Aircraft weight and center of gravity cockpit readout system

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364567, 235 61T, 73 65, G01M 112

Patent

active

044634285

ABSTRACT:
An aircraft system which provides the pilot with a continuous cockpit reat of the weight and center of gravity of an aircraft carrying an externally lifted load together with the impact on aircraft controllability of load shifts and fuel burnoff, by transmitting input signals from load cells installed in the lifting hook system, input signals from a fuel totalizer, and input data from a system keyboard to a system computer.

REFERENCES:
patent: 2559718 (1944-05-01), Goodlett et al.
patent: 2987254 (1961-06-01), Kolisch
patent: 3584503 (1971-06-01), Senour
patent: 3701279 (1972-10-01), Harris et al.
patent: 3746844 (1973-07-01), Azum et al.
patent: 4034334 (1977-07-01), Allyn
patent: 4110605 (1978-08-01), Miller
patent: 4225926 (1980-09-01), Wendt

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