mhurhangee/ep-ind-claims huggingface dataset:
An identification key generation apparatus comprising: an identification key provider comprising a plurality of inter-layer contacts or vias between the conductive layers of a semiconductor that serve as a plurality of resistors (210, 220, 230, 240) generated during manufacture based on a random connection state between the conductive layers due to a semiconductor process variation; a discriminator configured to discriminate a first group having a resistance value (R a, R b, R c, R d) greater than a first threshold value (R th.min) and less than a second threshold value (R th.max) among the plurality of resistors (210, 220, 230, 240); a reader configured to read at least one resistor (210, 220, 230, 240) that does not belong to the first group among the plurality of resistors (210, 220, 230, 240), and to provide an identification key in a form of a digital value; a controller configured to record, in a memory, information used to identify a resistor included in the first group among the plurality of resistors (210, 220, 230, 240); and wherein the information used to identify the resistor included in the first group is an address of the resistor included in the first group among the plurality of resistors (210, 220, 230, 240). an identification key provider comprising a plurality of inter-layer contacts or vias between the conductive layers of a semiconductor that serve as a plurality of resistors (210, 220, 230, 240) generated during manufacture based on a random connection state between the conductive layers due to a semiconductor process variation; a discriminator configured to discriminate a first group having a resistance value (R a, R b, R c, R d) greater than a first threshold value (R th.min) and less than a second threshold value (R th.max) among the plurality of resistors (210, 220, 230, 240); a reader configured to read at least one resistor (210, 220, 230, 240) that does not belong to the first group among the plurality of resistors (210, 220, 230, 240), and to provide an identification key in a form of a digital value; a controller configured to record, in a memory, information used to identify a resistor included in the first group among the plurality of resistors (210, 220, 230, 240); and wherein the information used to identify the resistor included in the first group is an address of the resistor included in the first group among the plurality of resistors (210, 220, 230, 240).
A collision-avoidance maneuvering method in congested water, in which when two ships (501, 401, 402) crossing each other on a course in congested water are likely to collide with each other, an own ship is maneuvered with collision avoidance while viewing another ship (401, 402) on a starboard side, the method comprising the steps of: maneuvering the own ship decelerated so as to avoid collision with the other ship (401, 402), the own ship being decelerated by astern power against an inertial force applied in a forward direction of the own ship, the own ship being continuously navigated on a current target course with a propulsion propeller always rotated forward at a stern of the own ship, the astern power being generated as propulsion of a propeller slipstream with rudder angles formed at a pair of right and left high-lift rudders (102, 103) disposed behind the propulsion propeller; controlling, in the decelerating maneuvering, the rudder angles formed at the high-lift rudders (102, 103) within a range from a rudder angle for applying a maximum propeller slipstream as the astern power to a rudder angle for eliminating ahead power of the propeller slipstream, and controlling the deceleration of the own ship by changing the astern power according to the rudder angles; and controlling the rudder angles of the high-lift rudders (102, 103) so as to continuously navigate the own ship on the target course by using the propulsion of the propeller slipstream as the ahead power after the other ship (401, 402) crosses the course of the own ship. maneuvering the own ship decelerated so as to avoid collision with the other ship (401, 402), the own ship being decelerated by astern power against an inertial force applied in a forward direction of the own ship, the own ship being continuously navigated on a current target course with a propulsion propeller always rotated forward at a stern of the own ship, the astern power being generated as propulsion of a propeller slipstream with rudder angles formed at a pair of right and left high-lift rudders (102, 103) disposed behind the propulsion propeller; controlling, in the decelerating maneuvering, the rudder angles formed at the high-lift rudders (102, 103) within a range from a rudder angle for applying a maximum propeller slipstream as the astern power to a rudder angle for eliminating ahead power of the propeller slipstream, and controlling the deceleration of the own ship by changing the astern power according to the rudder angles; and controlling the rudder angles of the high-lift rudders (102, 103) so as to continuously navigate the own ship on the target course by using the propulsion of the propeller slipstream as the ahead power after the other ship (401, 402) crosses the course of the own ship.
Method of modification of the properties of polylactide or compositions containing polylactide, characterized in that polylactide or compositions of polylactide with known additives are mixed with a plasticizer in proportions from 0.2 to 30 weight parts per 100 weight parts of the composition, the said plasticizer being selected from the group consisting of poly(propylene glycol) and poly(propylene oxide) with molecular mass ranging from 425 to 1000 g/mol.
An imidazolium sulfurane of the formula: wherein: R 1 and R 2 each independently represent hydrogen, alkyl, aralkyl, aryl, heteroaryl, each being optionally substituted by one or more hetero atoms selected from O, N, S or halogen, or R 1 and R 2 may together form a hydrocarbon ring structure, optionally substituted by one or more hetero atoms selected from O, N, S and halogen, including aliphatic hydrocarbons, aromatic hydrocarbons and heteroaromatic hydrocarbons; R 3 and R 4 each independently represent a lower alkyl group having 1 to 6 carbon atoms, each lower alkyl group being optionally substituted by one or more hetero atoms selected from O, N, S or halogen; X is an anion selected from halogen or a non- or weak-coordinating anion; Y represents a group of the formula -C≡W wherein W represents N, CR 5 or C-CO 2 R 5 wherein R 5 is selected from the group comprising C 1 to C 20 straight chain, branched chain or cyclic aliphatic hydrocarbons, optionally having one or more unsaturated bonds or C 6 to C 20 aromatic hydrocarbons and partially arene-hydrogenated hydrocarbons, each hydrocarbon optionally being substituted by one or more hetero atoms selected from O, N, S, halogen or a silylgroup; with the proviso, that a compound of the formula wherein R 1 and R 2 are hydrogen, R 3 and R 4 are methyl, X is Br and Y is CN is excluded. R 1 and R 2 each independently represent hydrogen, alkyl, aralkyl, aryl, heteroaryl, each being optionally substituted by one or more hetero atoms selected from O, N, S or halogen, or R 1 and R 2 may together form a hydrocarbon ring structure, optionally substituted by one or more hetero atoms selected from O, N, S and halogen, including aliphatic hydrocarbons, aromatic hydrocarbons and heteroaromatic hydrocarbons; R 3 and R 4 each independently represent a lower alkyl group having 1 to 6 carbon atoms, each lower alkyl group being optionally substituted by one or more hetero atoms selected from O, N, S or halogen; X is an anion selected from halogen or a non- or weak-coordinating anion; Y represents a group of the formula -C≡W wherein W represents N, CR 5 or C-CO 2 R 5 wherein R 5 is selected from the group comprising C 1 to C 20 straight chain, branched chain or cyclic aliphatic hydrocarbons, optionally having one or more unsaturated bonds or C 6 to C 20 aromatic hydrocarbons and partially arene-hydrogenated hydrocarbons, each hydrocarbon optionally being substituted by one or more hetero atoms selected from O, N, S, halogen or a silylgroup; with the proviso, that a compound of the formula wherein R 1 and R 2 are hydrogen, R 3 and R 4 are methyl, X is Br and Y is CN is excluded.
A thrust constant derivation method for deriving a thrust constant of a linear motor, the thrust constant representing an occurrence rate of a thrust in relation to a current in the linear motor which is provided with a track member which includes one of a magnet and a coil extending in a movement direction, and a moving body which includes the other of the magnet and the coil mounted to the track member in a movable manner, the linear motor generating a thrust in the movement direction between the magnet and the coil by causing a current to flow in the coil, wherein local thrust constants (N1-N6) which are local thrust constants (N1-N6) of a plurality of locations (X1-X6) on the track member are derived, and the thrust constants of arbitrary positions on the track member are derived based on the local thrust constants (N1-N6), characterized by an average value derivation step of moving the moving body along a long movement zone on the track member and deriving an average thrust constant, which is an average thrust constant in the long movement zone, based on an actual measurement; a local value derivation step of causing the moving body to perform micro-movements in the movement direction at each location (X1-X6) of the plurality of locations (X1-X6) and deriving each of the local thrust constants (N1-N6) at each location (X1-X6) based on each actual measurement; a local value correction step of calculating the difference (ΔN) between an average value of the local thrust constants and the average thrust constant and correcting the local thrust constant (N1-N6) of each location (X1-X6) by the difference (ΔN) to obtain a corrected thrust constant (Nc1-Nc6) of each location (X1-X6); and an interpolation derivation step of deriving the thrust constant (N) of an arbitrary position on the track member by interpolating the corrected thrust constants (Nc1-Nc6) of the locations (X1-X6), wherein the long movement zone is a total length zone in which the moving body is capable of moving on the track member or a zone obtained by subtracting a minimal startup acceleration zone (Ls) and a stopping deceleration zone (Le) from the total length zone.
A silicon purification device for separating and removing the evaporated impurities from the silicon melt generated by the heating and fusion of silicon at pressures below 500 Pa, the device comprising a processing chamber which includes crucible containing the silicon, a heating means, a pressure reduction means and an impurities condensation means for cooling and condensing the vapour of impurities evaporating from the liquid surface of the silicon melt, characterised in that the silicon purification device further comprises an impurities reception and containment means for receiving and containing impurities, the impurities reception and containment means being arranged such that during silicon purification processing, the impurities reception and containment means is located in standby position, and the vapour of the impurities is condensed by the impurities condensations means, and when the silicon purification processing is suspended and/or terminated, the impurities reception and containment means is located in an operating position between the impurities condensation means and the liquid surface of the silicon melt, receiving and containing the impurities dropping down.
Method of manufacturing a substrate for a front side type image sensor, comprising the following steps: - providing a donor substrate comprising a semiconductor material suitable for epitaxial growth of silicon-germanium, said semiconductor material being silicon; - forming an embrittlement zone (33, 41) by implantation of atomic species in the donor substrate so as to define a layer of silicon; - providing a support substrate; - bonding the donor substrate to the support substrate, with an electrically insulating layer at the bonding interface; - detaching the donor substrate according to said embrittlement zone so as to transfer the silicon layer onto the support substrate; - epitaxially growing silicon-germanium on the transferred silicon layer which serves as a seed layer so as to obtain on the transferred silicon layer a silicon-germanium layer with a thickness greater than 1 μm, the germanium content of said layer being less than or equal to 8%. - providing a donor substrate comprising a semiconductor material suitable for epitaxial growth of silicon-germanium, said semiconductor material being silicon; - forming an embrittlement zone (33, 41) by implantation of atomic species in the donor substrate so as to define a layer of silicon; - providing a support substrate; - bonding the donor substrate to the support substrate, with an electrically insulating layer at the bonding interface; - detaching the donor substrate according to said embrittlement zone so as to transfer the silicon layer onto the support substrate; - epitaxially growing silicon-germanium on the transferred silicon layer which serves as a seed layer so as to obtain on the transferred silicon layer a silicon-germanium layer with a thickness greater than 1 μm, the germanium content of said layer being less than or equal to 8%.
A method for preserving a color gamut of content of a source including a gamut mapping of said content, characterized by: - determining metadata describing said color gamut of content of a source, wherein the metadata includes color gamut of said source defined by a set of vertices with or without indexed facets in a chosen color space, the metadata including a FACET_MODE field indicative of whether the following data fields include indexed vertices, followed by a NUMBER_FACETS field indicative of the number of facets and packed facet indices dependent on the FACET_MODE; - communicating said metadata to a data channel for an adaptation of said gamut mapping that preserves saturation and contrast levels of the source. - determining metadata describing said color gamut of content of a source, wherein the metadata includes color gamut of said source defined by a set of vertices with or without indexed facets in a chosen color space, the metadata including a FACET_MODE field indicative of whether the following data fields include indexed vertices, followed by a NUMBER_FACETS field indicative of the number of facets and packed facet indices dependent on the FACET_MODE; - communicating said metadata to a data channel for an adaptation of said gamut mapping that preserves saturation and contrast levels of the source.
A refrigerator, comprising: a refrigerator body; a first inner container and a second inner container, the first inner container and the second inner container being both disposed in the refrigerator body; a wire tube evaporator and a coiled tube evaporator, the wire tube evaporator comprising a first wire tube evaporator provided in the first inner container and a second wire tube evaporator provided in the second inner container, the coiled tube evaporator comprising a first coiled tube evaporator wound on an outside of the first inner container and a second coiled tube evaporator wound on an outside of the second inner container, two ends of the first wire tube evaporator being each provided with a first connecting tube, the two first connecting tubes both extending out of the first inner container, the first coiled tube evaporator being connected to a free end of one of the two first connecting tubes, two ends of the second wire tube evaporator being each provided with a second connecting tube, the two second connecting tubes both extending out of the second inner container, the second coiled tube evaporator being connected to a free end of one of the two second connecting tubes, and a free end of the other of the two first connecting tubes and a free end of the other of the two second connecting tubes being connected. a refrigerator body; a first inner container and a second inner container, the first inner container and the second inner container being both disposed in the refrigerator body; a wire tube evaporator and a coiled tube evaporator, the wire tube evaporator comprising a first wire tube evaporator provided in the first inner container and a second wire tube evaporator provided in the second inner container, the coiled tube evaporator comprising a first coiled tube evaporator wound on an outside of the first inner container and a second coiled tube evaporator wound on an outside of the second inner container, two ends of the first wire tube evaporator being each provided with a first connecting tube, the two first connecting tubes both extending out of the first inner container, the first coiled tube evaporator being connected to a free end of one of the two first connecting tubes, two ends of the second wire tube evaporator being each provided with a second connecting tube, the two second connecting tubes both extending out of the second inner container, the second coiled tube evaporator being connected to a free end of one of the two second connecting tubes, and a free end of the other of the two first connecting tubes and a free end of the other of the two second connecting tubes being connected.
Cage for a ball bearing unit, the cage comprising: - a plurality of pockets each delimited by a respective spherical surface having a centre lying in a radial mid-plane of the bearing, - two half-cages (51, 52) substantially symmetrical about the mid-plane, and connected to one another, each half-cage having an annular body and a plurality of partially hemispherical cavities (64, 66, 68) axially facing the hemispherical cavities of the opposite half-cage so as to define therewith the pockets; - connecting means (69, 70) associated with each cage for connecting together the two half-cages; the cage comprising, for each half-cage (51, 52), two substantially concentric and circumferentially continuous radial ridges (56, 57) extending radially in opposite directions from each annular body, of which the first ridge extends in a radially outward direction for sealingly engaging a groove formed in the outer ring of the bearing unit, and the second ridge extends in a radially inward direction for sealingly engaging a groove formed in the inner ring of the bearing unit; characterized in that a plurality of axial projections (65, 67) defining the hemispherical cavities extends from one side of the annular body facing the mid-plane and includes: a first plurality of axial projections having respective concave surfaces lying in a same ideal spherical surface and substantially facing one another in pairs, and a second plurality of axial coupling projections, circumferentially thicker than those of the first plurality of axial projections, arranged alternately with the pairs of the first axial projections, each axial coupling projection providing a partially hemispherical cavity and, on both sides of this cavity in the circumferential direction, one of the connecting means or seats for mutual connection with the opposite half-cage. - a plurality of pockets each delimited by a respective spherical surface having a centre lying in a radial mid-plane of the bearing, - two half-cages (51, 52) substantially symmetrical about the mid-plane, and connected to one another, each half-cage having an annular body and a plurality of partially hemispherical cavities (64, 66, 68) axially facing the hemispherical cavities of the opposite half-cage so as to define therewith the pockets; - connecting means (69, 70) associated with each cage for connecting together the two half-cages; a first plurality of axial projections having respective concave surfaces lying in a same ideal spherical surface and substantially facing one another in pairs, and a second plurality of axial coupling projections, circumferentially thicker than those of the first plurality of axial projections, arranged alternately with the pairs of the first axial projections, each axial coupling projection providing a partially hemispherical cavity and, on both sides of this cavity in the circumferential direction, one of the connecting means or seats for mutual connection with the opposite half-cage.
A drive unit (10, 65) for a hybrid vehicle, the drive unit (10, 65) including a prime mover that includes an engine, a first motor, and a second motor, wherein a drive torque generated by the prime mover is delivered to an output element connected to drive wheels; a first differential mechanism that includes a first rotary element connected to the engine, a second rotary element, and a third rotary element; a second differential mechanism that includes a fourth rotary element connected to the second rotary element, a fifth rotary element connected to the first motor, and a sixth rotary element connected to the second motor and the output element; a first engagement device that selectively connects the first rotary element and the second rotary element or selectively connects the first rotary element and the third rotary element or selectively connects the second rotary element and the third rotary element when engaged; a second engagement device; and a third engagement device, characterized in that the second engagement device connects the third rotary element to the fifth rotary element or to the sixth rotary element when engaged; and the third engagement device connects the first rotary element and a predetermined stationary member when engaged. a prime mover that includes an engine, a first motor, and a second motor, wherein a drive torque generated by the prime mover is delivered to an output element connected to drive wheels; a first differential mechanism that includes a first rotary element connected to the engine, a second rotary element, and a third rotary element; a second differential mechanism that includes a fourth rotary element connected to the second rotary element, a fifth rotary element connected to the first motor, and a sixth rotary element connected to the second motor and the output element; a first engagement device that selectively connects the first rotary element and the second rotary element or selectively connects the first rotary element and the third rotary element or selectively connects the second rotary element and the third rotary element when engaged; a second engagement device; and a third engagement device, characterized in that the second engagement device connects the third rotary element to the fifth rotary element or to the sixth rotary element when engaged; and the third engagement device connects the first rotary element and a predetermined stationary member when engaged.
A system comprising: means for receiving a request from a Secure User Plane Location, SUPL, agent for at least one position estimate for a SUPL enabled terminal, SET, means for determining service capabilities of a SUPL Location Platform, SLP, means for selecting and requesting service from the SLP that is consistent with the service capabilities of the SLP; means for receiving from the SLP a service modification request with service parameters that are modified with respect to the service requested from the SLP; means for communicating with the SLP to determine at least one position estimate for the SET; and means for communicating with the SLP to provide to the SUPL agent at least one position estimate for the SET. means for receiving a request from a Secure User Plane Location, SUPL, agent for at least one position estimate for a SUPL enabled terminal, SET, means for determining service capabilities of a SUPL Location Platform, SLP, means for selecting and requesting service from the SLP that is consistent with the service capabilities of the SLP; means for receiving from the SLP a service modification request with service parameters that are modified with respect to the service requested from the SLP; means for communicating with the SLP to determine at least one position estimate for the SET; and means for communicating with the SLP to provide to the SUPL agent at least one position estimate for the SET.