Al-si-mg aluminum alloy aircraft structural component production method

An aircraft structural component, particularly a fuselage component, production method using rolled, extruded or forged products made of aluminum alloy with the following composition (% by weight): Si: 0.7-1.3; Mg: 0.6-1.1; Cu: 0.5-1.1; Mn: 0.3-0.8; Zn

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Bibliographische Detailangaben
Hauptverfasser: Lequeu, Philippe, Dif, Ronan
Format: Patent
Sprache:eng
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Zusammenfassung:An aircraft structural component, particularly a fuselage component, production method using rolled, extruded or forged products made of aluminum alloy with the following composition (% by weight): Si: 0.7-1.3; Mg: 0.6-1.1; Cu: 0.5-1.1; Mn: 0.3-0.8; Zn