Robert Wade Everett

Author:

Robert Andrew Everett

ISBN #:

0080410405

US Patent:

D469186, Jan 21, 2003

Filed:

Feb 27, 2001

Appl. No.:

29/137638

Inventors:

Robert A. Everett - Tulsa OK 74108

International Classification:

2503

US Classification:

D25 1

US Patent:

41576322, Jun 12, 1979

Filed:

Jun 10, 1977

Appl. No.:

5/805517

Inventors:

Robert A. Everett - Tulsa OK

International Classification:

A63H 2700

US Classification:

46 74D

Abstract:

An aerodynamic toy having a series of small extended airfoils contiguous to one another, forming a large unitary aerodynamic body, whose lift surfaces has disposed a number of small depressions. Most of the body's weight is distributed in the small extended airfoils, with placement of blind holes for the addition of extra weight. The lower surface is substantially flat at the periphery and then becomes concaved shaped. The concaved surface contains a hollow tube that holds fluid and has a dispenser at the lower end for dispersing of the fluid.

US Patent:

49759833, Dec 11, 1990

Filed:

Jun 5, 1989

Appl. No.:

7/361641

Inventors:

Robert A. Everett - Tulsa OK

International Classification:

A41D 2716

US Classification:

2 60

Abstract:

An improved shirt collar stay system that has a slot-like channel that surrounds and grips the vertical and horizontal edges of a shirt collar as a stay and as a fringe. The channel design has an upper vertical section and a lower section connected by linkage that can fold via pivot means to engage both vertical and lower edges of said collar. The said channels's length has a leg member with a curve containing protrusions on the contact portion of its surface of the leg member and also contains spring-like means. Both features are for gripping, when engaged with material or said collar's edges. The top portion of the upper vertical section of the channel has flexibility that engages and grips the top vertical portion of the collar and will follow a curved contour of such a collar design. The upper vertical section of the channel has on its outside surface an arm extension member with holes along its length as decorations and end holes become part of a locking means, when the lower section of the said channel is engaged with the horizontal collar's edge and locked onto studs that are part of the lower section of said channel's outside surface, so that when the end holes match up with a suitable lock-stud they can be snapped together as a positive engagement, and thus a shirt collar of a new appearance is presented.

US Patent:

D4492501, Oct 16, 2001

Filed:

Nov 4, 1999

Appl. No.:

D/113344

Inventors:

Robert A. Everett - Tulsa OK

International Classification:

0207

US Classification:

D11215

US Patent:

44524102, Jun 5, 1984

Filed:

Dec 18, 1981

Appl. No.:

6/332319

Inventors:

Robert A. Everett - Tulsa OK

International Classification:

B64C 2700
B64C 3906

US Classification:

244 122

Abstract:

An aircraft containing aerodynamic and gyroscopic stability that has a high angle of take-off and landing capabilities, with high speed horizontal powered flight, but is also able to sustain power-off flight with auto-rotation of its multiple extending airfoils. The fuselage has the shape of an inverted saucer with aerodynamic configuration and has an open circular track at its periphery; and riding in this track is a rotary frame and extended airfoil assembly that isin-line with the fuselage. Each extending airfoil contains solid weighted bodies at their tips and this rotary frame and extended airfoil assembly is rotated on the track by an internal power unit. The extending airfoils taper toward their tips and these tips have a knife sharp edge for penetrating the air resistance. Special flaps on the airfoils function for creating additional lift in the downwind quadrant, but in the power-off flight mode, when the rotary frame and extending airfoil assembly is disengaged; the dual purpose flap and trap flap combine to function to trap the slip-stream causing the rotary frame and extended airfoil assembly to rotate. Mounted to the surface of the fuselage are forward thrust engines with rearward extending booms on which are located the tail assembly with flight control surfaces.