Patent ID: 11905010
Assignee: nan
Field: Transport (Mechanical engineering)
Classification: CPC B  G  Y | IPC B

Claim 4:
5. The aircraft of claim 3 wherein the aircraft is a Short Takeoff and Landing (STOL) aircraft having a fuselage with a long axis and a primary engine providing controllable primary forward thrust to propel the aircraft, further comprising a first aileron implemented proximate an end of the first fixed wing extending from the fuselage, a second aileron implemented proximate an end of the second fixed wing, opposite the first fixed wing, the first slot having the length and a width through the first fixed wing proximate the first aileron, the slot length substantially orthogonal to the axis of the fuselage, the second slot having the length and a width through the second fixed wing proximate the second aileron, the slot length substantially orthogonal to the axis of the fuselage, and a control mechanism accessible to a user in a cockpit of the aircraft, the control mechanism enabling the user to drive the first and second electric motors in a same rotary direction, to reverse the rotary direction, and to drive the first and second electric motors at a same rpm in either rotary direction.