The present invention pertains to a manufacturing method for passenger door corner components (1) of aircraft or spacecraft, the method comprising using additive layer manufacturing (ALM) to form an integral passenger door corner component (1), the integral passenger door corner component (1) comprising a substantially cruciform shape having a frame coupling member with two frame couplings (2a, 2b) as end pieces, the frame coupling member (1) intersecting with a beam coupling member with two beam couplings (3a, 3b) as end pieces.
Passenger door corner component and manufacturing method for passenger door corner component of aircraft or spacecraft
Passagiertür-Eckenkomponente und Herstellungsverfahren für Passagiertür-Eckenkomponente eines Flugzeugs oder Raumfahrzeugs
Composant de coin de porte passager et procédé de fabrication d'un tel composant d'aéronef ou d'engin spatial
2018-09-12
Patent
Elektronische Ressource
Englisch
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