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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
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.
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