首页> 外国专利> Airplane chassis for reducing tire wear, has turbine blades, with which inner sides of wheels are set, where turbine blades are arranged at front sides of chassis inlet channels

Airplane chassis for reducing tire wear, has turbine blades, with which inner sides of wheels are set, where turbine blades are arranged at front sides of chassis inlet channels

机译:用于减少轮胎磨损的飞机底盘具有涡轮机叶片,轮毂叶片设置在涡轮机叶片的内侧,涡轮机叶片布置在底盘进气通道的前侧

摘要

The airplane chassis has turbine blades (1), with which the inner sides of the wheels are set, where the turbine blades are arranged at the front sides of the chassis inlet channels (2). The air flow is directed on the turbine blades through the inlet channels with nozzles (2'). The complicated mechanism of the chassis is not disturbed by the simple turbines (3).
机译:飞机底盘具有涡轮叶片(1),轮毂的内侧设置有涡轮叶片(1),涡轮叶片布置在底盘进气通道(2)的前侧。空气流通过带有喷嘴(2')的进气道引导到涡轮叶片上。底盘的复杂机构不受简单涡轮机(3)的干扰。

著录项

  • 公开/公告号DE102010045148A1

    专利类型

  • 公开/公告日2012-03-15

    原文格式PDF

  • 申请/专利权人 BIHLER GERHARD;

    申请/专利号DE20101045148

  • 发明设计人 BIHLER GERHARD;

    申请日2010-09-11

  • 分类号B64C25/40;

  • 国家 DE

  • 入库时间 2022-08-21 17:05:20

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