发明名称 METALLIC SANDWICH STRUCTURE HAVING SMALL BEND RADIUS
摘要 An acoustic-attenuating wall panel (162) for a nacelle of a turbine engine may include a radiused portion (172,174). The radiused portion (172,174) may include an airflow surface having a concave configuration and which may be exposed to an airflow passing through the nacelle. The radiused portion (172,174) may include an acoustic attenuating section.
申请公布号 WO2014042857(A3) 申请公布日期 2014.11.06
申请号 WO2013US56590 申请日期 2013.08.26
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 B64D33/02;F02C7/045 主分类号 B64D33/02
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