Fuel manifold inlet tube
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United States of America Patent
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Dec 11, 2007
Grant Date -
Jul 19, 2007
app pub date -
Jan 31, 2007
filing date -
Jan 27, 2004
priority date (Note) -
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status (Latency Note)
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Abstract
In a gas turbine engine, a fuel inlet tube comprising a body, a channel defined in the body and in fluid communication with a manifold, and a side inlet in fluid communication with the channel, the side inlet being sealingly isolated by at least two annular sealing members concentric with each other and disposed about the tube body at longitudinally spaced part points thereon.
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