CPC B64C 11/06 (2013.01) [B64C 11/30 (2013.01); F01D 7/00 (2013.01)] | 19 Claims |
1. A rotor assembly, comprising:
a rotor hub having a mast axis and a central access port, the access port being open in a direction substantially parallel to the mast axis; and
a crosshead, comprising:
a first upper tab and a first lower tab offset from the first upper tab in the direction substantially parallel to the mast axis, the first upper tab and the first lower tab defining a slot therebetween.
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