Turbopump system for driving a plurality of pumps
AssigneeSociete Nationale d'Etude et de Construction de Moteurs d'Aviation
InventorFrancois J. P. Mirville
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AssigneeSociete Nationale d'Etude et de Construction de Moteurs d'Aviation
InventorFrancois J. P. Mirville
Estimating the term…
A turbopump system for pumping two separate fluids is disclosed having a r of concentric turbine rotors located within a turbine casing, each directly connected to a pump impeller. The centrifugal pumps, which may be located on opposite sides of the turbine casing are separately connected to their respective fluids such that the two fluids may be pumped simultaneously. A propellant fluid is directed through a generally annular space defined between the concentric turbine rotors to rotate them in opposite directions. Turbine blades attached to each of the turbine rotors extend into this annular space in order to drive the turbine rotors. The pitches of the turbine blades are such that the rotors are driven in opposite directions and one of the turbine rotors may be driven at a different speed than the other.
A turbopump system for pumping two separate fluids comprising:
Dependencies are inferred from the claim text.