公开(公告)号：US20060011778A1

公开(公告)日：2006-01-19

申请号：US10891588

申请日：2004-07-15

Applicant: James Small ,  Donald Lacey ,  Lloyd Kinsey ,  Mark Zepeda

Inventor： James Small ,  Donald Lacey ,  Lloyd Kinsey ,  Mark Zepeda

IPC: B64C15/00

CPC classification number: B64C39/00

Abstract: A rotating wing aircraft has a rotating fuselage and wings. The aircraft is configured to rotate with the air passing over the wings because of the rotation providing the lift needed to keep the aircraft aloft. The wings have rudders coupled to them, such as at the tips of the wings, to provide force for laterally moving the aircraft. The aircraft may be able to remain airborne by hovering for a long period of time, on the order of days. Power for the aircraft may be provided by a central diesel electric generator, which provides power for electric motors that turn propellers that are on the wings. The aircraft may be used for any of a variety of applications, such as for surveillance, communications, or as a radar platform.

Abstract translation: 旋翼机具有旋转的机身和机翼。 飞机被配置为随着空气通过机翼而旋转，因为旋转提供了使飞机保持高空所需的升力。 机翼具有与它们相连的方向舵，例如在翼的顶端，以提供用于横向移动飞行器的力。 飞机可以通过在几天的时间内长时间徘徊而保持机载。 飞机的动力可以由中央柴油发电机提供，该发电机为转动在机翼上的螺旋桨的电动机提供动力。 该飞机可用于任何各种应用，例如用于监视，通信或作为雷达平台。