Electric vertical takeoff and landing aircraft
Номер патента: EP3784568A1
Опубликовано: 03-03-2021
Автор(ы): Thomas W. Melcher
Принадлежит: Individual
Опубликовано: 03-03-2021
Автор(ы): Thomas W. Melcher
Принадлежит: Individual
Реферат: An aircraft has a boom, a propulsion assembly coupled to a first end of the boom, and a first wing coupled to a second end of the boom. The propulsion assembly is coupled to the boom by a rotating joint. A second wing is optionally coupled to the rotating joint. The first wing is coupled to the boom by a rotating joint. The first wing is coupled to the rotating joint by a hinge. A vehicle with roll, pitch, and yaw maneuverability able to mirror the aircraft movements may be coupled to the second end of the boom. The vehicle body may be picked up with a vehicle chassis disconnected from the vehicle body. The boom houses an energy source to power the propulsion assembly. A rudder is coupled to the second end of the boom. A paddle is disposed between the propulsion assembly and the boom.
Vertical takeoff and landing aircraft with passive wing tilt
Номер патента: WO2019005131A1. Автор: Rodin LYASOFF,Zachary T. LOVERING,Geoff BOWERS. Владелец: Α^3 By Airbus Llc. Дата публикации: 2019-01-03.