Compressed circle flight display

Claim 2

An aircraft altimeter for indicating an altitude the altimeter comprising: an arcuate top portion having a first curvature, a first end and second end; an arcuate bottom portion having the first curvature, a first end, and a second end, and being opposedly spaced apart from the top portion; a first lateral edge having a second curvature less than the first curvature and extending from the first end of the top portion to the first end of the bottom portion; a second lateral edge having a third curvature less than the first curvature, and extending from the second end of the top portion to the second end of the bottom portion forming a display area therein; altitude indicia disposed at equal linear distances proximate a perimeter of the display area; an indicator indicating the altitude indicia based upon the altitude and traversing the altitude indicia at a constant rate for a given altitude rate of change; and wherein the perimeter is substantially equal to a circumference of a circle having the first curvature.

Claim 3

The aircraft altimeter of claim 1 wherein the first and second lateral edges are straight.

Claim 4

The aircraft altimeter of claim 1 wherein the indicator has a triangular shape with an indicating corner indicating the altitude indicia.

Claim 5

The aircraft altimeter of claim 3 wherein the indicator moves about the perimeter and rotates about the indicating corner based upon the altitude.

Claim 6

The aircraft altimeter of claim 1 and further comprising a numerical rolling drum indicator displaying a numerical value based upon the altitude.

Claim 7

The aircraft altimeter of claim 5 wherein the rolling drum indicator comprises a hundredths digit, and tens digit, and wherein the hundredths digit is larger than the tens digit.

Claim 8

The aircraft altimeter of claim 1 and further comprising a vertical speed indicator disposed proximate the perimeter of the display area and indicating vertical speed based upon a rate of change of the altitude.

Claim 9

An aircraft airspeed indicator for indicating an airspeed, the airspeed indicator comprising: a arcuate top portion having a first curvature, a first end, and a second end; an arcuate bottom portion having the first curvature, a first end, and a second end, and being opposedly spaced apart from the top portion; a first lateral edge having a second curvature less than the first curvature, and extending from the first end of the top portion to the first end of the bottom portion; a second lateral edge having a third curvature less than the first curvature, and extending from the second end of the top portion to the second end of the bottom portion forming a display area therein; airspeed indicia disposed at equal linear distances proximate a perimeter of the display area; an indicator indicating the airspeed indicia based upon the airspeed and traversing the airspeed indicia at a constant rate for a given airspeed rate of change; and wherein the perimeter is substantially equal to a circumference of a circle having the first curvature.

Claim 10

An aircraft airspeed indicator for indicating an airspeed, the airspeed indicator comprising: a arcuate top portion having a first curvature, a first end, and a second end; an arcuate bottom portion having the first curvature, a first end, and a second end, and being opposedly spaced apart from the top portion; a first lateral edge having a second curvature less than the first curvature, and extending from the first end of the top portion to the first end of the bottom portion; a second lateral edge having a third curvature less than the first curvature, and extending from the second end of the top portion to the second end of the bottom portion forming a display area therein; airspeed indicia disposed at equal linear distances proximate a perimeter of the display area; an indicator indicating the airspeed indicia based upon the airspeed and traversing the airspeed indicia at a constant rate for a given airspeed rate of change; and wherein the perimeter is substantially equal to a circumference of a circle having the first curvature.

Claim 11

The aircraft airspeed indicator of claim 8 wherein the first and second edges are straight.

Claim 12

The aircraft airspeed indicator of claim 8 wherein the indicator has a triangular shape with an indicating corner indicating the airspeed indicia.

Claim 13

The aircraft airspeed indicator of claim 10 wherein the indicator moves about the perimeter and rotates about the indicating corner based upon the airspeed.

Claim 14

The aircraft airspeed indicator of claim 8 and further comprising a numerical rolling drum indicator displaying a numerical value based upon the airspeed.

Claim 15

A primary flight display comprising: an airspeed indicator; an attitude indicator; a heading indicator; and an altimeter comprising: an arcuate top portion having a first curvature, a first end and a second end; an arcuate bottom portion having the first curvature, a first end and a second end, and being opposedly spaced apart from the top portion; a first straight edge connecting the first end of the top portion to the first end of the bottom portion; a second straight edge connecting the second end of the top portion to the second end of the bottom portion forming an altimeter display area between the top and bottom portions and between the first and second edges, wherein a perimeter of the altimeter display area is equal to a circumference of a circle having the first curvature further wherein altitude indicia are equally linearly spaced proximate the perimeter of the altimeter wherein an indicator traverses the altitude indicia at a constant rate for a given altitude rate of change.

Claim 16

A primary flight display comprising: an airspeed indicator; an attitude indicator; a heading indicator; and an altimeter comprising: an arcuate top portion having a first curvature, a first end and a second end; an arcuate bottom portion having the first curvature, a first end and a second end, and being opposedly spaced apart from the top portion; a first straight edge connecting the first end of the top portion to the first end of the bottom portion; a second straight edge connecting the second end of the top portion to the second end of the bottom portion forming an altimeter display area between the top and bottom portions and between the first and second edges, wherein a perimeter of the altimeter display area is equal to a circumference of a circle having the first curvature further wherein altitude indicia are equally linearly spaced proximate the perimeter of the altimeter wherein an indicator traverses the altitude indicia at a constant rate for a given altitude rate of change.

Claim 17

The primary flight display of claim 13 wherein the airspeed indicator comprises: an arcuate top portion having a second curvature, a first end and a second end; an arcuate bottom portion having the second curvature, a first end and a second end, and being opposedly spaced apart from the top portion; a first straight edge extending from the first end of the top portion to the first end of the bottom portion; a second straight edge extending from the second end of the top portion to the second end of the bottom portion forming an airspeed indicator display area between the top and bottom portions and between the first and second edges, wherein a perimeter of the airspeed indicator display area is equal to a circumference of a circle having the second curvature.

Claim 18

The primary flight display of claim 14 wherein the airspeed indicator and altimeter are disposed on opposite sides of the attitude indicator.

Claim 19

The primary flight display of claim 14 and further comprising a numerical rolling drum display disposed in a central portion of the airspeed indicator display area for numerically indicating airspeed based upon the airspeed.

Claim 20

The primary flight display of claim 13 and further comprising a vertical speed indicator disposed proximate the perimeter of the altimeter displaying a vertical speed based on a rate of change of the altitude.

Claim 21

The primary flight display of claim 13 and further comprising a numerical rolling drum display disposed in a central portion of the display area indicating the altitude, numerically, based upon the altitude.