and fluidly connected to a selective valve, and a second fuel reservoir fluidly connected to the selective valve. The selective valve connects one of the first fuel reservoir and the second fuel reservoir to the second fuel injection stage.
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