Aircraft takeoff velocity indicator system

Communications: electrical – Aircraft alarm or indicating systems – Takeoff indicator

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Details

340945, 340969, 701 15, 73178T, G08B 2100

Patent

active

061338575

ABSTRACT:
An aircraft instrument system that informs the pilot of whether, during the takeoff roll, the aircraft's acceleration rate is sufficient to ensure that V1 speed will be achieved at the expected time (and thus distance), and, if not, how far in distance the aircraft is lagging behind the required acceleration schedule.

REFERENCES:
patent: 2922982 (1960-01-01), Hoekstra
patent: 3025494 (1962-03-01), Andresen, Jr.
patent: 3128445 (1964-04-01), Hosford
patent: 3182498 (1965-05-01), Koletsky et al.
patent: 3863204 (1975-01-01), Hoekstra
patent: 4130015 (1978-12-01), Grover
patent: 4638437 (1987-01-01), Cleary et al.
patent: 4843554 (1989-06-01), Middleton et al.
patent: 4980833 (1990-12-01), Milligan et al.
patent: 5103224 (1992-04-01), Arad
patent: 5124700 (1992-06-01), Bonafe
patent: 5353022 (1994-10-01), Middleton et al.
patent: 5499025 (1996-03-01), Middleton et al.
J.H.H. Grover: "Towards safer take-offs" Flight International, p. 601-602, vol. 86, No. 2899, XP002054350, Oct. 1964.

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