Rotor blade non-counterbored retention assembly via a sliding clamped bushing
AssigneeLockheed Martin Corporation
InventorsDaniel George Schuster, Evan S. Tobin, David N. Schmaling
Life of this patent
Estimating the term…
Loading patent…
AssigneeLockheed Martin Corporation
InventorsDaniel George Schuster, Evan S. Tobin, David N. Schmaling
Estimating the term…
A rotor blade retention assembly includes a central hub, a rotor blade including an upper outer surface, a lower outer surface, a blade hole, and a proximal end coupled to the central hub, a strap member extending along a portion of the rotor blade such that a distal end receiving portion extends into the blade hole, and a retainer assembly disposed within the blade hole and coupled to the strap member. The retainer assembly includes an upper bushing and a lower bushing slidably disposed within the blade hole. The upper bushing includes a counterbored portion. The retainer assembly also includes an outboard blade pin disposed within the distal end receiving portion and includes a blade pin inner cavity.
A rotor blade retention assembly comprising:
A retainer assembly for use in a rotor blade retention assembly having a retainer cavity, the retainer assembly comprising:
A method for installing a retainer assembly of a rotor blade retention assembly having a central hub, a rotor blade having a blade hole, a blade inner cavity and a proximal end coupled to the central hub, and a strap member disposed within the blade inner cavity and including a distal end receiving portion, the retainer assembly having an upper bushing with an upper counterbored portion, a lower bushing, and a bushing inner cavity, a first fastener, a second fastener, and an outboard blade pin including a blade pin inner cavity, the method comprising:
A rotor blade retention assembly comprising:
Dependencies are inferred from the claim text.