A repair patch for a composite edge includes a plurality of laminations laid face-to-face in a lamination direction defined along a thickness direction of the blade edge. At least an uppermost one of the laminations includes first and second transverse peripheral edges and at least the first peripheral edge includes a first portion defining a first edge plane at a first axial location along the second peripheral edge and a second portion defining a second edge plane at a second axial location along the second peripheral edge.
REPAIR PATCH FOR ROTOR BLADE
2017-09-14
Patent
Electronic Resource
English
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge / 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 |
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