Gland leakage seal system
AssigneeRecurrent Engineering, LLC
InventorsLawrence Rhodes, Yakov Lerner
Life of this patent
Estimating the term…
Loading patent…
AssigneeRecurrent Engineering, LLC
InventorsLawrence Rhodes, Yakov Lerner
Estimating the term…
The present invention is directed to a turbine seal system. The turbine seal system captures working fluid which is escaping from a closed loop thermodynamic cycle system, condenses the captured working fluid, and returns the condensate back to the thermodynamic cycle system. The turbine seal system is configured to apply nitrogen, or other non-condensable, or other material, to capture or mix with the escaping working fluid. The combined mixture of working fluid which escapes the turbine and the nitrogen utilized to capture the working fluid is evacuated by an exhaust compressor which maintains a desired vacuum in a gland seal compartment of the turbine seal. The combined mixture can then be sent to a condenser to condense the working fluid vapor and evacuate the non-condensables, forming a working stream. Once the non-condensables have been evacuated, the working stream is pumped to a higher pressure, and prepared to be re-introduced into the thermodynamic cycle system.
A method for sealing a turbine of a thermodynamic cycle to minimize the escape of working fluid to the ambient environment, the method comprising:
A method for sealing a turbine within a thermodynamic cycle to minimize the escape of working fluid to the ambient environment, such that working fluid which escapes from the turbine is captured, condensed, and returned to the thermodynamic cycle the method comprising;
A method for sealing a turbine within a thermodynamic cycle to minimize the escape of working fluid to the ambient environment, wherein at least a portion of the working fluid that escapes from the turbine is captured, and returned to the thermodynamic cycle, the method comprising:
Dependencies are inferred from the claim text.