Thermodynamic cycle operating at low pressure using a radial turbine
AssigneeClimeon AB
InventorsMagnus Genrup, Olle Bergström, Joachim Karthauser, Kari Munukka, Esko Ahlbom, Per Askebjer
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AssigneeClimeon AB
InventorsMagnus Genrup, Olle Bergström, Joachim Karthauser, Kari Munukka, Esko Ahlbom, Per Askebjer
Estimating the term…
Expansion machines in thermodynamic cycles operate at low pressures, i.e. below 10 bar. The interplay among components including gas generator, expansion machine, heat exchangers and pressure reduction device (absorber or condenser) is optimized, resulting in configurations operating at the lowest achievable cost level. A single stage radial turbine characterized by a pressure ratio of 5-10, a dimensionless speed of about 0.7 and a loading coefficient of 0.7 is a preferred expansion machine for certain thermodynamic cycles involving CO2 gas to permit such radial turbines to operate close to their optimum design specification and highest efficiency level. Methods to handle liquids which may condense within or inside the turbine are also disclosed, as well as methods to handle axial pressure on bearings and methods to protect lubricant in bearings.
A method to operate a thermodynamic cycle involving a working gas/fluid whereby the working gas/fluid passes from a hot, upstream side to a cold, downstream side of the thermodynamic cycle through a system comprising an inlet channel, an expansion machine operating at pressures below 10 bar maximum pressure, and an electricity generator operably coupled to the expansion machine so as to generate electricity, wherein the method comprises:
A system to be used in a thermodynamic cycle involving a working gas/fluid passing from a hot, upstream side to a cold, downstream side of the thermodynamic cycle, the system comprising:
Dependencies are inferred from the claim text.