Aircraft and a retrofit cryogenic fuel system
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United States of America Patent
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Jul 11, 2017
Grant Date -
Dec 3, 2015
app pub date -
Nov 26, 2013
filing date -
Dec 28, 2012
priority date (Note) -
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Abstract
An aircraft having a turbine engine having a bleed air output line, a cryogenic fuel system having a cryogenic fuel tank for storing cryogenic fuel and a supply line operably coupling the tank to the turbine engine, and an on board inert gas generating system (OBIGGS) fluidly coupled to the bleed air output and having a nitrogen rich stream output line and an oxygen rich stream output line.
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