Del Foro GUP 18
Gustavo Francisco Labala patentó la turbina en USA.
Pedido ingresado el 20/04/2004,
US Patent 7065954 - Turbine, particularly useful for small aircraft
US Patent Issued on June 27, 2006
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.
http://www.patentst orm.us/patents/ 007065954. pdf
Saludos,
Andres Ullmann
Gustavo Francisco Labala patentó la turbina en USA.
Pedido ingresado el 20/04/2004,
US Patent 7065954 - Turbine, particularly useful for small aircraft
US Patent Issued on June 27, 2006
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.
http://www.patentst orm.us/patents/ 007065954. pdf
Saludos,
Andres Ullmann
