초록

An aircraft provides hovercraft power via fabric fans that produce lift for supporting the craft above an underlying support surface. Fabric fans are specially configured for maximum efficiency. In one embodiment, a helicopter utilizes the fan as part of a tail rotor assembly.

대표청구항 ▼

1. An aircraft, comprising: a) an air frame;b) a centrifugal fan that produces a cushion of air that elevates the air frame above an underlying support surface;c) the fan including a hub and multiple fabric stirrups;d) the stirrups including curved flexible portions forming a shroud; ande) wherein c

1. An aircraft, comprising: a) an air frame;b) a centrifugal fan that produces a cushion of air that elevates the air frame above an underlying support surface;c) the fan including a hub and multiple fabric stirrups;d) the stirrups including curved flexible portions forming a shroud; ande) wherein centrifugal forces stress the stirrups to maintain a desired stirrup geometry during rotation. 2. The aircraft of claim 1 wherein the aircraft is an unmanned aerial vehicle. 3. The aircraft of claim 1 wherein the aircraft has a cockpit for enabling it to be manned. 4. An aircraft, comprising: a) an air frame;b) a centrifugal fan that produces a cushion of air that elevates the air frame above an underlying support surface;c) the fan including a structural hub and multiple fabric stirrups mounted to the hub;d) the fabric stirrups including curved flexible portions forming a shroud; ande) wherein centrifugal forces stress the fabric stirrups to maintain a desired stirrup geometry during rotation. 5. The aircraft of claim 4 wherein the aircraft is an unmanned aerial vehicle. 6. The aircraft of claim 4 wherein the aircraft has a cockpit for enabling it to be manned. 7. The aircraft of claim 4 wherein the structural hub includes a ring. 8. The aircraft of claim 4 wherein the structural hub includes a plurality of radially extending spokes. 9. The aircraft of claim 7 wherein each stirrup is attached in part to the ring. 10. The aircraft of claim 8 wherein the structural hub includes a cylindrically shaped member. 11. The aircraft of claim 10 wherein the radially extending spokes connect to the cylindrically shaped member. 12. The aircraft of claim 4 wherein each stirrup carries an airfoil blade. 13. The aircraft of claim 4 wherein the structural hub includes a generally conically shaped portion. 14. The aircraft of claim 4 wherein the structural hub includes a tapered portion. 15. The aircraft of claim 14 wherein the structural hub includes a cylindrically shaped member and the tapered portion is attached to the cylindrically shaped member. 16. The aircraft of claim 7 wherein the structural hub includes a cylindrically shaped member and a tapered portion is attached to the cylindrically shaped member, and wherein each stirrup is connected to the ring and the tapered portion. 17. The aircraft of claim 4 wherein each stirrup has upper and lower flaps that are generally perpendicular to an axis of rotation of the hub. 18. The aircraft of claim 7 wherein each stirrup has upper and lower flaps that are generally perpendicular to an axis of rotation of the hub. 19. The aircraft of claim 13 wherein each stirrup has upper and lower flaps that are generally perpendicular to an axis of rotation of the hub. 20. The aircraft of claim 4 wherein each stirrup has a flange that attaches to both of the flaps forming a channel that is bounded by flanges of a pair of adjacent stirrups and by the flaps of a stirrup. 21. The aircraft of claim 4 wherein an air flow channel is positioned in between a pair of adjacent stirrups. 22. The aircraft of claim 4 wherein air flow through the fan is through an inlet and out via channels of the stirrups. 23. The aircraft of claim 9 wherein air flow through the fan is through an inlet surrounded by the ring and out via channels of the stirrups.