Tail cone for a microjet rotary turbine engine
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United States of America Patent
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Feb 6, 2018
Issued Date -
N/A
app pub date -
Jul 8, 2014
filing date -
May 12, 2011
priority date (Note) -
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Abstract
The invention relates to a rear casing for a turbine engine comprising a primary body generating a primary flow (10) to be ejected through a primary nozzle (6), said rear casing (7) being shaped so as to be positioned downstream from the primary body and to define, on the inside of the turbine engine, the path followed by the primary flow downstream from the primary nozzle (6). The tail cone is characterised in that it comprises a connection to a system for supplying a pressurised gas and at least one perforation (8) for injecting the pressurised gas through the perforation and into the primary flow. The casing preferably comprises at least one means for rotating same about the axis of rotation of the mobile elements of the primary body.
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