FIELD: aviation; polar control systems of helicopters and aeroplanes. SUBSTANCE: control stick includes lever 1 with handle 2 secured in cabin floor in gimbal joint with lateral control hinge 3 and longitudinal control hinge 4 whose movable members are connected with rods 13 of linkage. Axis of hinge 3 is inclined forward relative to longitudinal datum line through angle of 15-35 deg at neutral position of stick. EFFECT: enhanced reliability. 3 dwg
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Authors
Dates
1997-09-10—Published
1994-01-27—Filed