CPC B29C 70/38 (2013.01) [B29C 65/7814 (2013.01); B29C 65/7847 (2013.01); B29L 2031/3085 (2013.01); B32B 5/24 (2013.01); B32B 2250/02 (2013.01); B32B 2262/106 (2013.01); B32B 2605/18 (2013.01)] | 20 Claims |
1. A method for fabricating a composite part, the method comprising:
forming a skin panel preform comprising fiber reinforced material;
disposing rigid end caps at the skin panel preform at end locations of stringer preforms that will be placed at the skin panel preform;
locating the stringer preforms at the skin panel preform via the rigid end caps disposed at the skin panel preform; and
anchoring the stringer preforms to the skin panel preform between the rigid end caps.
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