A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric 5 motor (135) coupled to the first port 5 wing (115), and a first starboard swash plate (150) coupled between a first starboard rotor (130) and first starboard electric motor (140), the first starboard electric motor (140) coupled to the first starboard wing (120). WO 2015/012935 PCT/US2014/036863 CKz C-z C'7 /n /o /n Cn/
Vertical takeoff and landing (VTOL) air vehicle
2021-09-16
Patent
Electronic Resource
English