Turbine, particularly useful for small aircraft

Power plants – Combustion products used as motive fluid – Using special fuel or oxidizer

Reexamination Certificate

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Details

C060S737000, C060S039512, C060S039080, C184S011200, C184S006110, C184S006120, C184S006260, C415S016000, C415S112000

Reexamination Certificate

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07065954

ABSTRACT:
A turbine includes a combustion chamber with deflectors generating vortices in a secondary gas flow into the combustion chamber, thereby confining the flame front from penetrating into the cold region of the chamber under variable operating conditions, simplifying cooling of the chamber walls. The turbine further includes devices for decoupling vibrations between the high- and low-speed shafts, including a loosely mounted spline coupling the high-speed shaft to the step-down system and disk dampening means coupling the step-down system to the low-speed output shaft.

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patent: 2004324863 (2004-11-01), None

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