Flight indicator for a helicopter

Details Flight indicator for a helicopter Flight indicator for a helicopter

1997-06-06

1999-06-22

Oen, William

Measuring and testing

Navigation

Take-off and landing monitors

G01C 2100

Patent

active

059152737

ABSTRACT:
A flight indicator for an aircraft, intended to give the power margin available on at least one engine of the aircraft as a function of the flight conditions. The indicator includes sensors (2, 3, 4) capable of delivering data relating to various monitored parameters of the engine, device (5) for processing the data coming from the sensors (2, 3, 4), and display device (6) showing, on a display screen (7) the processed data relating to that parameter among the monitored engine parameters, whose current value is closest to the limiting value for such parameter, each limiting value being established taking the ambient pressure (P0) and ambient temperature (T0) into account, in real time.

REFERENCES:
patent: 4763285 (1988-08-01), Moore et al.
patent: 4780838 (1988-10-01), Adelson
patent: 4787053 (1988-11-01), Moore
patent: 5257190 (1993-10-01), Crane

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