| CPC B64C 11/28 (2013.01) [B64C 11/065 (2013.01); B64C 29/0033 (2013.01)] | 9 Claims |

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7. A blade lock for a tiltrotor aircraft to enable and disable a folding degree of freedom and a pitching degree of freedom of a rotor blade, the blade lock comprising:
a fold lock adapted to prevent folding of a rotor blade in a fold-lock position and to allow folding of the rotor blade in a pitch-lock position;
a pitch lock adapted to allow pitch movement of a rotor blade in a fold-lock position and to prevent pitch movement of the rotor blade in the pitch-lock position;
a spring-loaded link pivotally connected to both the fold lock and the pitch lock and adapted to provide passive, overcenter locking in the fold-lock position;
an actuator coupled to the pitch lock and adapted to move the pitch lock and the fold lock between the fold-lock and pitch-lock positions, wherein the actuator is a linear actuator having an actuator shaft that is coupled to the pitch lock;
a first attachment point on the pitch lock, the first attachment point separated from a pivot axis of the pitch lock by a first distance; and
a second attachment point on the pitch lock, the second attachment point separated from the pivot axis of the pitch lock by a second distance that is longer than the first distance;
wherein the spring-loaded link is pivotally connected to the first attachment point and the actuator is pivotally connected to the second attachment point.
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