Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
作者： Ramesh Thiagarajan , Suvankar Mishra , Robert Mark Chris , John R. Mccullough
DOI:
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摘要: A method of the present disclosure includes repairing a core stiffened structure with structural foam. Another splicing members together using joining member to foam stabilize during machining process. stabilizing prevent from crushing in autoclave pressure. The further have therein.
google.de 参考文章(116)
Thomas S. Scarpati, Robert J. Ford, Method of fabricating a composite aerodynamic rotorblade assembly ,(1976)
Joseph L. Sweetin, Gary J. Peffers, Marc J. Piehl, Douglas A. Frisch, Douglas L. Grose, Reinforced rampdown for composite structural member and method for same ,(2007)
E Fradenburgh, E Kiely, Aerodynamic blade with high stiffness-to-weight ratio ,(1970)
Barrie James Hayes, Dean Anthony Bugg, Method for filling and reinforcing honeycomb sandwich panels ,(1999)
Philip J. Ramey, Thomas A. Carstensen, Alex C. Dublinski, Composite molding apparatus for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores ,(1992)
Niels S. Mossbeck, Slow Acting Pocketed Spring Core Having Fill Material Inside Pockets ,(2011)
Nathalie Duret, Alain Fournier, Method of manufacturing a sandwich panel, made of composite material, and a panel thereby obtained ,(2000)
Eckstein Tibor, Holmes S Norvillie, Process for machining expanded honeycomb ,(1966)
John A. Violette, Charles E. K. Carlson, Reinforced full-spar composite rotor blade ,(1990)