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ADVANCED PARAFOIL AERIAL DELIVERY SYSTEM

机译:先进的翼型航空运输系统

摘要

A parafoil aerial transportation system is disclosed. The parafoil aerial transportation system comprises: a parachute unit which includes a main parachute, a plurality of front parachute lines connected to the front portion of the main parachute, a plurality of rear parachute lines connected to the rear portion of the main parachute, a first front riser connected to parachute lines positioned on the left of the front parachute lines, a second front riser connected to parachute lines positioned on the right of the front parachute lines, a third rear riser connected to parachute lines positioned on the left of the rear parachute lines, and a fourth rear riser connected to parachute lines positioned on the right of the rear parachute lines; and an automatic induction device unit which is positioned at the lower portion of the parachute unit, and is connected to each of the first front riser, the second front riser, the third rear riser, and the fourth rear riser, wherein the automatic induction device unit can simultaneously pull the first front riser and the second front riser and change the angle of incidence of the main parachute.
机译:公开了一种翼型航空运输系统。机翼航空运输系统包括:包括主降落伞的降落伞单元,连接到主降落伞的前部的多个前降落伞线,连接到主降落伞的后部的多个后降落伞线,第一前提升器连接到位于前降落伞线左侧的降落伞线,第二前提升器连接到位于前降落伞线右侧的降落伞线,第三后提升器连接到位于后降伞左侧的降落伞线线和连接到位于降落伞线右侧的降落伞线的第四后立管;自动感应装置单元,其位于降落伞单元的下部,并且连接到第一前立管,第二前立管,第三后立管和第四后立管中的每一个,其中,单元可以同时拉动第一前提升板和第二前提升板并更改主降落伞的入射角。

著录项

  • 公开/公告号KR101702573B1

    专利类型

  • 公开/公告日2017-02-06

    原文格式PDF

  • 申请/专利权人 NURI TECH CO. LTD.;JEONG DONG HO;

    申请/专利号KR20150173053

  • 发明设计人 JEONG DONG HO;

    申请日2015-12-07

  • 分类号B64D17;B64D17/34;G05D1/10;

  • 国家 KR

  • 入库时间 2022-08-21 13:26:09

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