← Back to Patent Explorer
US3929279A Expired / Lapsed US ⏱️ 0.0 years remaining

Flight path calculator

Assignee: Individual
•
Filing: 1974-05-14
•
Granted: 1975-12-30
•
Expires: 1994-05-14
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A flight slope calculator having relatively movable distance and altitude scales arranged to facilitate the vertical navigation of aircraft and in particular to permit a pilot to ascertain the point at which he should start his descent during the approach to an airfield.

Inventors

  • 👤 Hugh P K Dibley

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 20:47
CPC Classifications
G; G06; G06G; G06G1/00; G06G1/0005; G06G1/0052

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 302 words
A flight path calculator calibrated to display the descent path for a selected type of aircraft, comprising: a first member having a distance scale increasing linearly in a predetermined direction and calibrated in units of distance; a second member having an altitude scale increasing in said predetermined direction and calibrated in units of altitude, said altitude scale consisting of three portions: (a) a first portion having a range from zero to a predetermined deceleration altitude and calibrated such that equal lengths of said first portion and said distance scale correspond to units of descent and the distance flown by said aircraft during said descent, respectively, at the indicated air speed for flight of said aircraft below said deceleration altitude; (b) a second portion in which the altitude indicia is maintained at said deceleration altitude and having a length relative to said distance scale corresponding to the distance said aircraft would travel while decelerating from the indicated air speed for flight of said aircraft above said deceleration altitude to said indicated air speed below said deceleration altitude, one end of said second portion being coincident with the said deceleration altitude indicium of said first portion; and (c) a third portion having a range from said deceleration altitude to a selected maximum altitude and calibrated such that equal lengths of said third portion and said distance scales correspond to units of descent and the distance flown during that descent, respectively, at said speed above said deceleration altitude, said deceleration altitude indicium of said third portion being coincident with the other end of said second portion; and means for constraining said first and second members to move relative to each other while maintaining said distance and altitude scales juxtaposed so that the markings on one can be read off against the markings on the other.
Claim 2
Dependent Claim 302 words
A flight path calculator calibrated to display the descent path for a selected type of aircraft, comprising: a first member having a distance scale increasing linearly in a predetermined direction and calibrated in units of distance; a second member having an altitude scale increasing in said predetermined direction and calibrated in units of altitude, said altitude scale consisting of three portions: (a) a first portion having a range from zero to a predetermined deceleration altitude and calibrated such that equal lengths of said first portion and said distance scale correspond to units of descent and the distance flown by said aircraft during said descent, respectively, at the indicated air speed for flight of said aircraft below said deceleration altitude; (b) a second portion in which the altitude indicia is maintained at said deceleration altitude and having a length relative to said distance scale corresponding to the distance said aircraft would travel while decelerating from the indicated air speed for flight of said aircraft above said deceleration altitude to said indicated air speed below said deceleration altitude, one end of said second portion being coincident with the said deceleration altitude indicium of said first portion; and (c) a third portion having a range from said deceleration altitude to a selected maximum altitude and calibrated such that equal lengths of said third portion and said distance scales correspond to units of descent and the distance flown during that descent, respectively, at said speed above said deceleration altitude, said deceleration altitude indicium of said third portion being coincident with the other end of said second portion; and means for constraining said first and second members to move relative to each other while maintaining said distance and altitude scales juxtaposed so that the markings on one can be read off against the markings on the other.
Claim 3
Dependent Claim 29 words
A calculator as defined in claim 1, in which both members are circular and the coupling means interconnects the said members coaxially for relative rotation about the common axis.

References Cited (Backward Citations)

US2506299A Cited
US3279695A Cited
US3255961A Cited
US3609299A Cited
US3693873A Cited
US3825180A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-12-29 1979-06-30 1979-12-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-12-29 1983-06-30 1983-12-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-12-29 1987-06-30 1987-12-30 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag