Abstract: A cargo hook includes a main body; a load arm configured to be pivotally attached to the main body with a load arm pivot connection; a keeper configured to be pivotally attached to the main body through a keeper pivot connection; and a keeper control unit configured to have a keeper locked configuration that locks movement of the keeper about the keeper pivot connection with respect to the main body.

Abstract: An aircraft hoist system includes hoist equipment arranged in an aircraft, the hoist equipment including a motor, a cable, and a hook portion. The aircraft hoist system also includes at least one sensor configured to obtain measurements and a processor configured to analyze the measurements from the at least one sensor. The aircraft hoist system also includes the processor configured to determine motor control signals to control the motor based on an analysis of the measurements from the at least one sensor to reduce sway and/or oscillations of the cable while lifting a load. The aircraft hoist system also includes the processor configured to control the motor to lift the load with the cable based on the determined motor control signals.

Abstract: A hoist system includes a hook; a cable connected to the hook; a motor configured to move the hook and the cable; an overload protection device (OLPD) configured to limit loads imparted on one or more of the hook, the cable, and the motor. The hoist system further includes an emergency brake system configured to stop movement of at least the cable, where the emergency brake system is configured to operate in response to a manual control or automatically in response to a controller.

Abstract: A hoist system that includes a hook; a cable connected to the hook; a motor configured to move the hook and the cable; and an overload protection device (OLPD) configured to limit loads imparted on one or more of the hook, the cable, and the motor. The hoist system further includes an overload protection device (OLPD) slip detection system configured to detect activation of the overload protection device (OLPD).

Abstract: A hoist system includes a wire rope cable having a first end and a second end. The wire rope cable further including multiple strands twisted into a helical shape. The hoist system further including a lifting mechanism configured to attach to the first end of the wire rope cable. The lifting mechanism including at least one of a rotating drum and a set of frictional rollers. The hoist system further including a motor configured to rotate the lifting mechanism; and a housing configured to house the lifting mechanism, the motor, and at least part of the wire rope cable.

Abstract: An aircraft hoist system includes hoist equipment arranged in an aircraft, the hoist equipment including a motor, a cable, and a hook portion. The aircraft hoist system also includes at least one sensor configured to obtain measurements and a processor configured to analyze the measurements from the at least one sensor. The aircraft hoist system also includes the processor configured to determine motor control signals to control the motor based on an analysis of the measurements from the at least one sensor to reduce sway and/or oscillations of the cable while lifting a load. The aircraft hoist system also includes the processor configured to control the motor to lift the load with the cable based on the determined motor control signals.

Abstract: A hoist system includes a wire rope cable having a first end and a second end. The wire rope cable further including multiple strands twisted into a helical shape. The hoist system further including a lifting mechanism configured to attach to the first end of the wire rope cable. The lifting mechanism including at least one of a rotating drum and a set of frictional rollers. The hoist system further including a motor configured to rotate the lifting mechanism; and a housing configured to house the lifting mechanism, the motor, and at least part of the wire rope cable.