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Vertical take-off and landing detachable carrier and system for airborne and ground transportation

机译:机载和地面运输的垂直起降可分离载体和系统

摘要

An aircraft assembly includes at least one first wing portion providing a lift force during a horizontal flight, at least one wing opening disposed on a vertical axis of the at least one first wing portion, at least one vertical thruster positioned inside the at least one wing opening to provide vertical thrust during a vertical flight, and a mounting system including an open frame portion in a frame of the aircraft and at least one attachment member disposed in the open frame portion to attach at least one pod to the open frame portion in the aircraft frame. The aircraft assembly can further include at least one pod including a mounting frame to attach to the mounting system and a cabin to contain at least one of cargo and passengers.
机译:一种飞机组件,包括至少一个在水平飞行期间提供升力的第一机翼部分,设置在所述至少一个第一机翼部分的竖直轴线上的至少一个机翼开口,位于所述至少一个机翼内部的至少一个垂直推进器开口以在垂直飞行期间提供垂直推力,以及一种安装系统,其包括在飞行器的框架中的开放框架部分和布置在该开放框架部分中以将至少一个吊舱附接到该飞行器框架中的开放框架部分的至少一个附接构件。飞机框架。飞机组件可进一步包括至少一个吊舱,该吊舱包括:安装框架,其附接到安装系统;以及机舱,其容纳货物和乘客中的至少一个。

著录项

  • 公开/公告号US10040553B2

    专利类型

  • 公开/公告日2018-08-07

    原文格式PDF

  • 申请/专利权人 SUNLIGHT PHOTONICS INC.;

    申请/专利号US201715620178

  • 申请日2017-06-12

  • 分类号B64C39/02;B64C29;B64D9;G08G7/02;G05D1;G05D1/06;G05D1/10;G08G5;B64C39/10;G05D1/02;G08G5/02;G08G5/04;

  • 国家 US

  • 入库时间 2022-08-21 13:03:29

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