mhurhangee/ep-ind-claims huggingface dataset:
Method for serial data transmission between a basic module and a first expansion module, wherein the basic module and the first expansion module each comprise a first system interface (11, 21), which has four pins as a serial peripheral interface and two pins as a UART interface or as an I 2 C interface, characterised in that the first system interface of the basic module is connected to the first system interface of the expansion module and the data transmission between the basic module and the first expansion module via the serial peripheral interface is a cyclical data transmission and via the UART interface or I 2 C interface is an acyclical data transmission, wherein to exchange a data packet from the basic module to the first expansion module the basic module indicates to the first expansion module by means of at least one control bit in the cyclical data transmission with the first expansion module that a data packet is transmitted via the acyclical data transmission to the first expansion module and the data packet is then transmitted via the acyclical data transmission to the first expansion module.
An imaging system, comprising: a first portion of the system; a second portion (40, 2204) of the system, wherein the second portion (40, 2202) rotates with respect to the first portion; and characterized in that: the imaging system comprises a locking mechanism having a first lock portion on the first portion of the system and a second lock portion on the second portion (40, 2204) of the system, and wherein rotating the second portion (40, 2204) of the system to one or more pre-determined angles relative to the first portion of the system causes the first lock portion to engage with the second lock portion to prevent the second portion (40, 2204) of the system from rotating with respect to the first portion of the system. a first portion of the system; a second portion (40, 2204) of the system, wherein the second portion (40, 2202) rotates with respect to the first portion; and characterized in that: the imaging system comprises a locking mechanism having a first lock portion on the first portion of the system and a second lock portion on the second portion (40, 2204) of the system, and wherein rotating the second portion (40, 2204) of the system to one or more pre-determined angles relative to the first portion of the system causes the first lock portion to engage with the second lock portion to prevent the second portion (40, 2204) of the system from rotating with respect to the first portion of the system. the imaging system comprises a locking mechanism having a first lock portion on the first portion of the system and a second lock portion on the second portion (40, 2204) of the system, and wherein rotating the second portion (40, 2204) of the system to one or more pre-determined angles relative to the first portion of the system causes the first lock portion to engage with the second lock portion to prevent the second portion (40, 2204) of the system from rotating with respect to the first portion of the system.
A liquid ejection apparatus comprising a fluid line configured to extend into a tank and to receive a liquid, a rotary head being arranged on the fluid line and fitted with a rotary hub (110, 210) that comprises a liquid ejection nozzle (112, 212) for ejecting the liquid, the rotary head being rotatable in a first direction about a first geometrical axis and the rotary hub (110, 210) being rotatable in a second direction about a second geometrical axis that is offset from the first geometrical axis, such that the liquid ejected by the nozzle (112, 212) is ejected in a pattern towards an interior surface of the tank, wherein the liquid ejection nozzle (112, 212) comprises a first liquid outlet arranged to eject the liquid in form of a jet beam and in a first direction towards the interior surface of the tank, and a second liquid outlet arranged to eject the liquid in form of a spray beam in a second direction towards the interior surface of the tank such that the liquid diverges by an angle (θ1) of 20 ° to 90°, as seen in a first geometrical plane that is parallel to a center axis of the nozzle, which second direction is inclined to the second geometrical axis by an angle (ψ2) of 10° to 80°.
A method of generating a horizon for use in an Advanced Driver Assistance System (ADAS) of a vehicle, comprising: obtaining data representative of a pre-calculated route to be travelled by the vehicle; determining a most probable outgoing path that the vehicle may be expected to travel in the immediate future at a decision point, wherein the most probable path is the outgoing path corresponding to a portion of the pre-calculated route; using one or more of stored digital location-based data, vehicle data and driver data to determine data indicative of a relative probability that each of the other outgoing paths at the decision point will be taken by the vehicle; determining at least one alternative outgoing path that the vehicle may be expected to travel in the immediate future at the decision point based on the determined relative probability data; and generating the horizon using the determined most probable outgoing path and the at least one alternative outgoing path. obtaining data representative of a pre-calculated route to be travelled by the vehicle; determining a most probable outgoing path that the vehicle may be expected to travel in the immediate future at a decision point, wherein the most probable path is the outgoing path corresponding to a portion of the pre-calculated route; using one or more of stored digital location-based data, vehicle data and driver data to determine data indicative of a relative probability that each of the other outgoing paths at the decision point will be taken by the vehicle; determining at least one alternative outgoing path that the vehicle may be expected to travel in the immediate future at the decision point based on the determined relative probability data; and generating the horizon using the determined most probable outgoing path and the at least one alternative outgoing path.
A method for driving a solid oxide fuel cell comprising an anode, a cathode, and an electrolyte provided between the anode and the cathode and containing a ceria-based metal oxide, the method comprising: adjusting the solid oxide fuel cell to a driving temperature; reducing NiO of the anode to Ni by supplying a gas containing oxygen to the cathode and supplying a gas containing hydrogen to the anode; oxidizing the electrolyte by supplying the gas containing oxygen to the cathode and stopping the supply of the gas containing hydrogen to the reduced anode; and driving the solid oxide fuel cell by supplying a gas containing oxygen to the cathode and supplying a gas containing hydrogen to the reduced anode. adjusting the solid oxide fuel cell to a driving temperature; reducing NiO of the anode to Ni by supplying a gas containing oxygen to the cathode and supplying a gas containing hydrogen to the anode; oxidizing the electrolyte by supplying the gas containing oxygen to the cathode and stopping the supply of the gas containing hydrogen to the reduced anode; and driving the solid oxide fuel cell by supplying a gas containing oxygen to the cathode and supplying a gas containing hydrogen to the reduced anode.
A method of forming single crystal C-plane sapphire material comprising: seeding a melt fixture with a seed having a C-axis orientation substantially perpendicular to a longitudinal axis of a die opening; crystallizing single crystal sapphire above the die, the single crystal sapphire exhibiting a C-axis orientation substantially perpendicular to the sapphire's major surface; passing the sapphire through a first region exhibiting a first thermal gradient, the sapphire being at greater than 1850 °C; subsequently passing the sapphire through a second region exhibiting a second thermal gradient that is less than the first thermal gradient, the sapphire being at greater than 1850 °C; and cooling the C-plane sapphire to produce a material exhibiting fewer than 10,000 dislocations/cm 2 as detected using transmission X-ray diffraction topography based on Bragg diffraction. seeding a melt fixture with a seed having a C-axis orientation substantially perpendicular to a longitudinal axis of a die opening; crystallizing single crystal sapphire above the die, the single crystal sapphire exhibiting a C-axis orientation substantially perpendicular to the sapphire's major surface; passing the sapphire through a first region exhibiting a first thermal gradient, the sapphire being at greater than 1850 °C; subsequently passing the sapphire through a second region exhibiting a second thermal gradient that is less than the first thermal gradient, the sapphire being at greater than 1850 °C; and cooling the C-plane sapphire to produce a material exhibiting fewer than 10,000 dislocations/cm 2 as detected using transmission X-ray diffraction topography based on Bragg diffraction.
A rotating drum for infeeding material by gravity to its interior comprising: • a static shell comprising an inlet configured to enable the inlet of the material into the rotating drum to be carried out; • a rotating shell comprising a first helical blade or auger arranged inside said rotating shell, wherein the first helical blade or auger is configured to rotate together with the rotating shell; characterised in that the first helical blade or auger is also arranged at least partially inside the static shell. • a static shell comprising an inlet configured to enable the inlet of the material into the rotating drum to be carried out; • a rotating shell comprising a first helical blade or auger arranged inside said rotating shell, wherein the first helical blade or auger is configured to rotate together with the rotating shell;
Landing gear for aircraft comprising: - a landing gear strut extending along a main axis (X-X) of the landing gear; - at least one axle, mechanically connected to a first side of the strut; - at least one wheel, rotatably mounted about said at least one axle; - at least one damper arranged to dampen a sliding movement of said landing gear strut relative to the structure of the aircraft; the landing gear further comprises at least one pair of first and second parts (7, 8, 7', 8'), said first part (7, 7') having a steel substrate and a sliding layer (C, C') formed on this substrate, the second part (8, 8') being mounted in sliding contact against said sliding layer (C, C'), said mounting in sliding contact allowing a maximum rectilinear sliding amplitude (G, G') of this second (8, 8') part against said sliding layer (C, C') of the first part (7, 7'), strictly less than 0.5 mm, the sliding layer (C, C') being adapted to support, at least during the sliding, a surface pressure in excess of 50 MPa, wherein: - the sliding layer (C, C') is made of a zinc and nickel alloy comprising, in terms of percentage by weight of the alloy, between 12% and 18% nickel, at most 0.5% of other elements such as nickel and zinc, the remainder being zinc; and wherein - the first part also has a protective layer (P, P') against corrosion extending from the sliding layer (C, C'), this protective layer (P, P') being formed of said zinc and nickel alloy. - a landing gear strut extending along a main axis (X-X) of the landing gear; - at least one axle, mechanically connected to a first side of the strut; - at least one wheel, rotatably mounted about said at least one axle; - at least one damper arranged to dampen a sliding movement of said landing gear strut relative to the structure of the aircraft; - the sliding layer (C, C') is made of a zinc and nickel alloy comprising, in terms of percentage by weight of the alloy, between 12% and 18% nickel, at most 0.5% of other elements such as nickel and zinc, the remainder being zinc; and wherein - the first part also has a protective layer (P, P') against corrosion extending from the sliding layer (C, C'), this protective layer (P, P') being formed of said zinc and nickel alloy.
An electronic cigarette with an improved atomizer, comprising: an atomizing core; wherein the atomizing core comprises a liquid storage assembly and a heating assembly; the liquid storage assembly comprises a liquid storage chip, a PCB, and a liquid storage chip support; the liquid storage chip support is provided with a PCB receiving groove configured to receive the PCB; the liquid storage chip is fixed on the PCB; the heating assembly comprises a heating element and a heating element support; a pin is arranged on the heating element; the heating element support is provided with a heating element receiving groove and a second air guide hole, wherein the heating element receiving groove is configured to receive the heating element; a pin hole is arranged on a wall of the heating element receiving groove; the pin passes through the pin hole, so that the heating element is movably connected to the heating element support; the liquid storage chip is arranged corresponding to the heating element.
A method for operating a conveyor device, which comprises a plurality of drives (2, 2a...2c) located locally in succession in a conveying direction (z) for transporting objects (17... 19), by means of which a target path and/or a target speed of the objects (17... 19) is provided, characterized by the steps: - detecting at least a first value (W 1) of at least one physical characteristic of the objects (17... 19) at a first point in time (t 1) at a first position (P 1), - detecting at least a second value (W 2) of this at least one physical characteristic of the objects (17... 19) after a detection time period (t(x)) at a second point in time (t 2) at a second position (P 2), which is arranged at a detection distance (x) downstream from the first position (P 1), viewed in the conveying direction (z), and - carrying out a plausibility check with regard to the conformance of the first value (W 1) with the second value (W 2) as well as the change of location of the objects (17... 19), which presumably occurred between the detection of the first value (W 1) and the second value (W 2), based on a) the target path provided via the drives (2, 2a...2c) and/or b) the target speed provided via the drives (2, 2a...2c) in combination with the detection time period (t(x)). - detecting at least a first value (W 1) of at least one physical characteristic of the objects (17... 19) at a first point in time (t 1) at a first position (P 1), - detecting at least a second value (W 2) of this at least one physical characteristic of the objects (17... 19) after a detection time period (t(x)) at a second point in time (t 2) at a second position (P 2), which is arranged at a detection distance (x) downstream from the first position (P 1), viewed in the conveying direction (z), and - carrying out a plausibility check with regard to the conformance of the first value (W 1) with the second value (W 2) as well as the change of location of the objects (17... 19), which presumably occurred between the detection of the first value (W 1) and the second value (W 2), based on a) the target path provided via the drives (2, 2a...2c) and/or b) the target speed provided via the drives (2, 2a...2c) in combination with the detection time period (t(x)).
A residential skylight pivot grip assembly for an actuation of a residential skylight comprising a pivot grip and at least one bearing element, which can be fastened to a sash frame of the residential skylight, wherein the pivot grip is supported so as to be pivotably movable by means of the bearing element and has a coupling device for articulating an actuating element of the residential skylight on the pivot grip, and wherein the coupling device has a snap lock for snap-in holding of the actuating element on the pivot grip, characterized in that the pivot grip or the bearing element has a bearing lug, which is open on the edge, and the bearing element or the pivot grip has a bearing pin, wherein a guide opening for the bearing pin leads into the bearing lug and the bearing pin is embodied so as to be at least area by area non-round by means of a cross sectional reduction, so that it can be inserted into the bearing lug only in the case of a mounting angle of the pivot grip, which is located in a mounting angle area, with respect to the bearing element, for the purpose of which the guide opening, in its narrowest opening cross section, has dimensions, which are smaller than the diameter of the bearing pin and at least as large as the dimensions of the bearing pin in the area of the cross sectional reduction.
A reception apparatus comprising: a reception section configured to receive a container containing a video stream obtained by encoding high-frame-rate moving image data; a decoding section configured to decode the video stream to obtain the high-frame-rate moving image data; and a processing section configured to perform, based on blur control information inserted into a layer of the container and/or a layer of the video stream, a blurring process on the obtained high-frame-rate moving image data, wherein the blur control information gives weighting coefficients for individual frames in the blurring process for adding image data of neighboring frames to image data of a current frame. a reception section configured to receive a container containing a video stream obtained by encoding high-frame-rate moving image data; a decoding section configured to decode the video stream to obtain the high-frame-rate moving image data; and a processing section configured to perform, based on blur control information inserted into a layer of the container and/or a layer of the video stream, a blurring process on the obtained high-frame-rate moving image data, wherein the blur control information gives weighting coefficients for individual frames in the blurring process for adding image data of neighboring frames to image data of a current frame.
A static dissipative textile comprising a fabric having a first surface, an electrically conductive coating being disposed on the first surface of the fabric and having a conducting agent and a non-conductive binding agent, wherein the electrically conductive coating is disposed on the first surface of the fabric in a pattern of a plurality of lines, and wherein the lines have a resistance of between 10 6 and 10 13 ohms per 2.54 cm (per inch).
A positive active material for lithium secondary battery, wherein, it is a layered lithium metal compound comprising nickel, cobalt, and manganese, and aluminum, zirconium, and boron are doped, the lithium metal compound is represented by Chemical Formula 1 below: [Chemical Formula 1] Li a Ni x CO y Mn z 1-(x+y+z) O b in the Chemical Formula 1, it is 0.8≤a≤1.3, 1.8≤b≤2.2, 0.8≤x≤0.92, 0<y≤0.15, 0<z≤0.1, and 0<x+y+z<1; and the doping element M comprises Al, Zr, and B; the positive active material comprises a core portion and a shell portion of the core portion surface, the core portion and the shell portion is made of a composition containing Ni, Co, Mn, and M elements in the Chemical Formula 1; with respect to 1 mole of the entire metal containing Ni, Co, Mn, and M, a doping ratio of B among the doping elements M is 0.001 to 0.01 mol, with respect to 1 mole of the entire metal containing Ni, Co, Mn, and M, a doping ratio of Al among the doping elements M is 0.0002 to 0.01 mole, and with respect to 1 mole of the entire metal containing Ni, Co, Mn, and M, a doping ratio of Zr among the doping elements M is 0.0015 to 0.005 mol. the lithium metal compound is represented by Chemical Formula 1 below: [Chemical Formula 1] Li a Ni x CO y Mn z 1-(x+y+z) O b in the Chemical Formula 1, it is 0.8≤a≤1.3, 1.8≤b≤2.2, 0.8≤x≤0.92, 0<y≤0.15, 0<z≤0.1, and 0<x+y+z<1; and the doping element M comprises Al, Zr, and B; the positive active material comprises a core portion and a shell portion of the core portion surface, the core portion and the shell portion is made of a composition containing Ni, Co, Mn, and M elements in the Chemical Formula 1; with respect to 1 mole of the entire metal containing Ni, Co, Mn, and M, a doping ratio of B among the doping elements M is 0.001 to 0.01 mol, with respect to 1 mole of the entire metal containing Ni, Co, Mn, and M, a doping ratio of Al among the doping elements M is 0.0002 to 0.01 mole, and with respect to 1 mole of the entire metal containing Ni, Co, Mn, and M, a doping ratio of Zr among the doping elements M is 0.0015 to 0.005 mol.
An exhaust gas processing method, comprising: desulfurizing a catalyst by raising temperature of the catalyst to a predetermined value, if a front/end temperature difference ΔT is less than a predetermined temperature difference X, while a reducing agent is being injected; determining whether immediately after desulfurization the front/end temperature difference ΔT is above the predetermined temperature difference X; if the front/end temperature difference ΔT is not above the predetermined temperature difference X, determining whether fuel is replenished by detecting the fuel amount; if fuel is replenished, determining whether a travel distance, a fuel consumption amount, or a travel time exceeds a first reference value, after the desulfurization; if the travel distance, fuel consumption amount, or travel time does not exceed the first reference value, desulfurizing the catalyst irregularly; counting the number of times of the irregular desulfurization; and giving alarm that the high sulfur fuel is replenished, if the counting number is larger than a predetermined value. desulfurizing a catalyst by raising temperature of the catalyst to a predetermined value, if a front/end temperature difference ΔT is less than a predetermined temperature difference X, while a reducing agent is being injected; determining whether immediately after desulfurization the front/end temperature difference ΔT is above the predetermined temperature difference X; if the front/end temperature difference ΔT is not above the predetermined temperature difference X, determining whether fuel is replenished by detecting the fuel amount; if fuel is replenished, determining whether a travel distance, a fuel consumption amount, or a travel time exceeds a first reference value, after the desulfurization; if the travel distance, fuel consumption amount, or travel time does not exceed the first reference value, desulfurizing the catalyst irregularly; counting the number of times of the irregular desulfurization; and giving alarm that the high sulfur fuel is replenished, if the counting number is larger than a predetermined value.
Device of an oil distribution for a rotating planet carrier of a mechanical reduction gear of a turbomachine, this device being configured to be integral with a tubular member (16, 50) for supporting a bearing of the planet carrier, said device comprising an oil inlet and a row of oil outlets opening onto an external surface intended to be surrounded at least in part by the said member, characterized in that said device comprising at least two internal cavities connected in series by at least one calibrated orifice, one of said cavities, referred to as a receiving cavity being connected to said oil inlet, and internal calibrated channels for conveying oil which extends from said cavities to orifices of said external surface of the device to form said oil outlets.