Abstract: Systems and methods are provided for dynamically modeling and depicting overall emissions of the aviation industry and changes thereto when taking into account, for example, traffic growth and introduction of sustainability strategies, such as new and/or improved technologies, an increase in operational efficiency, and carbon offsets. Using the dynamic tool described herein, users can define scenarios on how to reduce emissions through the introduction of different sustainability strategies, both statically and over time, analyze the impact of those strategies on emissions, and understand the dependencies between select strategies.

Abstract: The present inventions provide a portable, reliable open and go system for training, proctoring and procedure support during medical interventions, procedures and all manner of diagnostics extending access to care to those unable to reach other facilities, among other things. The Envisimed™ brand of system brings near zero latency Cross Reality (X-Reality/XR) technology to medical procedure support and remote collaboration, extending the reach of global health-care equity past the institutional settings that are not available to all.

Abstract: A compressor (1) has a cast compressor casing (2) with an inlet port (3) oriented in an axial direction (AR), an intake chamber (4) with an impeller, a volute (5) and a pressure port (6) connected consecutively. The volute (5) orbits the intake chamber (4) and the pressure port (6) extends tangentially outwards from the volute (5). In the compressor casing (2), an air recirculation duct (7) has a suction-side duct (12) and pressure-side duct (13), which is connected to the inlet port (3) at a pressure connection point (13a) downstream of the impeller and downstream of a tongue formed by the volute (5) on an outer wall of the pressure connection (6) facing the volute. The suction-side duct (12) is connected to the inlet port (3) at a suction connection point (12a) upstream of the impeller.

Abstract: A catheter with a film composite structure. The catheter at least includes a polymer film that is shaped such that a first polymer film layer, which is arranged inwardly relative to the catheter, and a second polymer film layer, which is arranged outwardly relative to the catheter, are produced; one or more electrodes arranged at least partially on an outer surface of the film composite structure; and a conductor structure, which includes conductive tracks for the electrical connection of the electrodes and which is arranged at least in part between the first and second polymer film layers. An associated production method for the catheter is also contemplated herein.

Abstract: A circuit substrate of an extremely high frequency electronic component having an organic substrate material and at least one hollow space incorporated into the substrate material, the hollow space being provided, on at least part of its peripheral surfaces, with a metal layer and acting as a hollow waveguide for electrical signals with a carrier frequency of 10 GHz or higher, and being directly adjacent to an active component part, and thereby being electrically connected with such an active component part, or being electrically connected with it through a metal lead, in particular a strip line projecting into the hollow space.

Abstract: A stretchable electrode conductor arrangement for a medical implant, this stretchable electrode conductor arrangement having at least one zigzag or meandering conductor track on an insulating support with an insulating cover that is tightly connected with the support, embedding the conductor track, the support having an essentially non-stretchable material and being cut in a zigzag or meandering pattern to adapt it to the contour of the conductor track(s).

Abstract: An aerofoil wing with a main aerofoil, a high-lift flap movably arranged on the aerofoil wing by adjustment mechanisms. Each of the adjustment mechanisms including a first adjustment lever hinged to the main aerofoil via a first rotary linkage, with the formation of a first axis of rotation, a second adjustment lever hinged to the high-lift flap via a second rotary linkage, with the formation of a second axis of rotation, and a central linkage, with the formation of a third axis of rotation, such that the first, second and third axes of rotation pass through a common pole. The aerofoil wing further includes a drive device with a drive module mounted on the main aerofoil, and movable with respect to the drive module a drive lever coupled to the high-lift flap, and a stop device to limit the maximum extended setting of the high-lift flap.

Abstract: A catheter with a film composite structure. The catheter at least includes a polymer film that is shaped such that a first polymer film layer, which is arranged inwardly relative to the catheter, and a second polymer film layer, which is arranged outwardly relative to the catheter, are produced; one or more electrodes arranged at least partially on an outer surface of the film composite structure; and a conductor structure, which includes conductive tracks for the electrical connection of the electrodes and which is arranged at least in part between the first and second polymer film layers. An associated production method for the catheter is also contemplated herein.

Abstract: An aerofoil wing is provided, including a main aerofoil, and a high-lift flap, which is movably arranged on the wing using side-by-side adjustment mechanisms. Each adjustment mechanism includes a first adjustment lever, hinged to the main aerofoil via a first rotary linkage, forming a first rotation axis; a second adjustment lever, hinged to the high-lift flap via a second rotary linkage, forming a second rotation axis; and a central linkage, linking together the first and the second adjustment levers, forming a third rotation axis. The first, second and third rotation axes pass through a common pole. The wing has a drive device with a drive module mounted on the main aerofoil, and movable with respect to the drive module a drive lever, which is coupled to the high-lift flap. The wing has a stop device to limit the maximum extended setting of the high-lift flap.