首页> 外国专利> Aircraft i.e. double turboshaft engine civil transport airplane, has masking panels, where one of panels occupies retracted position in which panel is arranged in housings arranged in lower surface of wing

Aircraft i.e. double turboshaft engine civil transport airplane, has masking panels, where one of panels occupies retracted position in which panel is arranged in housings arranged in lower surface of wing

机译:飞机,即双涡轮轴发动机民用运输机,具有掩蔽板,其中一个板处于缩回位置,在该位置中板设置在机翼下表面中的壳体中

摘要

The aircraft i.e. double turboshaft engine civil transport airplane (1), has movable masking panels (13, 14) for reducing a part of noise emitted by engines. The engines are respectively suspended at wings (3) that are arranged laterally and symmetrically with respect to a fuselage (2). One of the panels occupies a deployed position in which the panel is projected under the wings laterally with respect to the corresponding engine or occupies a retracted position in which the panel is arranged in housings (12A, 12B) arranged in a lower surface (12) of the wings.
机译:飞机,即双涡轮轴发动机民用运输飞机(1),具有可移动的遮蔽板(13、14),用于减少发动机发出的一部分噪声。发动机分别悬挂在机翼(3)上,机翼相对于机身(2)横向且对称地布置。面板之一处于展开位置,在该展开位置中,面板相对于相应的发动机在机翼下方横向突出;或者在缩回位置,其中该面板被布置在布置在下表面(12)中的壳体(12A,12B)中。的翅膀。

著录项

  • 公开/公告号FR2942202A1

    专利类型

  • 公开/公告日2010-08-20

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号FR20090000740

  • 发明设计人 BURGUNDER SAMUEL;

    申请日2009-02-18

  • 分类号B64C7;B64D27/18;

  • 国家 FR

  • 入库时间 2022-08-21 18:26:35

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