TBTK_2209_V5
grabcad
Two different demo blade geometries suitable for current commercial aircraft engineswill be created and pin mechanical fixtures will be designed for them. By creating different configurations for these fixtures, structural analyzes for different clamping situations and modal analyzes for different pin placements will complete the comparison. Fixture design for optimum placement methodology in relation to the blade dimensions of the pins, taking into account the clamping and shear forces
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