首页> 外国专利> THRUST DIVERTING APPARATUS FOR JET PROPELLED VERTICAL LANDING AND TAKING-OFF FLIGHT VEHICLE

THRUST DIVERTING APPARATUS FOR JET PROPELLED VERTICAL LANDING AND TAKING-OFF FLIGHT VEHICLE

机译:喷气推进垂直着陆和起飞飞行器的推力转向装置

摘要

According to one embodiment of the present invention, the present invention has four lift nozzles and one main nozzle for vertical landing and taking-off in a jet engine so that cruising, vertical landing and taking-off and diversion flight of a flight vehicle are achieved by vector composition of thrust by gas sprayed from each nozzle. A thrust line diverting apparatus properly distributes and sprays turbine discharge gas and fan discharge compressed air to each nozzle in accordance with each flight mode. An after burner promotes temporary improvement of the thrust by fuel spray as necessary by being mounted on a gas pipe or a duct to the lift nozzle and the main nozzle from a thrust diverting apparatus.;COPYRIGHT KIPO 2020
机译:根据本发明的一个实施例,本发明具有四个升降喷嘴和一个主喷嘴,用于在喷气发动机中垂直着陆和起飞,从而实现飞行器的巡航,垂直着陆以及起飞和改道飞行。由每个喷嘴喷出的气体的推力矢量组成。推力线转向装置根据每个飞行模式将涡轮排放气体和风扇排放的压缩空气适当地分配并喷射到每个喷嘴。后燃器通过安装在从推力转移装置到提升喷嘴和主喷嘴的燃气管或导管上,根据需要通过燃料喷雾促进推力的暂时改善。; COPYRIGHT KIPO 2020

著录项

  • 公开/公告号KR102014726B1

    专利类型

  • 公开/公告日2019-08-27

    原文格式PDF

  • 申请/专利权人 KIM HYUNG OH;KIM KI BEOM;

    申请/专利号KR20190004952

  • 发明设计人 KIM HYUNG OHKR;KIM KI BEOMKR;

    申请日2019-01-15

  • 分类号B64C29;B64D27/16;

  • 国家 KR

  • 入库时间 2022-08-21 11:47:57

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