FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to cockpit stabilization system. System for gyrostabilisation of cockpit of manned aircraft includes gimbals suspension with axes of rotation, which contain electric servo drives, inner circular spar fixed by its outer side to axes of rotation and to spherical transparent cockpit of pilot along the whole circumference. Spherical transparent cockpit of pilot, fixed to aircraft body by means of external axes of electric servo drives rotation. At that, aircraft body is fixed to pilot cabin at extreme points of outer axes of rotation, to outer side of electric servo drives. Gyrostabilisation system also includes an armchair, a step for a pilot and a control panel of an aircraft with an on-board flight computer and an electronic gyroscope, fixed inside the spherical transparent cockpit of the pilot on the inner circular side member on its inner side. At that, onboard computer is configured to control electric motors of gimbal axes of rotation of gimbal suspension and conversion of received signals from electronic gyroscope and outputting control signals to corresponding servo-drives of axes of rotation for stabilization of spherical transparent cockpit of pilot in preset position - by roll, pitch and/or yaw.
EFFECT: proposed invention provides increased safety of piloting within the city and other saturated medium with large number of aircrafts due to wide viewing angle, reduced overloads, possibility to manually change cockpit position.
1 cl, 1 dwg
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Authors
Dates
2020-07-28—Published
2019-12-06—Filed