Helicopter airspeed indicating system

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Details

364431, 244 1713, 73509, G06F 1520

Patent

active

043002005

ABSTRACT:
This invention provides a helicopter airspeed indicating system for providing an indication of a theoretical airspeed of a helicopter in which it is fitted. The airspeed is calculated using measured weight and power values and a known relationship between power, weight and airspeed characteristics of the helicopter, and is particularly useful for providing an indication of helicopter airspeed at the low end of an overall speed range.

REFERENCES:
patent: 3761693 (1973-09-01), Fleury
patent: 3927306 (1975-12-01), Miller
patent: 3963372 (1976-06-01), McLain et al.
patent: 3969890 (1976-07-01), Nelson
patent: 4156912 (1979-05-01), Shigeta et al.
patent: 4236212 (1980-11-01), Arents

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