Method for creating a transition from an edge of an add-on part mounted on the outer surface of a rotor blade
A technology for rotor blades and additional parts, applied in the field of aerodynamic edge seals, can solve problems such as increasing manufacturing costs, achieve the effects of improving aerodynamic performance, contributing to the cost of defective products, and reducing the risk of wrinkling
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[0111] figure 1 An embodiment of an inventive edge seal S applied to an add-on 3, which may be any of a LEP cover, shell, TE cover, VG panel, TE panel, sensor panel, etc. is shown. The add-on 3 is attached to the outer surface 2 of the rotor blade 1 by means of an adhesive bonding layer 4 . For discussion purposes, the adhesive layer 4 may be considered an element of the attachment 3 . The height t of the add-on part 3 at its edge step 3E is the sum of the thickness of the add-on part 3 and the thickness of the adhesive layer 4 . The attachment edge 3E may be assumed to extend in the longitudinal direction of the rotor blade 1 . This figure clearly shows the "step" shape at the edge 3E of the add-on 3 . Using the inventive method, an edge seal S is formed along the add-on edge 3E. The edge seal S starts at a first point J1 at the attachment edge 3E and extends to a second point J2 whereby the height t of the seal S decreases gradually from a maximum at point J1 to a minimu...
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