There is provided a composite structure (3) formed of a composite member which extends in one direction, includes holes (5), and is made of fiber reinforced plastics. A tensile load and/or a compressive load are applied to the composite structure (3) in the one direction. Tensile stiffness and/or compression stiffness of peripheral areas (3a) of the holes (5) in the one direction is lower than tensile stiffness and/or compression stiffness of the other area (3b), which surrounds the peripheral areas (3a), in the one direction, and the width of the peripheral area (3a) in a direction orthogonal to the one direction is set to 1.1 times or less of the diameter of the hole (5) in the direction orthogonal to the one direction.
COMPOSITE MATERIAL STRUCTURAL BODY, AIRCRAFT WING AND AIRCRAFT BODY PROVIDED WITH SAME, AND METHOD OF MANUFACTURING COMPOSITE MATERIAL STRUCTURAL BODY
VERBUNDWERKSTOFF-STRUKTURKÖRPER, FLUGZEUGFLÜGEL UND FLUGZEUGRUMPF DAMIT SOWIE VERFAHREN ZUR HERSTELLUNG DES VERBUNDWERKSTOFF-STRUKTURKÖRPERS
CORPS STRUCTURAL DE MATIÈRE COMPOSITE, AILE D'AVION ET FUSELAGE D'AVION LE COMPORTANT, ET PROCÉDÉ DE FABRICATION D'UN CORPS STRUCTURAL DE MATIÈRE COMPOSITE
02.12.2015
Patent
Elektronische Ressource
Englisch
IPC: | B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / 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 |
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