发明名称 Crack and Delamination Stoppers For Aircraft Propulsion System Components
摘要 An inner fixed structure of a thrust reverser includes an inner skin, an outer skin, a cellular core disposed between the inner skin and the outer skin, and at least one crack and delamination stopper extending radially between the inner skin and the outer skin.
申请公布号 US2012291416(A1) 申请公布日期 2012.11.22
申请号 US201213470049 申请日期 2012.05.11
申请人 CHIOU SONG;YU JIA;HUBERT CLAUDE;LAYLAND MICHAEL;ROHR, INC. 发明人 CHIOU SONG;YU JIA;HUBERT CLAUDE;LAYLAND MICHAEL
分类号 B64D33/04;F02K3/04 主分类号 B64D33/04
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