首页> 外国专利> ELECTRIC VERTICAL TAKE-OFF AND LANDING BLENDED WING-BODY AIRCRAFT

ELECTRIC VERTICAL TAKE-OFF AND LANDING BLENDED WING-BODY AIRCRAFT

机译:电动垂直起降混合翼飞机

摘要

An electric vertical take-off and landing aircraft having a disc-shaped blended wing-body that houses power sources and controls. Thrust pod arms are attached to the blended wing-body and each arm has a one of a set of thruster pairs. An ingress/egress hatch is attached to the rear surface. Navigation and strobe lights are located on the outside edge. Front landing gear is attached to the upper surface including pair of parallel motor pod struts. Main landing gear is attached proximate the trailing edge and a set of right and left elevons is attached to the rear surface proximate the main landing gear. A cockpit area including a viewing window is formed on the blended-wing.
机译:垂直电动起降飞机,具有盘形混合翼体,可容纳动力源和控制装置。推力舱臂连接到混合机翼,每个臂具有一组推进器对中的一个。入口/出口舱门连接到后表面。导航灯和频闪灯位于外侧边缘。前起落架连接到包括一对平行的发动机舱支撑杆的上表面。主起落架靠近后缘附接,左右一组左脚架附接至主起落架附近的后表面。在混合翼上形成了包括观察窗的座舱区域。

著录项

  • 公开/公告号WO2019241768A1

    专利类型

  • 公开/公告日2019-12-19

    原文格式PDF

  • 申请/专利权人 ZEVA INC.;

    申请/专利号WO2019US37453

  • 发明设计人 TIBBITTS STEPHEN;GOULD BEN;

    申请日2019-06-17

  • 分类号B64C29;B64D45/08;

  • 国家 WO

  • 入库时间 2022-08-21 11:14:11

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