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 |