| 摘要 |
<p>The invention relates to an aircraft with a convertible flight system which can function as a helicopter and as an airplane and comprising a fuselage (1), a main vertical shaft rotor (2), propulsion means and moving wings (7) located on the lower part of the fuselage (1) which can oscillate between a retracted position (7′) in which they are concealed under the fuselage, and an extracted position in which they project from said fuselage so as to act as lifting wings in airplane flight mode.</p> |
