Windscreen deviation correcting pilot display

Claim 2

A virtual image display for an aircraft having a windscreen characterized by a symmetrically oriented center line, the display comprising: a light transmissive optical combining element laterally positioned across the windscreen and attached thereto; first image generating means located within the cockpit of the aircraft for projecting a first virtual image of preselected symbols on the right side of the combining element, with respect to the centerline; second image generating means located within the cockpit of the aircraft for projecting a second virtual image of separate preselected symbols on the left side of the combining element, with respect to the centerline, the right and left virtual images being contiguous; a pilot's head being locatable in a space where the field of view of each eye through the combining element includes the superposition of an observed object appearing outside the windscreen and the virtual image appearing on the same side of the centerline as that eye thereby avoiding either of the pilot's eyes from seeing the virtual image appearing on an opposite side of the centerline.

Claim 3

The system set forth in claim 1 together with means connected to the first and second image generating means for providing a correction factor to the position of each projected symbol as a function of azimuth and elevation symbol position on the combining means, thereby compensating for parallax error of the superimposed object and ensuring alignment between the superimposed object and the symbols.

Claim 4

The system set forth in claim 2 wherein eye boxes are defined when the pilot's head is correctly positioned to perceive the field of view, and further wherein the horizontal dimension of each eye box, if overlap is used, is less than the least interocular dimension of the population of pilots to be served by the system.

Claim 5

The system set forth in claim 3 wherein the symbols include instrument panel displays projected on a lower portion of the combining element so that a virtual image thereof appears in an area of a cockpit normally occupied by an instrument panel thereby enabling removal of conventional instrument panel displays.

Claim 6

The system set forth in claim 1 wherein eye boxes are defined when the pilot's head is correctly positioned to perceive the field of view, and further wherein the overlap in the horizontal dimension of each eye box, if used, is less that the least interocular dimension of the population of pilots to be served by the system.

Claim 7

The system set forth in claim 2, wherein the combining element has a preselected curvature and serves as a reflecting lens for collimating rays of light impinging thereon from the first and second generating means.

Claim 8

The system set forth in claim 5, wherein the combining element has a preselected curvature and serves as a reflecting lens for collimating rays of light impinging thereon from the first and second generating means.

Claim 11

The method set forth in claim 8 together with the step of correcting the positions of the projected virtual images as a function of azimuth and elevation position on the combining means, thereby avoiding a parallax error of the superimposed object and ensuring preselected alignment between the superimposed object and the symbols.

Claim 12

The method set forth in claim 8 wherein eye boxes are defined when the pilot's head is correctly positioned to perceive the field of view, and further wherein the possible overlap horizontal dimension of each eye box is less than the least interocular dimension of the population of pilots to be served by the system.

Claim 13

The method set forth in claim 8 wherein the symbols include instrument panel displays projected on a lower portion of the combining element so that a virtual image thereof appears in an area of a cockpit normally occupied by an instrument panel thereby enabling removal of conventional instrument panel displays.

Claim 14

The method set forth in claim 9 wherein eye boxes are defined when the pilot's head is correctly positioned to perceive the field of view, and further wherein the possible overlap in the horizontal dimension of each eye box is less than the least interocular dimension of the population of pilots to be served by the system, and still further whererin the symbols include instrument panel displays projected on a lower portion of the combining element so that a virtual image thereof appears in an area of a cockpit normally occupied by an instrument panel thereby enabling removal of conventional instrument panel displays.

Claim 15

A virtual image display for an aircraft having a windscreen characterized by a symmetrically oriented centerline, the display comprising: a light transmissive optical combining element laterally positioned across the windscreen and attached thereto, the combining element has a preselected curvature and serves as a reflecting lens for collimating rays of light impinging thereon from first and second image generating means; the first image generating means being located within the cockpit of the aircraft for projecting a first virtual image of preselected symbols on the right side of the combining element, with respect to the centerline; the second image generating means being located within the cockpit of the aircraft for projecting a second virtual image of separate preselected symbols on the left side of the combining element, with respect to the centerline, the right and left virtual images being contiguous; a pilot's head being locatable in a space where the field of view of each eye through the combining element includes the superposition of an observed object appearing outside the windscreen and the virtual image appearing on the same side of the centerline as that eye thereby avoiding either of the pilot's eyes from seeing the virtual image appearing on an opposite side of the centerline.

Claim 16

A virtual image display for an aircraft having a windscreen characterized by a symmetrically oriented centerline, the display comprising: a light transmissive optical combining element laterally positioned across the windscreen and attached thereto, the combining element has a preselected curvature and serves as a reflecting lens for collimating rays of light impinging thereon from first and second image generating means; the first image generating means being located within the cockpit of the aircraft for projecting a first virtual image of preselected symbols on the right side of the combining element, with respect to the centerline; the second image generating means being located within the cockpit of the aircraft for projecting a second virtual image of separate preselected symbols on the left side of the combining element, with respect to the centerline, the right and left virtual images being contiguous; a pilot's head being locatable in a space where the field of view of each eye through the combining element includes the superposition of an observed object appearing outside the windscreen and the virtual image appearing on the same side of the centerline as that eye thereby avoiding either of the pilot's eyes from seeing the virtual image appearing on an opposite side of the centerline.