Aircraft visual collision and avoidance device

Claim 2

a "see and be seen" device for use on aircraft capable of receiving light from at least a one direction and for redirecting it in multiple directions, comprising: (a) a reflective means; (b) a refracting means disposed adjacent to said reflective means for directing light toward said reflective means; whereby the reflected light causes said aircraft to be visually identified and located by any other aircraft pilots in the vicinity.

Claim 3

The "see and be seen" device of claim 1, wherein said reflective means is comprised of a plurality of circular concave elements for serving as a lens means, for intensifying light and for redirecting said intensified light outward in many directions.

Claim 4

The "see and be seen" device of claim 1, wherein said refracting means comprises an array of pyramid shaped refracting elements disposed so as to be capable of receiving and refracting light through an entire 360° horizontal plane and at least a 180° vertical plane and redirecting said light towards said at least one of said circular, concave lens means.

Claim 5

A "see and be seen" device capable of being disposed on various portions of an aircraft, capable of receiving light from at least a one direction and for redirecting it in many directions, comprising: (a) a reflecting means, having formed therein, an array of concave circular indentations for serving as a lens means for intensifying and directing said intensified light, outward in many directions; (b) a refracting means comprising an array of pyramid shaped elements disposed adjacent to and between said concave circular indentations for receiving light from at least one direction and for refracting and redirecting light toward said concave circular indentations; whereby, the reflected light causes said aircraft to be visually identified and located by any other aircraft pilots in the vicinity.

Claim 6

A "see and be seen" device capable of being disposed on various portions of an aircraft, capable of receiving light from at least a one direction and for redirecting it in many directions, comprising: (a) a reflecting means, having formed therein, an array of concave circular indentations for serving as a lens means for intensifying and directing said intensified light, outward in many directions; (b) a refracting means comprising an array of pyramid shaped elements disposed adjacent to and between said concave circular indentations for receiving light from at least one direction and for refracting and redirecting light toward said concave circular indentations; whereby, the reflected light causes said aircraft to be visually identified and located by any other aircraft pilots in the vicinity.

Claim 7

The "see and be seen" device of claim 4, wherein said concave circular elements are 1" in diameter and equally spaced one from the other in a uniform repeating pattern of four wide and five down.

Claim 8

The "see and be seen" device of claim 4, wherein said pyramid shaped refracting means are disposed in said uniform pattern so as to be adjacent to four of said circular indentations.

Claim 9

The "see and be seen" device of claim 4, wherein the base and height of each of said pyramid shaped refracting means is 3/8 of an inch.

Claim 10

The "see and be seen" device of claim 4, wherein said pyramid shaped refracting means is formed of a clear plastic.

Claim 11

The "see and be seen" device of claim 4 wherein each of said pyramid shaped refracting means is rotated about its principle axis so as to have a different principle axis angular relationship than any other refracting means, said angular displacement being a multiple of 3.75 degrees.

Claim 12

The "see and be seen" device of claim 4, wherein said device is formed from mirror coated plastic.

Claim 13

The "see and be seen" device of claim 4, wherein said "see and be seen" device can be affixed to strategic portions of said aircraft, such as; leading edge of wing, fuselage top, fuselage bottom, tail and other areas for optimum visual observation, without affecting the flying characteristics of the aircraft.