An aircraft wing construction of composite materials includes a wing spar having a web constructed of only pre-preg fabric and having first and second spar caps projecting at an angle from opposite edges of the web with the first and second spar caps being constructed of interleaved and alternating portions of the pre-preg fabric of the web and unidirectional pre-preg tapes.
COMPOSITE FABRIC WING SPAR WITH INTERLEAVED TAPE CAP PLIES
19.03.2020
Patent
Elektronische Ressource
Englisch
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