초록 ▼

An active air pressure control apparatus for a bearing sump cavity in a gas turbine engine includes a bearing assembly supporting a rotatable shaft that connects a rotatable power turbine and a rotatable compressor. The active air pressure control apparatus also includes a sump cavity surrounding th

An active air pressure control apparatus for a bearing sump cavity in a gas turbine engine includes a bearing assembly supporting a rotatable shaft that connects a rotatable power turbine and a rotatable compressor. The active air pressure control apparatus also includes a sump cavity surrounding the bearing assembly, a sump pressurization cavity in flow communication with a source of pressurized air and in flow communication with the sump cavity, and a sump vent tube in flow communication with the sump cavity and an air/oil separator. The active air pressure control apparatus includes an adjustable valve in the sump vent tube, and a controllable blower in flow communication with the sump vent tube.

대표청구항 ▼

What is claimed is: 1. Active air pressure control apparatus for a bearing sump cavity in a gas turbine engine comprising: a bearing assembly supporting a rotatable shaft connecting a rotatable power turbine and a rotatable compressor; a sump cavity surrounding said bearing assembly; a sump pressur

What is claimed is: 1. Active air pressure control apparatus for a bearing sump cavity in a gas turbine engine comprising: a bearing assembly supporting a rotatable shaft connecting a rotatable power turbine and a rotatable compressor; a sump cavity surrounding said bearing assembly; a sump pressurization cavity in flow communication with a source of pressurized air and in flow communication with said sump cavity via a labyrinth seal configured to minimize oil leakage into an interior cavity of said gas turbine engine; a sump vent tube in flow communication with said sump cavity and an air/oil separator; an adjustable valve positioned in said sump vent tube, capable of being set in said adjustable valve selectively positionable to one of a fully open position and a partially closed position; and a controllable blower in flow communication with said sump vent tube, wherein said controllable blower is turned off when the adjustable valve is set in the partially closed position and turned on when the adjustable valve is set to the fully open position. 2. The apparatus of claim 1 further comprising: a plurality of bearing assemblies for supporting said rotatable shaft; a plurality of sump cavities each surrounding a respective one of said bearing assemblies in flow communication with said sump vent tube; a plurality of sump pressurization cavities each in flow communication with a source of pressurized air and each in flow communication with a respective one of said sump cavities. 3. Active air pressure control apparatus for a plurality of bearing sump cavities in a gas turbine engine comprising: a plurality of bearing assemblies supporting a rotatable shaft connecting a rotatable power turbine and a rotatable compressor; a plurality of sump cavities each surrounding a respective one of said bearing assemblies; a plurality of sump pressurization cavities each in flow communication with a source of pressurized air and each in flow communication with a respective one of said sump cavities via a plurality of labyrinth seals configured to minimize oil leakage into an interior cavity of said gas turbine engine; a plurality of sump vent tubes each in flow communication with a respective one of said sump cavities and an air/oil separator; an adjustable valve positioned in each said sump vent tube, said adjustable valve selectively positionable to one of a fully open position and a partially closed position; and a controllable blower in flow communication with said sump vent tubes, wherein said controllable blower is turned off when the adjustable valves are set in the partially closed position and turned on when at least one of the adjustable valves is set to the fully open position. 4. The apparatus of claim 1, further comprising a pressure control system for controlling said adjustable valve. 5. The apparatus of claim 4, wherein said pressure control system sets said adjustable valve to the fully open position during idle operation and sub-idle operation of the gas turbine engine. 6. The apparatus of claim 4, wherein said pressure control system sets said adjustable valve to the partially closed position during above-idle operation of the gas turbine engine. 7. The apparatus of claim 4, wherein said pressure control system further controls said controllable blower. 8. The apparatus of claim 3, further comprising a pressure control system for separately controlling said adjustable valves. 9. The apparatus of claim 8, wherein, said pressure control system controls each said adjustable valve to maintain one or more of the following: a predetermined pressure in each said sump cavity and a predetermined air flow through each said sump vent tube. 10. The apparatus of claim 8, further comprising a controllable blower in flow communication with each said sump vent tube, wherein said pressure control system further controls said controllable blowers.