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US3865071A Expired / Lapsed US ⏱️ 0.0 years remaining

Aircraft take off indicator systems

Assignee: Israel Aircraft Industries Ltd
•
Filing: 1973-08-23
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Granted: 1975-02-11
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Expires: 1993-08-23
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Abstract

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.

Inventors

  • 👤 Jehuda Manor

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 15:07
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/0083; Y; Y10; Y10S; Y10S116/00; Y10S116/43

Claims Analysis

Total Claims: 6
Claim 1
Independent 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 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.

References Cited (Backward Citations)

US3048329A Cited
US3128445A Cited
US3182498A Cited
US3117312A Cited
US3111577A Cited
US3381656A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-02-10 1978-08-12 1979-02-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-02-10 1982-08-12 1983-02-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-02-10 1986-08-12 1987-02-11 $7700.00 Window Closed / Lapsed

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