Calibrated aircraft directional gyro for indicating holding patt

Details Calibrated aircraft directional gyro for indicating holding patt Calibrated aircraft directional gyro for indicating holding patt

1977-07-14

1979-05-15

Yasich, Daniel M.

Signals and indicators

Indicators

Scale structure

33 15C, 73178J, 116DIG43, 244 1R, G01C 1900, G08G 500

Patent

active

041541901

ABSTRACT:
A directional gyro for aircraft having on its stationary face plate, color zones referable separately to portions of the 360.degree. movable directional scale; each color zone indicating a particular entry procedure (direct, parallel, or tear drop) for the preselected radial.

REFERENCES:
patent: 2158925 (1939-05-01), Braswell
patent: 2613350 (1952-10-01), Kellogg
patent: 3496769 (1970-02-01), Vietor
patent: 3967236 (1976-06-01), Dietrich
patent: 4020787 (1977-05-01), Castro et al.

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