Aircraft banking angle indicator

Measuring and testing – Navigation – Take-off and landing monitors

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Details

244 79, 244179, 340975, G01C 1902

Patent

active

050957465

ABSTRACT:
An aircraft banking angle indicator which includes a banking angle sensing arrangement for generating an actual banking angle signal, a maximum banking angle input device for manually entering a selected maximum banking angle, a signal processing arrangement having respective inputs connected to the banking angle sensing arrangement and to the maximum banking angle input devices for generating an excessive banking output signal indicative of a banking angle exceeding the maximum banking angle, and an indicating arrangement having a signal input connected to the banking angle output signal for indicating the excessive banking angle.

REFERENCES:
patent: 4094200 (1978-06-01), Chombard

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