Abstract: The integration of a hinged door with a door leaf in a non-pressurized aircraft. The non-pressurized aircraft includes a canopy frame with a canopy frame cross-section profile. The canopy frame cross section profile has first and second canopy frame faces that are arranged at a predetermined angle relative to each other, and a third canopy frame face that is arranged between the first and second canopy frame faces. The non-pressurized aircraft further includes a hinge that is entirely arranged within the outline of the non-pressurized aircraft and pivotally mounts the door leaf to the third canopy frame face.

Abstract: The integration of a hinged door with a door leaf in a non-pressurized aircraft. The non-pressurized aircraft includes a canopy frame with a canopy frame cross-section profile. The canopy frame cross section profile has first and second canopy frame faces that are arranged at a predetermined angle relative to each other, and a third canopy frame face that is arranged between the first and second canopy frame faces. The non-pressurized aircraft further includes a hinge that is entirely arranged within the outline of the non-pressurized aircraft and pivotally mounts the door leaf to the third canopy frame face.

Abstract: A hospital or laboratory network including analytical devices for performing in-vitro diagnosis and a gateway is proposed. The network is configured to send a data package request including information regarding the analytical devices from the gateway to a remote service platform, receive from the remote service platform information regarding available data packages, determine a selection of the available data packages to be downloaded from the remote service platform specific to the analytical devices in the network, request the selection of the available data packages from the remote service platform, download the requested selection of the available data packages from the remote service platform, and provide the requested selection of the available data packages to the analytical devices.

Abstract: A composite reinforcement component for an aircraft or spacecraft, including a first element assembly aligned in a first extension plane, and a second element assembly aligned in a second, perpendicular, extension plane, the second element assembly intersecting the first element assembly at an intersection of the first and second extension planes. The first and second element assembly each have a pair of staggered comb components. Each comb component includes a base and a plurality of rectangular protrusions extending coplanar from the extension planes of the respective element assembly. The rectangular protrusions form comb teeth of one comb component which are overlapping with comb teeth of the other comb component of the pairs of comb components. The comb teeth of the first element assembly are offset along the intersection by a single comb tooth width with respect to the comb teeth of the second element assembly.

Abstract: A composite reinforcement component for an aircraft or spacecraft, including a first element assembly aligned in a first extension plane, and a second element assembly aligned in a second, perpendicular, extension plane, the second element assembly intersecting the first element assembly at an intersection of the first and second extension planes. The first and second element assembly each have a pair of staggered comb components. Each comb component includes a base and a plurality of rectangular protrusions extending coplanar from the extension planes of the respective element assembly. The rectangular protrusions form comb teeth of one comb component which are overlapping with comb teeth of the other comb component of the pairs of comb components. The comb teeth of the first element assembly are offset along the intersection by a single comb tooth width with respect to the comb teeth of the second element assembly.

Abstract: A method and apparatus for early fault detection in a centrifugal pump equipped with a balancing device, where the balancing device has an axial gap and optionally at least one radial gap through which a balancing flow is conducted, and with a spring element which acts on the balancing device to hold open the axial gap. Reliable information regarding impending faults is obtained while largely using existing elements by measuring the deformation of the spring element (10, 14) during operation of the centrifugal pump (24), and starting from the pump characteristics of the centrifugal pump (24) and the spring constant of the spring element (10, 14), drawing a conclusion regarding the instantaneous operating state of the centrifugal pump based on the measured deformation.

Abstract: A method and apparatus for early fault detection in a centrifugal pump equipped with a balancing device, where the balancing device has an axial gap and optionally at least one radial gap through which a balancing flow is conducted, and with a spring element which acts on the balancing device to hold open the axial gap. Reliable information regarding impending faults is obtained while largely using existing elements by measuring the deformation of the spring element (10, 14) during operation of the centrifugal pump (24), and starting from the pump characteristics of the centrifugal pump (24) and the spring constant of the spring element (10, 14), drawing a conclusion regarding the instantaneous operating state of the centrifugal pump based on the measured deformation.

Abstract: A hydrophilized separator material includes a plurality of synthetic fibers impregnated with 0.01 to 10 g/m2 of at least one of an alkali hydroxide and an alkali carbonate. In addition, a method for manufacturing such a separator material as well as an alkaline cell or battery containing such a separator material.