Abstract: A method for operating a laser device (1), wherein an optical frequency comb can be stabilized and the frequencies of the modes thereof are describable by the formula fm=m×frep+f0, where frep is a mode spacing, f0 is an offset frequency and m is a natural number. At least one signal (S1, S2, S3, S4) is determined, which correlates with an actual value of a degree of freedom (F), wherein the degree of freedom (F) is a linear combination of the offset frequency f0 and the mode spacing frep of the frequency comb. The actual value of the degree of freedom (F) is set in a predetermined capture range (F) of a second control unit (40) using a first control unit (10) on the basis of the signal. As soon as the capture range (?Fcapture) of the second control unit (40) is reached, the second control unit (40) is activated and the actual value is regulated to an intended value (?Fintended) with the aid of the second control unit (40).

Abstract: The present invention provides a calibration adapter (1) for drilling resistance measuring devices (10) which have at least one drilling needle receptacle which is coupled to a drive, a drilling needle (15), a guide sleeve (12) with a drilling needle outlet opening and an apparatus for drilling resistance detection and output. The invention further provides a calibration apparatus and a drilling resistance measuring apparatus, and also a method for calibrated drilling resistance measurement. The calibration adapter (1) has a main body (3) which has a coupling apparatus (5) in order to be releasably fastened to the drilling resistance measuring device (10) upstream of the drilling needle outlet opening and a drilling needle passage channel (33) which extends through the main body (3) and which is designed in such a way that it is aligned with the drilling needle outlet opening in a fastening arrangement of the calibration adapter (1) to the drilling resistance measuring device (10).

Abstract: A bearing housing of an exhaust gas turbocharger may include an encircling and inwardly open groove arranged in the bearing housing. The bearing housing may also include a housing cover that may have at least one forming portion formed plastically into the groove. The housing cover may be secured on the bearing housing via the at least one forming portion.

Abstract: The invention relates to a laser scanning device for mounting on the roof rack of a vehicle, comprising a base support, which is configured as an “X”, can be mounted on a roof rack and on which a laser scanning module that spans the fork of the “X” can be fixed.

Abstract: Active noise control systems and methods are disclosed that include generating with a first sub-system, anti-noise that is configured to reduce or cancel noise occurring at a listening position. Generating with a second sub-system, anti-noise that is configured to reduce or cancel noise occurring at the listening position. The first active noise control sub-system has a higher robustness than the second active noise control sub-system.

Abstract: A dimmable LED light unit, in particular for a passenger transportation vehicle, such as an aircraft, a road vehicle, a ship or a rail car, is disclosed that comprises a power input adapted to receive electrical power from a power source, at least one LED, and an LED drive and control module coupled between the power input and the at least one LED, wherein the LED drive and control module is adapted to receive an LED control signal indicative of a desired light intensity of the dimmable LED light unit.

Abstract: A microwave filter comprises at least one resonant filter element resonating at a resonant frequency and having a housing, a resonant filter cavity arranged in the housing and a resonator element arranged in the housing. At least two tuning elements are arranged on the housing of the resonant filter element and each extend into the cavity with a shaft portion, wherein the two tuning elements are movable with respect to the housing to adjust the length of the shaft portion extending into the housing and wherein the at least two tuning elements are constituted and designed such that by adjusting the length of the shaft portion of each tuning element extending into the housing a temperature drift of the resonant frequency is adjustable.

Abstract: An inflator (10), especially for a vehicle safety system, includes a combustion chamber (16) in which a solid propellant (18) combustible under the generation of gas is accommodated, and a compressed gas chamber (24) containing compressed gas (26), wherein even in the non-activated state of the inflator (10) a fluid communication exists between the combustion chamber (16) and the compressed gas chamber (24). The compressed gas (26) contains at least one inert gas as well as oxygen and at least one combustible gas, wherein the combustible gas is provided at a concentration at which no self-supporting conversion of the combustible gas with oxygen takes place.

Abstract: An erosion detector for an exterior aircraft lighting device is configured for detecting the state of erosion of an at least partially transparent cover of an exterior aircraft lighting device and includes: at least one light source, which is configured for radiating light onto the at least partially transparent cover; at least one light detection element, which is configured for detecting light reflected by the at least partially transparent cover and for providing a corresponding detection signal; and an evaluation unit, which is configured for evaluating the detection signal for determining the state of erosion of the at least partially transparent cover.

Abstract: Exemplary coating devices and exemplary coating methods for coating components with a coating agent, e.g., for painting motor vehicle body components with a paint, are disclosed. An exemplary coating device comprises an application device that applies the coating agent. The application device may include a paint head that discharges the coating agent out of at least one coating agent nozzle.

Abstract: Example apparatus and methods providing for the improved chemical conversion of the combustible components of a gaseous medium are disclosed. In some examples, the apparatus includes a guiding body that guides the flow of the gaseous medium within a reaction chamber of the apparatus. In some examples, the guiding body of the disclosed apparatus is configured to stabilize a residence period of the gaseous medium in the reaction chamber. In some examples, the guiding body results in a flow path of the gaseous medium within the reaction chamber being optimized and/or maximized, and/or results in a short circuit flow of the gaseous medium in the reaction chamber being suppressed. In some disclosed examples, the guiding body causes at least a portion of the flow path of the gaseous medium within the reaction chamber to take the form of a cyclone flow.

Abstract: A method for determining threshold signal power for a switching control module of a TDD switching sub-system includes setting a threshold signal power to a first value, wherein the threshold signal power is compared to a measured signal power of a downlink path signal of a telecommunication system from a measurement receiver; determining a first downlink signal time using the first value; adjusting the threshold signal power to a second value; determining a second downlink signal time using the second value; determining a difference between the first and second downlink signal times; when difference between the first and second downlink signal times does not exceed a predetermined threshold, determining whether the second downlink signal time corresponds to a valid downlink signal time; when second downlink signal time corresponds to a valid downlink signal time, setting a fixed threshold signal power for use during online operation of the switching control module.

Abstract: In one embodiment, a distributed antenna system comprises at least one master unit; at least one remote antenna unit coupled to the master unit and comprising a power amplifier to radiate a remote downlink radio frequency signal, the remote antenna unit further configured to receive a remote uplink radio frequency signal from at least one antenna, the remote downlink radio frequency signal comprises first and second downlink frequency bands and wherein the remote uplink radio frequency signal comprises first and second uplink frequency bands; a band suppression module comprising: a controller; an uplink band suppression element configured to apply an attenuation to suppress the first uplink frequency band in response to a signal from the controller; and a downlink band suppression element configured to apply an attenuation to suppress the first downlink frequency band in response to the signal from the band suppression controller.

Abstract: In one embodiment, a distributed antenna system comprises: at least one master unit; at least one remote antenna unit communicatively coupled via a switch to the master unit by a primary cable and a secondary cable both coupled to the switch, the remote antenna unit comprising a compensating link check module that outputs a control signal to the switch, wherein the switch selects between the primary and secondary cable in response to the control signal; wherein the compensating link check module controls the switch to momentarily select the secondary cable to perform a link check during which the remote unit measures a quality metric of a downlink signal received via the secondary cable; and upon initiation of the link check, the compensating link check module adjusts an attenuation of the downlink signal received on the secondary cable by loading calibration settings for the secondary cable into a compensation attenuator.

Abstract: A rudder blade is provided with a rudder blade hub, which, in comparison to rudder blades known from the prior art, has a lower overall weight and can be produced with a reduced outlay on materials and costs, while simultaneously ensuring a sufficiently high strength in order to be able to absorb the large forces and torques acting during operation of the rudder blade and to be able to conduct them away to a rudder stock. The rudder blade includes a leading edge, a trailing edge, a first side wall and a second side wall lying opposite the first side wall, and a rudder blade hub, which is arranged in a connection space, for connecting a rudder stock. The rudder blade hub has a hub body including an inner bore for receiving the rudder stock, and a hub outer surface running in the circumferential direction, for the hub outer surface to be entirety spaced apart from an inner side of the first side wall and from an inner side of the second side wall.

Abstract: The invention relates to a cable winch (100) for an aircraft or vehicle. The cable winch (100) has a central module (110), which can be or is attached to the aircraft or vehicle. The central module (110) is shaped in such a way that the central module can he or is mechanically connected to at least one further module (120, 130, 150, 160) of the cable winch (100) in a manually detachable manner by using at least one fastening device. The cable winch (100) also has a capstan drive module (120) for drawing a cable into the cable winch (100) and for letting the cable out of the cable winch (100). The capstan drive module (120) is shaped in such a way that the capstan drive module can be or is mechanically connected to the central module (110) in a manually detachable manner by using the at least one fastening device. The cable winch (100) also has a cable-winding module (130) for holding the cable by winding and unwinding the cable.

Abstract: An apparatus (10) blocks and adjusts a pressure for a hydraulically controllable actuator (12), particularly a lifting unit (16) of a machine (18). The apparatus (10) allows a working chamber (20, 22) to be selectively connected to a pressure supply unit (94) having a storage device (34) or to a discharge end (66), in particular a reservoir end, by a valve unit (38). In a controlling position of the valve unit (38), when the storage pressure in the storage device (34) is greater than the working pressure in the working chamber (20) of the actuator (12), the storage pressure is relieved in the direction of the discharge end (66) until the working pressure has been reached.

Abstract: A temperature control unit includes a ring-shaped magnetocaloric material temperature control body (28) over which heat transfer medium can flow, a rotatable temperature control body receiving housing (12), a temperature control body receiving space, temperature control sectors (I, II, III, IV) following each other in a circumferential direction, each with a cooling area (30) and a magnetic field heating area arranged next to the cooling area, in at least two adjacent temperature control sectors, a heat transfer medium circulation (40) from the magnetic field heating area of one sector to the cooling area of another sector and from the cooling area of the other sector to the magnetic field heating area of the one sector. In one sector, heat input fluid may flow through the cooling area—feeding heat into the sector or/and in one sector, heat discharge fluid may flow through the magnetic field heating area for discharging heat.

Abstract: The invention relates to a car park monitoring system for detecting free and occupied parking spaces in a car park area, comprising a detection unit and a camera system, the camera system being designed to supply image evidence from within the car park area, and the detection unit being designed to assign, depending on said image evidence, an occupation status to the parking spaces which indicates whether a parking pace is free or occupied. The car park monitoring system is characterized in that the detection unit is further designed to store the image evidence for at least one corresponding parking space as a first snapshot when the occupation status of the parking space in question changes from free to occupied, and additionally to store the image evidence as a second snapshot when a limiting condition is met.

Abstract: The invention relates to a painting booth for coating components, particularly for painting motor vehicle body components, with a booth wall (10) and a coating agent line (1), which runs from the exterior of the booth through the booth wall (10) into the interior of the booth. The invention proposes that the coating agent line (1) has an electrically conductive and axially running potential-compensating element (15) inside the line for electrically connecting the coating agent inside the line to an electrical reference potential, said potential-compensating element (15) extending from the exterior of the booth through the booth wall (10), so that the free end of the potential-compensating element (15) is inside the booth.