강화 열가소성 수지로 형성된 복합 윙박스 구조물. 복합 구조물은 탄소 섬유 보강재 및 구조물 제조 공정 동안 생성된 열을 국한시키기 위한 복수의 절연 요소를 포함한다. 윙박스를 제조하는 공정은 복수의 막의 내부에 일련의 절연 요소를 개재하는 단계 및 절연 요소와 막을 통합하여 적층체를 형성하는 단계를 포함한다. 이어서, 절연 요소가 지지 구조체의 위에 놓이도록 적층체가 지지 구조체와 정렬된다. 이어서, 적층체가 유도 용접과 같은 비접촉 가열 공정을 사용하여 지지 구조체에 융착된다.
A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding.
THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE
국부적인 절연 층을 갖는 열가소성 항공기 구조물 및 항공기 구조물을 형성하기 위한 방법
2023-02-28
Patent
Elektronische Ressource
Koreanisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge |
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