公开(公告)号：US20150375847A1

公开(公告)日：2015-12-31

申请号：US14587683

申请日：2014-12-31

Applicant: Google Inc.

Inventor： Peter Kinne ,  Damon Vander Lind ,  Gregor Cadman

IPC: B64C5/16 ,  F03D9/00 ,  B64C39/02

CPC classification number: B64C5/16 ,  B64C39/022 ,  F03D5/00 ,  F05B2240/40 ,  F05B2240/917 ,  F05B2240/921 ,  Y02E10/70 ,  Y02E10/728

Abstract: An aerial vehicle including a fuselage, a main wing attached to the fuselage, a support structure extending upwardly from the fuselage and having a front surface facing the main wing, an overhang positioned on a top of the support structure and extending towards the main wing, one or more rotating actuators positioned on the overhang, a rear elevator attached to the one or more rotating actuators that are configured to move the rear elevator from a flying mode position where a leading edge of the rear elevator faces the main wing to a hover mode position where the major surfaces of the rear elevator faces the main wing, and wherein the major surfaces of the rear elevator remain in front of the front surface of the support structure when the rear elevator is moved from the flying mode position to the hover mode position.

Abstract translation: 一种飞行器，包括机身，附接到机身的主翼，从机身向上延伸并具有面向主翼的前表面的支撑结构，位于支撑结构的顶部上延伸并向着主翼延伸的突出部， 一个或多个位于所述伸出部上的旋转致动器，附接到所述一个或多个旋转致动器的后部升降机，所述后部升降机构造成使所述后部升降机从所述后部升降机的前缘面向所述主翼的飞行模式位置移动到悬停模式 后升降梯的主表面朝向主翼的位置，并且其中当后电梯从飞行模式位置移动到悬停模式位置时，后电梯的主表面保持在支撑结构的前表面的前面 。