Extendable/retractable airfoil assembly for fixed wing aircraft

• US 6,241,195 B1
• Filed: 09/22/1999
• Issued: 06/05/2001
• Est. Priority Date: 04/10/1997
• Status: Expired due to Term

• Current Assignee: John R. Lee
• Original Assignee: Fred A. Wagner III
• Inventors: Wagner, Fred A. III
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US09/381,743
• Time in Patent Office: 622 Days
• Field of Search: 244/198, 244/218, 244/46, 244/49, 244/139, 114/104-107
• US Class Current: 244/218
• CPC Class Codes: B64C 3/54 Varying in area
• CPC Class Codes: Y02T 50/10 Drag reduction

Abstract

A retractable airfoil assembly (20) augments the wing surface area (28) of an aircraft (22) enabling it to fly without stalling at reduced speeds during takeoff and landing. The airfoil assembly includes flexible sails (42, 44) and a furling mast (24) for extending and retracting the sails. The furling mast includes a furling drum mounted for clockwise and counterclockwise rotation on a static tube (50). The flexible sail assembly also includes guide tracks (80) located along a leading edge (101) or tailing edge (40) of the wings. The tracks guide the flexible sails during extension and retraction. A drive cable (26) extends and retracts the sails (42, 44) along the guide tracks and maintains tension in the sails while they are extended.

Claims

1. A retractable airfoil assembly for selectively increasing the lift surface area of an aircraft of the type including a fixed wind structure comprising:

a furling drum mounted on the aircraft for rotation about a longitudinal axis;

a guide track disposed along the fixed wing structure;

first and second flexible sails movable coupled to the guide track and wrapped one over the other in overlapping relation around the furling drum;

sail drive apparatus attached to the sails for moving the sails along the guide tracks,

the sail drive apparatus comprising a rotatable cable drum and a drive cable wound about the retractable cable drum, the drive cable including a first end portion and a second end portion attached to the first sail and the second sail, respectively; and

rotary drive apparatus coupled to the furling drum for rotating it clockwise and counterclockwise.

2. A retractable airfoil assembly as set forth in claim 1, characterized in that each flexible sail when unfurled forms a triangular airfoil extension of the wing structure, each sail including a side portion attached to the furling drum and an end portion coupled to the drive apparatus.

3. A retractable airfoil assembly as set forth in claim 1, characterized in that:

a static tube is mounted on the aircraft and the furling drum is mounted for rotation on the static tube.

4. A retractable airfoil assembly as set forth in claim 1, characterized in that the drive apparatus is a reversible D.C. electrical motor.

5. A retractable airfoil assembly as set forth in claim 1, characterized in that the drive apparatus is a manually operated hand crank.

6. A retractable airfoil assembly as set forth in claim 1, characterized in that the drive apparatus is coupled to each sail and to the furling drum for moving each sail along the guide tract while simultaneously rotating the furling drum as the sails are furled and unfurled in a spiral pattern around the drum.

7. A retractable airfoil assembly as set forth in claim 1, characterized in that the guide track is disposed along a leading edge of the fixed wing structure.

8. A retractable airfoil assembly as set forth in claim 1, characterized in that the guide track includes a main guide track disposed along a trailing edge of the fixed wing structure.

9. A retractable airfoil assembly as set forth in claim 8, characterized in that:

an aileron track is disposed along the trailing edge of the fixed wing structure; and

,

a flexible guide track is disposed intermediate the aileron track and the main guide track.

10. A retractable airfoil assembly as set forth in claim 1, characterized in that:

the furling drum and the cable drum are mechanically linked together for concurrent rotation.

11. A retractable airfoil assembly as set forth in claim 1, including a static boom mounted on the aircraft, the furling drum being mounted for rotation on the static boom.