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US 2013/0192219A1 Aug.1,2013 12. The energy conversion system of claim 1, Wherein the turbine Wheel further comprises a plurality of turning vanes disposedintheaxial?oW passageandextendingcircumfer entiallyaroundtheshaft,thepluralityofturningvanesbeing con?guredtoturnthe?oW of?uidatleastfromoneofthe?rst and second radial directions to an axial direction. 13.A methodofrotatingashaft,comprising: directinga?uidfromaWave chamberthrougha?rstradial ?oW passage having a decreasing radius; sWirlingthe?uidWhiledirectingthe?uidthroughthe?rst radial?oW passage; directingthe?uidbetWeena?rstpluralityofimpulsetur binebladescoupledtotheshaft; turningthe?uidinanaxial?oW passageafterdirectingthe ?uid betWeen the ?rst plurality of impulse turbine blades; directing the ?uid betWeen a second plurality of impulse turbinebladescoupledtotheshaftafterturningthe?uid; and directing the ?uid from the second plurality of impulse turbine blades through a second radial ?oW passage havinganincreasingradius. 14. The method of claim 13, Wherein sWirling the ?uid comprises channeling the ?uid betWeen a ?rst plurality of noZZle vanes to provide a ?rst exit sWirl angle of from about 20 degrees to about 50 degrees. 15.Themethodofclaim14,furthercomprisingreversing the?oW ofthe?uidcomprising: directingthe?uidthroughthesecond?oWpassagetoWard thesecondpluralityofturbineblades; sWirling the ?uid While directing the ?uid through the second radial ?oW passage With the second plurality of noZZle vanes to provide a second exit sWirl angle that is substantiallyequaltothe?rstexitsWirlangle; directing the ?uid past the second plurality of impulse turbinebladesintotheaxial?oW passage; turningthemotive?uidintheaxial?oW passage; directingthe?uidfromtheaxial?oW passagetothe?rst pluralityofimpulseturbineblades;and directing the ?uid through the ?rst ?oW passage, past the ?rst plurality of noZZle vanes, and to the Wave chamber. 16. The method of claim 13, Wherein directing the ?uid fromthesecondpluralityofimpulseturbinebladesthrough thesecondradial?oWpassagecompriseschannelingthe?uid through a second plurality of noZZle vanes, Wherein each noZZle vane of the ?rst and second pluralities of noZZle vanes hasasubstantiallyrectangularprismshape. 17. The method of claim 13, Wherein sWirling the ?uid comprisesdirectingthe?uidthroughascrollduct. 18.An apparatusforconvertingenergyinanoscillating ?uid?oW intorotationalenergy,comprising: a base disposed proximal a Wave chamber; acaphavinganoutercircumferenceandbeingspacedapart fromthebase; a turbine Wheel attached to a shaft and disposed betWeen the cap and the base, the turbine Wheel having ?rst and second roWs of impulse turbine blades and a plurality of turning vanes, the ?rst and second roWs of impulse tur bine blades being separated axially apart, the turbine Wheelde?ninganaxial?oW passageextendingbetWeen the ?rst and second roWs of impulse blades, and the plurality of turning vanes extending at least partially throughtheaxial?oW passage; an annular member disposed around the turbine Wheel and having?rstandsecondmembersthatconvergetogether proximaltheturbineWheel,the?rstmemberandthecap at least partially de?ning a ?rst radial ?oW passage extendingfromtheoutercircumferenceofthecaptothe turbine Wheel, the second member at least partially de?ningasecondradial?oW passageextendingfromthe Wave chamber to the turbine Wheel; and a ?rst plurality of noZZle vanes coupled to the cap and the ?rst member of the annular member and spanning the ?rst radial ?oW passage, the ?rst plurality of noZZle vanes being substantially rectilinear. 19. The apparatus of claim 18, Wherein the ?rst member comprises a volute shaped scroll duct. 20.Theapparatusofclaim18,furthercomprisingasecond pluralityofmale vanescoupledtothebaseandthesecond memberoftheannularmemberandspanningthesecond?oW passage, Wherein the ?rst and second pluralities of noZZle vanes are oriented at a substantially uniform angle With respect to a radial line extending from the shaft and are disposed at a ?rst radial distance from the shaft Wherein the ?rst and second pluralities of noZZle vanes are substantially identicalinshape. 21. The energy conversion system of claim 1, Wherein the ?rstandsecondradial?oW passageseachextendpurelyradi aly. 22. The apparatus of claim 18, Wherein the ?rst and second radial ?oW passages extend substantially perpendicular to a central axis of the shaft. 23. The apparatus of claim 20, Wherein the ?rst and second roWs of impulse turbine blades are offset from the shaft by a secondradialdistance,the?rstradialdistancebeinggreater than the second radial distance. 24. The apparatus of claim 23, Wherein the ?rst radial distance is about tWice the second radial distance. * * * * *PDF Image | ENERGY CONVERSION SYSTEM WITH RADIAL FLOW TURBINE
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