Flight control indicator for aircraft

Details Flight control indicator for aircraft Flight control indicator for aircraft

1998-12-10

1999-11-16

Swarthout, Brent A.

Communications: electrical

Aircraft alarm or indicating systems

Nonairplane

73178H, 244 1711, 340863, 701 14, G08B 2100

Patent

active

059865806

ABSTRACT:
A flight control indicator for twin-engine aircraft, in particular a rotary-wing aircraft comprising two turboengines for driving at least one rotor, intended to provide the power margin available on the engines of the aircraft as a function of the flight conditions. Display means (6) presents a single dial (8) furnished with two needles (9.sub.1, 9.sub.2), each of them corresponding to a respective engine, and positioned in such a way that, when the engines are operating normally, the two needles are merged.

REFERENCES:
patent: 3287965 (1966-11-01), Brahm et al.
patent: 3616691 (1971-11-01), Brandau
patent: 4034605 (1977-07-01), Green
patent: 4179938 (1979-12-01), Schramm
patent: 4736331 (1988-04-01), Lappos et al.
patent: 5339244 (1994-08-01), Stiles, Jr. et al.
patent: 5886649 (1999-03-01), Francois

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