mhurhangee/ep-ind-claims huggingface dataset:
Capacitive information carrier in which information is encoded by an information pattern comprising a first and a second electrically conductive area on an electrically non-conductive substrate, wherein each conductive area comprises one or more sub-sections (2, 3), wherein said information is detectable by a capacitive touch screen comprising intersection points formed from driving electrodes and sensing electrodes characterized in that at least one sub-section of the second electrically conductive area connects at least two sub-sections of the first electrically conductive area and the at least two sub-sections of the first electrically conductive area cover at least two different intersection points of the touch screen when brought into contact with said touch screen, said two different intersection points of the touch screen corresponding to two different driving electrodes (5, 6) of the touch screen, wherein the capacitive information carrier is a self-grounding carrier due to the arrangement of the electrically conductive areas, self-grounding occurring when the driving electrode corresponding to one of said two different intersection points is active and the driving electrode corresponding to the other of said two different intersection points is inactive.
Washing device comprising a washing chamber housing enclosing a washing chamber and being provided with an access opening closable by an access door, a movement system arranged in the washing chamber and a drive unit for the movement system, characterized in that the washing chamber housing and the drive unit for the movement system are arranged in an interior space of an outer housing and that the interior space is connected to an exhaust air conduit discharging air from the interior space of the outer housing at least during operation of the washing device and conveying it to an external exhaust air conduit.
A camera module thin film heater, comprising: a first heating structure including a first electrode, and a first thin film heating body electrically connected to the first electrode and having a variable resistance corresponding to a heating temperature; a second heating structure insulated from the first heating structure, and including a second electrode, and the second thin film heating body electrically connected to the second electrode and having a variable resistance corresponding to a heating temperature; and an insulation member having an opening to insulate the first and second heating structures(525, 550) and exposing a portion of the first and second electrodes(510, 530), characterized in that the first electrode includes a first electrode pattern and a second electrode pattern overlapped with the first electrode pattern, the second electrode includes a third electrode pattern and a fourth electrode pattern overlapped with the third electrode pattern, and the first thin film heating body is interposed between the first and second electrode patterns(512, 514), and the second thin film heating body is interposed between the third and fourth electrode patterns(532, 534), and wherein the camera module thin film heater further comprises third electrodes disposed at an outside of the insulation member to be electrically connected to the second pattern of the first electrode and the fourth pattern of the second electrode through the opening. a second heating structure insulated from the first heating structure, and including a second electrode, and the second thin film heating body electrically connected to the second electrode and having a variable resistance corresponding to a heating temperature; and an insulation member having an opening to insulate the first and second heating structures(525, 550) and exposing a portion of the first and second electrodes(510, 530), characterized in that the first electrode includes a first electrode pattern and a second electrode pattern overlapped with the first electrode pattern, the second electrode includes a third electrode pattern and a fourth electrode pattern overlapped with the third electrode pattern, and the first thin film heating body is interposed between the first and second electrode patterns(512, 514), and the second thin film heating body is interposed between the third and fourth electrode patterns(532, 534), and wherein the camera module thin film heater further comprises third electrodes disposed at an outside of the insulation member to be electrically connected to the second pattern of the first electrode and the fourth pattern of the second electrode through the opening.
An agent for lightening keratinic fibers, containing, in a cosmetically acceptable carrier, at least one anionic, carboxylic-acid-containing surfactant, at least one non-ionic surfactant and at least hydrogen peroxide, the agent additionally containing at least one acylpyridinium derivative of formula, where R1 is a C 1 -C 6 alkyl group, a C 2 -C 6 alkenyl group, a C 2 -C 6 hydroxyalkyl group, a C 1 -C 6 alkoxy C 2 -C 6 alkyl group, a carboxy C 2 -C 6 alkyl group, an aryl C 1 -C 6 alkyl group, a heteroaryl C 1 -C 6 alkyl group, an aryl group or a heteroaryl group, R2, R3 and R4 are each, independently of one another, hydrogen, a C 1 -C 6 alkyl group, a halogen atom or a C 1 -C 6 acyl group, provided that at least one of the functional groups R2, R3 and R4 is a C 1 -C 6 acyl group, X- is a physiologically acceptable anion, characterized in that the agent contains at least one anionic, carboxylic-acid-containing surfactant which is selected from the alkyl glucoside carboxylic acids. R1 is a C 1 -C 6 alkyl group, a C 2 -C 6 alkenyl group, a C 2 -C 6 hydroxyalkyl group, a C 1 -C 6 alkoxy C 2 -C 6 alkyl group, a carboxy C 2 -C 6 alkyl group, an aryl C 1 -C 6 alkyl group, a heteroaryl C 1 -C 6 alkyl group, an aryl group or a heteroaryl group, R2, R3 and R4 are each, independently of one another, hydrogen, a C 1 -C 6 alkyl group, a halogen atom or a C 1 -C 6 acyl group, provided that at least one of the functional groups R2, R3 and R4 is a C 1 -C 6 acyl group, X- is a physiologically acceptable anion,
A fiber filament having a diameter of 5 μm to 25 μm and comprising a silicate-based glass composition, the glass composition comprising: 50-70 wt.% SiO 2, 0.01-10 wt.% P 2 O 5, 10-30 wt.% Na 2 O, 0.01-10 wt.% CaO, 0.01-10 wt.% MO, and 15-30 wt.% R 2 O, wherein MO is the sum of MgO, CaO, SrO, BeO, and BaO, and wherein R 2 O is the sum of Na 2 O, K 2 O, Li 2 O, Rb 2 O, and Cs 2 O, characterised in that the fiber filament further comprises: a biopolymer coating including at least one of: polylactic acid, polyglycolic acid, co-polymers thereof (PLGA), poly D,L-lactic acid (PDLLA), poly 3-hydroxybutyrate (P), alginate, polycaprolactone, or polyvinyl-alcohol. 50-70 wt.% SiO 2, 0.01-10 wt.% P 2 O 5, 10-30 wt.% Na 2 O, 0.01-10 wt.% CaO, 0.01-10 wt.% MO, and 15-30 wt.% R 2 O, wherein MO is the sum of MgO, CaO, SrO, BeO, and BaO, and wherein R 2 O is the sum of Na 2 O, K 2 O, Li 2 O, Rb 2 O, and Cs 2 O, characterised in that the fiber filament further comprises: a biopolymer coating including at least one of: polylactic acid, polyglycolic acid, co-polymers thereof (PLGA), poly D,L-lactic acid (PDLLA), poly 3-hydroxybutyrate (P), alginate, polycaprolactone, or polyvinyl-alcohol.
A tripod joint comprising an outer joint element having formed therein a number of elongated axially extending tracks that are distributed across the inner circumference thereof; an inner joint element having a number of radial axle journals that are distributed across the outer circumference thereof; at least a number of rollers that correspond to the number of axle journals, wherein each roller is pivotably held by a central bore hole on the associated axle journal and being in engagement with the elongated tracks, wherein the roller is displaceable in the associated track in the axial direction of the outer joint element; wherein each axle journal, on its circumference, has two outer, diametrically opposed ball end faces for engaging into the borehole; wherein the bore hole has a cylindrical part for engaging into the ball end faces for displaceably supporting the roller in relation to the axle journal, and at least a necked-down portion (9d, e) adjoining in an axial direction to form a constant junction on one side of the cylindrical part and engaging behind the associated ball end face to limit the displacement movement, and wherein the necked-down portion is arranged such that, in at least one position of the tripod joint, the necked-down portion (9d, e) abuts the axle journal, and characterized in that the roller comprises an outer ring, an inner ring comprising the bore hole, as well as rolling elements optionally arranged therebetween, that the outer ring, in relation to inner ring, is displaceable in an axial direction of the axle journal; and that the tripod joint is configured such that, at the latest at maximal bending of the tripod joint, the outer ring, in relation to the inner ring, is displaced in the axial direction of the axle journal, and the inner ring is displaced on the axle journal in relation to the position with non-bended tripod joint; and that, with increasing bending of the tripod joint from the non-bended position, initially the inner ring is displaced on the axle journal and subsequently the outer ring is displaced in relation to the inner ring in an axial direction of the axle journal.
Inerting device for one or several aircraft fuel tanks, which device includes at the least: - an inert gas generator supplied with purged air diverted from the engines and/or air drawn from the passenger compartment, - means of determining the inert gas requirement of the aircraft tank or tanks in real time during the use of the said aircraft, - means of regulating the flow rates of the inert gas generator, - means of controlled distribution of the inert gas to the various tanks and/or the various compartments of a tank and, - a control unit, on the one hand, capable of determining in real time a flow setting for the inert gas generator according to the inert gas requirement of the tank or tanks transmitted by determining means, said setting of being transmitted in real time to the regulating means, and on the other hand, capable of determining the inert gas distribution control settings for the various tanks and/or the various compartments of a tank, with said settings being transmitted to the said controlled distribution means in real time. characterized in that these determination means include: - a multitude of sensors capable of measuring in real time, in the tank or the tanks and/or the various compartments of a tank, the volume of fuel, and/or the quantity of oxygen, and/or the temperature, - information processing means relative to the flight of the aircraft and, - means of calculating the inert gas requirement as a function of measurements from the sensors, and information relative to the flight of the aircraft. - an inert gas generator supplied with purged air diverted from the engines and/or air drawn from the passenger compartment, - means of determining the inert gas requirement of the aircraft tank or tanks in real time during the use of the said aircraft, - means of regulating the flow rates of the inert gas generator, - means of controlled distribution of the inert gas to the various tanks and/or the various compartments of a tank and, - a control unit, on the one hand, capable of determining in real time a flow setting for the inert gas generator according to the inert gas requirement of the tank or tanks transmitted by determining means, said setting of being transmitted in real time to the regulating means, and on the other hand, capable of determining the inert gas distribution control settings for the various tanks and/or the various compartments of a tank, with said settings being transmitted to the said controlled distribution means in real time. - a multitude of sensors capable of measuring in real time, in the tank or the tanks and/or the various compartments of a tank, the volume of fuel, and/or the quantity of oxygen, and/or the temperature, - information processing means relative to the flight of the aircraft and, - means of calculating the inert gas requirement as a function of measurements from the sensors, and information relative to the flight of the aircraft.
An image processing apparatus comprising: obtaining means for obtaining a plurality of radiation projection images from a digital radiation detector; and reconstructing means (115, 116, 117) for executing a filtering process on the plurality of radiation projection images using a reconstruction filter and a reconstructing process to create a tomographic image on the basis of the obtained plurality of filtered projection images; characterised in that the image processing apparatus further comprises: processing means (113, 114) for calculating a function value depending on a difference value (p) between a first, filtering-target pixel (q) and a second, peripheral pixel (q') of the target pixel and for multiplying a reconstruction filter coefficient by the function value, thus reducing an influence on the filtering process of the first pixel (q) in a radiation projection image to be supplied to the reconstruction means, the influence being exerted by the second pixel (q'). obtaining means for obtaining a plurality of radiation projection images from a digital radiation detector; and reconstructing means (115, 116, 117) for executing a filtering process on the plurality of radiation projection images using a reconstruction filter and a reconstructing process to create a tomographic image on the basis of the obtained plurality of filtered projection images; characterised in that the image processing apparatus further comprises: processing means (113, 114) for calculating a function value depending on a difference value (p) between a first, filtering-target pixel (q) and a second, peripheral pixel (q') of the target pixel and for multiplying a reconstruction filter coefficient by the function value, thus reducing an influence on the filtering process of the first pixel (q) in a radiation projection image to be supplied to the reconstruction means, the influence being exerted by the second pixel (q'). processing means (113, 114) for calculating a function value depending on a difference value (p) between a first, filtering-target pixel (q) and a second, peripheral pixel (q') of the target pixel and for multiplying a reconstruction filter coefficient by the function value, thus reducing an influence on the filtering process of the first pixel (q) in a radiation projection image to be supplied to the reconstruction means, the influence being exerted by the second pixel (q').
A method for detecting an optical network, wherein the method comprises: receiving, by a management device, a reflection peak power reported by a testing device, wherein the reflection peak power is a reflection peak power of an optical splitter that is obtained by the testing device according to a reflected optical signal, the reflected optical signal is an optical signal obtained by reflecting, by the optical splitter, a testing optical signal that is sent by the testing device and is transmitted to the optical splitter through an optical cable, N+1 optical output ports are disposed on the optical splitter, N is a natural number, N optical output ports of the N+1 optical output ports are configured to transmit a received optical signal to N optical network units, ONUs, through N distribution optical fibers according to a ratio of 1:N, a reflective film is disposed on an end surface of one optical output port except the N optical output ports, and the testing optical signal is reflected by using the reflective film; and detecting the optical network by comparing the reflection peak power with a preset reflection power of the optical splitter. receiving, by a management device, a reflection peak power reported by a testing device, wherein the reflection peak power is a reflection peak power of an optical splitter that is obtained by the testing device according to a reflected optical signal, the reflected optical signal is an optical signal obtained by reflecting, by the optical splitter, a testing optical signal that is sent by the testing device and is transmitted to the optical splitter through an optical cable, N+1 optical output ports are disposed on the optical splitter, N is a natural number, N optical output ports of the N+1 optical output ports are configured to transmit a received optical signal to N optical network units, ONUs, through N distribution optical fibers according to a ratio of 1:N, a reflective film is disposed on an end surface of one optical output port except the N optical output ports, and the testing optical signal is reflected by using the reflective film; and detecting the optical network by comparing the reflection peak power with a preset reflection power of the optical splitter.
Method for tracing the origin of foodstuff, using a device equipped with a form of tray that can be accepted in the foodstuff. whereby, the foodstuff is sold with the device whereby, each device is already allocated a code when loading with the foodstuff, is legible from the outside and is located on the outside of the device characterized in that, each code is individual and individually identifies each of the devices.
A process for removing hydrogen sulfide from a sulfide-containing liquid effluent of an anaerobic reactor treating waste water containing at least 100 mg/l of sulfur compounds on elemental sulfur basis, comprising: (i) contacting, in an upper part of a downflow stripper column, substantially all of the liquid effluent of the anaerobic reactor in counter current with treated product gas of the anaerobic reactor to absorb hydrogen sulfide in the treated product gas, producing a desulfurised effluent and a sulfide-loaded gas, (ii) collecting the desulfurised effluent after said contacting in a lower part of the column, (iia) allowing the liquid effluent collected in step (ii) to degas in the lower part of the column, (iii) discharging a part of the collected effluent degassed in step (iia) as a treated effluent, (iv) adding a non-discharged part of the collected effluent degassed in step (iia) to a mixing tank, which is part of the column or which is connected to the column by a liquid line, and mixing it with influent waste water, (v) feeding the mixed liquid thus obtained to the anaerobic reactor, and (vi) desulfurising the sulfide-loaded gas produced in step (i) to produce the treated product gas. (i) contacting, in an upper part of a downflow stripper column, substantially all of the liquid effluent of the anaerobic reactor in counter current with treated product gas of the anaerobic reactor to absorb hydrogen sulfide in the treated product gas, producing a desulfurised effluent and a sulfide-loaded gas, (ii) collecting the desulfurised effluent after said contacting in a lower part of the column, (iia) allowing the liquid effluent collected in step (ii) to degas in the lower part of the column, (iii) discharging a part of the collected effluent degassed in step (iia) as a treated effluent, (iv) adding a non-discharged part of the collected effluent degassed in step (iia) to a mixing tank, which is part of the column or which is connected to the column by a liquid line, and mixing it with influent waste water, (v) feeding the mixed liquid thus obtained to the anaerobic reactor, and (vi) desulfurising the sulfide-loaded gas produced in step (i) to produce the treated product gas.
A wind turbine drive control device for controlling at least one drive device for moving two structures (10, 20) included in a wind power generation device relative to each other, the at least one drive device comprising an electromagnetic brake, respectively, and the wind power generation device comprising a hydraulic brake, the wind turbine drive control device comprising: a control unit for controlling the at least one drive device so as to cause a force generated by the electromagnetic brake respectively included in the at least one drive device during a stop period in which the two structures (10, 20) are stopped relative to each other to fix the two structures relative to each other to be reduced or zero when a predetermined timing is reached during the stop period while temporarily only a force generated by the hydraulic brake is applied to fix the two structures relative to each other.
A device to help combat bruxism, including a structure designed to be worn on the head of a person, said structure including a headband having a plane of symmetry on either side of which it extends, said structure including two arms symmetrical with respect to said plane of symmetry, said two arms being connected to said headband by a first arm end, said device being characterised in that the two said arms extend downwards from the headband and each have a second free arm end, said second free arm end of each of the arms being at such a distance from the headband that it is able to be positioned against a masseter muscle when said person is wearing said structure and said second end including a masseter circuit, able to detect contraction of the masseter muscle on which said free arm end is positioned, said free end including a vibration device able to adopt either an operating state wherein it emits vibrations, or a standby state wherein it does not emit vibrations, said device including an analysis and control module, communicating with said masseter circuits, and with said vibration devices, said analysis and control module being able to collect and analyse data relating to said contractions detected, and able to control shifting of the vibration devices from said standby state to said operating state, and vice versa. said structure including two arms symmetrical with respect to said plane of symmetry, said two arms being connected to said headband by a first arm end, said device being characterised in that the two said arms extend downwards from the headband and each have a second free arm end, said second free arm end of each of the arms being at such a distance from the headband that it is able to be positioned against a masseter muscle when said person is wearing said structure and said second end including a masseter circuit, able to detect contraction of the masseter muscle on which said free arm end is positioned, said free end including a vibration device able to adopt either an operating state wherein it emits vibrations, or a standby state wherein it does not emit vibrations, said device including an analysis and control module, communicating with said masseter circuits, and with said vibration devices, said analysis and control module being able to collect and analyse data relating to said contractions detected, and able to control shifting of the vibration devices from said standby state to said operating state, and vice versa.
A method of lithography by applying a radiation to at least a pattern to be exposed on a resinated support, comprising at least a step of generating a selected point spread function of said radiation and a step of applying a selected deconvolution method to said pattern to be exposed by said point spread function, said lithography method being characterised in that said point spread function is selected so as to model only the effects of forward scattering of said radiation and in that said deconvolution method is selected from the methods modelling the interactions of said radiation with said resinated support by a joint probability distribution of said interactions.