Abstract: A clamp assembly includes a first jaw and a second jaw cooperatively positioned to receive the fixation element. A gate is displaceable relative to the first jaw and moveable between an open condition where the gate and the first jaw form an opening of a first size allowing introduction of the fixation element between the first and second jaws and a locking condition where the opening formed by the gate and the first jaw has a second size that prevents removal of the fixation element out from between the first and second jaws.

Abstract: Systems and methods for releasing a spacecraft payload at a substantially constant velocity are disclosed. A linear actuator is used that includes a spring loaded and fluid filled chamber. The spring drives against a piston within the chamber that includes a control orifice that restricts the fluid flowing from one side of the piston to the other and results in a substantially constant damped motion of the piston. The piston drives a rod from the chamber that is attached to a capture device that holds a flange of the spacecraft payload. The capture device moves along a linear guide toward an open end. Spring loaded latches are held in a closed position by the side walls of the guide as the capture device moves. The latches release the flange as exit the open end of the guide.

Abstract: A nuclear power plant (18) and its heat exhanger (26) are enclosed in an envelope (22) which is suspended above a bored shaft (14) from a support stem (30). When appropriate, the stem (30) can be melted by a furnace (34) to drop the envelope (22) to the bottom of the shaft (14). Sand (42) can then be dropped onto the envelope (22) through a drainage pipe (46). While the nuclear power plant (18) is operating and suspended in the shaft, spent fuel rods (70) are dropped into a sand blasting machine's hopper (130), mixed with sand and dropped into a bag (134) containing a small explosive device. The bag (134) is then dropped to the bottom of the shaft (14) and the explosive detonated to scatter the contents of the bag (134). Optionally, more sand or earth is then added to reduce heat and radiation to acceptable levels.

Abstract: The present invention relates to a release mechanism (1) for use in supporting a load (6) from a crane. The release mechanism (1) comprises a remotely operable release hook (2) for supporting by a cable (4) a load (6). The hook (2) is provided with an ejector lever (8) for releasing the cable from the hook (6) upon actuation of the ejection lever (8). Connected above the hook (2) by a cable link (10) is a control unit (12) arranged for controlling the ejector lever (8) on the hook (2). The control unit (12) and the ejector lever (8) are connected together by a communication cable (14) carrying pressurised hydraulic fluid. The control unit and the hook are substantially spaced apart.