发明名称 Aerodynamic accelerator device for aircraft landing gear
摘要 In order to set the wheels of the landing gear of an aircraft rotating before their contact with the ground, with the aim of avoiding wear on the tyres, a system of small blades is arranged on the wheel. These small blades, similar to those of an anemometer, in the relative flow of the air due to the speed of the aircraft impart a rotational movement to the wheels. <IMAGE>
申请公布号 FR2600619(A1) 申请公布日期 1987.12.31
申请号 FR19860009171 申请日期 1986.06.25
申请人 HURTADO OLIVIER 发明人
分类号 B64C25/40;(IPC1-7):B64C25/40;B64C25/36 主分类号 B64C25/40
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