Protection system and turbo engine with a protection system
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United States of America Patent
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May 7, 2019
Grant Date -
Oct 13, 2016
app pub date -
Apr 8, 2016
filing date -
Apr 10, 2015
priority date (Note) -
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Abstract
A protection system for a turbo engine, in particular an aircraft engine is provided. The turbo engine comprises at least one fluid duct element with a casing device comprising at least one casing section, encasing at least partially the at least one fluid duct element, said casing device comprising at least one fluid escaping means, wherein the casing device is intended to at least partially contain and/or deflect a fluid stemming from a burst event at the fluid duct element event in order to at least partially protect the turbo engine.
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