Abstract: A corrector has a strength of a central hexapole field (?HP2) which is selected such that the threefold axial astigmatism (A2) vanishes and the strengths of two equal outer hexapole fields (?HP1,3) are selected such that the overall corrector (5) does not have a sixfold axial astigmatism (A5). The length (L) of the central multipole element (2) in relation to the lengths (L?) of the multipole elements (1 and 3) is chosen such that the axial three-lobed aberration of sixth order (D6) vanishes. A separation between the outer multipole elements (1 and 3) and round lenses (7?, 8?) further spaced apart from a symmetry plane (6) of the corrector corresponds to the focal length (f?) of those round lenses (7?, 8?) plus an additional separation (?z) which is chosen such that the axial three-lobed aberration of fourth order (D4) vanishes for the given lengths L and L?.

Abstract: Systems and methods are provided for acoustic echo canceling. In one embodiment, a system for canceling acoustic echoes comprises one or more microphones configured to pick up sound generated by a sound source and transferred from the sound source to the one or more microphones via one or more unknown transfer paths having one or more unknown transfer functions, and to provide one or more electrical microphone signals therefrom, one or more adaptive filters for approximating the one or more unknown transfer functions with one or more estimated transfer functions and filtering one or more electrical signals representative of the sound generated by the sound source with the one or more estimated transfer functions to provide one or more estimated signals therefrom, and a microphone calibration block configured to individually attenuate or amplify the one or more electrical microphone signals dependent on the one or more estimated transfer functions.

Abstract: A shift signal transmitter for a manual transmission of a vehicle, in particular of a motorcycle, includes a shift rod for force-transmitting coupling to a foot lever, optionally with the interposition of an extension rod. The shift rod is guided along its longitudinal axis in an axially displaceable manner between two axial stops in an, in particular sleeve-shaped, housing. A connecting piece, which serves for coupling to a shift lever, is rigidly connected to the housing opposite to an internal axial end of the shift rod. A distance sensor for contact-free distance measurement is disposed within the housing opposite to the internal axial end of the shift rod and a sensor area of the distance sensor is oriented radially relative to the longitudinal axis. A shift apparatus for a manual transmission of a vehicle is also provided.

Abstract: An antenna device (1) for emitting electromagnetic waves has a waveguide (2), which in turn has two plates (3) made of an electrically conductive material and arranged parallel to one another, between which a dielectric material is arranged. The antenna device (1) has a feed-in device (4), with which electromagnetic waves can be coupled into the waveguide (2), which then propagate along the waveguide (2) and are emitted at an edge (5) of the waveguide (2) at a distance from the feed-in device (4). According to the invention, using a control device of the antenna device (1), the dielectric material can be influenced in such a way that a first region (9) having a first permittivity and at least one second region (10) having a second permittivity are formed, such that the electromagnetic waves coupled into the waveguide (2) propagate preferably through the first region (9) and are emitted in this preferred propagation direction (11).

Abstract: Techniques are provided to more accurately determine reflected power, reflection coefficient, and/or voltage standing wave to permit prompt protection of components such as power amplifiers and notify communication system operators. This is accomplished by more accurately determining an amplitude and phase of an output reflected signal at an output port of a bidirectional coupler as a function of the following: an amplitude and a phase of a coupled forward signal coupled into a forward coupled port of the bidirectional coupler; an amplitude and a phase of a coupled reverse signal coupled into a reverse coupled port of the bidirectional coupler; an electrical transmission parameter from an input port of the bidirectional coupler to the forward coupled port; an electrical transmission parameter from the input port to the reverse coupled port; and an electrical transmission parameter from an output port of the bidirectional coupler to the reverse coupled port.

Abstract: The invention relates to a propellant cage (10) for an inflator, especially for a tubular inflator of an airbag module, comprising a substantially tubular base (11) which forms, on the one hand, a gas inlet opening (12a) and, on the other hand, a gas outlet opening (12b) along its longitudinal axis (L), wherein at least one lateral gas flow opening (13) is configured in a circumferential wall (12) of the base (11), wherein the base (11) includes a radially outwardly extending collar (11c) having at least one frontal gas flow opening (14) in the area of the gas flow opening (12c).

Abstract: The invention relates to EPI lighting which allows transmitted light-bright field- or transmitted light-dark field-imaging or phase contrast imaging of a microscopic sample. For this purpose, a flat reflector is used which is located opposite the observer side and which brings about a deflection of the illumination beam of light. The flat reflector has a plane normal and an effective perpendicular which differs from the plane normal, or it is in the form of a retroreflector.

Abstract: In a method for thickening a plastically deformable hollow body wall of a hollow body, with effective radial support of the unthickened hollow body wall on an outer supporting face of an outer mold and with effective radial support of the hollow body wall on an inner supporting face of an inner supporting body, the hollow body is acted on by a compressive force by two application members at application points by moving the application members towards one another in the axial direction with a compressing movement. The application points on the hollow body are distanced from one another in the axial direction. An expansion space of the outer mold is arranged between the application points.

Abstract: A stackable system container having a base part, with a respective coupling device for connection to a further system container fastened on two opposite side walls of the base part such that it can be moved between a rest position, in which the coupling device can be disengaged from a further system container, and a coupling position, in which the coupling device can be engaged with the further system container. In order to provide for structurally identical system containers to be stacked optionally in a dimensionally stable, interconnected manner or separately, and therefore such that they can easily be singulated, each coupling device is assigned a locking element, which locks the respective coupling device releasably in the rest position.

Abstract: The disclosed subject matter relates to a laser scanner for scanning a ground from a seaborne or airborne vehicle, comprising a scanning unit for emitting a fan-shaped scan pattern made of laser beams fanned out about a scan axis and for receiving the laser beams reflected off the ground and an evaluation unit connected to the scanning unit for evaluating the laser beams that are received. The laser scanner is characterized by a measuring unit that is designed to measure the height of the vehicle above ground, and an actuation device that can be anchored to the vehicle and that is connected to the measuring unit. The actuation device is designed to rotate the fan-shaped scan pattern of the scanning unit with respect to the vehicle about a first actuation axis that is different from the scan axis, depending on the measured height above the ground.

Abstract: An aircraft beacon light is provided for emitting flashes of red light into an environment around an aircraft. The aircraft beacon light includes a support plate having a central portion; a plurality of LEDs, arranged on the support plate around the central portion and facing away from the support plate; an annular light splitting element, having a proximate side arranged over and facing the plurality of LEDs, wherein the proximate side has reflective portions and transmissive portions; and at least one light conditioning element for redirecting light having passed through the transmissive portions of the proximate side of the annular light splitting element.

Abstract: A combustion chamber assembly unit for a fuel-operated vehicle heater includes a combustion chamber housing (14) elongated in a direction of a housing longitudinal axis (L), with a combustion chamber (16) radially outwardly bounded by a circumferential wall (18), and with a combustion chamber bottom (20) axially delimiting the combustion chamber (16). A combustion air feed volume (36) is provided that is open to the combustion chamber (16) via a plurality of passage openings (38). A cooling medium feed device (46) is provided for feeding a liquid cooling medium to the combustion air feed volume (36).

Abstract: A device for cultivating plants is provided, comprising a watering device, an illuminating device, one or more seed mats, and a control unit configured to control the watering device and the illuminating device by means of a program controller, wherein the program controller comprises watering data and illuminating data which is individually matched to the one or more seed mats.

Abstract: The invention relates to a method for pitch angle measurement and/or for constructing a pitch angle measurement system on a rotor blade (100) of a wind turbine, the rotor blade comprising a blade root (114) and extending along a longitudinal blade axis (180). The rotor blade is rotatably mounted, by its blade root (114), to rotate about the longitudinal blade axis (180), on a rotor hub (20) of the wind turbine, the rotor hub rotating or being rotatable about a rotor axis (36). At least one chord line direction indicator (430) is firmly connected to the rotor blade (100) at a distance from the blade root (114), and defines a chord line direction indicator direction (160) indicative of a direction of a chord line (140) of the rotor blade (100) at the location of the chord line direction indicator (430).

Abstract: The present disclosure describes devices, systems, and methods for synchronizing multiple-input/multiple-output (“MIMO”) signals or other signals in telecommunication systems. Some aspects may involve transmitting signals between a head-end unit and remote units of a telecommunication system. A first delay of a signal path between the head-end unit and a first remote unit of the remote units may be determined to be greater than each delay of signal paths between the head-end unit and other remote units. Based on the first delay, the telecommunication system may be configured to delay transmission of additional signals such that the additional signals are simultaneously transmitted to another unit by either the head-end unit or the remote units.

Abstract: Domestic data are transmitted in the form of data messages from a data source to a memory in an unsynchronized manner in time slots via a freely accessible and accordingly heavily used transmission channel. On account of the interfering influences on the long data messages which occur in this case, the transmission of the data messages must be repeated several times until a data message is received without interference once. A comparator is used to determine a packet error rate from the ratio of the number of data messages received without interference over a certain period to the number of data messages actually transmitted during the period. A predefined packet error rate can be adaptively complied with despite varying transmission circumstances by varying the repeated transmissions per unit time.

Abstract: Communicating between components that are part of an IP network and a control device includes coupling the IP network to a dedicated cellular network, the control device communicating directly with network components of the dedicated cellular network, and transferring data between the components and the control device at a quality of service levels that corresponds to a quality of service level provided for voice communications in a non-dedicated cellular network. The IP network may include a cloud having core services that provide control signals to the control device. Quality of service parameters may be prioritized by an ICS management component of the core services of the cloud. The ICS management component may provide cellular network services parameters that are used to control the core services of the cloud and the quality of service parameters. A subset of resources of the dedicated cellular network may be reserved for industrial control systems.

Abstract: Securely deploying a software component to a control device of an industrial control system includes generating a first validation credential and a second validation credential corresponding to the first validation credential. The second credential is installed on the control device. A digital signature or a hash value is generated using the first validation credential and is associated with the software component, which is transmitted with the digital signature or the hash value to the control device. The digital signature or the hash value is validated using the second validation credential. In response to the digital signature or the hash value being valid, the software component is installed on the control device. The first validation credential may be generated and stored within a hardware security module and may be inaccessible from outside of the hardware security module. The second validation credential may be derived from the first validation credential.

Abstract: In various embodiments, an apparatus for growing plants is provided. The apparatus may include an irrigation apparatus, an illumination apparatus, a climate control device, an accommodating space for accommodating one or more seed mats, a controller which is configured to control the irrigation apparatus, the illumination apparatus and the climate control apparatus by means of a program controller, at least one air humidity sensor for determining an air humidity in the accommodating space, and at least one temperature sensor for determining an air temperature in the accommodating space.

Abstract: An exterior aircraft light comprises at least one switchable illumination circuit. Each of the at least one switchable illumination circuits comprises at least one light source, a temperature detector configured for detecting the temperature of the at least one light source and providing a temperature signal, an electric switch for selectively switching power flow to the at least one light source on and off, and a control circuit which is coupled to the temperature detector and to the electric switch. The control circuit is configured for driving the electric switch based on the temperature signal provided by the temperature detector to repeatedly switch power flow to the at least one light source on and off.