A method and apparatus for manufacturing a composite stringer. A composite material and foam are laid up onto a tool in the form of a stringer. The foam has a plurality of structural members within the foam. The plurality of structural members has a number of orientations to resist a number of loads. The composite material, the foam in the form of the stringer, and the plurality of structural members are cured to form the composite stringer.
申请公布号
WO2010065330(A1)
申请公布日期
2010.06.10
申请号
WO2009US65195
申请日期
2009.11.19
申请人
THE BOEING COMPANY;SENIBI, SIMON, D.;VAN WEST, BARRY, P.;GUZMAN, JUAN, CARLOS;MCCARVILLE, DOUGLAS, A.;ROTTER, DANIEL, M.
