STIFFENED COMPOSITE PANELS AND METHOD OF THEIR MANUFACTURE
摘要
A stiffened panel comprises a composite panel, and a stiffener including a base flange on the composite panel. The base flange is tapered towards the panel. The stiffened panel further comprises a composite overwrap layer on only the composite panel and a tapered surface of the base flange.
申请公布号
CA2911447(A1)
申请公布日期
2015.02.12
申请号
CA20132911447
申请日期
2013.08.09
申请人
THE BOEING COMPANY
发明人
ROSS, JOSHUA AMORY;CUDA, SHANE FRANK;MCLAUGHLIN, MARK RONALD;RUSH, MICHAEL ROBERT;FARR, COLIN LEE;SMITH, DAVID BRUCE;DESAI, NIHAR ASHOKKUMAR;KENNEDY, THOMAS JOSEPH;DEOBALD, LYLE RAY
