Method and apparatus for generating lift

• US 7,677,502 B2
• Filed: 09/29/2005
• Issued: 03/16/2010
• Est. Priority Date: 09/29/2005
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Droney, Christopher K., Cummings, Darold B., Lawson, Edward L.
• Primary Examiner(s): Dinh; Tien
• Assistant Examiner(s): Sanderson; Joseph W
• Application Number:
  US11/238,347
• Publication Number:
  US 20070069066A1
• Time in Patent Office: 1,629 Days
• Field of Search: None
• US Class Current: 244/207
• CPC Class Codes: B64C 2230/04 by actively generating fluid flow
• CPC Class Codes: B64C 9/18 by single flaps
• CPC Class Codes: B64C 9/38 Jet flaps
• CPC Class Codes: Y02T 50/10 Drag reduction
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

A method of generating lift for a vehicle including heating a flow of gas using a gas generator mounted on the vehicle that contributes no more than about ten percent of thrust used to propel the vehicle in a forward direction, and driving a lift fan using the heated gas flow to generate lift for the vehicle.

Claims

1. A method of generating lift for an aircraft, said method comprising:

heating a flow of gas using a gas generator mounted on the aircraft that contributes no more than about ten percent of thrust used to propel the aircraft in a forward direction;

driving a lift fan using the heated gas flow to generate lift for the aircraft; and

directing at least a portion of the heated gas exiting the lift fan over a wing control surface of the aircraft, including directing at least a portion of the heated gas over an internally blown flap (IBF) of the aircraft.

2. A method in accordance with claim 1 further comprising directing at least a portion of gas exiting the lift fan into an internal compartment of the vehicle.

3. A method in accordance with claim 1 wherein at least a portion of the heated gas flow exits the lift fan and mixes with air exiting the lift fan.

4. A method in accordance with claim 1 further comprising generating electrical power using at least a portion of the heated gas flow from the gas generator.

5. A method in accordance with claim 1 further comprising further heating the heated gas flow downstream from the gas generator.

6. An airframe comprising:

a body;

a wing coupled to the body;

a gas generator mounted on the body for heating a flow of gas, said gas generator contributing no more than about ten percent of thrust used to propel the body in a forward direction;

a lift fan mounted on the body for generating lift for the body, said lift fan being fluidically coupled with the gas generator for driving the lift fan from at least a portion of the heated gas flow; and

an internally blown flap mounted on the wing for affecting an aerodynamic property of at least a portion of the wing, said lift fan being positioned on the body to direct at least a portion of the heated gas exiting the lift fan over the internally blown flap.

7. An airframe in accordance with claim 6 further comprising a duct mounted on the body and positioned to receive the heated gas flow exiting the lift fan and divert the heated gas flow over a compartment opening of the airframe as an air curtain.

8. An airframe in accordance with claim 6 wherein at least a portion of the heated gas flow exits the lift fan and mixes with air exiting the lift fan.

9. An airframe in accordance with claim 6 wherein the lift fan comprises an axial fan.

10. An airframe in accordance with claim 6 wherein the lift fan comprises a centrifugal compressor.

11. An airframe in accordance with claim 6 further comprising a duct mounted on the body and positioned to receive gas exiting the lift fan and direct the received gas into an internal compartment of the body.

12. An airframe in accordance with claim 6 further comprising an augmenter operably connected between the gas generator and the lift fan for heating the heated gas flow downstream from the gas generator.

13. An airframe in accordance with claim 6 further comprising a diverter operably connected between the lift fan and the gas generator for directing at least a portion of the heated gas flow into the lift fan.

14. An airframe in accordance with claim 13 further comprising a power turbine mounted on the body for generating electrical power and being fluidically coupled with the gas generator, said diverter being operably connected between the gas generator and the power turbine for directing at least a portion of the heated gas flow from the gas generator into the power turbine.

15. An aircraft comprising:

a frame;

a wing coupled to the frame;

an engine mounted on the frame for propelling the aircraft in a forward direction;

a gas generator mounted on the frame for heating a flow of gas, said gas generator contributing no more than about ten percent of thrust used to propel the aircraft in the forward direction; and

a lift fan mounted on the frame for generating lift for the aircraft, said lift fan being fluidically coupled with the gas generator for driving the lift fan from at least a portion of the heated gas flow; and

an internally blown flap mounted on the wing for affecting an aerodynamic property of at least a portion of the wing, said lift fan being positioned on the body to direct at least a portion of the heated gas exiting the lift fan over the internally blown flap.

16. An aircraft in accordance with claim 15 further comprising a duct mounted on the body and positioned to receive the heated gas flow exiting the lift fan and divert the heated gas flow over a compartment opening of the aircraft as an air curtain.

17. An aircraft in accordance with claim 15 wherein at least a portion of the heated gas flow exits the lift fan and mixes with air exiting the lift fan.

18. An aircraft in accordance with claim 15 wherein the lift fan comprises an axial fan.

19. An aircraft in accordance with claim 15 wherein the lift fan comprises a centrifugal compressor.

20. An aircraft in accordance with claim 15 further comprising a duct mounted on the frame and positioned to receive gas exiting the lift fan and direct the received gas into an internal compartment of the vehicle.

21. An aircraft in accordance with claim 15 further comprising an augmenter operably connected between the gas generator and the lift fan for heating the heated gas flow downstream from the gas generator.

22. An aircraft in accordance with claim 15 further comprising a diverter operably connected between the lift fan and the gas generator for directing at least a portion of the heated gas flow into the lift fan.

23. An aircraft in accordance with claim 15 further comprising a power turbine mounted on the frame for generating electrical power, said diverter being operably connected between the gas generator and the power turbine for directing at least a portion of the heated gas flow from the gas generator into the power turbine.