发明名称 Metallic sandwich structure having small bend radius
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.
申请公布号 US9168716(B2) 申请公布日期 2015.10.27
申请号 US201213620679 申请日期 2012.09.14
申请人 The Boeing Company 发明人 Benedetti Brenda;Farrell Robert S.;Leon Luis R.;Lan Justin H.;Booker Garry A.
分类号 B64D45/02;B32B3/12;B32B15/01;B32B3/28;B64D29/06;F02K1/82;F02C7/045;B64D33/02 主分类号 B64D45/02
代理机构 代理人
主权项 1. An acoustic-attenuating wall panel, comprising: a radiused portion of an inner wall panel of a nacelle; the radiused portion including an airflow surface having a concave configuration being exposed to an airflow; and the radiused portion comprising an acoustic attenuating section and formed as a honeycomb sandwich structure having a honeycomb core sandwiched between a pair of face sheets; the honeycomb core in the radiused portion has a cell width that is the same as the cell width of the honeycomb core in at least one of the following portions of the inner wall panel: a barrel portion, an upper bifurcation, a lower bifurcation.
地址 Chicago IL US