Abstract: Devices and methods for operating a diaphragm compressor. Embodiments of the present disclosure comprise an oil piston being driven to pressurize work oil against the diaphragm of the compressor. In embodiments, an injection pump provides a supplemental flow of work oil in the region of pressurized fluid, and such pump may be part of an actively controlled system. In embodiments, a pressure relief valve vents an overpump flow of work oil, and such valve may be variable. Embodiments provide feedback and control mechanisms, including control of the injection pump and the relief valve.

Abstract: Various methods and devices are provided for allowing multiple surgical instruments to be inserted into sealing elements of a single surgical access device. The sealing elements can be movable along predefined pathways within the device to allow surgical instruments inserted through the sealing elements to be moved laterally, rotationally, angularly, and vertically relative to a central longitudinal axis of the device for ease of manipulation within a patient's body while maintaining insufflation.

Abstract: Devices and methods for operating a diaphragm compressor. Embodiments of the present disclosure comprise an oil piston being driven to pressurize work oil against the diaphragm of the compressor. In embodiments, an injection pump provides a supplemental flow of work oil in the region of pressurized fluid, and such pump may be part of an actively controlled system. In embodiments, a pressure relief valve vents an overpump flow of work oil, and such valve may be variable. Embodiments provide feedback and control mechanisms, including control of the injection pump and the relief valve.

Abstract: A fan brake system for controlling an industrial fan system, the fan brake system including a fan brake having a brake pad movable on the fan brake to selectively engage the fan system. An actuator including a motor can be operable to cause the fan brake to perform a braking procedure on the fan system to resist rotational movement of the fan system. A controller can be communicated with the actuator, the controller operable to selectively cause the actuator and the fan brake to perform the braking procedure, wherein the controller is operable to monitor and control power being supplied to the motor of the actuator during the braking procedure to maintain a torque output of the motor according to a predetermined torque profile during the braking procedure.

Abstract: A fan brake system for controlling an industrial fan system, the fan brake system including a fan brake having a brake pad movable on the fan brake to selectively engage the fan system. An actuator including a motor can be operable to cause the fan brake to perform a braking procedure on the fan system to resist rotational movement of the fan system. A controller can be communicated with the actuator, the controller operable to selectively cause the actuator and the fan brake to perform the braking procedure, wherein the controller is operable to monitor and control power being supplied to the motor of the actuator during the braking procedure to maintain a torque output of the motor according to a predetermined torque profile during the braking procedure.

Abstract: Devices and methods for operating a diaphragm compressor. Embodiments of the present disclosure comprise an oil piston being driven to pressurize work oil against the diaphragm of the compressor. In embodiments, an injection pump provides a supplemental flow of work oil in the region of pressurized fluid, and such pump may be part of an actively controlled system. In embodiments, a pressure relief valve vents an overpump flow of work oil, and such valve may be variable. Embodiments provide feedback and control mechanisms, including control of the injection pump and the relief valve.

Abstract: A fan brake system for controlling an industrial fan system, the fan brake system including a fan brake having a brake pad movable on the fan brake to selectively engage the fan system. An actuator including a motor can be operable to cause the fan brake to perform a braking procedure on the fan system to resist rotational movement of the fan system. A controller can be communicated with the actuator, the controller operable to selectively cause the actuator and the fan brake to perform the braking procedure, wherein the controller is operable to monitor and control power being supplied to the motor of the actuator during the braking procedure to maintain a torque output of the motor according to a predetermined torque profile during the braking procedure.

Abstract: A fishing bait especially designed for jig fishing in which there is a vane pivotally secured at an intermediate portion of the shank portion of the fishing bait, the vane pivotally swinging back and forth between two spaced protuberances so as to alternately engage them to produce sound waves. The protuberances may be in the form of beads secured to and surrounding the shank portion of the bait. Or, the protuberances may be in the form of outwardly bent portions of the shank portion of the bait. The upper of the protuberances is preferably smaller than the lower one. The vane preferably has at least one aperture therethrough to allow water to pass through the vane and thus increase the ease with which the vane can move back and forth between the protuberances. The vane is preferably of metal and of a thickness of between 0.018 and 0.023 inches. The bait has a hook portion as well as a shank portion, and the hook portion and the shank portion are shown as being integral with each other.

Abstract: A transom missile launching system is configured to mount rigidly above the water line on the stern of ships designated to carry missile type ordnance. The missile launcher consists of two symmetrical modules containing eight missile cells each. Missiles are launched in the normal mode from a "all up round" canister at a fixed angle of about 60.degree. from a line athwartship both to port and to starboard. At this angle the probability of launch into a wave in heavy seas due to ship roll is eliminated. The missiles propulsion motor exhaust gases are vented directly overboard at launch without being directed either within the ship or across the weather deck. At ignition a water tight cover at the base of the launching chamber is blown directly overboard into the water by the exhaust gas pressure and a path is therefore provided for the exhaust gas to be discharged directly into the sea.