Abstract: The invention relates to a method and to a device for the energy management of a system having a number of components according to an economic market model approach. At least one of the components is characterized by a non-monotonic price-performance or price-power relation. By taking into consideration the non-monotonic price-performance or price-power relation, a realistic description of the at least one component is provided and thus used to improve energy management of the system.

Abstract: A method for operating a solar thermal power plant comprising multiple solar radiation receivers operated using a molten salt as the heat transfer medium, wherein each solar radiation receiver comprises a reflector device and an absorber tube, includes: preheating of the absorber tubes, in the state in which said tubes are empty of the molten salt, to a temperature T by concentrating solar radiation on the absorber tubes by means of the reflector devices, wherein the temperature T is greater than or equal to the melting temperature of the salt; after reaching the temperature T: introduction of the molten salt into the absorber tubes and recirculated conduction of the molten salt through the absorber tubes while simultaneously repositioning the reflector devices depending on the position of the sun; on ending the operation: release of the molten salt out of the absorber tubes.

Abstract: A reflector antenna for synthetic aperture radar, having a reflector including a reflector surface, a vertex, and an optical axis. The reflector antenna also as a plurality of antenna elements arranged side by side and in a row, for transmitting radar transmission signals and receiving radar reception signals produced from a reflection on a surface. The reflector is designed as a one-dimensional defocused reflector having two focal planes. The optical axis coincides with the line of inter-section of two imaginary planes extending at right angles to one another. The reflector has, in a first (X-) plane, a first (X-) focal plane that extends at right angles thereto and to the optical axis, and, in a second (Y-) plane, a second (Y-) focal plane which extends at right angles thereto and to the optical axis. The second (Y-) focal plane is at a greater distance from the vertex than the first (X-) focal plane.

Abstract: To connect conventional or laparoscopic instruments to a robot that can be used for medical applications, there can be a device that has a first and a second circular cylinder segment having a continuous center bore is connected with the angled first segment affixed to the free end of a robot arm. This connection can be by way of an articulated joint that can be rotated by 180°. On one end surface of the second segment, there can be a third segment in the form of a flange, having a bore that is coaxial with the continuous center bore in the second segment. There is also a rolling joint which can be used to allow the device to rotate. Around the bore of the flange, there can be supply technology and data technology connection elements and a locking mechanism for coupling end effectors on and off.

Abstract: The invention relates to a device and to a method for determining the position of a vehicle on or above a planet surface. The proposed device comprises a first means (101) for determining a first position (P1(t)) of the vehicle, a second means (102) for determining a movement direction (BR(t)) of the vehicle, a third means (103) for providing a number (n) of fixed point data, wherein the fixed point data specify, at least for significant radar objects (FROi) arranged in a stationary manner on the planet surface, the radar signature (RSFROi) thereof and the position (PFROi) thereof, where i=1, 2, . . .

Abstract: A method for the calculation of flight paths taking into consideration events of relevance for the radiation dose comprises the following steps: a) collection of radiation data for atmospheric radiation (10); b) examination of the radiation data and conclusion about an event of relevance for radiation dose generating a temporary increase in exposure; c) creation of a model using the radiation data, wherein the model contains at least one estimate of the geographical location of a region with a radiation intensity increased by the event of relevance for radiation dose; d) determination of flight-relevant parameters; e) calculation of a possible flight path in the light of the flight-relevant parameters taking into consideration the model created in step c), wherein the flight path is adjusted in respect of a reduction of exposure to radiation.

Abstract: The invention relates to a minimally invasive instrument comprising an enlargeable sensor head with a flat sensor element that has resilient properties. In order to enable an improved minimally invasive instrument, the sensor element comprises a film element with a first layer and with a second layer distanced from the first layer by means of spacers, wherein the sensor element comprises, arranged between the layers of the film element, expansion-sensitive, polymer-based resistance elements for picking up tactile stimuli.

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: The invention relates to a device for mounting an object to a structure in a vibration-free manner. The device has an elastic arrangement that supports the object at the structure in a stiff manner in the directions of at least two of the total of six translational and rotational degrees of freedom and in a soft manner in the directions of at least one of the total of six translational and rotational degrees of freedom. Main modes of motion of the object in the directions of the rigid support have natural frequencies that are higher than any main mode of motion of the object in any direction of the soft support at least by a factor of ten. The soft support is undamped, and a damping device is provided for any main mode of motion of the object in any direction of the soft support.

Abstract: A fin stabilizer for stabilizing a watercraft against rolling movements includes a main fin configured to be pivoted by a watercraft-side fin drive, a tail fin, and an elastically deformable connection between the main fin and the tail fin, the elastically deformable connection being configured to flex whenever a water force acting on the tail fin is greater than a predetermined amount.

Abstract: The present invention refers to a system for the metabolization of organic substances, comprising at least one housing with an elongated space. The housing has at least one inlet opening at the top end portion for the introduction of liquids with organic substances therein and at least one outlet opening for liquids at the bottom end portion. The inlet opening and the outlet opening are in communication with the elongated space, where the elongated space extends from the top end portion to the bottom end portion of the housing. Further, the system for metabolization comprises at least one planting opening provided on the housing between the inlet opening and the outlet opening for the accommodation of a support element for plants, the planting opening being in communication with the elongated space, and a porous filler material provided in the elongated space.

Abstract: The invention relates to an Automatic Identification System (AIS) ship's transceiver for sending and receiving AIS radio signals, wherein the position can be taken as a basis and/or adjacent ships can be taken as a basis for activating or deactivating the emission of AIS radio signals of a second AIS radio signal type for satellite-assisted monitoring.

Abstract: The invention relates to an AIS ship transceiver which, after reception of an AIS base station message, validates the transmitting AIS base station and activates or deactivates the emitting of AIS radio signals in dependence on the validation.

Abstract: The invention relates to a liquid jet scalpel comprising a nozzle (12) for discharge of pressurized liquid (14) in the direction of tissue (16) that is to be manipulated, and a distance measuring device (18) for measuring the distance between the nozzle (12) and the tissue (16) that is to be manipulated. The invention further relates to a method for operating a liquid jet scalpel.

Abstract: The present invention relates to a process for performing a chemical reaction consisting of at least two sequential reversible steps characterized by being performed in a cycle, and to a reactor for performing such process.

Abstract: A method for the calculation of flight paths taking into consideration events of relevance for the radiation dose comprises the following steps: a) collection of radiation data for atmospheric radiation (10); b) examination of the radiation data and conclusion about an event of relevance for radiation dose generating a temporary increase in exposure; c) creation of a model using the radiation data, wherein the model contains at least one estimate of the geographical location of a region with a radiation intensity increased by the event of relevance for radiation dose; d) determination of flight-relevant parameters; e) calculation of a possible flight path in the light of the flight-relevant parameters taking into consideration the model created in step c), wherein the flight path is adjusted in respect of a reduction of exposure to radiation.

Abstract: The device for receiving signals which have carrier frequencies and codes, said signals being navigation or communication signals, has multiple individual antennas (114) for receiving a signal, each individual antenna (114) having an antenna output (116) at which the received signal is present. Furthermore, the device is provided with an analog preprocessing unit (122) for preprocessing the signals received by the individual antennas (114), said preprocessing unit (122) having signal transmitting and signal preprocessing channels (124) which are assigned to the individual antennas (114), and the device is provided with a digital signal processor (134). The device additionally has a calibration signal generating unit (148) for generating a calibration signal which, like the signals received by the individual antennas (114), has a carrier frequency and a code and which is used for calibrating the propagation time and the phase of the signal transmission paths.

Abstract: AltBOC-modulated satellite navigation signals transmitted in the two partial bands E5a and E5b of the so-called E5 frequency band are received using a common antenna (19) and thereafter are processed separately in an analog manner in the HF front-end in two physically different incoming signal paths for the two partial bands and then digitized and coherently summed to form a complete digital E5 band signal, which is fed to a digital signal processor, in which code acquisition and code tracking are performed using PRN reference code sequences produced in the receiver and tracking of the carrier phase is performed and raw data for the final navigation calculation are determined therefrom.

Abstract: Minimally invasive instrument for robotic surgery including a functional element, a force, torque and/or pressure transmission device for transmitting force, torque and/or pressure from a drive to the functional element, a coupling device for coupling the instrument to a medical robot such that the functional element can be actuated by the drive, wherein an operating element for manually operating the functional element in a state in which the instrument is uncoupled from the medical robot.

Abstract: A force/moment sensor for measurement of three orthogonal forces and three orthogonal moments, comprises an inner holding element which is surrounded by an outer holding element. The two holding elements are connected to each other by deformation elements. For each deformation element, at least one deformation transducer is provided. The force/moment sensor is preferably monolithic, and the deformation transducers, formed as strain gauges, are preferably arranged in one plane or in two preferably parallel planes.