Abstract: A battery module for a vehicle, in particular for an aircraft, comprises two end plates and a cell stack comprising an arrangement of several interconnected battery cells, in particular pouch cells, that are arranged in a row along a stacking direction, wherein the cell stack is sandwiched between the two end plates in the stacking direction, wherein the battery module further comprises a separate tube-like enclosure comprising a heat insulating material, the tube-like enclosure having a front opening and a back opening that are closed by the end plates, so that the tube-like enclosure and the two end plates form a housing in which the cell stack is accommodated.

Abstract: The present invention relates to an aircraft, comprising a fuselage, at least one pair of wings and a battery system for providing power to electrical systems of the aircraft, wherein the battery system comprises at least one battery pack, each battery pack comprises a number of individual battery modules, which are directly or indirectly coupled to one another, and the at least one battery pack is disposed between an inner structural wall defining an interior space of the fuselage and an outer fairing wall of the fuselage. The fuselage is provided with a rack mounting mechanism comprising a number of mounting brackets, each for exchangeably mounting one of the battery modules to the aircraft, and each of the battery packs is a virtual battery pack, which is obtained by electrically connecting a predetermined number of the battery modules.

Abstract: A battery module for a vehicle, in particular for an aircraft, comprises a housing, a cell stack accommodated in the housing, an internal channel system for heat transfer fluid disposed in the housing, a fluid inlet connector and a fluid outlet connector connected to the internal channel system and adapted to being connected to an external thermal management system, wherein the fluid inlet connector and the fluid outlet connector are self-sealing connectors molded into the housing, preferably self-sealing and dripless connectors.

Abstract: A fluid handling device includes a receiving container with a piston arranged therein in a displaceable manner, such that the volume of a fluid receiving reservoir may be changed by a displacement of the piston. In addition, the fluid handling device includes an actuation mechanism configured to displace a carrier bearing upon actuation of the former. Finally, the fluid handling device includes a spring mechanism configured to transfer a force from the carrier bearing to the piston so as to effect, in response to displacement of the carrier bearing in a first direction, a displacement of the piston within the receiving container such that a volume of the fluid reservoir is increased.

Abstract: A fuselage cell structure for an aircraft includes at least two skin panels including at least one double shell skin panel and at least one monolithic skin panel. At least one longitudinal brace or a transverse brace is disposed so as to form at least one of longitudinal seam or a transverse seam between the double shell skin panel and the monolithic skin panel. The fuselage cell structure includes at least one of a longitudinal bracket and a load transfer point. The longitudinal bracket is disposed in a region of the longitudinal seam and includes a first and a second longitudinal flanges disposed offset with respect to one another and connected by a web. The load transfer point is disposed in a region of the transverse seam so as to connect the longitudinal brace disposed on the monolithic skin panel to the double shell skin panel.

Abstract: A laser protection cabin separates a working space for laser processing from a working space environment and includes a first wall area, in particular a ceiling area, and a second wall area, in particular a lateral wall area. The second wall area, on its interior side facing the working area, in particular in a sub-area adjacent to the first wall area, has a laser beam reflector in order to reflect laser radiation, created during laser processing, onto the first wall area. The first wall area has a surface, on its interior side facing the working area, which absorbs and/or diffusely scatters the laser radiation.

Abstract: A window element for a double-shell skin field of an aircraft fuselage cell includes a window frame having a window module disposed in the frame, wherein the frame is disposed in an opening of the double-shell skin field, and wherein the frame is connected to the double-shell skin field by a surrounding embrasure profile positioned against a core structure of the skin field at least in some regions, wherein the core structure includes an inner and an outer covering layer.

Abstract: A fluid handling device includes a receiving container with a piston arranged therein in a displaceable manner, such that the volume of a fluid receiving reservoir may be changed by a displacement of the piston. In addition, the fluid handling device includes an actuation mechanism configured to displace a carrier bearing upon actuation of the former. Finally, the fluid handling device includes a spring mechanism configured to transfer a force from the carrier bearing to the piston so as to effect, in response to displacement of the carrier bearing in a first direction, a displacement of the piston within the receiving container such that a volume of the fluid reservoir is increased.

Abstract: A laser protection cabin separates a working space for laser processing from a working space environment and includes a first wall area, in particular a ceiling area, and a second wall area, in particular a lateral wall area. The second wall area, on its interior side facing the working area, in particular in a sub-area adjacent to the first wall area, has a laser beam reflector in order to reflect laser radiation, created during laser processing, onto the first wall area. The first wall area has a surface, on its interior side facing the working area, which absorbs and/or diffusely scatters the laser radiation.

Abstract: A fuselage cell structure for an aircraft includes at least two skin panels including at least one double shell skin panel and at least one monolithic skin panel. At least one brace which is at least one of a longitudinal and a transverse brace is disposed so as to form at least one of a longitudinal seam and a transverse seam between the at least one double shell skin panel and the at least one monolithic skin panel. The fuselage cell structure includes at least one of a longitudinal bracket and a load transfer point. The longitudinal bracket is disposed in a region of the longitudinal seam and includes a first and a second longitudinal flange that are disposed offset with respect to one another and connected by a web. The load transfer point is disposed in a region of the transverse seam so as to connect the longitudinal brace disposed on the at least one monolithic skin panel to the at least one double shell skin panel.

Abstract: A window element for a double-shell skin field of an aircraft fuselage cell includes a window frame having a window module disposed in the frame, wherein the frame is disposed in an opening of the double-shell skin field, and wherein the frame is connected to the double-shell skin field by a surrounding embrasure profile positioned against a core structure of the skin field at least in some regions, wherein the core structure includes an inner and an outer covering layer.

Abstract: A mechanical arrangement for moving workpieces and/or processing remnants from processing of a workpiece comprises a load carrier and a load carrier drive. Part of the load carrier drive is formed by a rigid chain which is acted upon by a chain driving wheel supported on the load carrier. Owing to that action, the chain driving wheel takes the load carrier with it to a target position. In the process, the chain driving wheel moves together with the load carrier relative to a chain abutment against which the rigid chain is braced. Systems for processing workpieces are provided, which make use of a mechanical arrangement of the above-mentioned kind.

Abstract: So that a catheter can be made visible in ultrasound images easily and with relatively little effort, and hence positional control of a catheter can be enabled with relatively little effort, an ultrasound marking recognizable in the body of a living being by means of ultrasound is provided at the distal end of a catheter, wherein the catheter has a lumen, and the ultrasound marking is arranged in the lumen near the distal end such that it is removable via a proximal end of the catheter.

Abstract: A mechanical arrangement for moving workpieces and/or processing remnants from processing of a workpiece comprises a load carrier and a load carrier drive. Part of the load carrier drive is formed by a rigid chain which is acted upon by a chain driving wheel supported on the load carrier. Owing to that action, the chain driving wheel takes the load carrier with it to a target position. In the process, the chain driving wheel moves together with the load carrier relative to a chain abutment against which the rigid chain is braced. Systems for processing workpieces are provided, which make use of a mechanical arrangement of the above-mentioned kind.

Abstract: A fluid pressure measurement unit is manufactured by steps of providing a measurement element with a measurement chip arranged on a first chip carrier side and a plurality of socket-shaped terminal contacts for contacting contact terminals of the measurement chip, the socket-shaped terminal contacts protruding from a second chip carrier side opposite from the chip carrier first side; providing a housing element comprising a plurality of receiving holes in a housing element first side which are implemented to receive the socket-shaped terminal contacts when combining the housing element with the measurement element, wherein the receiving holes extend from the housing element first side to a housing element second side opposite from the housing element first side; and combining the measurement element and the housing element, wherein the second chip carrier side is opposite from the housing element first side and the socket-shaped terminal contacts are arranged in the receiving holes.

Abstract: A method for manufacturing a component of a fluid pressure measurement unit includes the step of providing a measurement element with a measurement chip arranged on a first side of the chip carrier and a plurality of socket-shaped terminal contacts for contacting contact terminals of the measurement chip, wherein the socket-shaped terminal contacts protrude from a second side of the chip carrier opposite from the first side of the chip carrier.

Abstract: A thermal camouflage tarpaulin for hiding heat sources against detection in a thermal image, comprising a base textile composed of a loop-formingly knitted or woven glass fabric is provided on the side which is remote from the heat source with a compound whose reflectance values are in the region of a visual camouflage and/or in the infrared region. Said base textile is provided on that side which faces the heat source with a free-standing polyester film to which has been applied a vapor-deposited coating which reflects thermal radiation.

Abstract: A thermal camouflage tarpaulin for hiding heat sources against detection in a thermal image, comprising a base textile composed of a loop-formingly knitted or woven glass fabric is provided on the side which is remote from the heat source with a compound whose reflectance values are in the region of a visual camouflage and/or in the infrared region. Said base textile is provided on that side which faces the heat source with a free-standing polyester film to which has been applied a vapor-deposited coating which reflects thermal radiation.

Abstract: Siloxene and siloxene derivatives are compatible with silicon and may be generated as epitaxial layer on a silicon monocrystal. This permits the production of novel and advantageous electroluminescent devices, such as displays, image converters, optoelectric integrated circuits. Siloxene and siloxene derivatives may also be advantageously employed in lasers as laser-active material and in fluorescent lamps or tubes as luminescent material.