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EQUIPMENT OF AN AIRCRAFT ENGINE COMPARTMENT, ENGINE, ENGINE COMPARTMENT AND ASSOCIATED AIRCRAFT

机译:飞机发动机舱,发动机,发动机舱和相关飞机的设备

摘要

The invention relates to an equipment (3) of an engine compartment of an aircraft, characterized in that the equipment (3) comprises a housing (6) comprising a wall (7), the housing (6) defining further an interior volume (8) of the equipment (3), the equipment (3) further comprising a fan (14), the fan (14) comprising a body (21), the body (21) of the fan (14) comprising an outer surface (22), a portion of the outer surface (22) of the fan housing (21) being in contact or integral with a portion of the wall (7) of the housing (6) equipment (3), an outlet (14S) of the fan (14) opening into the interior volume (8) of the equipment (3) for circulating in the interior volume (8) a flow of cooling gas.
机译:本发明涉及飞机发动机舱的设备(3),其特征在于,设备(3)包括具有壁(7)的壳体(6),该壳体(6)进一步限定内部空间(8)在设备(3)的一个)中,设备(3)还包括风扇(14),风扇(14)包括主体(21),风扇(14)的主体(21)包括外表面(22) ),风扇外壳(21)的外表面(22)的一部分与外壳(6)设备(3)的壁(7)的一部分接触或成为一体,风扇的出口(14S)风扇(14)通向设备(3)的内部容积(8),以在内部容积(8)中循环冷却气流。

著录项

  • 公开/公告号FR3027287A1

    专利类型

  • 公开/公告日2016-04-22

    原文格式PDF

  • 申请/专利权人 TECHNOFAN;

    申请/专利号FR20140059964

  • 申请日2014-10-16

  • 分类号B64D33;

  • 国家 FR

  • 入库时间 2022-08-21 14:08:30

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