-
-
公开(公告)号:EP2895392A2
公开(公告)日:2015-07-22
申请号:EP13760168.8
申请日:2013-08-26
申请人: The Boeing Company
摘要: An acoustic-attenuating wall panel for a nacelle of a turbine engine may include a radiused portion. The radiused portion may include an airflow surface having a concave configuration and which may be exposed to an airflow passing through the nacelle. The radiused portion may include an acoustic attenuating section.
-