公开(公告)号：WO2017184270A3

公开(公告)日：2017-10-26

申请号：PCT/US2017/022262

申请日：2017-03-14

Applicant: SWIFT ENGINEERING, INC.

Inventor： MOSHE, Jonathan

IPC: B64C3/38 ,  B64C29/02 ,  B64C27/22

Abstract: A tailsitter aircraft includes one or more rotatable wings. The tailsitter aircraft optionally includes a fuselage from which wing supports extend. Each rotatable wing optionally includes a rotatable wing section having an inboard portion proximate to the fuselage, and an outboard portion distal from the fuselage. The rotatable wing section may be rotatably attached to the wing support and configured to rotate between a vertical flight configuration in which the inboard portion is positioned on an opposing side of the wing support relative to the outboard portion, and a horizontal flight configuration different from the vertical flight configuration. The wings may be rotated during flight to transition between horizontal and vertical flight configurations, and they may be rotated about multiple axes.

公开(公告)号：WO2017184270A2

公开(公告)日：2017-10-26

申请号：PCT/US2017/022262

申请日：2017-03-14

Applicant: SWIFT ENGINEERING, INC.

Inventor： MOSHE, Jonathan

Abstract: A tailsitter aircraft includes one or more rotatable wings. The tailsitter aircraft optionally includes a fuselage from which wing supports extend. Each rotatable wing optionally includes a rotatable wing section having an inboard portion proximate to the fuselage, and an outboard portion distal from the fuselage. The rotatable wing section may be rotatably attached to the wing support and configured to rotate between a vertical flight configuration in which the inboard portion is positioned on an opposing side of the wing support relative to the outboard portion, and a horizontal flight configuration different from the vertical flight configuration. The wings may be rotated during flight to transition between horizontal and vertical flight configurations, and they may be rotated about multiple axes.

Abstract translation: 尾翼飞机包括一个或多个可旋转的机翼。 尾翼飞机可选地包括机翼支撑从其延伸的机身。 每个可旋转翼可选地包括具有靠近机身的内侧部分和远离机身的外侧部分的可旋转机翼部分。 可旋转的机翼部分可以可旋转地附接到机翼支架并且被配置成在垂直飞行配置和水平飞行配置之间旋转，在所述垂直飞行配置中，内侧部分位于机翼支架的相对侧上相对于外侧部分， 垂直飞行配置。 在飞行期间，机翼可以旋转以在水平和垂直飞行配置之间转换，并且它们可以围绕多个轴旋转。

公开(公告)号：EP3439951A2

公开(公告)日：2019-02-13

申请号：EP17786296.8

申请日：2017-03-14

Applicant: Swift Engineering, Inc.

Inventor： MOSHE, Jonathan

IPC: B64C3/38 ,  B64C29/02 ,  B64C27/22

公开(公告)号：EP3439951B1

公开(公告)日：2020-11-25

申请号：EP17786296.8

申请日：2017-03-14

Applicant: Swift Engineering, Inc.

Inventor： MOSHE, Jonathan

IPC: B64C3/38 ,  B64C29/02 ,  B64C27/22 ,  B64C29/00