mhurhangee/patent-ind-claim-en huggingface dataset:
Adjusting device for a vehicle seat, comprising a first adjustable assembly for a first pair of rails, a second adjustable assembly for a second pair of rails, and comprising an electric motor , wherein the electric motor is operatively connected both to an adjusting gearing of the first adjustable assembly and to an adjusting gearing of the second adjustable assembly by at least one output shaft , wherein a motor carrier is provided which receives the electric motor , wherein the motor carrier is fastened to each of the two adjustable assemblies by an adapter , and characterized in that the respective adapter is connected to an upper web of a seat rail of the associated pair of rails by fastening means and the motor carrier is mounted on both sides on a respective adapter by bearing bushings or fingers , and wherein the motor carrier is manufactured integrally from a metallic material, and the adapters are manufactured from a non-metallic material. the motor carrier is fastened to each of the two adjustable assemblies by an adapter , and characterized in that the respective adapter is connected to an upper web of a seat rail of the associated pair of rails by fastening means and the motor carrier is mounted on both sides on a respective adapter by bearing bushings or fingers , and wherein the motor carrier is manufactured integrally from a metallic material, and the adapters are manufactured from a non-metallic material.
A system comprising: a multiplexer having a wavelength pass-band; and an optical network unit (ONU) optically coupled to the multiplexer , the ONU comprising a tunable laser configured to continuously transmit an optical signal to the multiplexer in a burst-on state and a burst-off state, the ONU configured to perform operations comprising: while in the burst-on state, tuning the tunable laser to transmit the optical signal at a transmit wavelength within the wavelength pass-band of the multiplexer , the multiplexer configured to allow passage therethrough of the optical signal at the transmit wavelength; and while in the burst-off state, tuning the tunable laser to transmit the optical signal at a non-transmit wavelength outside of the wavelength pass-band of the multiplexer , the multiplexer configured to block passage therethrough of the optical signal at the non-transmit wavelength. a multiplexer having a wavelength pass-band; and an optical network unit (ONU) optically coupled to the multiplexer , the ONU comprising a tunable laser configured to continuously transmit an optical signal to the multiplexer in a burst-on state and a burst-off state, the ONU configured to perform operations comprising: while in the burst-on state, tuning the tunable laser to transmit the optical signal at a transmit wavelength within the wavelength pass-band of the multiplexer , the multiplexer configured to allow passage therethrough of the optical signal at the transmit wavelength; and while in the burst-off state, tuning the tunable laser to transmit the optical signal at a non-transmit wavelength outside of the wavelength pass-band of the multiplexer , the multiplexer configured to block passage therethrough of the optical signal at the non-transmit wavelength. while in the burst-on state, tuning the tunable laser to transmit the optical signal at a transmit wavelength within the wavelength pass-band of the multiplexer , the multiplexer configured to allow passage therethrough of the optical signal at the transmit wavelength; and while in the burst-off state, tuning the tunable laser to transmit the optical signal at a non-transmit wavelength outside of the wavelength pass-band of the multiplexer , the multiplexer configured to block passage therethrough of the optical signal at the non-transmit wavelength.
A laundry treatment apparatus comprising: a housing provided with an opening in a front thereof; a tub installed in the housing ; a drum rotatably installed in the tub ; and a storage unit introduced into and withdrawn from the housing through the opening , the storage unit for storing a detergent therein; and a supply case disposed in the housing to accommodate the storage unit introduced through the opening , wherein the supply case comprises: an introduction detector coupled to the supply case and configured to detect whether the storage unit is introduced; characterised in that the laundry treatment apparatus further comprises an overhang positioned over the introduction detector and protruding outside from the supply case to block water from falling on the introduction detector . a housing provided with an opening in a front thereof; a tub installed in the housing ; a drum rotatably installed in the tub ; and a storage unit introduced into and withdrawn from the housing through the opening , the storage unit for storing a detergent therein; and a supply case disposed in the housing to accommodate the storage unit introduced through the opening , wherein the supply case comprises: an introduction detector coupled to the supply case and configured to detect whether the storage unit is introduced; characterised in that the laundry treatment apparatus further comprises an overhang positioned over the introduction detector and protruding outside from the supply case to block water from falling on the introduction detector . an introduction detector coupled to the supply case and configured to detect whether the storage unit is introduced; characterised in that the laundry treatment apparatus further comprises an overhang positioned over the introduction detector and protruding outside from the supply case to block water from falling on the introduction detector .
A homology directed repair (HDR) donor vector comprising a nucleic acid molecule, wherein the nucleic acid molecule comprises a nucleotide sequence comprising an insertion cassette, wherein the insertion cassette comprises a nucleic acid sequence to be inserted into the genome of a cell and wherein the insertion cassette is flanked by two nucleotide sequences encoding two negative selection markers, wherein each of the two negative selection markers comprises a ccdb gene flanked by restriction enzyme cleavage sites.
A powder material comprising a dendritic structure and ceramics particles , wherein the dendritic structure and the ceramics particles exist together and the dendritic structure has a cemented carbide composition or a cermet composition, wherein the ceramics particles have a polygonal shape, wherein the cemented carbide composition refers to a configuration which includes W and carbon, the balance being at least one selected from Fe, Ni, Co, and Cr, and wherein the cermet composition refers to a configuration which includes at least one of a Group 4 transition metal, a Group 5 transition metal, a Group 6 transition metal except for W, Al, and Si, and at least one of oxygen, carbon, and nitrogen, the balance being at least one selected from Fe, Ni, Co, and Cr, the cemented carbide composition or the cermet composition containing at least 5 at% or more of at least one of a Group 4 transition metal, a Group 5 transition metal, a Group 6 transition metal, Si, and Al, and at least one of oxygen, carbon, and nitrogen.
A fuel tank inerting system for an aircraft, the system comprising: a fuel tank ; a first reactant source fluidly connected to the fuel tank, the first reactant source arranged to receive fuel from the fuel tank; a second reactant source ; a catalytic reactor arranged to receive a first reactant from the first reactant source and a second reactant from the second reactant source to generate an inert gas that is supplied to the fuel tank to fill an ullage space of the fuel tank; a heat exchanger arranged between the catalytic reactor and the fuel tank and configured to at least one of cool and condense an output from the catalytic reactor to separate out the inert gas; and a controller configured to perform a light-off operation of the catalytic reactor by controlling at least one light-off parameter and, after light-off occurs, adjusting the at least one light-off parameter to an operating level, wherein the at least one light-off parameter comprises a space velocity through the catalytic reactor. a fuel tank ; a first reactant source fluidly connected to the fuel tank, the first reactant source arranged to receive fuel from the fuel tank; a second reactant source ; a catalytic reactor arranged to receive a first reactant from the first reactant source and a second reactant from the second reactant source to generate an inert gas that is supplied to the fuel tank to fill an ullage space of the fuel tank; a heat exchanger arranged between the catalytic reactor and the fuel tank and configured to at least one of cool and condense an output from the catalytic reactor to separate out the inert gas; and a controller configured to perform a light-off operation of the catalytic reactor by controlling at least one light-off parameter and, after light-off occurs, adjusting the at least one light-off parameter to an operating level, wherein the at least one light-off parameter comprises a space velocity through the catalytic reactor.
Aerated fat-based confectionery material having a continuous lipid phase, a porosity of between 1 and 80 % and containing less than 5 % water by weight, wherein, at a temperature at which the lipid phase has a solid lipid content between 0.1 and 80%, the fat-based confectionery material comprises gas bubbles having at least 50 % of their surface occupied by crystals, the crystals comprising a glyceride selected from the group consisting of monoglycerides, diglycerides, triglycerides, esters of monoglycerides, esters of diglycerides and combinations of these, wherein the crystals comprising a glyceride occupying the surface of the gas bubbles form layers having an average thickness below 5 μm and wherein the aerated fat-based confectionery material contains more than 95 % by weight of total lipids of glycerides all of whose fatty acids have a carbon chain length less than 22.
A steel beam that is arranged to serve together with concrete as a bearing composite structure for various slab systems, wherein the steel beam comprises a frame formed by a first web part , a second web part , a base plate and a horizontal top part , the first web part and the second web part are arranged side by side at a distance from each other, the first web part and the second web part are joined at a first end of the first web part and a first end of the second web part by means of the horizontal top part , the first web part and the second web part are joined at a second end of the first web part and a second end of the second web part by means of the base plate , the base plate , the first web part , the second web part and the horizontal top part are arranged to form a space that can be filled with concrete, the steel beam further comprises a hollow member arranged inside the space , the hollow member is sealed so that penetration of concrete into the hollow member is prevented when the steel beam is filled with concrete, and the hollow member is attached to the frame for preventing movement of the hollow member in relation to the frame , and the cross section of the frame forms a quadrangular shape and the hollow member comprises a tube, characterized in that the hollow tube member is attached to each corner of the quadrangular shape using connecting pieces , one end of each being attached to the hollow tube member and another end of each being attached to the respective corner of the quadrangular shape, and in that the hollow tube member is capped at each end of the tube.
A system 100 for acquiring and correlating session-related information from an Internet Protocol Multimedia Subsystem, IMS , the system being configured to acquire (S302) control plane information from control plane signalling tapped at a Proxy Call Session Control Function, P-CSCF, ; acquire (S304) user plane information from user plane traffic tapped at an access gateway, AGW, ; acquire (S306) context information from tapped signalling at an Iq interface between the P-CSCF and the AGW ; and correlate (S308) the control plane information and the user plane information acquired for a particular session using the acquired context information. acquire (S302) control plane information from control plane signalling tapped at a Proxy Call Session Control Function, P-CSCF, ; acquire (S304) user plane information from user plane traffic tapped at an access gateway, AGW, ; acquire (S306) context information from tapped signalling at an Iq interface between the P-CSCF and the AGW ; and correlate (S308) the control plane information and the user plane information acquired for a particular session using the acquired context information.
A method for maintaining time and frequency synchronization when a micro-cell base station is in an off state, comprising: detecting a signal sent by a macro-cell base station or the micro-cell base station in a subframe at a predefined position when the micro-cell base station is in an off state, wherein the signal is a pilot signal for maintaining time and frequency synchronization, and the pilot signal comprises a subframe position and configuration information; and performing an operation for maintaining time and frequency synchronization with the micro-cell base station based on the pilot signal sent in the subframe at the predefined position. detecting a signal sent by a macro-cell base station or the micro-cell base station in a subframe at a predefined position when the micro-cell base station is in an off state, wherein the signal is a pilot signal for maintaining time and frequency synchronization, and the pilot signal comprises a subframe position and configuration information; and performing an operation for maintaining time and frequency synchronization with the micro-cell base station based on the pilot signal sent in the subframe at the predefined position.
A method for communicating sensor data pertaining to detected weather between aircraft , the method comprising: receiving, by a transmitting aircraft , a query from a requesting aircraft for sensor information at a geographic area of interest that is beyond a radar range limit of a radar system of the requesting aircraft , wherein the received query includes an aircraft identifier; acquiring sensor data from at least one sensor configured to sense weather data residing in the transmitting aircraft that is in the geographic area of interest ; comparing the aircraft identifier with an identifier of the transmitting aircraft ; and in response to the aircraft identifier corresponding to the identifier of the transmitting aircraft and if the transmitting aircraft is within communication range of the requesting aircraft , transmitting a signal comprising the sensor data from the transmitting aircraft to the requesting aircraft in response to receiving the query; and if the transmitting aircraft is not within communication range of the requesting aircraft , transmitting the signal comprising the sensor data from the transmitting aircraft to an intervening aircraft to relay the signal to the requesting aircraft in response to receiving the query. receiving, by a transmitting aircraft , a query from a requesting aircraft for sensor information at a geographic area of interest that is beyond a radar range limit of a radar system of the requesting aircraft , wherein the received query includes an aircraft identifier; acquiring sensor data from at least one sensor configured to sense weather data residing in the transmitting aircraft that is in the geographic area of interest ; comparing the aircraft identifier with an identifier of the transmitting aircraft ; and in response to the aircraft identifier corresponding to the identifier of the transmitting aircraft and if the transmitting aircraft is within communication range of the requesting aircraft , transmitting a signal comprising the sensor data from the transmitting aircraft to the requesting aircraft in response to receiving the query; and if the transmitting aircraft is not within communication range of the requesting aircraft , transmitting the signal comprising the sensor data from the transmitting aircraft to an intervening aircraft to relay the signal to the requesting aircraft in response to receiving the query.
A method of manufacturing a ceramic composite for light conversion, comprising: applying a CMP process to a surface of a solidified body with a structure in which an Al 2 O 3 phase and a fluorescence emitting crystalline phase of oxides other than Al 2 O 3 are continuously and three-dimensionally entangled with each other is, wherein pH of a polishing liquid is adjusted between 11 and 12 when performing a CMP process. applying a CMP process to a surface of a solidified body with a structure in which an Al 2 O 3 phase and a fluorescence emitting crystalline phase of oxides other than Al 2 O 3 are continuously and three-dimensionally entangled with each other is, wherein pH of a polishing liquid is adjusted between 11 and 12 when performing a CMP process.
A double side laser welding method for joining a gear case and a ring gear being abutted against each other in a weld part , the method including first welding to be performed from one side with respect to the weld part and second welding to be performed from the other side, characterized in that the second welding to be performed after the first welding includes heat amount adjustment to adjust a heat input amount with respect to the weld part so that welding distortion corresponding to a target distortion amount to cancel a displacement generated by the first welding is generated, and wherein the heat amount adjustment includes: preparing a test gear case and a test ring gear respectively identical to the gear case and the ring gear ; determining the target distortion amount based on a result of welding distortion due to the first welding and the second welding performed on the test gear case and the test ring gear; and adjusting the heat input amount to the weld part to generate the welding distortion corresponding to the determined distortion amount. characterized in that the second welding to be performed after the first welding includes heat amount adjustment to adjust a heat input amount with respect to the weld part so that welding distortion corresponding to a target distortion amount to cancel a displacement generated by the first welding is generated, and wherein the heat amount adjustment includes: preparing a test gear case and a test ring gear respectively identical to the gear case and the ring gear ; determining the target distortion amount based on a result of welding distortion due to the first welding and the second welding performed on the test gear case and the test ring gear; and adjusting the heat input amount to the weld part to generate the welding distortion corresponding to the determined distortion amount. preparing a test gear case and a test ring gear respectively identical to the gear case and the ring gear ; determining the target distortion amount based on a result of welding distortion due to the first welding and the second welding performed on the test gear case and the test ring gear; and adjusting the heat input amount to the weld part to generate the welding distortion corresponding to the determined distortion amount.
Use of at least one compound of general formula : R-S n -R' in which: • R and R', which may be identical or different, represent, independently of each other, a linear or branched hydrocarbon-based radical, containing from 1 to 12 carbon atoms and optionally one or more unsaturations in the form of double and/or triple bonds; • n represents an integer between 1 and 8, limits inclusive, preferably between 1 and 6, limits inclusive, more preferably between 1 and 4, limits inclusive, more preferentially between 2 and 8, limits inclusive, better still between 2 and 6, and most particularly between 2 and 4, limits inclusive; for maintaining the viscosity of liquid sulfur at a value below 60 000 mPa.s, preferably below 30 000 mPa.s, more preferably below 10 000 mPa.s and advantageously below 5000 mPa.s, said at least one compound of formula being used without addition of organohalogen compound. • R and R', which may be identical or different, represent, independently of each other, a linear or branched hydrocarbon-based radical, containing from 1 to 12 carbon atoms and optionally one or more unsaturations in the form of double and/or triple bonds; • n represents an integer between 1 and 8, limits inclusive, preferably between 1 and 6, limits inclusive, more preferably between 1 and 4, limits inclusive, more preferentially between 2 and 8, limits inclusive, better still between 2 and 6, and most particularly between 2 and 4, limits inclusive;
A display comprising first light-scattering regions each provided with linear protrusions and/or recesses having the same longitudinal direction, wherein directions of the linear protrusions and/or recesses of the respective light-scattering regions are different from each other, characterized in that in at least one of the first light-scattering regions , intervals of the linear protrusions and/or recesses in a light-scattering axis are arranged at random, the light-scattering axis being a direction in which the light-scattering region represents a maximum light-scattering ability, and the display further comprises a second light-scattering region provided with protrusions and/or recesses each having a shape other than a linear shape. first light-scattering regions each provided with linear protrusions and/or recesses having the same longitudinal direction, wherein directions of the linear protrusions and/or recesses of the respective light-scattering regions are different from each other, characterized in that in at least one of the first light-scattering regions , intervals of the linear protrusions and/or recesses in a light-scattering axis are arranged at random, the light-scattering axis being a direction in which the light-scattering region represents a maximum light-scattering ability, and the display further comprises a second light-scattering region provided with protrusions and/or recesses each having a shape other than a linear shape.
A method for accessing a communication network for a mobile terminal via an unlicensed wireless access network, comprising determining, by the mobile terminal, location information of an access point of the unlicensed wireless access network and selecting, by the mobile terminal, a communication network that fulfils carrier grade requirements based on said location information, wherein the carrier grade requirements are regulatory requirements in a country or area corresponding to the location of the access point, said regulatory requirements comprising lawful interception capabilities, the method further comprising accessing the selected communication network via said access point .
A support bar for cable trays, said support bar being a hollow profile extruded from a polymer material in the form of a rail, having an outer perimeter with a rectangular cross-section, and comprising a base wall , two side walls facing one another, and an open wall , said open wall facing said base wall and comprising a continuous opening extending along the entire length of said support bar , such that said open wall has a flat outer surface extending on both sides of said continuous opening , said side walls forming two facing flanges projecting towards the inside of said support bar , each of said flanges having a lower face oriented towards said base wall and an upper face, opposite said lower face, forming said flat outer surface of the open wall , and said side walls forming two facing protrusions projecting towards the inside of said support bar below said lower face of said flanges , and such that said protrusions do not cover said lower face of said flanges in a direction orthogonal to said base wall , characterized in that it comprises two inner walls each of them joining said base wall and said protrusion of one of said side walls , each of said inner walls extending next to one of said side walls , such that said base wall , said side wall , and said inner wall together demarcate an empty space .