Abstract: The service life of gun barrels of firearms with a high cyclic rate can be extended by means of the cooling device of the invention. To this end, coolant (7) is conveyed from a reservoir (6) into a pressure cylinder (10) by drawing up a hydraulic cylinder (13), while the feed line (14) to the gun barrel is closed. Thereafter the hydraulic piston (13) is moved in the opposite direction by a pressure reversal and the coolant (7) in the pressure cylinder (10) is placed under a defined operating pressure. Prior to triggering a volley, the feed line (14) is opened, so that the coolant (7) can flow via the feed line (14) and the nozzle (16) to the gun barrel (1). The coolant (7) is pushed back by the gas pressure respectively being created when a shot is fired, and following the lowering of the gas pressure to the operating pressure, it is again injected into the gun barrel (1).

Abstract: A bio-hazardous waste processor and optional encasement is described that uses a coolant such as liquid nitrogen to make the waste brittle in the hopper before crushing, keep the waste brittle in the down chute after crushing and also during shredding in the demolition chamber. After shredding, a fog of sterilant is used to disinfect the waste. The apparatus comprises an input hopper with a crushing wheel and dead plate towards its base to reduce the size of large particles, and a down chute which leads the crushed waste from the crushing wheel to a demolition chamber. In the demolition chamber, shredding is implemented by: one or more hammers and one or more commercially available off-the-shelf saw blades, the hammer(s) and saw blade(s) rotating in the same or opposite directions; or, one or more commercially available off-the-shelf dado saw blades, adjacent dados rotating in opposite directions.

Abstract: In connection with a projectile, the effective substance (4) is designed as a projectile core (3), which is held in place by a propulsion reflector sheath (1) and a propulsion reflector back (2). The data reception coil (13) and the power supply (14) are arranged in the propulsion reflection back (2), while the remaining elements (9, 10, 11, 12) of the programmable time fuse (8) are installed in the projectile core (3, 25). Predetermined breaking points are provided in the propulsion reflector sheath (1) and the propulsion reflector back (2), so that following the firing of the projectile, the propulsion reflector sheath (1) and the propulsion reflector back (2) with the data reception coil (13) and the power supply (14) are separated, and only the projectile core (3) with the remaining elements (9, 10, 11, 12) of the programmable time fuse (8) alone continue to travel.

Abstract: A family of compounds has been found to be useful for right-shifting hemoglobin towards a low oxygen affinity state. The effect has particular application in a wide variety of treatments including hypoxia, hypothermia, ischemia, stroke, ARDS, COPD, surgical blood loss, acute nonvolemic hemodilutions, wounds, diabetic ulcers, chronic leg ulcers, pressure sores, tissue transplants, and sepsis. The compounds are capable of acting on hemoglobin in whole blood.

Abstract: A family of compounds has been found to be useful for right-shifting hemoglobin towards a low oxygen affinity state. The effect has particular application in a wide variety of treatments including hypoxia, hypothermia, ischemia, stroke, ARDS, COPD, surgical blood loss, acute nonvolemic hemodilutions, wounds, diabetic ulcers, chronic leg ulcers, pressure sores, tissue transplants, and sepsis. The compounds are capable of acting on hemoglobin in whole blood.