The present invention provides a method for (i) repairing a structural weakness, or (ii) preventing or inhibiting the initiation of a structural weakness, or (iii) preventing or inhibiting the progression of a structural weakness in an aircraft frame element, the method comprising the step of bonding a plurality of particles to the element, the bonding being effected under conditions allowing the plurality of metallic particles to form a substantially continuous layer over the area of weakness, or the predicted area of weakness. 9W OWN OAMM ------------------------------------------------ ---------------- i yon ----------------- T*eTd Do, SPD POO
METHODS FOR RESTORING AN AIRCRAFT FRAME ELEMENT
29.04.2021
Patent
Elektronische Ressource
Englisch
IPC: | C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL / B21D WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL , Bearbeiten oder Verarbeiten von Blechen, Metallrohren, -stangen oder -profilen ohne wesentliches Abtragen des Werkstoffs / 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 |
TIBKAT | 1997
|Springer Verlag | 2022
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