Method and equipment for making roll and pitch data inputs into

Machine element or mechanism – Gyroscopes – Gyroscope control

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74 534, 73178R, 33330, 340 27AT, 340 27NA, G01C 1902, G01C 1900, G08G 500

Patent

active

040942007

ABSTRACT:
In a gyro horizon type of equipment, roll corrections are fed to the aircraft symbol which is a normally fixed display element and pitch correction is introduced on a movable display element or drum with modification of the position of the display elements of the instrument gyro as a function of an interconnection of the instrument gyro with a gyromaster reference through comparators connected to each of the roll and pitch systems.

REFERENCES:
patent: 2620669 (1952-12-01), Braddon
patent: 2696597 (1954-12-01), Chombard
patent: 2752792 (1956-07-01), Draper et al.
patent: 2796594 (1957-06-01), Chombard
patent: 2892180 (1959-06-01), Smith
patent: 2898766 (1959-08-01), Pittman
patent: 2949780 (1960-08-01), Williams
patent: 3015962 (1962-01-01), Wrigley et al.
patent: 3213416 (1965-10-01), Joline
patent: 3263646 (1966-08-01), Arnold et al.
patent: 3404571 (1968-10-01), Schlitt
patent: 3451275 (1969-06-01), Atkin
patent: 3490281 (1970-01-01), Ainsworth
patent: 3521597 (1970-07-01), Chombard
F. Postlethwaite, "An Italian Artificial Horizon"-Aircraft Engineering Maine, Oct., 1944, pp. 288-289.

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