Roger Andrew Thompson

Address:

926 W Mierianne St, Houston, TX 77088

VIN:

1J4FA54157L178934

Make:

JEEP

Model:

WRANGLER

Year:

2007

US Patent:

6409357, Jun 25, 2002

Filed:

Jan 12, 2001

Appl. No.:

09/758281

Inventors:

Roger R. Thompson - Sea Bright NJ 07760
Robin A. Thompson - Sea Bright NJ 07760

International Classification:

A47B 1900

US Classification:

362 98, 362 99, 362155, 362156

Abstract:

A page of printed information content between front and back covers is automatically illuminated when the covers are folded away from one another by a source of illumination affixed to at least one of the covers adjacent an edge surface thereof, while the other of the covers includes a notch in opposite position to overlie the source when the covers are folded closed, thereby retaining the page substantially flatâwith electronic switch means serving to energize the illumination source only when the front and back covers are separated.

US Patent:

44298439, Feb 7, 1984

Filed:

Mar 24, 1982

Appl. No.:

6/361421

Inventors:

Roger A. Thompson - Houston TX

International Classification:

B64C 2306

US Classification:

244199

Abstract:

A device for enhancing the lift capability of an aircraft wing is characterized by at least one forwardly projecting finger member mounted on the leading edge of the wing. The finger generates counter-rotating vortices, each in contact with the other, trailing backwardly across the upper surface of the wing behind the fingers as the airflow moves upwardly and around the lateral edges of the finger. As the counter-rotating vortices trail backwardly over the upper surface of the wing, a blockage effect is created and the airflow patterns across the wing are modified to produce an increase in lift.

US Patent:

43232094, Apr 6, 1982

Filed:

Nov 13, 1978

Appl. No.:

5/960221

Inventors:

Roger A. Thompson - Houston TX

International Classification:

B64C 2306

US Classification:

244199

Abstract:

A device for enhancing the lift capability of an aircraft wing is characterized by at least one forwardly projecting finger member mounted on the leading edge of the wing. The finger generates counter-rotating vortices, each in contact with the other, trailing backwardly across substantially the entire upper surface of the wing behind the fingers as the airflow moves upwardly and around the lateral edges of the finger. As the counter-rotating vortices trail backwardly over the upper surface of the wing, a blockage effect is created and the airflow patterns across the wing are modified to produce an increase in lift.