B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 11/20 (2006.01) F01D 5/30 (2006.01) F01D 7/00 (2006.01)
Patent
CA 2721783
A propeller blade assembly comprises a plurality of propeller blades each connected to a hub via at least one bearing assembly. Each of the blades and the bearing assemblies is preloaded, wherein the preload is applied over a preload path which includes a blade root portion of each blade and the bearing assemblies, and a spring is provided in the preload path. In the event of wear of the components of the propeller blade assembly, the spring maintains the preload force. A method of applying the preload to the propeller blade assembly is also disclosed.
Craig Wilson And Company
Ge Aviation Systems Limited
LandOfFree
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