公开(公告)号：WO2014053057A1

公开(公告)日：2014-04-10

申请号：PCT/CA2013/000846

申请日：2013-10-04

Applicant: SKYKAR INC. ,  LENG, Marcus

Inventor： LENG, Marcus

IPC: B64D27/24 ,  B64C27/22 ,  B64C27/28 ,  B64C29/00 ,  B64C39/08

CPC classification number: B64C27/26 ,  B60L11/1805 ,  B60L11/1859 ,  B60L11/1861 ,  B64C1/26 ,  B64C11/46 ,  B64C15/02 ,  B64C29/00 ,  B64C29/0025 ,  B64C29/02 ,  B64C39/026 ,  B64D17/00 ,  B64D27/24 ,  B64D31/12 ,  B64D33/08

Abstract: An aerial vehicle includes at least one wing, a plurality of thrust producing elements on the at least one wing, a plurality of electric motors equal to the number of thrust producing elements for individually driving each of the thrust producing elements, at least one battery for providing power to the motors, and a flight control system to control the operation of the vehicle. The aerial vehicle may include a fuselage configuration to facilitate takeoffs and landings in horizontal, vertical and transient orientations, redundant control and thrust elements to improve reliability and means of controlling the orientation stability of the vehicle in low power and multiple loss of propulsion system situations. Method of flying an aerial vehicle includes the variation of the rotational speed of the thrust producing elements to achieve active vehicle control.

Abstract translation: 飞行器包括至少一个机翼，在所述至少一个机翼上的多个推力产生元件，多个电动马达等于用于单独驱动每个所述推力产生元件的推力产生元件的数量，至少一个用于 向电动机供电，以及用于控制车辆操作的飞行控制系统。 飞行器可以包括机身配置，以便于在水平，垂直和瞬态取向中的起飞和着陆，冗余控制和推力元件以提高可靠性，并且在低功率和多功率推进系统情况下，控制车辆的定向稳定性。 飞行器的飞行方法包括推力产生元件的旋转速度的变化，以实现主动的车辆控制。