METHOD TO INCREASE STRENGTH AND TOUGHNESS OF AIRCRAFT STRUCTURAL COMPONENTS

A method to increase strength and toughness of aircraft structural components is disclosed. An examplary component includes a composite structure (208) of an aircraft, a stringer (200) coupled to the composite structure (208) of the aircraft, where the stringer (200) and the composite structure (208...

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Bibliographische Detailangaben
Hauptverfasser:	CHENG, Jiangtian, BEHZADPOUR, Forouzan
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	PERFORMING OPERATIONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	A method to increase strength and toughness of aircraft structural components is disclosed. An examplary component includes a composite structure (208) of an aircraft, a stringer (200) coupled to the composite structure (208) of the aircraft, where the stringer (200) and the composite structure (208) form a stringer radius gap. A gap filler (202) is disposed in the stringer radius gap, which includes chopped fibers randomly distributed throughout an entire volume of the gap filler (202).