An aircraft wing construction of composite materials includes a wing spar 34 having a web 44 constructed of only pre-preg fabric and having first 56 and second 66 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
VERBUNDSTOFFFLÜGELHOLM MIT INEINANDERGREIFENDEN BANDDECKLAGEN
LONGERON D'AILE EN TISSU COMPOSITE COMPORTANT DES NAPPES DE SOMMET À BANDE ENTRELACÉE
29.09.2021
Patent
Elektronische Ressource
Englisch
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