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DEVICE FOR LANDING WHEELS SPIN-UP DURING FLIGHT BEFORE PLANE LANDING

机译:飞机着陆前着陆时车轮自旋的装置

摘要

FIELD: air transport.;SUBSTANCE: device for landing wheels spin-up during flight before plane landing includes landing gear leg with wheel and spin-up mechanism. Landing wheel is equipped with turbine buckets fixed at sides of wheel tread. Air intake is equipped at landing gear leg with air intake regulators and nozzles directed from overhead onto turbine buckets located at the front wheel tread in flight direction.;EFFECT: decrease in energy costs for wheel spin-up and simplification of spin-up mechanism.;7 dwg
机译:技术领域:航空运输;实质:在飞机着陆之前的飞行过程中,起落架旋转的装置包括具有轮和起旋机构的起落架腿。起落架在轮辋的侧面装有涡轮机叶片。进气装置在起落架腿处装有进气调节器和喷嘴,这些进气调节器和喷嘴从头顶指向在飞行方向上位于前轮踏面处的涡轮叶片。效果:降低了车轮旋转所需的能源成本并简化了旋转起始机构。 ; 7 dwg

著录项

  • 公开/公告号RU2384467C2

    专利类型

  • 公开/公告日2010-03-20

    原文格式PDF

  • 申请/专利权人 BELJAEV VJACHESLAV IVANOVICH;

    申请/专利号RU20080112090

  • 发明设计人 BELJAEV VJACHESLAV IVANOVICH;

    申请日2008-04-01

  • 分类号B64C25/40;

  • 国家 RU

  • 入库时间 2022-08-21 18:29:47

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