公开(公告)号：WO2009066073A1

公开(公告)日：2009-05-28

申请号：PCT/GB2008/003890

申请日：2008-11-20

Applicant: QINETIQ LIMITED ,  HOTHI, Inderpal, Singh ,  STOACKLEY, Jon, Robert ,  STOACKLEY, Steven, John

Inventor： HOTHI, Inderpal, Singh ,  STOACKLEY, Jon, Robert ,  STOACKLEY, Steven, John

IPC: B64C29/02 ,  B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088

Abstract: An unmanned aerial vehicle (UAV) (1) in the form of a "tail sitter" flying wing (1) adapted for vertical take off and landing and transitions between flight as a helicopter and wing-borne flight. The vehicle is electrically powered from onboard batteries and equipped with rotors (7) on miniature helicopter rotor heads (8) at the tips of the wing for both lift, during take off and landing, and forward thrust. In planform the wing (1) comprises, to each side of its longitudinal axis, an inner section (2) with swept back leading and trailing edges, and an outer section (3) with a leading edge more perpendicular to the longitudinal axis, being only mildly swept back or substantially unswept, and a swept forward trailing edge.

Abstract translation: 一种以“直升机”飞翼（1）形式的无人机（UAV）（1），适用于垂直起飞和着陆，并且作为直升机和机翼飞行之间的飞行过渡。 车辆由车载电池供电，并在机翼顶部的微型直升机转子头（8）上配备转子（7），用于升降机，起飞和着陆期间以及向前推力。 在平面状中，翼（1）在其纵向轴线的每一侧包括具有扫掠的前缘和后缘的内部部分（2）和具有更垂直于纵向轴线的前缘的外部部分（3），其中， 只有轻微地扫过或基本上没有扫过，并且扫掠前缘。

公开(公告)号：EP2212199B1

公开(公告)日：2016-06-01

申请号：EP08851341.1

申请日：2008-11-20

Applicant: QinetiQ Limited

Inventor： HOTHI, Inderpal, Singh ,  STOACKLEY, Jon, Robert ,  STOACKLEY, Steven, John

IPC: B64C29/02 ,  B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088

公开(公告)号：EP2212199A1

公开(公告)日：2010-08-04

申请号：EP08851341.1

申请日：2008-11-20

Applicant: QinetiQ Limited

Inventor： HOTHI, Inderpal, Singh ,  STOACKLEY, Jon, Robert ,  STOACKLEY, Steven, John

IPC: B64C29/02 ,  B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088

Abstract: An unmanned aerial vehicle (UAV) (1) in the form of a 'tail sitter' flying wing (1) adapted for vertical take off and landing and transitions between flight as a helicopter and wing-borne flight. The vehicle is electrically powered from onboard batteries and equipped with rotors (7) on miniature helicopter rotor heads (8) at the tips of the wing for both lift, during take off and landing, and forward thrust. In planform the wing (1) comprises, to each side of its longitudinal axis, an inner section (2) with swept back leading and trailing edges, and an outer section (3) with a leading edge more perpendicular to the longitudinal axis, being only mildly swept back or substantially unswept, and a swept forward trailing edge.

Abstract translation: 无人驾驶飞行器（UAV）（1）采用“尾翼”飞行翼（1）的形式，适用于垂直起飞和降落，以及直升机和机翼飞行之间的飞行过渡。 该车辆由机载电池供电，并且在机翼顶端的微型直升机旋翼头（8）上配备有转子（7），用于升降，起飞和着陆期间以及向前推力。 在平面形式中，机翼（1）在其纵向轴线的每一侧包括具有前后扫掠后缘的内部部分（2）和具有更加垂直于纵向轴线的前缘的外部部分（3）， 只是轻微地扫过或基本没有扫过，并且向前扫过。