发明名称 Systems and methods for assembling a skin of a composite structure
摘要 Systems and methods for assembling a skin of a composite structure on an outer surface of an inner mold line layup mandrel. The systems and methods include receiving a plurality of ply kits, assembling the plurality of ply kits to form a skin segment that defines a portion of the skin, and affixing the skin segment to the outer surface of the layup mandrel. The assembling includes transferring a respective ply kit of the plurality of ply kits to a non-planar transfer tool, compacting the respective ply kit on the non-planar transfer tool, and repeating the transferring and the compacting for each ply kit in the plurality of ply kits to form the skin segment.
申请公布号 US9199418(B1) 申请公布日期 2015.12.01
申请号 US201514604549 申请日期 2015.01.23
申请人 The Boeing Company 发明人 Rotter Daniel M.;Chang Paul Chih-Yung;Coxon Brad A.;Nelson Paul E.;Madden Kimberlee;Macias Henry;Noel Jennifer Sue;Jeppesen Eugene H.;Willden Kurtis S.;Berg Arvid J.;Phillips Richard V.;Metschan Stephen Lee;Kirchmeier Stephen K.;Anderson Joseph D.;Boner Scott A.
分类号 B29C70/30;B29D99/00;B29C43/36 主分类号 B29C70/30
代理机构 Dascenzo Intellectual Property Law, P.C. 代理人 Dascenzo Intellectual Property Law, P.C.
主权项 1. A system for assembling a composite structure, the system comprising: a supply of ply kits, wherein each ply kit in the supply of ply kits includes a plurality of plies of a composite material; a skin segment assembly system, wherein the skin segment assembly system includes: (i) a non-planar transfer tool that is configured to simultaneously support at least two ply kits from the supply of ply kits on a non-planar upward-facing surface thereof; and (ii) a compaction tool that is configured to compact the at least two ply kits on the non-planar transfer tool to form a skin segment; and a layup mandrel that is configured to receive the skin segment on an outer surface thereof.
地址 Chicago IL US