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<blockquote data-quote="Shandor" data-source="post: 590705" data-attributes="member: 50">Del Foro GUP 18Gustavo Francisco Labala patentó la turbina en USA.Pedido ingresado el 20/04/2004,US Patent 7065954 - Turbine, particularly useful for small aircraftUS Patent Issued on June 27, 2006A turbine includes a combustion chamber with deflectors generating vorticesin a secondary gas flow into the combustion chamber, thereby confining theflame front from penetrating into the cold region of the chamber undervariable operating conditions, simplifying cooling of the chamber walls. Theturbine further includes devices for decoupling vibrations between the high-and low-speed shafts, including a loosely mounted spline coupling thehigh-speed shaft to the step-down system and disk dampening means couplingthe step-down system to the low-speed output shaft.<a href="http://www.patentst" target="_blank">http://www.patentst</a> orm.us/patents/ 007065954. pdfSaludos,Andres Ullmann</blockquote>

[QUOTE="Shandor, post: 590705, member: 50"] 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. [url]http://www.patentst[/url] orm.us/patents/ 007065954. pdf Saludos, Andres Ullmann [/QUOTE]

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