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In an exemplary variable area nozzle, a fixed duct section has an inlet and an outlet oriented approximately perpendicular to the inlet. A controllable nozzle member is disposed adjacent the outlet of the fixed duct section. The controllable nozzle member has an area that is adjustable to maintain a

In an exemplary variable area nozzle, a fixed duct section has an inlet and an outlet oriented approximately perpendicular to the inlet. A controllable nozzle member is disposed adjacent the outlet of the fixed duct section. The controllable nozzle member has an area that is adjustable to maintain a substantially constant nozzle pressure ratio. The controllable nozzle member may include first and second flap doors hinged and pivotable in opposite directions between an open position and a closed position and that also may be hinged and pivotable in a same direction so thrust from gas exiting the nozzle is vectorable. When disposed in rotor tips of an aircraft capable of rotary wing flight and fixed wing flight, the variable area nozzle may maintain a substantially constant nozzle pressure ratio near an optimized nozzle pressure ratio as the aircraft transitions from rotary wing flight to fixed wing flight.

대표청구항 ▼

What is claimed is: 1. A variable area nozzle comprising: a fixed duct section having an inlet and an outlet that is oriented substantially perpendicular to the inlet; and a controllable nozzle member disposed adjacent the outlet of the fixed duct section, the controllable nozzle member having a fi

What is claimed is: 1. A variable area nozzle comprising: a fixed duct section having an inlet and an outlet that is oriented substantially perpendicular to the inlet; and a controllable nozzle member disposed adjacent the outlet of the fixed duct section, the controllable nozzle member having a first flap door and a second flap door, wherein the first flap door and the second flap door present a smoothly contoured inner surface to vary a nozzle throat height and a nozzle pressure of the variable area nozzle based on a deployment angle of the first flap door and the second flap door, wherein the first flap door and the second flap door are each independently rotated by actuators in a first direction and in a second direction opposite of the first direction, wherein the first flap door and the second flap door are rotated in opposite directions to maintainable positions including an open position, a closed position and at least one intermediate position to vary the nozzle throat height and the nozzle pressure, and wherein the first flap door and the second flap door are rotated in a same direction to vector a flow of an exhaust gas in the first direction and in the second direction relative to the outlet of the fixed duct section. 2. The nozzle of claim 1, wherein an outlet area of the controllable nozzle member is controlled using the actuators to maintain a nozzle pressure ratio between 1.80:1 and 1.90:1. 3. The nozzle of claim 2, wherein the nozzle pressure ratio is maintained through a range of exhaust gas conditions. 4. The nozzle of claim 3, wherein the nozzle pressure ratio is maintained at about 1.89:1. 5. The nozzle of claim 1, wherein the actuators include a push rod. 6. The nozzle of claim 1, wherein the fixed duct section includes one of: a plurality of individual ducts; and a plurality of turning vanes. 7. The nozzle of claim 1, wherein the controllable nozzle member is adjusted based on a thrust schedule that relates the nozzle throat height to various exhaust gas conditions. 8. The nozzle of claim 1, wherein the actuators include an electric motor. 9. The nozzle of claim 1, wherein the actuators include a hydraulic actuator. 10. The nozzle of claim 1, wherein a first flap door interface hingeably joining the first flap door to the fixed duct section does not include internal, flow surface discontinuities. 11. The nozzle of claim 1, wherein the controllable nozzle member is controlled using the actuators independently of an exhaust valve that controls exhaust entering the fixed duct section. 12. The nozzle of claim 1, wherein, when the first flap door and the second flap door are positioned at the at least one intermediate position, the flow of the exhaust gas is at choked flow. 13. The nozzle of claim 12, wherein the first flap door and the second flap door are rotated to at least one second intermediate position between the open position and the closed position, and wherein when the first flap door and the second flap door are at the at least one second intermediate position, the flow of the exhaust gas is at choked flow. 14. A variable area nozzle comprising: a fixed duct section having an inlet and an outlet that is oriented substantially perpendicular to the inlet and that is configured to route exhaust gases to supply thrust; and a controllable nozzle member disposed adjacent the outlet of the fixed duct section and configured to direct the exhaust gases received from the fixed duct section, the controllable nozzle member comprising a first flap door and a second flap door, wherein a hinge axis of the first flap door is at a center of a first edge of the fixed duct section and the first flap door is smoothly contoured to the fixed duct section throughout a range of motion of the first flap door between a downward vector position and an upward vector position, and wherein a hinge axis of the second flap door is at a center of a second edge of the fixed duct section and the second flap door is smoothly contoured to the fixed duct section throughout a range of motion of the second flap door between the downward vector position and the upward vector position, wherein when the first flap door and the second flap door are rotated to the downward vector position, the first flap door and the second flap door direct a portion of the thrust downward, and wherein when the first flap door and the second flap door are rotated to the upward vector position, the first flap door and the second flap door direct a portion of the thrust upward; wherein a nozzle area formed between the first flap door and the second flap door is controlled using actuators throughout a range of maintainable deployment angles of the first flap door and the second flap door to vary a nozzle throat height and nozzle pressure, wherein the range of maintainable deployment angles of the first flap door and the second flap door includes a fully open position and at least one partially open position. 15. The variable area nozzle of claim 14, wherein the first flap door and the second flap door are independently and incrementally rotated using the actuators. 16. The variable area nozzle of claim 15, wherein the first flap door and the second flap door are rotated in first opposite directions to increase the nozzle throat height and the nozzle pressure and are rotated in second opposite directions to decrease the nozzle throat height and the nozzle pressure. 17. The variable area nozzle of claim 16, wherein the first flap door and the second flap door are each moveable to a closed position, wherein in the closed position a second edge of the first flap door meets a second edge of the second flap door when the first flap door and the second flap door are rotated in the second opposite directions to the closed position. 18. The variable area nozzle of claim 17, wherein the first flap door is moved by a first actuator and the second flap door is moved by a second actuator. 19. The variable area nozzle of claim 18, wherein at least one of the first actuator and the second actuator includes a push rod. 20. The variable area nozzle of claim 18, wherein at least one of the first actuator and the second actuator includes an electric motor. 21. The variable area nozzle of claim 18, wherein at least one of the first actuator and the second actuator includes a hydraulic actuator. 22. The variable area nozzle of claim 14, wherein when the first flap door and the second flap door are deployed at the at least one partially open position, the exhaust gases are at choked flow. 23. A rotor/wing comprising: a rotor having first and second rotor blades that extend from a middle section of the rotor toward first and second end sections of the rotor, respectively, the first and second rotor blades defining first and second ducts that extend from the middle section toward the first and second end sections, respectively, the first and second rotor blades each having a leading edge and a trailing edge; and a variable area nozzle including: a fixed duct section disposed in each of the first and second rotor blades at the trailing edges of the first and second end sections, each of the fixed duct sections having an inlet and an outlet that is oriented substantially perpendicular to the inlet; and a controllable nozzle member disposed adjacent the outlet of a corresponding fixed duct section, the controllable nozzle member having a first flap door and a second flap door, wherein the first flap door and the second flap door present a smoothly contoured inner surface to vary a nozzle throat height and a nozzle pressure of the variable area nozzle based on a deployment angle of the first flap door and the second flap door, wherein the first flap door and the second flap door are each independently rotated by actuators in a first direction and in a second direction opposite of the first direction, wherein the first flap door and the second flap door are rotated in opposite directions to maintainable positions including an open position, a closed position and at least one intermediate position to vary the nozzle throat height and the nozzle pressure, and wherein the first flap door and the second flap door are rotated in a same direction to vector a flow of an exhaust gas in the first direction and in the second direction relative to the outlet of the corresponding fixed duct section. 24. An aircraft capable of rotary wing flight and fixed wing flight, the aircraft comprising: a fuselage; a rotor/wing including: a hub disposed on an upper surface of the fuselage; and a rotor attached to the hub, the rotor being rotatable during rotary wing flight and the rotor being lockable in a fixed position during fixed wing flight, the rotor including: first and second rotor blades that extend from a middle section of the rotor toward first and second end sections of the rotor, respectively, the first and second rotor blades defining first and second ducts that extend from the middle section toward the first and second end sections, respectively, the first and second rotor blades each having a leading edge and a trailing edge; a variable area nozzle including: a fixed duct section disposed in each of the first and second rotor blades at the trailing edges of the first and second end sections, each of the fixed duct sections having an inlet and an outlet that is oriented substantially perpendicular to the inlet; and a controllable nozzle member disposed adjacent the outlet of a corresponding fixed duct section, the controllable nozzle member having a first flap door and a second flap door, wherein the first flap door and the second flap door present a smoothly contoured inner surface to vary a nozzle throat height and a nozzle pressure of the variable area nozzle based on a deployment angle of the first flap door and the second flap door, wherein the first flap door and the second flap door are each independently rotated by actuators in a first direction and in a second direction opposite of the first direction, wherein the first flap door and the second flap door are rotated in opposite directions to maintainable positions including an open position, a closed position and at least one intermediate position to vary the nozzle throat height and the nozzle pressure, and wherein the first flap door and the second flap door are rotated in a same direction to vector a flow of an exhaust gas in the first direction and in the second direction relative to the outlet of the corresponding fixed duct section; and a canard disposed on the fuselage forward of the rotor/wing, the canard being configured to generate lift as the aircraft transitions from rotary wing flight to fixed wing flight.