항공기(4)용 박스형 구조물(1)의 제조 방법을 기술하며, 이 구조물(1)은 제1 길이방향 단부(1a)와 제2 길이방향 단부(1b) 사이에서 길이방향(a)을 따라 연장되고, 제1 길이방향 벽(5); 제1 벽(5)과 대향하고 0이 아닌 양만큼 제 1 벽(5)으로부터 간격을 두고 배치되는 제2 길이방향 벽(6); 제1 벽(5)과 제2 벽(6) 사이에서 길이방향으로 연장하는 복수의 스파(7); 및 제1 길이방향 단부와 제2 길이방향 단부 사이에 개재된 횡방향 섹터(s1)에서 스파(7)에 대해 횡방향으로 배치된 적어도 하나의 보강 리브(23)를 포함하고; 각각의 스파는 횡방향 섹터(s1)에 대응하는 축좌표(x)로부터 제2 길이방향 단부까지 길이방향으로 연장하는 재료 결핍부를 획정하는 스파 캐비티(21)를 가지므로 제1 벽, 제2 벽 및 스파를 일체로 결합한 후에도 박스형 구조물(1)의 구조적 특성을 해치지 않고 보강 리브(23)를 쉽게 삽입할 수 있다.

    A method for manufacturing a box-shaped structure for aircrafts (1) is described (4), the structure (1) extending along a longitudinal direction (A) between a first longitudinal end (1a) and a second longitudinal end (1b), and comprising: a first longitudinal wall (5); a second longitudinal wall (6) facing the first wall (5) and arranged spaced from the first wall (5) by a non-zero amount; a plurality of spars (7) extending longitudinally and between said first wall (5) and second wall (6); and at least one reinforcing rib (23) arranged transversal to the spars (7) at a transversal sector (S1) interposed between the first and the second longitudinal end; each spar has a spar cavity (21) defining a lack of material extending longitudinally from an axial coordinate (X), which corresponds to the transversal sector (S1), up to the second longitudinal end, so that the reinforcing rib (23) can be easily inserted even after the integral coupling between the first wall, the second wall and the spars without compromising the structural properties of the box-shaped structure (1).


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    Titel :

    METHOD FOR MANUFACTURING A BOX-SHAPED STRUCTURE IN COMPOSITE MATERIAL FOR AIRCRAFTS


    Weitere Titelangaben:

    복합재에 의한 항공기용 박스형 구조물의 제조 방법


    Beteiligte:

    Erscheinungsdatum :

    20.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge / B29K Index-Schema für Formmassen oder Materialien für Verstärkungen, Füllstoffe oder vorgeformte Teile, z.B. Einlagen in Verbindung mit den Unterklassen B29B, B29C oder B29D , INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS / 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 / B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand



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