Abstract: A retractable component actuator that comprises a first portion, fixable to a fixed component and comprising a first engagement feature, and a second portion, fixable to a retractable component and comprising a second engagement feature releasably supportable on the first engagement feature. The retractable component actuator further comprises an automated drive mechanism operable to move the first engagement feature upward and downward relative to the fixed component when the first portion is fixed to the fixed component. Downward movement of the second engagement feature relative to the first engagement feature is constrained by the first engagement feature. Upward movement of the second engagement feature relative to the first engagement feature is unconstrained by the first engagement feature. The second engagement feature is upwardly and downwardly co-movable, relative to the fixed component, with the first engagement feature.

Abstract: A hydraulic lock for a hydraulic system includes a flow control valve and a second check valve. The flow control valve having a first inlet, a first outlet, a first check valve and a flow restrictor, each of the first check valve and the flow restrictor being communicably coupled to the first inlet and the first outlet and being arranged in parallel between the first inlet and the first outlet. The second check valve having a second inlet and a second outlet, the second inlet being communicably coupled to the first outlet, the second check valve further having a ball seating surface having an aperture there through, a ball, and a resilient member biasing the ball towards the ball seating surface to seal the aperture, the aperture being communicably coupled to the second inlet and the second outlet.

Abstract: A hydraulic lock for a hydraulic system includes a flow control valve and a second check valve. The flow control valve having a first inlet, a first outlet, a first check valve and a flow restrictor, each of the first check valve and the flow restrictor being communicably coupled to the first inlet and the first outlet and being arranged in parallel between the first inlet and the first outlet. The second check valve having a second inlet and a second outlet, the second inlet being communicably coupled to the first outlet, the second check valve further having a ball seating surface having an aperture there through, a ball, and a resilient member biasing the ball towards the ball seating surface to seal the aperture, the aperture being communicably coupled to the second inlet and the second outlet.

Abstract: A retractable component actuator that comprises a first portion, fixable to a fixed component and comprising a first engagement feature, and a second portion, fixable to a retractable component and comprising a second engagement feature releasably supportable on the first engagement feature. The retractable component actuator further comprises an automated drive mechanism operable to move the first engagement feature upward and downward relative to the fixed component when the first portion is fixed to the fixed component. Downward movement of the second engagement feature relative to the first engagement feature is constrained by the first engagement feature. Upward movement of the second engagement feature relative to the first engagement feature is unconstrained by the first engagement feature. The second engagement feature is upwardly and downwardly co-movable, relative to the fixed component, with the first engagement feature.

Abstract: Systems and methods are provided that lock thrust reversers and also drive fan nozzles of an aircraft. One system includes a coupling configured to selectively engage and disengage. While engaged, the coupling is configured to rotate to drive a Variable Area Fan Nozzle (VAFN), at least a portion of which is on a translating portion of a thrust reverser of an aircraft. Furthermore, while engaged the coupling is configured to prevent displacement of the translating portion.

Abstract: Systems and methods are provided that lock thrust reversers and also drive fan nozzles of an aircraft. One system includes a coupling configured to selectively engage and disengage. While engaged, the coupling is configured to rotate to drive a Variable Area Fan Nozzle (VAFN), at least a portion of which is on a translating portion of a thrust reverser of an aircraft. Furthermore, while engaged the coupling is configured to prevent displacement of the translating portion.