Rotor hub for propeller-driven aircraft, and assembly comprising such a rotor hub
AssigneeMaxon International AG
InventorsLuise LOESKOW, Marco SICHER, Roman MEIER,
Life of this patent
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Abstract
The present disclosure relates to a rotor hub, in particular for propeller-driven aircraft. The rotor hub has a hole for receiving a drive shaft. The hole has an internal thread which is designed to interact with an external thread of the drive shaft and to detachably connect the rotor hub to the drive shaft. The hole also has an annular groove for receiving an O-ring that is suitable for inhibiting a relative movement between the rotor hub and the drive shaft.
Claims17
A rotor hub for propeller-driven aircraft, comprising a hole for receiving a drive shaft, the hole comprising an internal thread which is designed to interact with an external thread of the drive shaft and to detachably connect the rotor hub to the drive shaft, wherein the hole has an annular groove for receiving an O-ring which is suitable for inhibiting a relative movement between the rotor hub and the drive shaft.
Dependencies are inferred from the claim text.