Primary flight display system having a vertical linear altimeter

Claim 2

An electronic vertical linear scale aircraft altimeter display device comprising: a frame having a top side, a bottom side, a right side and a left side; said top side and said bottom side disposed in a parallel configuration; said right side and said left side disposed in a parallel configuration and separating said top side and said bottom side; a fixed horizontal index reference bar, disposed parallel with said top side and said bottom side, for providing a fixed reference line; a first display area, disposed adjacent to said fixed horizontal index reference bar, for providing a plurality of least significant digits, of a multi-digit numeral, said plurality of least significant digits arranged in a predetermined fashion in a first moving linear array; a second display area, disposed adjacent said first display area, for providing a plurality of reference marks arranged in a second moving linear array; and, a third display area, disposed adjacent said first display area, for providing at least a single more significant digit, of said multi-digit numeral, which is next more significant than said least significant digits.

Claim 3

A device of claim 1 wherein said first moving linear array of said plurality of least significant digits is organized in ten groups of, equally spaced apart, three digit numerals, with the two least significant digits, in each group, being zeros and the most significant digit increasing in numerical order from zero to nine.

Claim 4

A device of claim 2 wherein said plurality of reference marks are horizontal linear marks, spaced apart at a predetermined equal distance.

Claim 5

A device of claim 3 wherein said third display area is disposed adjacent to said first display area and at a point horizontal with said fixed horizontal index reference bar.

Claim 6

A device of claim 1 wherein said second display area further providing a ground reference bar, extending from said bottom side toward said top side and further disposed over said plurality of reference marks, so that, said reference marks are occluded by said ground reference bar.

Claim 7

A device of claim 5 wherein said second display area further providing a decision height reference bar positioned above said ground reference bar for providing decision height information.

Claim 8

A device of claim 6 wherein more significant digit of said third display area, is a digit which scrolls vertically within said third display area.

Claim 9

Apparatus as defined in claim 1 wherein said reference marks are all non-numbered.

Claim 10

A primary flight display system comprising: means for sensing altitude above sea level and generating an altitude above sea level signal; means for sensing the altitude above the ground and generating an altitude above the ground signal; a display means having a frame having a top side, a bottom side, a right side and a left side; said top side and said bottom side disposed in a parallel configuration; said right side and said left side disposed in a parallel configuration and separating said top side and said bottom side; a fixed horizontal index reference bar, disposed parallel with said top side and said bottom side, for providing a fixed reference line; a first display area, disposed adjacent to said fixed horizontal index reference bar, for providing a plurality of least significant digits, of a multi-digit numeral, said plurality of least significant digits arranged in a predetermined fashion in a first moving linear array; a second display area, disposed adjacent said first display area, for providing a plurality of reference marks arranged in a second moving linear array; a third display area, disposed adjacent said first display area, for providing at least a single more significant digit, of said multi-digit numeral, which is next more significant than said least significant digits; and, means for manipulating said first display area, said second display area, and said third display area in response to said altitude above sea level signal.

Claim 11

A primary flight display system comprising: means for sensing altitude above sea level and generating an altitude above sea level signal; means for sensing the altitude above the ground and generating an altitude above the ground signal; a display means having a frame having a top side, a bottom side, a right side and a left side; said top side and said bottom side disposed in a parallel configuration; said right side and said left side disposed in a parallel configuration and separating said top side and said bottom side; a fixed horizontal index reference bar, disposed parallel with said top side and said bottom side, for providing a fixed reference line; a first display area, disposed adjacent to said fixed horizontal index reference bar, for providing a plurality of least significant digits, of a multi-digit numeral, said plurality of least significant digits arranged in a predetermined fashion in a first moving linear array; a second display area, disposed adjacent said first display area, for providing a plurality of reference marks arranged in a second moving linear array; a third display area, disposed adjacent said first display area, for providing at least a single more significant digit, of said multi-digit numeral, which is next more significant than said least significant digits; and, means for manipulating said first display area, said second display area, and said third display area in response to said altitude above sea level signal.

Claim 12

A system of claim 9 wherein said means for sensing altitude above sea level is a barometric altimeter.

Claim 13

A system of claim 10 wherein said means for sensing altitude above the ground comprises a radio altimeter.

Claim 14

A system of claim 11 wherein said display means further comprises a liquid crystal display.

Claim 15

A system of claim 11 wherein said display means further comprises a cathode ray tube.

Claim 16

A system of claim 13 wherein said means for manipulating further comprises a microprocessor.

Claim 17

A system of claim 14 wherein said second display area further providing a ground reference bar, extending from said bottom side toward said top side and further disposed over said plurality of reference marks, so that, said reference marks are occluded by said ground reference bar.

Claim 18

A system of claim 15 wherein said second display area further providing a decision height reference bar positioned above said ground reference bar for providing decision height information.

Claim 19

A system of claim 16 wherein said third display area is disposed adjacent to said first display area and at a point horizontal with said fixed horizontal index reference bar.

Claim 20

A system of claim 17 wherein said plurality of reference marks are horizontal linear marks, spaced apart at a predetermined equal distance.

Claim 21

A primary flight display system comprising: a barometric altimeter; a radio altimeter; a liquid crystal display device having a frame having a top side, a bottom side, a right side and a left side; said top side and said bottom side disposed in a parallel configuration; said right side and said left side disposed in a parallel configuration and separating said top side and said bottom side; a fixed horizontal index reference bar, disposed parallel with said top side and said bottom side, for providing a fixed reference point; a first display area, disposed adjacent to said fixed horizontal index reference bar, for providing a plurality of least significant digits, of a multi-digit numeral, said plurality of least significant digits arranged in a predetermined fashion in a first moving linear array; a second display area, disposed adjacent said first display area, for providing a plurality of reference marks arranged in a second moving linear array; a third display area, disposed adjacent said first display area, for providing at least a single more significant digit, of said multi-digit numeral, which is next more significant than said least significant digits; and, a microprocessor, coupled with said radio altimeter, said barometric altimeter and said liquid crystal display, for manipulating said first display area, said second display area, and said third display area of said liquid crystal display in response to said altitude above sea level signal.

Claim 22

A primary flight display system comprising: a barometric altimeter; a radio altimeter; a liquid crystal display device having a frame having a top side, a bottom side, a right side and a left side; said top side and said bottom side disposed in a parallel configuration; said right side and said left side disposed in a parallel configuration and separating said top side and said bottom side; a fixed horizontal index reference bar, disposed parallel with said top side and said bottom side, for providing a fixed reference point; a first display area, disposed adjacent to said fixed horizontal index reference bar, for providing a plurality of least significant digits, of a multi-digit numeral, said plurality of least significant digits arranged in a predetermined fashion in a first moving linear array; a second display area, disposed adjacent said first display area, for providing a plurality of reference marks arranged in a second moving linear array; a third display area, disposed adjacent said first display area, for providing at least a single more significant digit, of said multi-digit numeral, which is next more significant than said least significant digits; and, a microprocessor, coupled with said radio altimeter, said barometric altimeter and said liquid crystal display, for manipulating said first display area, said second display area, and said third display area of said liquid crystal display in response to said altitude above sea level signal.

Claim 23

A device of claim 19 wherein said second display area further providing a ground reference bar, extending from said bottom side toward said top side and further disposed over said plurality of reference marks, so that, said reference marks are occluded by said ground reference bar.

Claim 24

A device of claim 20 wherein said second display area further providing a decision height reference bar positioned above said ground reference bar for providing decision height information.

Claim 25

A display of altitude data formulated for use by an aircraft pilot in which a single, complete altitude figure is presented along with sliding scales of fine altitude figures, and coarse altitude marks, said display generated by: constructing an image including coarse altitude marks, all non-numbered, vertically spaced apart and referenced to a central position on a selected part of a video screen; constructing an image including fine altitude figures spaced apart and referenced to a central position on a selected part of a video screen along side said part used for said altitude marks; and, constructing an image including an exact altitude figure only at said central position on said video screen.

Claim 26

A display of altitude data formulated for use by an aircraft pilot in which a single, complete altitude figure is presented along with sliding scales of fine altitude figures, and coarse altitude marks, said display generated by: constructing an image including coarse altitude marks, all non-numbered, vertically spaced apart and referenced to a central position on a selected part of a video screen; constructing an image including fine altitude figures spaced apart and referenced to a central position on a selected part of a video screen along side said part used for said altitude marks; and, constructing an image including an exact altitude figure only at said central position on said video screen.

Claim 27

An improved primary flight display of the type having a vertical linear altimeter therein, the improvement comprising: a non-numbered coarse altitude image area, for displaying a series of ruled altitude markings which are capable of vertical translational motion; a numbered fine scale image area, juxtaposed with said non-numbered coarse image area, said fine scale image area for displaying numerals in vertical translational movement; and, a current altitude figure disposed at a fixed central index and further disposed over said coarse altitude image area.

Claim 28

An improved primary flight display of the type having a vertical linear altimeter therein, the improvement comprising: a non-numbered coarse altitude image area, for displaying a series of ruled altitude markings which are capable of vertical translational motion; a numbered fine scale image area, juxtaposed with said non-numbered coarse image area, said fine scale image area for displaying numerals in vertical translational movement; and, a current altitude figure disposed at a fixed central index and further disposed over said coarse altitude image area.