Abstract: A beverage production system, comprising a cup dispensing station configured to dispense cups, a beverage dispensing station configured to dispense a beverage, and a turntable assembly. The turntable assembly comprising a central axis, an inner turntable including a first row of cup receptacles, and an outer turntable including a second row of cup receptacles. The outer turntable is disposed circumferentially about the inner turntable, and the outer turntable is configured to rotate about the central axis to align the cup receptacles of the second row with the cup dispensing station and the beverage dispensing station. The turntable assembly is configured to align an opening in a cup receptacle in the second row with an opening in a cup receptacle in the first row. A slide assembly includes an arm configured to slide a cup positioned in the cup receptacle in the second row into the aligned opening of the cup receptacle in the first row.

Abstract: A composite spar for a helicopter rotor blade includes upper and lower side-wall regions and forward and aft conic regions wherein the conic regions further define transition and closure subregions. Constant width crossplies and unidirectional plies are stacked and arranged to form crossply and unidirectional laminates. The crossply laminates form the upper and lower sidewall regions and end portions thereof extend into the forward and aft conic regions to form a staggered distribution of structural joints and slip plane interfaces therein. The crossply laminates are comprised of high modulus fibers which are oriented within a range of .+-.42.degree. to about .+-.38.degree. relative to the longitudinal axis of the composite spar. The unidirectional laminates form the upper and lower sidewall regions and have end portions extending into the transition subregions.