| 摘要 |
<p>The main purpose of the invention is to give a VTOL-plane better flight performance than previously was possible. This purpose is achieved by giving the plane two counter rotating dual blade rotors on a common geometric axis, where each of these rotors can change the main angle between rotor blades from the normal 180 degrees in hover mode to app 30.40 degrees in flight mode. At transition to flight mode - one rotor blade is stopped at app 90 degrees from the fuselage while the other blade keeps rotating until app 120.130 degrees angle from flight direction and stops. This activity takes place at the same time for both rotors and results in two stationary wing pairs with the right orientation for the normal flight mode.</p> |
