Systems and methods utilizing turbine compressor discharge for hydrostatic manifold purge
AssigneeBJ Energy Solutions, LLC
InventorsTony Yeung, Ricardo Rodriguez-Ramon, Joseph Foster
Life of this patent
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AssigneeBJ Energy Solutions, LLC
InventorsTony Yeung, Ricardo Rodriguez-Ramon, Joseph Foster
Estimating the term…
Embodiments of systems and methods for air recovery are disclosed. The diverted pressurized air may be used to supply a hydrostatic purge to the unutilized portion of a turbine engine fuel manifold circuit to ensure that exhaust gases from the utilized side of the fuel manifold circuit do not enter the portion of the alternative fuel manifold circuit rack. The assembly used to remove compressor section pressurized air may include a flow control orifice, line pressure measuring instrumentation, non-return valves, isolation valves and hard stainless-steel tubing assemblies. In some embodiments, a turbine compressor section diverter system may include a small air receiver used to increase the volume of air supplying the manifold to aid in potential pressure and flow disruptions from a turbine engine compressor section.
A manifold pressurization system comprising:
A method of operating a dual fuel engine positioned to operate on a liquid fuel and a gaseous fuel, the method comprising:
A manifold pressurization system comprising:
Dependencies are inferred from the claim text.