Abstract The present invention relates to aircraft take-off indicator systems, for displaying air speed and distance covered during take-off run, and the point-of-no-return for take-off abort. The aircraft indicator system comprises a first measuring device measuring aircraft air speed and having a first scale displaying said measurement, and a second measuring device measuring distance covered during take-off run and having a second scale displaying said measurement. The second scale is parallel to and laterally of the first scale; and a pre-settable marker is disposed to bridge both of said scales and pre-settable so as to be aligned with a predetermined point on each, thereby providing a continuous indication of whether the minimum airspeed for a safe take-off will be reached before the point-of-no-return.
An aircraft indicator system, comprising: a first measuring device measuring aircraft air speed and having a first scale displaying said measurement, a second measuring device measuring distance covered during take-off run and having a second scale displaying said measurement; said second scale being parallel to and laterally of said first scale; and a pre-settable marker disposed to bridge both of said scales and presettable so as to be aligned with a predetermined point on the second scale corresponding to the point-of-no-return of the aircraft upon take-off, and with a predetermined point on the first scale corresponding to the indicated air speed at that point to assure a safe take-off, whereby visual observation during take-off of the measurements displayed by the two scales with reference to said presettable marker provides a continuous indication of whether the minimum air speed for a safe take-off will be reached before the point-of-no-return.
Claim 2
Dependent Claim
148 words
An aircraft indicator system, comprising: a first measuring device measuring aircraft air speed and having a first scale displaying said measurement, a second measuring device measuring distance covered during take-off run and having a second scale displaying said measurement; said second scale being parallel to and laterally of said first scale; and a pre-settable marker disposed to bridge both of said scales and presettable so as to be aligned with a predetermined point on the second scale corresponding to the point-of-no-return of the aircraft upon take-off, and with a predetermined point on the first scale corresponding to the indicated air speed at that point to assure a safe take-off, whereby visual observation during take-off of the measurements displayed by the two scales with reference to said presettable marker provides a continuous indication of whether the minimum air speed for a safe take-off will be reached before the point-of-no-return.
Claim 3
Dependent Claim
40 words
A system of claim 1, wherein one of said scales is displaceable with respect to the other, such that a given value of air speed on said first scale can be placed opposite a given distance on said second scale.
Claim 4
Dependent Claim
20 words
A system according to claim 1 wherein said first and second scales are both vertical scales disposed in side-by-side relationship.
Claim 5
Dependent Claim
16 words
A system of claim 2, wherein said displaceable scale is that of said aircraft air speed.
Claim 6
Dependent Claim
17 words
A system of claim 1, wherein said marker is a bridging bar pre-settable by a rotary knob.