System and method for rotorcraft blade storage

Abstract

A device is provided. The device includes a first pillar. The first pillar includes a bottom portion having an opening. The first pillar further includes a top portion coupled to the bottom portion by a middle portion. The top portion includes a plurality of shelves stacked along a common axis intersecting the bottom portion. Each of the shelves has a respective recess. The first pillar further includes a plurality of clamps. Each of the shelves has a respective clamp of the clamps. Each respective clamp and respective recess of the shelves forms an airfoil cross-sectional shape. The first pillar further includes a plurality of locks. Each of the shelves has a respective lock of the locks. Each of the locks has a first locking portion on respective shelves and a second locking portion on respective clamps of the shelves.

Dependencies are inferred from the claim text.