A hybrid composite structure (20) includes a molded thermoplastic composite component (22) and a laminate thermoplastic composite component (36) co-welded together. The molded component (22) is reinforced with discontinuous fibers, and the laminate component (36) is reinforced with continuous fibers.
AEROSPACE STRUCTURAL MEMBER WITH HYBRID COMPOSITE STRUCTURE
LUFT- UND RAUMFAHRT-STRUKTURELEMENT MIT HYBRIDER VERBUNDSTRUKTUR
ÉLÉMENT STRUCTURAL AÉROSPATIAL À STRUCTURE COMPOSITE HYBRIDE
2022-01-05
Patent
Elektronische Ressource
Englisch