Gas turbine engine lube oil system
AssigneeSolar Turbines Incorporated
InventorsAlin Cezar Postescu, Behnam Heydari
Life of this patent
Estimating the term…
Abstract
A gas turbine engine lube oil system (740) includes a first passage (750) and a second passage (760). The first passage (750) includes a first elongated compartment (751) with a closed end (752) and a first open end (753) distal to the closed end (752). The first passage (750) also includes a plurality of bearing return line connection points. The second passage (760) includes a second elongated compartment (761) with a suction end (762) and a second open end (763) distal to the suction end (762). The first open end (753) is in flow communication with the second open end (763).
Claims20
A gas turbine engine lube oil system comprising:
- a first passage having
- a first elongated compartment including
- a closed end,
- a first open end distal to the closed end, and
- a plurality of bearing return line connection points;
- a second passage having
- a second elongated compartment including
- a suction end, and
- a second open end distal to the suction end;
- and
- wherein the first open end is in flow communication with the second open end.
A gas turbine engine lube oil system comprising:
- a first elongated compartment having
- a closed end, and
- a first open end distal to the closed end;
- a second elongated compartment parallel and adjacent to the first elongated compartment, the second elongated compartment having
- a suction end adjacent to the closed end, and
- a second open end distal to the suction end and adjacent to the first open end;
- and a sub-divided containment area having
- a first compartment in flow communication with the first open end,
- a second compartment in flow communication with the second open end, and
- a flow transfer compartment in flow communication with the first compartment at a location distal to the first open end and in flow communication with the second compartment at a location distal to the second open end,
- wherein bulkheads sub-divide the first compartment, the second compartment, and the flow transfer compartment;
- wherein the first elongated compartment and first compartment form a first passage and the second elongated compartment and second compartment form a second passage, and the first passage is configured to connect to a of bearing return lines.
A method for deaerating lube oil in a gas turbine engine lube oil system, the method comprising:
- returning lube oil from gas turbine engine bearing assemblies to a first passage of an elongated passage lube oil tank;
- flowing the lube oil from bearing return line connection points in the first passage through the first passage to a first flow transfer connection point and away from a closed end of the first passage, the first flow transfer connection point being distal to the closed end of the first passage;
- transferring the lube oil from the from the first flow transfer connection point to a second flow transfer connection point of a second passage of the elongated passage lube oil tank by a flow connection means, the second passage being in flow isolation from the first passage except for the flow connection means;
- and
- flowing the lube oil from the second flow connection point to a suction end of the second passage, the second flow connection point being distal to the suction end.
Dependencies are inferred from the claim text.