Abstract: The invention relates to the use of a polysilazane solution which comprises a polysilazane of the formula 1 where n has been adjusted so that the polysilazane has a number-average molar mass of from 150 to 150 000 g/mol, and also comprises a solvent and a catalyst, as a primer for the coating of a surface with fluorosilanes or with fluorine-containing condensates.

Abstract: The invention relates to a phosphorus-containing flame retardant formulation for cellulose-containing moldings, comprising from 0.1 to 99.9% by weight of a resin of an organic nitrogen compound and from 0.1 to 99.9% by weight of a phosphorus-containing flame retardant.

Abstract: A supply device in a passenger cabin, such as an aircraft passenger cabin, includes a first panel or “function panel” having one or more comfort elements, operating elements, visual display elements, and communication elements; and a second panel or an “infill panel”, which includes flexible supply channels. The panels are guided and lined up in a rail system of a PSC channel that is arranged in the direction of flight above a passenger seat row. The function panels are individually positionable in the PSC channel relative to the passenger seat row, wherein the infill panel synchronously follows a linear actuating movement of the function panel, and in this process automatically compensates for the distance dimension S1 between function panels that are positioned so as to be spaced apart from each other.

Abstract: The invention relates to a process for preparing enantiomerically enriched aryl-aminopropanols and to their use and also to intermediates.

Abstract: A module for an aircraft having a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane. The frame device is adapted for attachment to the fuselage structure of the aircraft at a second location, wherein the second location is not in the floor plane.

Abstract: The present invention is an electronic device comprising a counter driven by an input clock signal for counting clock cycles and providing a count. A clock signal generating stage provides a first set of phase shifted clock signals having m different phases. The electronic device determines n least significant bits of the count of the counter from the logic states of the first set of m phase shifted clock signals.

Abstract: The invention is related to a process for preparing compounds of the formula IV by means of conversion of aromatic aldehydes of the formula I using ?-ketoximes of the formula II via N-oxides of the formula III to halomethyloxazoles of the formula IV, wherein R1, R2, R3, R4, R5, R6, R7, R8, X1, X2, X3, o, n1 and n2 are as defined herein.

Abstract: The invention relates to an aircraft with a connection element for connecting at least one first conduit element or the like positioned in a supply chamber of an aircraft with at least one second conduit element positioned in a cabin chamber of the aircraft, wherein supply chamber and cabin chamber are separated from each other by means of a separation element, substantially comprising a connection part comprising fastening elements for fastening the first and second conduit element. Known connection elements have the disadvantage that there occur sealing problems due to the fastening of the fastening element at the outside of the connection part at the end facing the cabin chamber. A further disadvantage is that the connection elements protrude into the cabin chamber and form stumble edges there.

Abstract: Nowadays in aircraft on-board inert gas generation systems (OBIGGS) are used to generate inert gases. Cooled bleed air of engines or auxiliary turbines is fed to said OBIGGS systems. According to an embodiment of the present invention, an air supply device for an OBIGGS system in an aircraft is proposed that comprises a bleed position (1,2). By way of the bleed position (1,2), air from an air conditioning unit (4,5) on board the aircraft can be bled and can be fed to the OBIGGS system. There is thus no need for an additional heat exchanger and an additional ram-air channel. Maintenance expenditure and air resistance are thus reduced.

Abstract: The present invention provides a method for operating and/or for controlling a man-machine interface unit (MMI) for a finite user group environment. Utterances out of a group of user are repeatedly received. A process of user identification is carried out based on said received utterances. The process of user identification comprises a set of clustering so as to enable an enrolment-free performance.

Abstract: Film-bitumen combination with at least three layers is used in particular as a membrane to cover roof areas. At least two film layers of the combination are made from different materials.

Abstract: A ski boot sole for cooperating with a ski binding to releasably hold the sole in the binding, the sole having a forward toe sole extending rearwardly from the front of the sole to a forward gap, a toe exterior insert in the forward gap which is located over a forward depression in the base of the ski boot, a central sole extending rearwardly from the front gap, a heel exterior insert located in a rearward gap over a rearward depression in the boot base and a heel sole extending from the rearward end of the rearward gap at least to the end of the boot. The foregoing boot sole is in combination with the base of the boot, and the base has forward and rearward recesses for receiving toe holders rotating about longitudinally extending axes and heel holders rotating about a transverse axis for releasably locking the respective toe exterior insert and heel exterior insert to the binding.

Abstract: An adjustable orifice (10) for use in an air conditioning system, in particular an aircraft air conditioning system, comprises a first orifice element (18) which has an orifice frame (20) as well as a first orifice area (22), wherein when the orifice (10) is assembled at a duct (12) of the air conditioning system the first orifice area (22) of the first orifice element (18) leaves open a part of a cross section of the duct (12) The orifice (10) also comprises a second orifice element (32) with a second orifice area (34), wherein when the orifice (10) is assembled at the duct (12) the second is orifice area (34) of the second orifice element (32) leaves open a part of the cross section of the duct (12).

Abstract: A flight guidance and navigation display (10) for a helicopter, includes a three-dimensional, semicircular flight guidance and navigation tunnel (12) to display a planned flight path of the helicopter; a circular surface (14), which is integrated in the flight guidance and navigation tunnel (12), which circular surface (14) includes a diameter that corresponds to that of the flight guidance and navigation tunnel (12), for displaying a longitudinal position within the flight guidance and navigation tunnel (12); a flight path prediction icon (16) for displaying a position of the helicopter relative to the flight guidance and navigation tunnel (12); and a command signal (18) that relates to the air speed, wherein via the command signal (18) a deviation from a reference speed that has been predetermined by flight planning is displayed.

Abstract: A method for interpolating a previous and subsequent image of an input image sequence, including: determining fidelity information for at least one motion vector that is descriptive for motion between a previous and subsequent image, wherein the fidelity information is descriptive for the level and accuracy of the motion, determining classification information for the at least one motion vector, wherein the classification information depends on the fidelity information, the classification information being descriptive for the motion type of the motion, and selecting an interpolation method in dependence of the determined classification information.

Abstract: A glass pane having at least one electrical functional element is provided. The functional element comprises at least one electrical conductor and at least one terminal area located at an end of the electrical conductor, wherein the electrical conductor and the terminal area are formed from an electrically conductive layer deposited on a surface of the glass pane. A terminal wire is connected to the at least one terminal area by a soldered joint by way of a metal block having a flat contact area, and the flat contact area is soldered on a corresponding terminal area. A method for forming such a connection is also disclosed.

Abstract: A user profile and/or the suggestions computed based thereon are obtained taking a special set of user features into account. The user features are defined to represent a typical general behaviour of an individual user in respect to the application where the user profile is used. In other words, for each application where a user profile is used a special set of user features are defined which are able to represent a typical general behaviour of an individual user. Based on these user features the weights in the list of word-weight pairs or weighted keywords which represents the user profile are computed or influenced during the creation of the user profile, and/or a mufti-user profile is split during the creation of an individual user profile from a mufti-user profile, and/or during specification of a suggestion a user history which is used to create the user profile, and/or the user profile, and/or the suggestion results are filtered.

Abstract: A system for improving the air quality in a pressure cabin of an aircraft comprises a recirculation air circuit by means of which a portion of the cabin air, referred to as recirculation air, is withdrawn from the pressure cabin, filtered and then recirculated into the pressure cabin. To increase the oxygen partial pressure of the air fed back into the pressure cabin, the quantity of recirculation air is passed wholly or partially through a nitrogen generator (52) which generates nitrogen and an oxygen-containing waste gas from the recirculation air supplied. The oxygen-containing waste gas of the nitrogen generator (52), together with any remaining quantity of recirculation air untreated by the nitrogen generator (52), is recirculated into the pressure cabin. The nitrogen generator (52), to which only recirculation air is supplied, utilises a pressure gradient existing in flight between the pressure cabin and the outside of the aircraft for nitrogen generation.

Abstract: The invention relates to a detector for measuring scattered light in liquids having a housing, a transparent, flexible tube for transporting liquid through the housing, a light emitter, and a light detector. Two parallel surfaces are formed in the housing, between which the tube is arranged such that two opposing tube walls are formed in a planar parallel manner. The light emitter is arranged in such a way that the optical axis thereof is perpendicular to the parallel surfaces of the first tube wall, and the light detector is adjacent to the light emitter, the optical axes of the light emitter and light detector forming an angle smaller than 90°. The invention also relates to a method for detecting the presence of blood and for the quantitative determination of biological marker substances, especially bilirubin, in solution, and to a device for treating blood containing the detector.

Abstract: An intermediate product for the manufacture of a hollow fiber-composite component having a shape and dimensions, includes a three-dimensional, hollow preform of reinforcing fiber material corresponding to the shape and the dimensions with a three-dimensional reinforcing fiber structure which is formed from at least one planar, single- or multi-layer blank of two-dimensional, web-like reinforcing fiber material matching the dimensions, and a closable total cross-sectional profile with at least two hollow chambers located adjacent to each other and separated from each other by a rib-like partition. The partition is formed by an overlap region of the at least one blank which is stitched in two dimensions by a compacting seam which fixes the shape and dimensions of the rib-like partition as well as its position relative to adjacent regions of the blank and prefixes, precompacts and reinforces the reinforcing fiber material in the region of the partition.