mhurhangee/patent-ind-claim-en huggingface dataset:
An adjusting device for the longitudinal adjustment of a vehicle seat (F), comprising - at least one rail for defining a longitudinal seat axis (L) along which a seat base (G) of the vehicle seat (F) is adjustable, and for supporting at least one adjusting unit (2.1, 2.2) of the adjusting device , and - at least two shiftably guided adjusting units (2.1, 2.2) arranged one behind the other along the longitudinal seat axis (L), to which the seat base (G) is to be fixed in order to be adjustable along the longitudinal seat axis (L), characterized in that the at least two adjusting units (2.1, 2.2) are adjustable relative to each other along the longitudinal seat axis (L), and each adjusting unit (2.1, 2.2) is assigned a separate drive (4.1, 4.2) for the power-operated adjustment along the longitudinal seat axis (L), wherein for the power-operated adjustment of the at least two adjusting units (2.1, 2.2) a common, stationary spindle and two spindle nuts each assigned to an adjusting unit (2.1, 2.2) and each meshing with the spindle are provided. - at least one rail for defining a longitudinal seat axis (L) along which a seat base (G) of the vehicle seat (F) is adjustable, and for supporting at least one adjusting unit (2.1, 2.2) of the adjusting device , and - at least two shiftably guided adjusting units (2.1, 2.2) arranged one behind the other along the longitudinal seat axis (L), to which the seat base (G) is to be fixed in order to be adjustable along the longitudinal seat axis (L),
A heat transfer material comprising insoluble fine particles of cobalt (II, III) oxide, iron (II, III) oxide, zirconium (IV) oxide, aluminum oxide, silicon dioxide and zinc molybdate.
A user equipment, UE , configured to operate in a wireless communication system, the UE comprising: a controller configured to: identify a pool of hybrid automatic repeat request, HARQ, process numbers which is configured by a base station, for transmission on a sidelink channel; sense and search one or more sidelink control information, SCI, transmissions received on a physical sidelink control channel, PSCCH of one or more other UEs to determine whether any HARQ process numbers are being used by the one or more other UEs; exclude the detected HARQ process numbers from the pool of the HARQ process numbers based on the searched one or more SCI transmissions, wherein a detected HARQ process number is not excluded if the corresponding UE has finished the maximal allowed retransmission number; select a HARQ process number from remaining HARQ process numbers in the pool of the HARQ process numbers; generate sidelink control information, SCI, including the selected HARQ process number; and a transmitter coupled with the controller and configured to perform a transmission or re-transmission of a packet including sidelink data based on the generated SCI with the selected HARQ process number to another UE on the sidelink channel. identify a pool of hybrid automatic repeat request, HARQ, process numbers which is configured by a base station, for transmission on a sidelink channel; sense and search one or more sidelink control information, SCI, transmissions received on a physical sidelink control channel, PSCCH of one or more other UEs to determine whether any HARQ process numbers are being used by the one or more other UEs; exclude the detected HARQ process numbers from the pool of the HARQ process numbers based on the searched one or more SCI transmissions, wherein a detected HARQ process number is not excluded if the corresponding UE has finished the maximal allowed retransmission number; select a HARQ process number from remaining HARQ process numbers in the pool of the HARQ process numbers; generate sidelink control information, SCI, including the selected HARQ process number; and a transmitter coupled with the controller and configured to perform a transmission or re-transmission of a packet including sidelink data based on the generated SCI with the selected HARQ process number to another UE on the sidelink channel.
An aircraft position control system configured to keep an aircraft at target coordinates in an inertial space with respect to a target landing point that moves, the aircraft position control system comprising: an acceleration correction processing unit configured to, based on acceleration of the aircraft and an attitude of the aircraft , output first attitude correction acceleration in which the acceleration in an aircraft axis coordinate system is converted to acceleration in an inertial space coordinate system; a complementary filter configured to, based on the first attitude correction acceleration and inertial velocity of the aircraft , which is the velocity in an aircraft coordinate system with the aircraft as the origin, output second attitude correction acceleration in which a drift component included in the first attitude correction acceleration is removed; a smoothing processing unit configured to, based on the second attitude correction acceleration and relative coordinates between the aircraft and the target landing point , output smoothed relative coordinates obtained by smoothing the relative coordinates; a feedback control unit configured to calculate a control quantity of the aircraft on the basis of the smoothed relative coordinates; and a flight control unit configured to execute the position control of the aircraft on the basis of the control quantity. an acceleration correction processing unit configured to, based on acceleration of the aircraft and an attitude of the aircraft , output first attitude correction acceleration in which the acceleration in an aircraft axis coordinate system is converted to acceleration in an inertial space coordinate system; a complementary filter configured to, based on the first attitude correction acceleration and inertial velocity of the aircraft , which is the velocity in an aircraft coordinate system with the aircraft as the origin, output second attitude correction acceleration in which a drift component included in the first attitude correction acceleration is removed; a smoothing processing unit configured to, based on the second attitude correction acceleration and relative coordinates between the aircraft and the target landing point , output smoothed relative coordinates obtained by smoothing the relative coordinates; a feedback control unit configured to calculate a control quantity of the aircraft on the basis of the smoothed relative coordinates; and a flight control unit configured to execute the position control of the aircraft on the basis of the control quantity.
A method of manufacturing a decal used in the production of a matrix array sensor for a touch 2. screen, comprising the steps of: providing a flexible release layer having a first surface ; printing a conductive ink layer on said first surface; and printing an adhesive layer onto said conductive ink layer; wherein said step of printing a conductive ink layer comprises printing conductive ink to form at least one patterned element , characterised in that : said first surface is a non-uniform surface consisting of indentations , and said conductive ink layer comprises a corresponding non-uniform surface induced by the non-uniform surface of the first surface ,. providing a flexible release layer having a first surface ; printing a conductive ink layer on said first surface; and printing an adhesive layer onto said conductive ink layer; wherein said step of printing a conductive ink layer comprises printing conductive ink to form at least one patterned element , characterised in that : said first surface is a non-uniform surface consisting of indentations , and said conductive ink layer comprises a corresponding non-uniform surface induced by the non-uniform surface of the first surface ,.
A method for grinding a hydraulic binder, comprising: a) introducing: - a hydraulic binder, and - a composition B comprising at least one grinding aid B, into the first chamber of a horizontal grinder comprising several chambers , including a first chamber and a last chamber , each chamber being separated from the adjacent chamber by a diaphragm , whereby a composition β comprising the hydraulic binder and composition B is obtained in the first chamber , b) grinding composition β in the horizontal grinder , whereby composition β moves from the first chamber to the last chamber and a ground composition C is obtained at the outlet of the last chamber , characterised in that , at the grinding step, it comprises introducing into the last chamber a composition A comprising at least one grinding aid A comprising an aminoalcohol, composition A differing from composition β. a) introducing: - a hydraulic binder, and - a composition B comprising at least one grinding aid B, into the first chamber of a horizontal grinder comprising several chambers , including a first chamber and a last chamber , each chamber being separated from the adjacent chamber by a diaphragm , whereby a composition β comprising the hydraulic binder and composition B is obtained in the first chamber , - a hydraulic binder, and - a composition B comprising at least one grinding aid B, into the first chamber of a horizontal grinder comprising several chambers , including a first chamber and a last chamber , each chamber being separated from the adjacent chamber by a diaphragm , whereby a composition β comprising the hydraulic binder and composition B is obtained in the first chamber , into the first chamber of a horizontal grinder comprising several chambers , including a first chamber and a last chamber , each chamber being separated from the adjacent chamber by a diaphragm , whereby a composition β comprising the hydraulic binder and composition B is obtained in the first chamber , b) grinding composition β in the horizontal grinder , whereby composition β moves from the first chamber to the last chamber and a ground composition C is obtained at the outlet of the last chamber ,
A method of coating a leading edge surface of an airfoil with an elastomeric protective coating, comprising: applying a liquid elastomeric material selected from the group consisting of polyurethane, polyurea and fluoroelastomer having a viscosity between a brushable coating up to the viscosity of a flowable caulking compound to said airfoil leading edge surface using a flexible applicator capable of conforming to said airfoil leading edge surface while being drawn lengthwise along the airfoil leading edge surface; thereby depositing a layer of the liquid elastomeric material on the leading edge surface of the airfoil. applying a liquid elastomeric material selected from the group consisting of polyurethane, polyurea and fluoroelastomer having a viscosity between a brushable coating up to the viscosity of a flowable caulking compound to said airfoil leading edge surface using a flexible applicator capable of conforming to said airfoil leading edge surface while being drawn lengthwise along the airfoil leading edge surface; thereby depositing a layer of the liquid elastomeric material on the leading edge surface of the airfoil.
An implantable blood pump system comprising: a housing having an inlet and an outlet and configured to be implanted at a patient's heart; a membrane disposed within the housing ; a skirt disposed within the housing and coupled to the membrane , the skirt sized and shaped to extend toward the inlet and to curve toward the outlet , and the skirt configured to divide a delivery channel into an upper delivery channel and a lower delivery channel that leads to respective flow channels , wherein the flow channels are separated by the membrane ; and an actuator disposed within the housing , the actuator configured to cause the membrane to reciprocate and deform in a wave-like manner, wherein during operation blood enters the inlet , flows toward the skirt which guides the blood through the delivery channels towards the upper and lower surfaces of the membrane through the flow channels , and is propelled across the membrane to the outlet . a housing having an inlet and an outlet and configured to be implanted at a patient's heart; a membrane disposed within the housing ; a skirt disposed within the housing and coupled to the membrane , the skirt sized and shaped to extend toward the inlet and to curve toward the outlet , and the skirt configured to divide a delivery channel into an upper delivery channel and a lower delivery channel that leads to respective flow channels , wherein the flow channels are separated by the membrane ; and an actuator disposed within the housing , the actuator configured to cause the membrane to reciprocate and deform in a wave-like manner, wherein during operation blood enters the inlet , flows toward the skirt which guides the blood through the delivery channels towards the upper and lower surfaces of the membrane through the flow channels , and is propelled across the membrane to the outlet .
A nozzle for introduction of coolant to a cutting edge for metal chip removing machining, said nozzle having a single through hole for a fastening member and having at least one internal coolant channel for fluid having a flow direction (F), the at least one internal coolant channel having a length, wherein the at least one internal coolant channel comprises grooves extending internally at least partially along the coolant channel , the at least one internal coolant channel extending from a first opening to a second opening (19;19';19"), said first opening is connectable to a coolant supply conduit in a holder body , said second opening (19;19';19") serving as exit for the coolant at the forward end , said nozzle having a forward end , a rear end and a bottom face , said single through hole extending between the bottom face and an opposite top face , characterized in that the at least one internal coolant channel and the first opening are spaced from the single through hole .
A wiper blade for the windshield of a vehicle, notably a motor vehicle, comprising - a blade rubber having elastic tongues , - a body consisting of an upper body containing a one-piece rigid strip and of a lower body to which said blade rubber is attached, - a spoiler extending from said body and having an aerodynamic profile between a leading edge and a trailing edge, the blade having a boundary between the body and the spoiler that is defined by a horizontal surface passing through the leading edge of said profile, characterized in that said spoiler extends horizontally downstream beyond a part, virtual or otherwise, defined as forming the mirror image, about a vertical plane passing through a lower end of the blade rubber , of that part of the body that is situated upstream of this same vertical plane and in that the rigid strip does not extend upstream beyond the part of the body that holds the blade rubber and the elastic tongues . - a blade rubber having elastic tongues , - a body consisting of an upper body containing a one-piece rigid strip and of a lower body to which said blade rubber is attached, - a spoiler extending from said body and having an aerodynamic profile between a leading edge and a trailing edge, the blade having a boundary between the body and the spoiler that is defined by a horizontal surface passing through the leading edge of said profile,
Process for producing a synthesis gas by catalytic steam reforming of a hydrocarbon feedstock in a steam reforming unit, said reforming unit optionally generating a flue gas, wherein water is removed from the synthesis gas as a process condensate, wherein boiler feed water is introduced in the process, and wherein said process produces at least two separate steam streams: i) a pure steam stream which is generated from at least a portion of said boiler feed water (BFW) by the cooling of synthesis gas, and ii) a process steam stream which is generated by evaporating at least a portion of the process condensate by the cooling of synthesis gas; and wherein step ii) is conducted in a process condensate boiler (PC-boiler); and wherein step ii) also comprises the cooling of at least a portion of said pure steam stream, and/or the cooling of said flue gas.
Contact dryer for drying moist material, consisting of at least one drying tube , in which the material to be dried can be conveyed and on the outer side of which there is a heating medium in a casing tube at least partially surrounding the drying tube , wherein at least one further drying tube is arranged in the casing tube , formed as a pressure vessel, and the at least two drying tubes are formed in such a way that the material to be dried cannot mix along at least one longitudinal section of the at least two drying tubes , wherein the casing tube does not perform a rotating movement and the heating medium is water vapour or an organic medium, which during operation changes to an at least partially gaseous or vaporous phase when heat is supplied and condenses back to the liquid phase when heat is removed, wherein in the casing tube there is at least one heating tube , through which heat can be supplied to the heating medium , and the heating tube is arranged in such a way that the heating medium at least partially surrounds the heating tube during operation or that the at least one heating tube is outside the casing tube and is connected to the casing tube in such a way that the heating region, in which the at least one heating tube is arranged, and the drying region, in which the at least two drying tubes are arranged in the casing tube , represent a common pressure vessel, wherein the drying region is arranged above the heating region in such a way that the condensate from the drying region flows into the heating region, driven by gravitational force.
A composition for encapsulating an organic electronic element, comprising an olefin-based resin, a curable monomer, and a curable oligomer which is comprised in an amount of 20 to 90 parts by weight relative to 100 parts by weight of the olefin-based resin and has a glass transition temperature of 55°C or less after curing; wherein the curable oligomer does not comprise epoxy acrylate.
A household appliance comprising a heat pump having a closed refrigerant circuit for guiding a flow of a refrigerant, and integrated into the refrigerant circuit a heat source for providing heating by condensing the refrigerant, an expansion device for expanding the flow and located downstream of the heat source , a heat sink for providing cooling by evaporating the refrigerant, and located downstream of the expansion device , and a compressor system for driving and compressing the flow and located downstream of the heat sink and upstream of the heat source , the household appliance also comprising a control device for controlling operation of the household appliance and a heating device for providing heating to the heat pump, the household appliance further comprising a sensor system for determining a superheating temperature of the refrigerant as a difference between an outlet temperature of the refrigerant at an outlet of the heat sink and an inlet temperature of the refrigerant at an inlet of the heat sink as the refrigerant exits the heat sink , and the control device being connected to the sensor system and the heating device , and being configured for operating the heating device in dependence of the superheating temperature, characterized in that the compressor system comprises an accumulator for accumulating refrigerant received from the heat sink , and a compressor located downstream of the accumulator for driving and compressing the refrigerant, and wherein the heating device is arranged for providing heating to the accumulator .
A system for the superimposition of holographic opacity modulation states for holographic, light field, virtual, augmented or mixed reality applications, the system comprising: a first electromagnetic energy waveguide relay system configured such that electromagnetic energy passing therethrough is directed according to a first 4D plenoptic function; a second electromagnetic energy waveguide relay system following the first electromagnetic energy waveguide relay system , the second electromagnetic energy waveguide relay system configured such that electromagnetic energy passing therethrough is directed according to a second 4D plenoptic function, the second 4D plenoptic function inverse of the first 4D plenoptic function; and a first electromagnetic energy modulation element disposed in a first location in the first electromagnetic energy waveguide relay system , in a second location in the second electromagnetic energy waveguide relay system or in a third location in between the first electromagnetic energy waveguide relay system and the second electromagnetic energy waveguide relay system , the first electromagnetic energy modulation element configured to modulate electromagnetic energy passing therethrough. a first electromagnetic energy waveguide relay system configured such that electromagnetic energy passing therethrough is directed according to a first 4D plenoptic function; a second electromagnetic energy waveguide relay system following the first electromagnetic energy waveguide relay system , the second electromagnetic energy waveguide relay system configured such that electromagnetic energy passing therethrough is directed according to a second 4D plenoptic function, the second 4D plenoptic function inverse of the first 4D plenoptic function; and a first electromagnetic energy modulation element disposed in a first location in the first electromagnetic energy waveguide relay system , in a second location in the second electromagnetic energy waveguide relay system or in a third location in between the first electromagnetic energy waveguide relay system and the second electromagnetic energy waveguide relay system , the first electromagnetic energy modulation element configured to modulate electromagnetic energy passing therethrough.
An organometallic complex, characterized in that it consists of at least two elements of amino acid and at least two different metals, the molar ratio of amino acid per metal being 1-to-1, wherein the amino acid is glycine, and the metals are chosen from the group consisting of zinc, copper, iron, manganese, cobalt, calcium, molybdenum, chromium and magnesium.