Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
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United States of America Patent
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Mar 26, 2013
Grant Date -
Sep 4, 2008
app pub date -
Oct 20, 2005
filing date -
Nov 5, 2004
priority date (Note) -
Expired
status (Latency Note)
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Abstract
A stator for installation in a rear section of a jet engine includes a plurality of guide vanes which extend in the radial direction of the stator and between them define ducts for leading a gas. A first side of the stator in its axial direction defines an inlet for the gas and a second side, opposite the first side, defines an outlet for the gas. The guide vanes have such a shape that together they at least substantially cover the gas inlet viewed in the axial direction of the stator from the outlet side thereof.
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