초록 ▼

A method of supplying air to a vehicle is provided, wherein the method includes modulating a flow of air from between a fan assembly of a turbofan engine and a high pressure compressor of the turbofan engine with a core driven fan stage coupled in parallel to the high pressure compressor. The method

A method of supplying air to a vehicle is provided, wherein the method includes modulating a flow of air from between a fan assembly of a turbofan engine and a high pressure compressor of the turbofan engine with a core driven fan stage coupled in parallel to the high pressure compressor. The method also includes channeling the air from the core driven fan stage to the vehicle.

대표청구항 ▼

What is claimed is: 1. A method of supplying air to a vehicle, said method comprising: modulating, using an inlet guide vane, a flow of air from between a fan assembly of a turbofan engine and a high pressure compressor of the turbofan engine with a core driven fan stage coupled in parallel to the

What is claimed is: 1. A method of supplying air to a vehicle, said method comprising: modulating, using an inlet guide vane, a flow of air from between a fan assembly of a turbofan engine and a high pressure compressor of the turbofan engine with a core driven fan stage coupled in parallel to the high pressure compressor; and channeling the air from the core driven fan stage to the vehicle. 2. A method in accordance with claim 1 further comprising independently modulating the flow of the air between substantially zero air flow and a maximum discharge air flow. 3. A method in accordance with claim 1 further comprising channeling the air through a collector system to an external port of the engine for vehicle use. 4. A method in accordance with claim 1 further comprising channeling excess air not used by the vehicle through a relief port to a by-pass duct for use in engine thrust production. 5. A method in accordance with claim 1 further comprising increasing a pressure ratio of the core driven fan stage within a range of approximately 1.2 to approximately 2. 6. An air supply system for a vehicle having a turbofan engine including an inlet guide vane, said system comprising a core driven fan stage coupled in parallel with a high pressure compressor of the turbofan engine, at least one of said core driven fan stage and said inlet guide vane configured to modulate a flow of air from between a fan assembly of the engine and said high pressure compressor, said core driven fan stage further configured to channel the air to the vehicle. 7. A system in accordance with claim 6 wherein said inlet guide vane independently varies the flow of the air between substantially zero air flow and a maximum discharge air flow. 8. A system in accordance with claim 6 further comprising a collector system to channel the air to an external port of the engine for vehicle use. 9. A system in accordance with claim 6 further comprising a relief port configured to channel air not used by the vehicle to a by-pass duct for use in engine thrust production. 10. A system in accordance with claim 6 configured to increase the pressure ratio of the core driven fan stage within a range of approximately 1.2 to approximately 2. 11. A turbofan engine for a vehicle, said engine comprising: a fan assembly; a high pressure compressor; and an air supply system, said system comprising a core driven fan stage coupled in parallel with said high pressure compressor and an inlet guide vane, at least one of said inlet guide vane and said core driven fan stage configured to modulate a flow of air from between said fan assembly and said high pressure compressor, said core driven fan stage further configured to channel the air to the vehicle. 12. A turbofan engine in accordance with claim 11 wherein said inlet guide vane independently varies the air flow between substantially zero air flow and maximum discharge air flow. 13. A turbofan engine in accordance with claim 11 wherein said air supply system further comprises a collector system to channel the air to an external port of the engine for vehicle use. 14. A turbofan engine in accordance with claim 11 wherein said air supply system further comprises a relief port configured to direct air not used by the vehicle to a by-pass duct for use in engine thrust production. 15. A turbofan engine in accordance with claim 11 wherein said air supply system is configured to increase the pressure ratio of the core driven fan stage within a range of approximately 1.2 to approximately 2.