A method is provided for repairing a structural weakness, preventing or inhibiting the initiation of a structural weakness, or preventing or inhibiting the progression of a structural weakness in an aircraft frame element. The method includes bonding a plurality of particles to the element such that the plurality of metallic particles form a continuous layer over the area of weakness, or the predicted area of weakness. The metallic particles may be applied by a cold spray process such as supersonic particle deposition.
METHODS FOR RESTORING AN AIRCRAFT FRAME ELEMENT
2016-11-24
Patent
Electronic Resource
English
IPC: | 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 / B64C AEROPLANES , Flugzeuge / C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL |
TIBKAT | 1997
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