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1.发明授权Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction 有权弹性变形侧边缘连接，用于后缘翼片气动噪声降低公开(公告)号：US08695925B2
公开(公告)日：2014-04-15
申请号：US13326779
申请日：2011-12-15
申请人： Mehdi R. Khorrami , David P. Lockard , James B. Moore , Ji Su , Travis L. Turner , John C. Lin , Karen M. Taminger , Seun K. Kahng , Scott A. Verden
发明人： Mehdi R. Khorrami , David P. Lockard , James B. Moore , Ji Su , Travis L. Turner , John C. Lin , Karen M. Taminger , Seun K. Kahng , Scott A. Verden
摘要： A system is provided for reducing aeroacoustic noise generated by an aircraft having wings equipped with trailing-edge flaps. The system includes a plurality of elastically deformable structures. Each structure is coupled to and along one of the side edges of one of the trailing-edge flaps, and is coupled to a portion of one of the wings that is adjacent to the one of the side edges. The structures elastically deform when the trailing-edge flaps are deployed away from the wings.
摘要翻译： 提供了一种用于减少由具有后缘翼片的翼的飞行器产生的航空声学噪声的系统。 该系统包括多个可弹性变形的结构。 每个结构联接到并沿着一个后缘翼片的一个侧边缘，并且联接到与一个侧边缘相邻的翼中的一个的一部分。 当后缘襟翼远离翼片时，结构弹性变形。
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2.发明申请公开(公告)号：US20120153086A1
公开(公告)日：2012-06-21
申请号：US13326779
申请日：2011-12-15
申请人： Mehdi R. Khorrami , David P. Lockard , James B. Moore , Ji Su , Travis L. Turner , John C. Lin , Karen M. Taminger , Seun K. Kahng , Scott A. Verden
发明人： Mehdi R. Khorrami , David P. Lockard , James B. Moore , Ji Su , Travis L. Turner , John C. Lin , Karen M. Taminger , Seun K. Kahng , Scott A. Verden
IPC分类号： B64C9/16
摘要： A system is provided for reducing aeroacoustic noise generated by an aircraft having wings equipped with trailing-edge flaps. The system includes a plurality of elastically deformable structures. Each structure is coupled to and along one of the side edges of one of the trailing-edge flaps, and is coupled to a portion of one of the wings that is adjacent to the one of the side edges. The structures elastically deform when the trailing-edge flaps are deployed away from the wings.
摘要翻译： 提供了一种用于减少由具有后缘翼片的翼的飞行器产生的航空声学噪声的系统。 该系统包括多个可弹性变形的结构。 每个结构联接到并沿着一个后缘翼片的一个侧边缘，并且联接到与一个侧边缘相邻的翼中的一个的一部分。 当后缘襟翼远离翼片时，结构弹性变形。
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