| 摘要 |
The Primary Plane Orientation Device may be orientated such that the lifting surface, and or propulsion group of the aerial vehicle rotates about an axis through the Primary Plane. The Primary Plane, then, may be orientated at any chosen angular offset from the vehicle axis such that the lifting surfaces can produce thrust at said angle to the vehicle axis. The orientation of the Primary plane may then smoothly transform to other desired angles such that the aerial vehicle remains unstalled during conversion between VTOL-rotary and fixed wing flight. The lifting surface, and/or propulsion groups may then be fixed in any orientation to the axis of the vehicle to produce fixed wing lift, or propulsion in line with the fuselage or at various offsets from the fuselage. |
