Electrical power generation system and method for mitigating corona discharge

Abstract

A power generation system including a housing defining a cavity and having an inlet for receiving a fluid that is used to cool and pressurize the cavity and an outlet for removing the fluid from the cavity. The system also may include a rotor having a first end positioned within the cavity of the housing and a second end, a plurality of bearings, positioned to contact the rotor, for providing radial support to the rotor, and a turbine connected to the second end of the rotor. Further, the system may include a heat sink positioned within the cavity and between the housing and the rotor, an electronic component attached to the heat sink, and a reaction chamber for receiving the fluid from the outlet and for producing a substance that is directed to the turbine causing it to rotate.

1 . A power generation system for mitigating corona discharge, comprising: 
 a housing defining a cavity and having an inlet for receiving a fluid that is used to cool and pressurize the cavity and an outlet for removing the fluid from the cavity;    a rotor having a first end positioned within the cavity of the housing and a second end;    a plurality of bearings positioned to provide radial support to the rotor;    a turbine connected to the second end of the rotor;    a heat sink positioned within the cavity and between the housing and the rotor;    an electronic component attached to the heat sink; and    a reaction chamber for receiving the fluid from the outlet and for producing a substance that is directed to the turbine causing it to rotate.    
   
   
       2 . The system as defined in  claim 1 , wherein the fluid is selected from a group consisting of a hydrogen gas, a nitrogen gas, a helium gas, an oxygen gas, an alcohol, a liquid rocket propellant, a liquid hydrogen, a liquid nitrogen, a liquid oxygen and combinations thereof.  
   
   
       3 . The system as defined in  claim 1 , wherein the fluid is introduced into the cavity at a substantially constant rate.  
   
   
       4 . The system as defined in  claim 1 , further comprising a supply conduit for receiving a second fluid and directing the second fluid to the reaction chamber.  
   
   
       5 . The system as defined in  claim 4 , wherein the second fluid is selected from a group consisting of a hydrogen gas, a nitrogen gas, a helium gas, an oxygen gas, an alcohol, a liquid rocket propellant, a liquid hydrogen, a liquid nitrogen, a liquid oxygen and combinations thereof.  
   
   
       6 . The system as defined in  claim 1 , wherein the electrical device is selected from a group consisting of an electromagnetic interference filter, a resistor, an inverter, a gate driver, a sensor, a power supply, a controller and combinations thereof.  
   
   
       7 . The system as defined in  claim 1 , further comprising a thrust disc connected to the first end of the rotor and a plurality of thrust bearings, positioned to contact the thrust disc, for providing axial support to the rotor.  
   
   
       8 . The system as defined in  claim 7 , wherein the plurality of bearings and the plurality of thrust bearings are foil bearings.  
   
   
       9 . The system as defined in  claim 1 , further comprising a stator attached to the heat sink and positioned adjacent to the rotor.  
   
   
       10 . An electrical power generation system for mitigating corona discharge, comprising: 
 an outer housing defining a chamber and having an input conduit for receiving a fluid that is used to cool and pressurize the chamber and an output conduit for removing the fluid from the chamber;    a turbine positioned adjacent to the outer housing;    a rotor positioned within the chamber and connected to the turbine for rotating about a central axis;    an inner housing positioned within the chamber and between the outer housing and the rotor;    a plurality of electronic components attached to the inner housing and cooled by the fluid;    a stator attached to the inner housing and positioned adjacent to the rotor;    a plurality of bearings, positioned adjacent to the stator, for providing radial support to the rotor and cooled by the fluid; and    a reaction chamber for receiving the fluid from the output conduit and producing a material that is directed to the turbine causing it to rotate.    
   
   
       11 . The system as defined in  claim 10 , further comprising a supply conduit for receiving a second fluid and directing the second fluid to the reaction chamber.  
   
   
       12 . The system as defined in  claim 10 , wherein the plurality of electrical components are selected from a group consisting of an electromagnetic interference filter, a bleed resistor, an inverter, a gate driver, a sensor, a power supply, a controller and combinations thereof.  
   
   
       13 . The system as defined in  claim 10 , further comprising a thrust disc connected to the rotor and a plurality of thrust bearings, positioned adjacent to the thrust disc, for providing axial support to the rotor.  
   
   
       14 . The system as defined in  claim 13 , wherein the plurality of bearings and the plurality of thrust bearings are self-acting, hydrodynamic foil bearings.  
   
   
       15 . A method for mitigating corona discharge, comprising: 
 introducing a fluid into a cavity defined by an outer housing, the fluid being used to pressurize the cavity and to cool a rotor, a stator, a plurality of bearings and a plurality of electrical components;    removing the fluid from the cavity; and    directing the fluid into a reaction chamber that produces a material used to cause a turbine that is attached to the rotor to rotate.    
   
   
       16 . The method as defined in  claim 15 , wherein the fluid is selected from a group consisting of a hydrogen gas, a nitrogen gas, a helium gas, an oxygen gas, an alcohol, a liquid rocket propellant, a liquid hydrogen, a liquid nitrogen, a liquid oxygen and combinations thereof.  
   
   
       17 . The method as defined in  claim 15 , further comprising introducing a second fluid into the reaction chamber to be combined with the fluid.  
   
   
       18 . The method as defined in  claim 17 , wherein the second fluid is selected from a group consisting of a hydrogen gas, a nitrogen gas, a helium gas, an oxygen gas, an alcohol, a liquid rocket propellant, a liquid hydrogen, a liquid nitrogen, a liquid oxygen and combinations thereof.  
   
   
       19 . The method as defined in  claim 15 , further comprising directing the fluid to a heat sink to cool the heat sink, wherein the stator and the plurality of electrical components are attached to the heat sink.  
   
   
       20 . The method as defined in  claim 15 , wherein the plurality of electronic components are selected from a group consisting of an electromagnetic interference filter, a bleed resistor, an inverter, a gate driver, a sensor, a power supply, a controller and combinations thereof.