FIELD: aviation.
SUBSTANCE: back-up control panel of the aircraft wing mechanization contains the mode switch button and the double handle-trigger of the back-up control unit displayed on the front panel of the control panel for at least one type of transformable mechanization elements such as the wing flaps of the aircraft. The unit is mounted in a housing, structurally made in the form of a flat frame with a closed rectangular contour open on opposite sides, in the upper part of which a horizontal axis is fixed, on which the said trigger is mounted with the possibility of rotation, consisting of two coaxial two-armed levers of the first kind. The levers are made with the possibility of simultaneous or autonomous action on the electromechanical toggle switches of the back-up control of the release/retraction of the aircraft wing flaps, fixed on the lower element of the said frame.
EFFECT: minimization of time for activating the back-up control, visual control of the sign of switching on the main or back-up control modes, increasing the compactness of the units of the back-up control panel, reducing the dimensions of the front panel of the control panel, reducing the material consumption and labor intensity of manufacturing the device as a whole.
1 cl, 5 dwg
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|
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Authors
Dates
2021-08-25—Published
2020-12-29—Filed