Aircraft attitude display instrument

Details Aircraft attitude display instrument Aircraft attitude display instrument

1982-02-08

1983-12-13

Haroian, Harry N.

Geometrical instruments

Indicator of direction of force traversing natural media

Gyroscopically controlled or stabilized

G01C 1900

Patent

active

044198329

ABSTRACT:
An aircraft attitude indicator employing a gyro driven tape display. The tape takes the form of a closed loop stretched about a carrier mechanism, and includes a viewable horizon indication. The tape further includes a set of perforations which, preferably, are engaged and driven by sprocket teeth borne on a sprocket wheel member attached to the pitch gimbal of the gyro. The tape travels in response to tilt of the gyro spin axis relative to the aircraft, and in a direction so that reversed pitch sensing is accomplished.

REFERENCES:
patent: 3039200 (1962-06-01), Vibert

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