Abstract: A system for use during a surgical procedure includes a control unit configured to obtain a horizontal pelvic line (HPL) and a central sacral vertical line (CSVL); obtain a horizontal shoulder line (HSL) and an orthogonal midline (OM); compare the HPL and the CSVL with the HSL and the OM; determine an angle between the HPL and the HSL; and convert the angle to a patient position.

Abstract: An aircraft includes wings having integrated ducted fans. The integrated ducted fans each have a duct with a stiffness ring. Each stiffness ring is made up of stiffness boxes and circular-arc-shaped ring segments. The stiffness boxes can include first stiffness boxes and second stiffness boxes, and the first stiffness boxes and second stiffness boxes differ in terms of height.

Abstract: A method for producing a base body of a valve housing for a hydraulic control valve includes machining a front-side section of a control edge into an unmachined base body for the base body with a cutting process in a front-side machining step. In the cutting process, a cutting tool is guided from a coupling side through a machining valve pocket to the front-side section of the control edge.

Abstract: A dental lighting system (10) for selectively illuminating a treatment site (12) on a patient sitting on a treatment chair (14). The system includes at least one monitoring device (32, 32?) configured to determine characteristics of a treatment site (12) on a patient and at least one lighting unit (22, 24) configured to generate an illuminated area (34) onto the treatment site (12) by emitting a first light beam (36) in an upright state in which the treatment chair (14) is in an upright position and by emitting a second light beam (38) in a lying state in which the treatment chair (14) is in a lying position. The at least one lighting unit (22, 24) is configured to set a shape of the illuminated area (34) based on the characteristics of the treatment site (12).

Abstract: A method removes a follower plate of a device for transporting viscous material out of a barrel-like container. The device has the follower plate for closing the container, which is open at the top and has a container base and a container casing extending upwards from the base, the follower plate being movable toward and away from the base. A force measuring sensor measures a force exerted by a container onto a placement surface; the controller switches the ventilation mode to the lifting mode if the force exerted by the container onto the placement surface exceeds a first target force value; and the controller switches the lifting mode to the ventilation mode if the force exerted by the container onto the placement surface falls below a second target force value, and/or the at least one sensor measures the position of the container relative to a stationary point.

Abstract: A device and a method for identifying a motion pattern of a person that allow suitable feedback about an identified motion pattern to be produced in real time, to address the disadvantage that there is no provision for direct feedback to the person in the event of abnormal behavior being detected. This is achieved by virtue of a device for identifying a motion pattern of a person having at least one sensor for capturing motion parameters and at least one evaluation unit, which is couplable to the at least one sensor, for evaluating the motion parameters and for producing a motion pattern.

Abstract: A ducted fan for an aircraft includes a rotor-side fan and a stator-side duct that surrounds the rotor-side fan. The stator-side duct includes an inner wall facing the rotor-side fan and an outer wall averted from the fan. The ducted fan further includes a fastening device configured to support mounting of the ducted fan on a structural component of the aircraft. The fastening device includes a pin and a guide body. The guide body is configured to receive and guide the pin, the pin is insertable proceeding from the inner wall into a recess of the guide body, a first end of the pin protrudes relative to the outer wall, and the pin is configured to be mounted, via the first end, on a bearing of the structural component of the aircraft.

Abstract: A fifth wheel configured to reversibly couple a trailer to a tractor including a coupling plate configured to receive a journal element of the trailer and a bearing block configured to pivotably bear the coupling plate about a pivot axis, in particular about a horizontally extending pivot axis, at least one distance sensor being provided which determines a distance with respect to a reference surface, the at least one distance sensor and/or the reference surface being arranged as part of the bearing block or on the bearing block.

Abstract: A ducted fan for an aircraft includes a rotor-side fan and a stator-side duct that surrounds the rotor-side fan. The stator-side duct includes an inner wall facing the rotor-side fan and an outer wall averted from the fan. The ducted fan further includes a fastening device configured to support mounting of the ducted fan on a structural component of the aircraft. The fastening device includes a pin and a guide body. The guide body is configured to receive and guide the pin, the pin is insertable proceeding from the inner wall into a recess of the guide body, a first end of the pin protrudes relative to the outer wall, and the pin is configured to be mounted, via the first end, on a bearing of the structural component of the aircraft.

Abstract: A ducted fan for an aircraft includes a rotor-side fan and a stator-side duct that surrounds the rotor-side fan. The stator-side duct includes an inner wall facing the rotor-side fan and an outer wall averted from the fan. The inner wall and outer wall each includes at least one layer composed of fiber-reinforced plastic. At least two honeycomb cores are arranged between the inner wall and the outer wall, the at least two honeycomb cores abutting against one another in an axial direction of the ducted fan. The honeycombs of the at least two honeycomb cores extend at least substantially in a radial direction of the ducted fan. A first of the at least two honeycomb cores is, at least in a region of an abutting surface that adjoins another of the at least two honeycomb cores, enwound or encased by at least one layer composed of fiber-reinforced plastic.

Abstract: An aircraft includes wings with integrated ducted fans. The ducted fans each have a duct, and each respective duct is made up of inlet regions and outlet regions. Different ducts of different ducted fans can have different construction variants, but the outlet regions of respective ducts can be of identical or mirror-symmetrical shape with respect to one another in all construction variants.

Abstract: An aircraft includes wings having integrated ducted fans. The integrated ducted fans each have a duct with a stiffness ring. Each stiffness ring is made up of stiffness boxes and circular-arc-shaped ring segments. The stiffness boxes can include first stiffness boxes and second stiffness boxes, and the first stiffness boxes and second stiffness boxes differ in terms of height.

Abstract: An aircraft includes wings with integrated ducted fans. The ducted fans each have a duct with cutouts and a guide grille fitted into the cutouts. The guide grilles can be adhesively bonded into the cutouts. The ducted fans can have different construction variants of the duct, wherein the cutouts have a corresponding shape across all construction variants.

Abstract: A fastening device for fastening a prosthesis shaft to a prosthetic knee joint that has a proximal top part and a distal bottom part, which are mounted on one another to pivot about a prosthetic knee joint axis. The fastening device has a distal bracket for attachment to the bottom part or to a lower-leg tube. At least one strut extends in the proximal direction from the holder beyond the prosthetic knee joint axis and on the strut a receptacle is arranged proximally to the prosthetic knee joint axis for pivotally mounting the prosthesis shaft about a shaft pivot access. At least one force transfer element is fastened offset to the to the shaft pivot access at a proximal bearing point to transfer a pivoting movement of the prosthesis shaft. The force transfer element is coupled to the top part at a distal bearing point in such a way that a pivoting movement of the prosthesis shaft about the shaft pivot axis causes a pivoting movement of the top part about the prosthetic knee joint axis.

Abstract: A method removes a follower plate of a device for transporting viscous material out of a barrel-like container. The device has the follower plate for closing the container, which is open at the top and has a container base and a container casing extending upwards from the base, the follower plate being movable toward and away from the base. A force measuring sensor measures a force exerted by a container onto a placement surface; the controller switches the ventilation mode to the lifting mode if the force exerted by the container onto the placement surface exceeds a first target force value; and the controller switches the lifting mode to the ventilation mode if the force exerted by the container onto the placement surface falls below a second target force value, and/or the at least one sensor measures the position of the container relative to a stationary point.

Abstract: A device for conveying viscous material out of a barrel-like container which has a container base and a container shell which extends upward from the container base, having a follower plate for closing off the container. The follower plate having a material outlet opening and a ventilation opening. There is a pump for conveying the viscous material through the material outlet opening, and a ventilation device for introducing compressed air through the ventilation opening, and a lowering device for lowering the follower plate in the container. A discharge valve is provided which, in a first switching position, blocks a line which leads out of the first pressure chamber, and which, in a second switching position, opens the line for the purposes of discharging pressure medium out of the first pressure chamber.

Abstract: A device for applying a pasty mass having an at least two-component, curable adhesive or sealant includes a housing, a lance, which is accommodated in the housing and can be rotated about a longitudinal housing axis and in the interior of which a material supply channel extends to a lance tip bounding the lance in the axial direction for each component of the adhesive or sealant, and a rotary feed-through for introducing the component of the adhesive or sealant into the respective material supply channel through a jacket of the housing, wherein a closing valve is associated with each material supply channel, which closing valve can close the material supply channel at a valve seat.

Abstract: A face shield and light source assembly is disclosed wherein a light source is mounted to be pivotally movable independently of a face shield.