mhurhangee/ep-ind-claims huggingface dataset:
Nurse call system comprising - a central controller arranged for processing and distributing nurse call messages, - an input/output device connected with said central controller via a first communication link of a nurse call network, - a handset for making a nurse call, said handset being arranged for communicating with said input/output device via a wired electrical connection and comprising a call button provided with a status indicator for indicating a call being present or not, and a processing means capable of monitoring said status indicator and said call button, said handset being connected to said central controller via said first communication link through said input/output device, characterised in that said processing means of said handset is arranged for, on detection at hardware level of a faulty operation of the communication between the handset and the input/output device, establishing as a second path a second network communication link between said handset and said central controller, whereby said input/output device is avoided. - a central controller arranged for processing and distributing nurse call messages, - an input/output device connected with said central controller via a first communication link of a nurse call network, - a handset for making a nurse call, said handset being arranged for communicating with said input/output device via a wired electrical connection and comprising a call button provided with a status indicator for indicating a call being present or not, and a processing means capable of monitoring said status indicator and said call button, said handset being connected to said central controller via said first communication link through said input/output device,
A method of operating an imaging device with a two-dimensional field of image sensors as well as an evaluation unit which is capable of reading out and processing the pixel signals (i), representing output signals of image sensors combined by a binning operation, at a maximum rate of no more than G max, in which method - at least one parameter is preset in order to define a sub-region of the field, - any remaining parameters for defining the sub-region as well as the binning factor b and the imaging rate f are defined in such a manner that the maximum rate G max of the evaluation unit is not exceeded during the reading out of all pixel signals from the sub-region. - at least one parameter is preset in order to define a sub-region of the field, - any remaining parameters for defining the sub-region as well as the binning factor b and the imaging rate f are defined in such a manner that the maximum rate G max of the evaluation unit is not exceeded during the reading out of all pixel signals from the sub-region.
A transmission signal generating apparatus comprising: a symbol generator (101, 102, 1001) configured to generate information symbols; a pilot symbol generator configured to generate a pilot symbol; and a modulator configured to modulate transmission data with a modulation scheme determined based on information including the power of a carrier for transmitting from a base station apparatus to a terminal apparatus, the power of an interfering wave and noise power; wherein the transmission data is modulated with a modulation scheme determined from at least two types of modulation schemes including a phase shift keying modulation scheme and a 16 quadrature amplitude modulation scheme; whereby when transmission data is modulated with the 16 quadrature amplitude modulation scheme and data is transmitted in a frame structure in which a pilot symbol, comprising of a single symbol, is inserted in every three or more successive information symbols, the symbol transmitted immediately before the pilot symbol and the symbol transmitted immediately after the pilot symbol are arranged on a virtual line connecting the pilot symbol and the origin of the inphase-quadrature plane of the 16 quadrature amplitude modulation scheme; and wherein the signal point of the symbol immediately before the pilot symbol and the signal point of the symbol immediately after the pilot symbol, are not signal points of the 16 Quadrature amplitude modulation scheme. a symbol generator (101, 102, 1001) configured to generate information symbols; a pilot symbol generator configured to generate a pilot symbol; and a modulator configured to modulate transmission data with a modulation scheme determined based on information including the power of a carrier for transmitting from a base station apparatus to a terminal apparatus, the power of an interfering wave and noise power; wherein the transmission data is modulated with a modulation scheme determined from at least two types of modulation schemes including a phase shift keying modulation scheme and a 16 quadrature amplitude modulation scheme; whereby when transmission data is modulated with the 16 quadrature amplitude modulation scheme and data is transmitted in a frame structure in which a pilot symbol, comprising of a single symbol, is inserted in every three or more successive information symbols, the symbol transmitted immediately before the pilot symbol and the symbol transmitted immediately after the pilot symbol are arranged on a virtual line connecting the pilot symbol and the origin of the inphase-quadrature plane of the 16 quadrature amplitude modulation scheme; and wherein the signal point of the symbol immediately before the pilot symbol and the signal point of the symbol immediately after the pilot symbol, are not signal points of the 16 Quadrature amplitude modulation scheme.
A liquid rocket engine using a booster pump driven by an electric motor, the liquid rocket engine comprising: a main combustor to receive and combust an oxidant and a fuel; a main oxidant line to guide the oxidant accommodated in an oxidant tank to the main combustor; a main fuel line to guide the fuel accommodated in a fuel tank to the main combustor; an oxidant pump installed at the main oxidant line; a fuel pump installed at the main fuel line; an oxidant booster pump installed at the main oxidant line between the oxidant tank and the oxidant pump; a fuel booster pump installed at the main fuel line between the fuel tank and the fuel pump; an electric motor installed between the oxidant booster pump and the fuel booster pump with an interval therebetween and driving the oxidant booster pump and the fuel booster pump; a cooling line branched from a side of the main oxidant line to guide a part of the oxidant to the electric motor, or branched from a side of the main fuel line to guide a part of the fuel to the electric motor; a cooler connected to the cooling line so as to allow fluid flow therebetween and installed at the electric motor; and a condenser installed at the cooling line, wherein at least one of the oxidant and the fuel is transferred to the cooling line to cool the electric motor. a main combustor to receive and combust an oxidant and a fuel; a main oxidant line to guide the oxidant accommodated in an oxidant tank to the main combustor; a main fuel line to guide the fuel accommodated in a fuel tank to the main combustor; an oxidant pump installed at the main oxidant line; a fuel pump installed at the main fuel line; an oxidant booster pump installed at the main oxidant line between the oxidant tank and the oxidant pump; a fuel booster pump installed at the main fuel line between the fuel tank and the fuel pump; an electric motor installed between the oxidant booster pump and the fuel booster pump with an interval therebetween and driving the oxidant booster pump and the fuel booster pump; a cooling line branched from a side of the main oxidant line to guide a part of the oxidant to the electric motor, or branched from a side of the main fuel line to guide a part of the fuel to the electric motor; a cooler connected to the cooling line so as to allow fluid flow therebetween and installed at the electric motor; and a condenser installed at the cooling line, wherein at least one of the oxidant and the fuel is transferred to the cooling line to cool the electric motor.
A semiconductor device (10, 110), characterized by comprising: a semiconductor element region exposed at one surface of a semiconductor substrate, a semiconductor element is formed within the semiconductor element region; a peripheral termination region exposed at the one surface of the semiconductor substrate, formed around the semiconductor element region, and formed of a single conductive type semiconductor; a peripheral electrode formed on a surface of the peripheral termination region and along a circumference of the semiconductor substrate, and electrically connected with the peripheral termination region; an insulating film formed on the surface of the peripheral termination region and between the peripheral electrode and the semiconductor element region; and at least one intermediate electrode (40, 41a, 41b, 41c) formed on the insulating film, characterized in that a thickness of the insulating film under said at least one intermediate electrode (40, 41a, 41b, 41c) is smaller at a side of the peripheral electrode than at a side of the semiconductor element region. a semiconductor element region exposed at one surface of a semiconductor substrate, a semiconductor element is formed within the semiconductor element region; a peripheral termination region exposed at the one surface of the semiconductor substrate, formed around the semiconductor element region, and formed of a single conductive type semiconductor; a peripheral electrode formed on a surface of the peripheral termination region and along a circumference of the semiconductor substrate, and electrically connected with the peripheral termination region; an insulating film formed on the surface of the peripheral termination region and between the peripheral electrode and the semiconductor element region; and at least one intermediate electrode (40, 41a, 41b, 41c) formed on the insulating film, characterized in that a thickness of the insulating film under said at least one intermediate electrode (40, 41a, 41b, 41c) is smaller at a side of the peripheral electrode than at a side of the semiconductor element region.
Lifting support assembly for a motorized road vehicle having a chassis, in particular for mobile homes, sales vehicles or special-purpose vehicles, wherein the lifting support assembly has a plurality of, in particular four lifting supports (4, 7) with a control device, wherein the lifting support assembly has a safety device for the safe functioning of the lifting supports (4, 7), characterized in that the safety device has at least one interface (76, 76') which is provided and designed to form the signal-transmitting connection to a signal generator for a starting signal of the road vehicle and to a warning device and to an operator control device as well as, if appropriate, to a vehicle controller, wherein the safety device is controlled in such a way that when a starting signal of the signal generator is received and there is a critical position of the lifting support, in particular in the case of contact with the ground, said safety device emits a warning signal via the warning device and retains the current lifting support position.
A method of performing a hybrid automatic repeat request, HARQ, process operation using a frequency division duplex, FDD, frame structure by a base station, BS, in a wireless communication system, the method comprising: transmitting information regarding the number of HARQ processes to a relay node, RN through a higher layer signaling; wherein the number of HARQ processes is determined according to subframes configured for transmission between the BS and the RN, and wherein the HARQ processes are consecutively assigned to subframes configured for the RN-to-the BS transmission. transmitting information regarding the number of HARQ processes to a relay node, RN through a higher layer signaling; wherein the number of HARQ processes is determined according to subframes configured for transmission between the BS and the RN, and wherein the HARQ processes are consecutively assigned to subframes configured for the RN-to-the BS transmission.
A compound of formula (Aa), or a pharmaceutically acceptable salt, a hydrate or a solvate, a crystal form, or a stereoisomer thereof, wherein, R 1, R 2, R 3, R 4, R 5, R 6, R 7, R 8, R 9, R 10, R 11 and R 12 are each independently selected from hydrogen or deuterium; X is selected from CH 3, CD 3, CHD 2 or CH 2 D; with the proviso that if X is CH 3, then at least one of R 1, R 2, R 3, R 4, R 5, R 6, R 7, R 8, R 9, R 10, R 11 and R 12 is deuterium, wherein the compound is selected from the group consisting of R 1, R 2, R 3, R 4, R 5, R 6, R 7, R 8, R 9, R 10, R 11 and R 12 are each independently selected from hydrogen or deuterium; X is selected from CH 3, CD 3, CHD 2 or CH 2 D; with the proviso that if X is CH 3, then at least one of R 1, R 2, R 3, R 4, R 5, R 6, R 7, R 8, R 9, R 10, R 11 and R 12 is deuterium, wherein the compound is selected from the group consisting of
Measuring arrangement for measuring the application force of a disc brake, comprising: a) two components of the disc brake which can be moved, in particular displaced, relative to one another along a displacement distance when an application force is applied; b) at least one application force sensor having a housing; c) a measuring object (7, 7') which is one of the two components or can be fixedly connected to one of the two components, and has at least one metallic end face or at least one target object with at least one metallic end face for contactless interaction with the application force sensor; and d) an evaluation unit, wherein e) the application force sensor is configured as an eddy current sensor for sensing displacement along the displacement distance with the evaluation unit for converting the sensed displacement into a measurement variable as a measure of the application force, and wherein f) the application force sensor and the measuring object (7, 7') can be attached to the respective component of the two components in such a way that they can be removed again, characterised in that g) the at least one metallic end face is formed spherically. a) two components of the disc brake which can be moved, in particular displaced, relative to one another along a displacement distance when an application force is applied; b) at least one application force sensor having a housing; c) a measuring object (7, 7') which is one of the two components or can be fixedly connected to one of the two components, and has at least one metallic end face or at least one target object with at least one metallic end face for contactless interaction with the application force sensor; and d) an evaluation unit, wherein e) the application force sensor is configured as an eddy current sensor for sensing displacement along the displacement distance with the evaluation unit for converting the sensed displacement into a measurement variable as a measure of the application force, and wherein f) the application force sensor and the measuring object (7, 7') can be attached to the respective component of the two components in such a way that they can be removed again, characterised in that g) the at least one metallic end face is formed spherically.
An aerosol generating device configured to operate with a consumable article comprising a substrate portion containing a solid substrate and defining an external surface; the aerosol generating device comprising a heating chamber extending along a chamber axis and configured to receive at least the substrate portion of the consumable article; the heating chamber comprising a plurality of contact walls (40, 41) designed to be in contact with the external surface of the substrate portion of the consumable article, the aerosol generating device being characterized in that the plurality of contact walls (40, 41) comprises a bottom wall arranged substantially perpendicularly to the chamber axis and at least one lateral wall arranged substantially parallel to the chamber axis, the bottom wall being in contact with the or each lateral wall along a common border; the heating chamber further comprising a heating element extending from a centre of the bottom wall parallel to the or at least one lateral wall; the heating chamber further comprising an inlet portion (45; 50; 60) comprising an inlet hole (52A, 52B; 62A, 62B) of an airflow path extending through the substrate portion of the consumable article when it is received in the heating chamber and when the device is operated to generate aerosol; said inlet portion (45; 50; 60) extending on the bottom wall and/or on the or at least one lateral wall to create an airflow gradient at least at a region of the heating chamber adjacent to this inlet portion, said airflow gradient extending from the centre of the bottom wall until the common border. the aerosol generating device comprising a heating chamber extending along a chamber axis and configured to receive at least the substrate portion of the consumable article; the heating chamber comprising a plurality of contact walls (40, 41) designed to be in contact with the external surface of the substrate portion of the consumable article, the aerosol generating device being characterized in that the plurality of contact walls (40, 41) comprises a bottom wall arranged substantially perpendicularly to the chamber axis and at least one lateral wall arranged substantially parallel to the chamber axis, the bottom wall being in contact with the or each lateral wall along a common border; the heating chamber further comprising a heating element extending from a centre of the bottom wall parallel to the or at least one lateral wall; the heating chamber further comprising an inlet portion (45; 50; 60) comprising an inlet hole (52A, 52B; 62A, 62B) of an airflow path extending through the substrate portion of the consumable article when it is received in the heating chamber and when the device is operated to generate aerosol; said inlet portion (45; 50; 60) extending on the bottom wall and/or on the or at least one lateral wall to create an airflow gradient at least at a region of the heating chamber adjacent to this inlet portion, said airflow gradient extending from the centre of the bottom wall until the common border.
A lithium secondary battery comprising: a positive electrode; a negative electrode; and an electrolyte interposed between the positive electrode and the negative electrode, wherein a passivation layer is formed on at least one portion of a surface of the negative electrode after initial cycle of charging and discharging of the lithium secondary battery, wherein the passivation layer comprises a particulate passivation layer and a film-like passivation layer, wherein a thickness of the film-like passivation layer is 10 nm or greater, wherein a thickness of the particulate passivation layer is from about 100 nm to about 600 nm. a positive electrode; a negative electrode; and an electrolyte interposed between the positive electrode and the negative electrode, wherein a passivation layer is formed on at least one portion of a surface of the negative electrode after initial cycle of charging and discharging of the lithium secondary battery, wherein the passivation layer comprises a particulate passivation layer and a film-like passivation layer, wherein a thickness of the film-like passivation layer is 10 nm or greater, wherein a thickness of the particulate passivation layer is from about 100 nm to about 600 nm.
Landing gear mechanism for aircraft, preferably for cargo aircraft, comprising at least a first connecting arm and a second connecting arm, shock absorber elements (1', 1), at least a front wheel and a rear wheel each associated with one of the connecting arms (2', 2), characterized by comprising a balance beam element which is indirectly linked to said front and rear wheels (3' 3) through each one of the connecting arms (2', 2) and each of the shock absorber elements (1', 1), respectively, so that the front portion of the balance beam element is hingedly connected to a first portion of the first shock absorber element, which in turn has a second portion hingedly connected to a first portion of the first connecting arm, which in turn has a second portion hingedly connectable to the aircraft structure, and said rear portion of the balance beam element is hingedly connected to a first portion of the second shock absorber element, which in turn has a second portion hingedly connected to a first portion of the second connecting arm, which in turn has a second portion hingedly connectable to the aircraft structure, further comprising a positioning damper element hingedly connectable to the aircraft structure and also connected, directly or indirectly, to a portion of the body of the balance beam element.
Electrical cabinet comprising a main busbar built in a continuous manner, a secondary busbar (B'), supporting insulators, secondary supporting insulators, a mechanical protection system, a splice connection set (4, 5), derivation connections, switch sets and direct connection cables; characterized in that the main busbar presents a triple wall in its lower portion which comprises central holes equidistant from each other in all its extension, that is, length, a substantially-cubic hollow-shape lower structure, where the triple wall is aligned to one of the side walls of the lower structure, a substantially-cubic hollow-shape upper structure, where the upper structure is interconnected to the lower structure by means of a double central wall placed in its side portions, where in said double central wall there are three sets of holes, where each set contains five holes equidistant from each other, in a manner that a set of holes is in the central portion of the length of the double central wall and the other two in each extremity of the length of the referred double central wall; and in that the secondary busbar (B') contains an additional triple wall and a sole central structure having a substantially-hollow cubic shape, wherein the additional triple wall is located in the central portion of the lower wall of the sole central structure.
A vane for a gas turbine engine comprising: a composite airfoil having pressure and suction sides (41,43) extending outwardly from an airfoil base to an airfoil tip, chordwise spaced apart leading and trailing edges (LE,TE) of the composite airfoil at or near forward and aft ends (48,50) of the vane, an outer vane mount, the composite airfoil supported by the outer vane mount, the outer vane mount including one or more outer spars (130,132) integral with and extending radially inwardly from an outer bridge of the outer vane mount, one or more outer pockets (134,136) extending radially into the composite airfoil from the airfoil tip, and the outer spars received within the one or more outer pockets respectively; wherein the outer bridge extends axially between chordwise spaced apart forward and aft sets of pressure and suction side ears (110,112) for attaching the vane to a fan frame when in use an extending circumferentially or perpendicularly away from pressure and suction side surfaces (104,106) of the outer vane mount, wherein the pressure and suction side surfaces (104,106) of the outer vane mount conform to the shape of the pressure and suction sides (100,102) of the composite airfoil. a composite airfoil having pressure and suction sides (41,43) extending outwardly from an airfoil base to an airfoil tip, chordwise spaced apart leading and trailing edges (LE,TE) of the composite airfoil at or near forward and aft ends (48,50) of the vane, an outer vane mount, the composite airfoil supported by the outer vane mount, the outer vane mount including one or more outer spars (130,132) integral with and extending radially inwardly from an outer bridge of the outer vane mount, one or more outer pockets (134,136) extending radially into the composite airfoil from the airfoil tip, and the outer spars received within the one or more outer pockets respectively;