Abstract: Method of producing a gas-tight solid electrolyte layer for a high-temperature fuel cell, wherein a layer is produced from a metal oxide material and metal particles are incorporated in the layer during production of the layer, the metal particles being oxidizable, and wherein the metal particles are subsequently oxidized.

Abstract: A carrier device for an electrochemical functional unit is provided, comprising a frame unit consisting of an electrically conductive material and at least one window area which consists of an electrically conductive material and is integrally formed on the frame unit, wherein the at least one window area is produced from a porous material and is permeable to gas via its porosity and wherein the frame unit is impermeable to gas in its solid material.

Abstract: The subcarriers in an OFDM communication system or OFDM-based multicarrier communication system are multiplied with weighting factors, determined so that in accordance with an optimization criterion the side lobes are minimized in a determined frequency domain. In determining the weighting factors constraints can be taken into account to further boost system power output.

Abstract: A ceramic armoring is provided, comprising a first ceramic layer which has a plurality of segments that are functionally separated by crack stoppers, wherein the crack stoppers serve to prevent cracks propagating from one segment to another segment, at least one second ceramic layer which has a plurality of segments that are functionally separated by crack stoppers, and at least one bonding layer by means of which the first ceramic layer and the second ceramic layer are joined together, wherein the segments of the first ceramic layer are offset with respect to the segments of the second ceramic layer.

Abstract: A wing for of aircraft has a wing tip shape that has a profile that extends in the direction of the span of the wing, and across the direction of the span of the wing extends from the wing leading edge to the wing trailing edge. The profile is delimited by a first skin and a second skin, with a winglet, arranged on the wing end. The winglet is substantially planar, and has a transition region arranged between the wing and the winglet, that extends from a connection on the wing to a connection on the winglet. The curvature of the local dihedral can increase in the transition region from a low level or a level of zero at or near the wing intersection in the outboard direction.

Abstract: A tool for a resin transfer moulding method comprises a cavity, a resin trap and a transition region, wherein the cavity is designed such that a component can be accommodated in it. Furthermore, the resin trap is integrated in the tool, and the transition region is designed such that with it a connection between the cavity and the resin trap can be established.

Abstract: An assembly for wireless energy communication to an implanted device comprises an external belt (7) accommodating a wearer control (1) followed by controller (2), a battery pack (4), an inverter (3), a transmission coil (8) connected in parallel by a plurality of capacitors, and an infrared transceiver 9. Provided furthermore is an implanted device comprising a receiver coil (11) having the same dimensions as the transmission coil (8), a rectifier following said receiver coil (11), an infrared transceiver (10) followed by a controller and an sensor assembly (17) assigned thereto as well as a battery pack (16) for powering said implanted device via an energy manager (14).

Abstract: In a method for controlling a robot arm, which is particularly suitable for use in medical applications, a robot arm (10) with a redundant number of joints is used. A torque acting in at least one joint (12a, 12b) is sensed. By means of a control device, the torque acting in this joint (12a, 12b) is controlled to become substantially 0.

Abstract: The invention relates to a method for automatically generating graphic display instruments for measured, regulation and/or control values, comprising the following steps: a) selection of a display instrument type; b) dynamic calculation of reproduction positions for reading-aid information in accordance with the type of display instrument that has been selected and with defined parameters; c) generation of the selected display instrument with the reading-aid positions in the calculated reproduction positions by means of respective classified generation objects; and d) display of the measured, regulation and/or control values in conjunction with the generated display instrument on a display.

Abstract: A method is provided for controlling the alignment of a heliostat with respect to a receiver, wherein an image sensor device is arranged on a mirror device of the heliostat, wherein the heliostat is aligned by the image sensor device using image recognition in such a way that a first angle of a first vector pointing towards the sun, relative to a prescribed vector of the mirror device, and a second angle of a second vector pointing towards a prescribed target area of the receiver, relative to the prescribed vector, are in a relationship to each other which is dependent upon the prescribed vector of the mirror device, and wherein images of the sun and the prescribed target area and their position relative to the prescribed vector are determined.

Abstract: For the detection of geotectonic signals triggered by a geotectonic event, an infrasonic wave accompanying the geotectonic event and being generated at the ground and temperature fluctuations are utilized, causing a modulation of an airglow. The modulation of the airglow is detected from the ground by means of an infrared spectrometer and the mesopause temperature is measured with a high temporal resolution. For the detection of a geostationary event, a number of simultaneously operated infrared spectrometers is provided in regions sensitive to geotectonic events.

Abstract: Disclosed is an implantable two-chamber system for supporting the left ventricle of the heart. Each of the two pumping chambers (1, 1?) of the two-chamber system has the shape of a ventricular bag comprising an inlet (11) that is embodied at one end at an acute angle (a) to an outlet (12), directly next the outlet (12). Furthermore, a pressure plate (2) is rotatably mounted externally in two arms (5) which are movably retained on the output shaft (9) of a drive unit (15) such that the center of motion (8) of the arms (5), which lies on the output shaft (9), is located on the side of the pumping chambers (, 1?) facing away from adapters (4, 4?), and thus outside the pumping chambers (1, 1?). The angle between the inlet (11) and the outlet (12) of each pumping chamber ranges from 30° to 60°. The maximum width in the inlet and outlet zone of each of the pumping chambers (1, 1?) amounts to about 65 to 72 percent of the length of the respective pumping chamber.

Abstract: The Method for transmitting a signal from a transmitter in an area around the transmitter via a satellite comprising the steps of transmitting a first signal having a first frequency from the transmitter to a satellite having a retrodirective antenna array comprising receiving antennas and transmitting antennas, receiving the signal transmitted from the transmitter by the receiving antennas of the retrodirective antenna array as first signals wherein the first signals received by the receiving antennas have a phase relation among each other defined by the geometric arrangement of the receiving antennas, and retrodirectively re-transmitting second signals from the transmitting antennas of the antenna array of the satellite in the direction towards the transmitter in the form of a beam with the transmitter located substantially in the center of the beam wherein the second signal has a second frequency different from the first frequency and wherein the phase relations among the second signal transmitted from

Abstract: This application describes a tool, an arrangement, and a method of manufacturing a component. The manufacturing of the component is achieved by a resin transfer from a storage chamber via a transfer line into a working chamber. Before the resin transfer, taking place, for example by a compressed air charging of the storage chamber, the storage chamber is filled with an amount of resin adjusted to the size of the component. furthermore, a semi-finished product, consisting of cut-to-size reinforcement fibers, is inserted into the working chamber that is adjusted to the form of the component to be produced. Storage chamber, transfer line, and working chamber are configured in a one-piece mould casing of the tool. The application further describes a component manufactured by the above-mentioned tool or by the above-mentioned method respectively.

Abstract: There is provided a method for controlling the combustion in a combustion chamber with a combustion space, wherein fuel in fluid form and oxidiser in fluid form are blown into the combustion space, in which at least one control jet is generated in the combustion space, which influences the flow of fuel and/or oxidiser in the combustion space, wherein the mass flow component of the at least one control jet lies between 1% and 7% of the total mass flow, the at least one control jet is generated such that it varies over time, the at least one control jet is generated by being blown in or extracted through one or more ports in a combustion chamber wall, which coincide with one or more ports for blowing in and/or extracting fuel and/or oxidiser, and the at least one control jet is generated so that a degree of swirl of the fuel flow and/or oxidiser flow is reduced by means thereof.

Abstract: In order to make a drive device available on the basis of a gel-type propellant, in particular, for a flying object, comprising at least one tank for gel-type propellant, a combustion chamber and a device for supplying propellant to the combustion chamber, which is of a simple construction it is suggested that at least one radiation impinging device be provided for acting on gel-type propellant with electromagnetic radiation and/or at least one heating device for heating gel-type propellant in order to improve the flow behavior

Abstract: In order, on the one hand, to achieve a high mechanical long-term stability of and, on the other hand, to have the possibility of guiding a stream of gas, in particular, a stream of gas consisting of a reactive process gas through a heating block for an apparatus for the thermal treatment of a substrate, in particular, a semiconductor substrate, wherein the apparatus has a space accommodating the substrate and the heating block on at least one side of the space accommodating the substrate, the substrate being treatable thermally by means of the heating block in a mechanically non-contact manner, it is suggested that the heating block be designed as a fiber composite member, that the fiber composite member be designed with passages for a stream of gas passing through it from one flat side to the other flat side.

Abstract: In order to provide a method of operating a solar thermal power plant, in which a heat transfer medium is evaporated endothermally by solar radiation in an evaporator section, wherein the evaporator section comprises a plurality of evaporator branches, among which the heat transfer medium is distributed, in which method non-uniform radiation conditions of the evaporator section may be effectively taken into consideration, it is provided that the mass flow distribution at the evaporator section is controlled, wherein the mass flows are adjusted individually at all or a majority of the evaporator branches and a controlled variable is a variable characterizing a spatial energy rise in a respective evaporator branch in a region of the evaporator branch where the heat transfer medium has not yet evaporated.

Abstract: A temperature sensitive paint comprises a binder for forming a polymer matrix, a transition metal complex embedded in the binder and displaying a temperature dependent fluorescence, the fluorescence of the transition metal complex showing a maximum relative temperature sensitivity per Kelvin at a first temperature, and a rare earth complex also embedded in the binder and displaying a temperature dependent fluorescence, the fluorescence of the rare earth complex showing a maximum relative temperature sensitivity per Kelvin at a second temperature. The second temperature is higher than the first temperature by 50 to 150 Kelvin so that the overall temperature range covered by both complexes as temperature probes is extended.

Abstract: A method and a device for redundantly supplying several electric servomotors or drive motors by a common power electronics unit particularly in an aircraft, wherein the power electronics unit contains a number of electronic motor control units, and wherein the electric motors are operated with nominal power if the electronic motor control units are fully functional. The motors are operated with the available residual power of the motor control units if partial failure of the motor control units occurs. The motors may be operated sequentially or simultaneously.