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公开(公告)号:US10029780B2
公开(公告)日:2018-07-24
申请号:US14902850
申请日:2013-08-09
Applicant: The Boeing Company
Inventor: Joshua Amory Ross , Shane Frank Cuda , Mark Ronald McLaughlin , Michael Robert Rush , Colin Lee Farr , David Bruce Smith , Nihar Ashokkumar Desai , Thomas Joseph Kennedy , Lyle Ray Deobald
IPC: B64C3/26 , B29D99/00 , B29C70/30 , B64C3/18 , B29K105/08
Abstract: 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.
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公开(公告)号:US20160176500A1
公开(公告)日:2016-06-23
申请号:US14902850
申请日:2013-08-09
Applicant: THE BOEING COMPANY
Inventor: Joshua Amory Ross , Shane Frank Cuda , Mark Ronald McLaughlin , Michael Robert Rush , Colin Lee Farr , David Bruce Smith , Nihar Ashokkumar Desai , Thomas Joseph Kennedy , Lyle Ray Deobald
CPC classification number: B64C3/26 , B29C70/30 , B29D99/0014 , B29K2105/0872 , B64C3/18 , Y02T50/43
Abstract: 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.
Abstract translation: 加强板包括复合板,以及在复合板上包括基部凸缘的加强件。 底座法兰朝向面板逐渐变细。 加强板还包括仅在复合板上的复合外包层和基底凸缘的锥形表面。
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