发明名称 Panel for performing acoustic treatment in nacelle of aircraft, has resistive layer whose face is in contact with air flow in honeycomb structure and reflecting layer, and openings form angle with layer lower than specific degree
摘要 <p>The panel (44) has an acoustically resistive layer (48) whose face is in contact with an air flow (46) in a honeycomb structure (50) and a reflecting layer (52). The acoustically resistive layer includes openings (54) inclined in a direction of the air flow to make communication with zones arranged on both sides of the acoustically resistive layer. The openings form an angle (alpha) with the acoustically resistive layer lower than 45 degree, where the angle lies between 15 and 45 degrees.</p>
申请公布号 FR2962586(A1) 申请公布日期 2012.01.13
申请号 FR20100055600 申请日期 2010.07.09
申请人 AIRBUS OPERATIONS 发明人 PORTE ALAIN;CHELIN FREDERIC;SURPLY THIERRY
分类号 G10K11/16;B64D29/00 主分类号 G10K11/16
代理机构 代理人
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