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Airship and berthing port

机译:飞艇和停泊港

摘要

An airship comprises a fuselage and a supporting structure positioned within the fuselage. An air passageway extends through the fuselage in an axial direction, with this air passageway having air inlet openings at the forward end of the airship with a first passageway tapering inwardly to provide a venturi in a mid region of the airship. A second passageway downstream of the venturi continues to the rear end of the airship where it flow-connects to a variable pitch rearwardly projecting air nozzle. An air turbine is mounted in the narrowest region of the venturi and is adapted to generate electricity. A plurality of adjustable air wings project outwardly from the surface of the fuselage, these air wings being arranged in circumferential rows. Cargo areas are provided at the bottom of the fuselage. A unique berthing post is used with the airship.
机译:飞艇包括机身和位于机身内的支撑结构。空气通道沿轴向延伸穿过机身,该空气通道在飞艇的前端具有进气口,第一通道向内逐渐变细以在飞艇的中间区域提供文丘里管。文丘里管下游的第二个通道一直延伸到飞艇的后端,在此处它与可变螺距的向后突出的空气喷嘴流动连接。空气涡轮机安装在文丘里管的最窄区域中,并适于发电。多个可调节的空气翼从机身表面向外突出,这些空气翼沿圆周排排列。机身底部提供货物区域。飞艇使用一个独特的停泊处。

著录项

  • 公开/公告号US6766982B2

    专利类型

  • 公开/公告日2004-07-27

    原文格式PDF

  • 申请/专利权人 DRUCKER ERNEST ROBERT;

    申请/专利号US20030650854

  • 发明设计人 ERNEST ROBERT DRUCKER;

    申请日2003-08-29

  • 分类号B64B10/20;

  • 国家 US

  • 入库时间 2022-08-21 23:18:18

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