Abstract: A projectile and method for producing the projectile. The projectile having a projectile main body which has a recess for receiving explosive and which, at least in part, has a preferably cylindrical lateral surface oriented along a longitudinal axis of the projectile main body. At least one fragmentation group includes at least two mutually adjacent, ring-shaped fragmentation bodies which are threaded on along the lateral surface and forming a fragmentation portion of the projectile. At least mutually adjacent fragmentation bodies of a fragmentation group are interconnected by at least one weld bead.

Abstract: A heat exchanger for transferring heat between a coolant and refrigerant, the heat exchanger comprising a heating device for heating the refrigerant and the coolant, comprises a bottom wall forming an end-face end of a stack of at least two flow volumes through which the refrigerant or coolant flows, a first flow volume for the refrigerant to flow through, which first flow volume is adjacent to the bottom wall and is connected to a first fluid inlet and to a first fluid outlet, which are configured to produce a connection to a refrigerant circuit, the first flow volume additionally being defined by a first partition opposite the bottom wall, and a second flow volume for the coolant to flow through, which second flow volume is adjacent to the first partition and opposite the first flow volume and is connected to a second fluid inlet and to a second fluid outlet.

Abstract: Aspects of the subject disclosure may include, for example, identifying an uncrewed aerial vehicle (UAV) for route planning and power management, obtaining information regarding the UAV, a present location of the UAV, a destination location for the UAV, or a combination thereof, determining, based on the information, a need for the UAV to recharge a power source of the UAV as part of a journey of the UAV from the present location of the UAV to the destination location for the UAV, responsive to the determining the need, identifying a recharging station associated with a network for recharging the power source of the UAV, and calculating a flight path for the UAV in accordance with the identifying the recharging station. Other embodiments are disclosed.

Abstract: A method produces an injection molded part. A plastic material is injected into a cavity for forming the injection molded part. The plastic material in a flow line region of the cavity, where the plastic material from two directions coincides during an injection molding process, is at least partially removed from the cavity via at least two overflow points and, in so doing, is locally swirled or mixed between the overflow points.

Abstract: A method produces an injection molded part. A plastic material is injected into a cavity for forming the injection molded part. The plastic material in a flow line region of the cavity, where the plastic material from two directions coincides during an injection molding process, is at least partially removed from the cavity via at least two overflow points and, in so doing, is locally swirled or mixed between the overflow points.

Abstract: A method produces an injection molded part. A plastic material is injected into a cavity for forming the injection molded part. The plastic material in a flow line region of the cavity, where the plastic material from two directions coincides during an injection molding process, is at least partially removed from the cavity via at least two overflow points and, in so doing, is locally swirled or mixed between the overflow points.

Abstract: A method produces an injection molded part. A plastic material is injected into a cavity for forming the injection molded part. The plastic material in a flow line region of the cavity, where the plastic material from two directions coincides during an injection molding process, is at least partially removed from the cavity via at least two overflow points and, in so doing, is locally swirled or mixed between the overflow points.

Abstract: Aspects of the subject disclosure may include, for example, identifying an uncrewed aerial vehicle (UAV) for route planning and power management, obtaining information regarding the UAV, a present location of the UAV, a destination location for the UAV, or a combination thereof, determining, based on the information, a need for the UAV to recharge a power source of the UAV as part of a journey of the UAV from the present location of the UAV to the destination location for the UAV, responsive to the determining the need, identifying a recharging station associated with a network for recharging the power source of the UAV, and calculating a flight path for the UAV in accordance with the identifying the recharging station. Other embodiments are disclosed.

Abstract: A gas burner for use in low-oxygen environments in which the oxygen concentration is insufficient to ensure complete combustion. The burner includes a central air supply that is annularly surrounded by a gas supply, thereby preventing the fuel from burning out with a delay in places where burn-out is detrimental to a system or plant.

Abstract: A component group is provided for joining together vehicle parts which have to be aligned, adjusted and fastened relative to one another during assembly. The component group includes at least two components which are fastened to the vehicle parts to be connected together and which are able to be displaced relative to one another and which are able to be fixed to one another after adjustment. A simple, rapid and reliable alignment of vehicle parts relative to one another is permitted.

Abstract: A gas burner for use in low-oxygen environments in which the oxygen concentration is insufficient to ensure complete combustion. The burner includes a central air supply that is annularly surrounded by a gas supply, thereby preventing the fuel from burning out with a delay in places where burn-out is detrimental to a system or plant.

Abstract: A component group is provided for joining together vehicle parts which have to be aligned, adjusted and fastened relative to one another during assembly. The component group includes at least two components which are fastened to the vehicle parts to be connected together and which are able to be displaced relative to one another and which are able to be fixed to one another after adjustment. A simple, rapid and reliable alignment of vehicle parts relative to one another is permitted.

Abstract: A method for producing wide strips of copper is performed by pouring a molten liquid into a revolving wide strip mold via a distribution container and a pour nozzle. A surface of the molten metal in the distribution container is maintained at a constant level above the place where the pour nozzle is fixed in the distribution container in the range of 75 mm to 90 mm with respect to the level of the bath surface of the mold. The molten metal is guided by an ascending channel from the distribution container to the pour nozzle and is distributed within the pour nozzle symmetrically over a width corresponding to the width of the strip. Within the pour nozzle, the molten metal is guided through first and second flow restrictors and is separated into numerous small individual flows in a vertical direction over the entire strip width of the mold.

Abstract: A method for producing wide strips of copper is performed by pouring a molten liquid into a revolving wide strip mold via a distribution container and a pour nozzle. A surface of the molten metal in the distribution container is maintained at a constant level above the place where the pour nozzle is fixed in the distribution container in the range of 75 mm to 90 mm with respect to the level of the bath surface of the mold. The molten metal is guided by an ascending channel from the distribution container to the pour nozzle and is distributed within the pour nozzle symmetrically over a width corresponding to the width of the strip. Within the pour nozzle, the molten metal is guided through first and second flow restrictors and is separated into numerous small individual flows in a vertical direction over the entire strip width of the mold.

Abstract: An electric machine including armature equipped with armature slots for accommodating armature coils, a commutator equipped with commutator segments, and a first and second hammer brush that each rest against the commutator in sliding fashion by means of a spring lever, in which at least one armature coil is comprised of two partial coils that are situated symmetrically to each other in relation to the rotation axis of the armature and the partial coils are connected to two adjacent commutator segments of the commutator.