| 摘要 |
<p>Gyroscopic stabilizer for aircrafts comprising a toroidal rotor (2), housed on a shaft (3), a motor (4), at least a level sensor and being characterized in that said shaft (3) is constrained to at least a hinge (5), and to at least a sliding constraint (6) housed between the motor (4) and the toroidal rotor (2), said toroidal rotor (2) being arranged between at least a hinge (5) and at least a sliding constraint (6).</p> |
