Gas ejection cone for aircraft turbojet engines
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United States of America Patent
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Apr 4, 2017
Issued Date -
N/A
app pub date -
Sep 12, 2014
filing date -
Mar 20, 2012
priority date (Note) -
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Abstract
A gas ejection cone includes a cylindrical-shaped front cone portion, a conical-shaped rear cone portion, a ventilation tube and a support bearing of this drainage and/or ventilation tube. The ventilation tube extends inside the cylindrical-shaped front and conical-shaped rear cone portions and emerges at the end of the conical-shaped rear cone portion. In particular, the conical-shaped rear cone portion includes a front sub-portion connected to the cylindrical-shaped front cone portion, and a rear sub-portion removably secured to the front sub-portion. The rear sub-portion is further equipped with an outlet port of the ventilation tube.
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