A jaw pivoting about an axis for clamping the shell, a lower end of the jaw receives the shell to allow closure. The notch intended to interfere with a catch of a cam to retain the jaw in the closed position. The cam is rigidly connected to a pivoting lever which allows the catch to be moved from the path of the notch to allow the jaw to open. The lever is to be pivotally activated through the force of an external component. The device includes a first and second spring each acting on the lever in an opposing manner, the second spring being stiffer than the first spring. The effect of the first spring is to lift the lever. The second spring counters the action of the first spring in order to delay the lifting of the lever and the catch when removing the component.

A method to load stores on an aircraft, the method may be controlled by one or more controller and may include one or more acts of loading stores onto corresponding lift portions; determining a relative position of the aircraft; positioning the stores relative to the determined position of the aircraft; and securing the stores to corresponding hardpoints (HPs) of the aircraft.

A method to load stores on an aircraft, the method may be controlled by one or more controller and may include one or more acts of loading stores onto corresponding lift portions; determining a relative position of the aircraft; positioning the stores relative to the determined position of the aircraft; and securing the stores to corresponding hardpoints (HPs) of the aircraft.

A method to load stores on an aircraft, the method may be controlled by one or more controller and may include one or more acts of loading stores onto corresponding lift portions; determining a relative position of the aircraft; positioning the stores relative to the determined position of the aircraft; and securing the stores to corresponding hardpoints (HPs) of the aircraft.

A method to load stores on an aircraft, the method may be controlled by one or more controller and may include one or more acts of loading stores onto corresponding lift portions; determining a relative position of the aircraft; positioning the stores relative to the determined position of the aircraft; and securing the stores to corresponding hardpoints (HPs) of the aircraft.

An ammunition packing apparatus comprises an ammunition feeder receiving ammunition cartons and horizontally arranging the ammunition cartons in a left or right direction, an ammunition vertical conveyor vertically conveying the ammunition cartons to an ammunition horizontal conveyor, the ammunition horizontal conveyor advancing the ammunition cartons to an ammunition inserter, an ammunition pouch mounter placing and fastening empty ammunition pouches in a flat and stretched position, an ammunition pouch opener opening mouths of the ammunition pouches, and the ammunition inserter advancing and inserting the ammunition cartons into the ammunition pouches, wherein the ammunition inserter includes spade-shaped inserting blades surrounding left and right surfaces and bottom surfaces of the ammunition cartons to allow the ammunition cartons to be inserted without being stuck to rims of the ammunition pouches and ammunition return preventers preventing the ammunition cartons from moving back when the ammunition inserting blades return after advancing and inserting the ammunition cartons.

A fluid power actuator includes a fluid power actuator housing, a piston assembly, and a screw assembly. The piston assembly is constructed and arranged to move relative to the fluid power actuator housing in response to changes in fluid pressure within the fluid power actuator housing. The screw assembly couples with the fluid power actuator housing and the piston assembly. The screw assembly is constructed and arranged to control movement of the piston assembly relative to the fluid power actuator housing. Such a fluid power actuator is well-suited for various applications such as in loading equipment which is involved in high precision munitions loading, among others.

A fluid power actuator includes a fluid power actuator housing, a piston assembly, and a screw assembly. The piston assembly is constructed and arranged to move relative to the fluid power actuator housing in response to changes in fluid pressure within the fluid power actuator housing. The screw assembly couples with the fluid power actuator housing and the piston assembly. The screw assembly is constructed and arranged to control movement of the piston assembly relative to the fluid power actuator housing. Such a fluid power actuator is well-suited for various applications such as in loading equipment which is involved in high precision munitions loading, among others.

A method to load stores on an aircraft, the method may be controlled by one or more controller and may include one or more acts of loading stores onto corresponding lift portions; determining a relative position of the aircraft; positioning the stores relative to the determined position of the aircraft; and securing the stores to corresponding hardpoints (HPs) of the aircraft.

A method to load stores on an aircraft, the method may be controlled by one or more controller and may include one or more acts of loading stores onto corresponding lift portions; determining a relative position of the aircraft; positioning the stores relative to the determined position of the aircraft; and securing the stores to corresponding hardpoints (HPs) of the aircraft.