mhurhangee/patent-ind-claim-en huggingface dataset:
A photoelectric conversion element comprising: a first electrode ; a hole blocking layer ; a photoelectric conversion layer ; a second electrode ; a third electrode ; a photoelectric conversion part in which the first electrode , the hole blocking layer , the photoelectric conversion layer , and the second electrode are stacked; an electrode contact part in which the second electrode is in contact with the third electrode ; and a division part dividing the photoelectric conversion part and the electrode contact part , characterized in that an area S1, defined as the total area where the second electrode is in contact with the third electrode in the electrode contact part , and an area S2, defined as the total area of the photoelectric conversion part , satisfy expression below: 1.0 × 10 − 5 ≤ 100 × S 1 / S 2 a first electrode ; a hole blocking layer ; a photoelectric conversion layer ; a second electrode ; a third electrode ; a photoelectric conversion part in which the first electrode , the hole blocking layer , the photoelectric conversion layer , and the second electrode are stacked; an electrode contact part in which the second electrode is in contact with the third electrode ; and a division part dividing the photoelectric conversion part and the electrode contact part , characterized in that an area S1, defined as the total area where the second electrode is in contact with the third electrode in the electrode contact part , and an area S2, defined as the total area of the photoelectric conversion part , satisfy expression below: 1.0 × 10 − 5 ≤ 100 × S 1 / S 2
Polybenzoxazine sulfide whose repeating units include at least one unit corresponding to formula (I) or (II): in which the two oxazine rings are connected together via a central aromatic group, the benzene ring of which bears one, two, three or four groups of formula -S x -R in which "x" is an integer from 1 to 8 and R represents hydrogen or a hydrocarbon-based group including 1 to 10 carbon atoms and optionally a heteroatom chosen from O, S, N and P; in which the two symbols "*" identical or different represent any attachment of the unit to a carbon atom or to a heteroatom; and in which one or more hydrogen atoms of at least one or of each benzene nucleus of the two oxazine rings, and also those of the central benzene ring, may optionally also be substituted with various substituents.
A method of manufacturing a flexible organic light-emitting display device , the method comprising: forming a lower flexible substrate assembly including a first flexible substrate , a thin film transistor and an organic light emitting element disposed over an upper surface of the first flexible substrate , the organic light emitting element configured to emit white light and is electrically connected to the thin film transistor ; forming an upper flexible substrate assembly including a second flexible substrate , a color filter layer and a touch sensing unit disposed over a lower surface of the second flexible substrate, the touch sensing unit including an insulating film layer and a first electrode pattern and a second electrode pattern formed thereon; and bonding together the lower flexible substrate assembly and the upper flexible substrate assembly using a bonding layer , wherein the first electrode pattern is on a lower surface of the insulating film layer and the second electrode pattern is on an upper surface of the insulating film layer , and wherein the touch sensing unit is disposed between the color filter layer and the bonding layer such that the first electrode pattern is in direct contact with the bonding layer . forming a lower flexible substrate assembly including a first flexible substrate , a thin film transistor and an organic light emitting element disposed over an upper surface of the first flexible substrate , the organic light emitting element configured to emit white light and is electrically connected to the thin film transistor ; forming an upper flexible substrate assembly including a second flexible substrate , a color filter layer and a touch sensing unit disposed over a lower surface of the second flexible substrate, the touch sensing unit including an insulating film layer and a first electrode pattern and a second electrode pattern formed thereon; and bonding together the lower flexible substrate assembly and the upper flexible substrate assembly using a bonding layer , wherein the first electrode pattern is on a lower surface of the insulating film layer and the second electrode pattern is on an upper surface of the insulating film layer , and wherein the touch sensing unit is disposed between the color filter layer and the bonding layer such that the first electrode pattern is in direct contact with the bonding layer .
A therapeutic composition comprising: a. acellular amniotic membrane particles; b. a carrier fluid; wherein the acellular amniotic membrane particles consist essentially of micronized amniotic membrane; wherein the carrier comprises an acellular amniotic fluid; and wherein the therapeutic composition is essentially free of any viable amniotic membrane cells or viable amniotic fluid cells. a. acellular amniotic membrane particles; b. a carrier fluid;
A method for estimation of state of health of a rechargeable battery , the method comprising: obtaining input data of a set of predetermined battery features that jointly indicates State of Health of the battery , applying a plurality of machine learning algorithms to conduct state of health estimation of the battery , wherein each machine learning algorithm, based on obtained input data from the battery features, calculates an estimation of state of health of the battery , as well as quantitative estimation of a confidence interval/value of the state of health estimation of the battery , and applying a Kalman filter based fusion algorithm for combining the state of health estimations from all of said plurality of machine learning algorithms, for providing a fused state of health estimation. obtaining input data of a set of predetermined battery features that jointly indicates State of Health of the battery , applying a plurality of machine learning algorithms to conduct state of health estimation of the battery , wherein each machine learning algorithm, based on obtained input data from the battery features, calculates an estimation of state of health of the battery , as well as quantitative estimation of a confidence interval/value of the state of health estimation of the battery , and applying a Kalman filter based fusion algorithm for combining the state of health estimations from all of said plurality of machine learning algorithms, for providing a fused state of health estimation.
An in-vehicle charging apparatus for charging a storage battery installed in a vehicle from a power supply provided outside the vehicle through a power line extending via an earth leakage circuit-breaker , the apparatus comprising: a storage section adapted to store vehicle information relating to the vehicle; a vehicle-side power line communication, PLC, communication control section adapted to output a control signal for closing the earth leakage circuit-breaker , and subsequently to establish a PLC communication line using the power line as a communication line and transmit the vehicle information stored in the storage section to the outside of the vehicle, when determining that the vehicle information stored in the storage section needs to be transmitted to the outside of the vehicle, wherein the vehicle-side PLC communication control section is adapted to perform control such that the earth leakage circuit-breaker is turned OFF upon completion of the transmission of the vehicle information. a storage section adapted to store vehicle information relating to the vehicle; a vehicle-side power line communication, PLC, communication control section adapted to output a control signal for closing the earth leakage circuit-breaker , and subsequently to establish a PLC communication line using the power line as a communication line and transmit the vehicle information stored in the storage section to the outside of the vehicle, when determining that the vehicle information stored in the storage section needs to be transmitted to the outside of the vehicle, wherein the vehicle-side PLC communication control section is adapted to perform control such that the earth leakage circuit-breaker is turned OFF upon completion of the transmission of the vehicle information.
A system for neutralizing a target aerial vehicle (104a; 104b), comprising: a projectile launching mechanism (200a; 200b); a projectile launchable by the projectile launching mechanism (200a; 200b); an aerial vehicle countermeasure ; and characterized in that the system further comprises a counter-attack unmanned aerial vehicle (UAV) that is supported by and separable from the projectile and which comprises the aerial vehicle countermeasure , wherein the projectile comprises a first housing section and a second housing section that are releasably coupled to each other and that define an inner chamber that contains the counter-attack UAV in a folded position, wherein, in response to detection of a target aerial vehicle (104a; 104b), the projectile launching mechanism (200a; 200b) is configured to launch the projectile , wherein the projectile further comprises a housing release mechanism configured to at least partially separate the first housing section from the second housing section to expose the inner chamber, thereby facilitating separation and release the counter-attack UAV from the projectile , and wherein upon release of the counter-attack UAV from the projectile , the counter-attack UAV is operable to neutralize the target aerial vehicle (104a; 104b) with the aerial vehicle countermeasure . a projectile launching mechanism (200a; 200b); a projectile launchable by the projectile launching mechanism (200a; 200b); an aerial vehicle countermeasure ; and characterized in that the system further comprises a counter-attack unmanned aerial vehicle (UAV) that is supported by and separable from the projectile and which comprises the aerial vehicle countermeasure , wherein the projectile comprises a first housing section and a second housing section that are releasably coupled to each other and that define an inner chamber that contains the counter-attack UAV in a folded position, wherein, in response to detection of a target aerial vehicle (104a; 104b), the projectile launching mechanism (200a; 200b) is configured to launch the projectile , wherein the projectile further comprises a housing release mechanism configured to at least partially separate the first housing section from the second housing section to expose the inner chamber, thereby facilitating separation and release the counter-attack UAV from the projectile , and wherein upon release of the counter-attack UAV from the projectile , the counter-attack UAV is operable to neutralize the target aerial vehicle (104a; 104b) with the aerial vehicle countermeasure .
An assembly for a turbomachine of an aircraft, the assembly comprising: - a metal gas outlet for the turbomachine, - a central element for ejecting gas, which is annular about an axis (X) and adapted to have gas ejected around it by the turbomachine, from upstream to downstream, and - a connecting flange interposed between, upstream, the metal gas outlet for the turbomachine, and downstream, the central element , to connect them together, the connecting flange comprising an annular portion , and, circumferentially, flexible tabs individually having, axially: -- a first end at which the tab is connected to said annular portion, and -- a second free end at which said tab is attached with the central element , the second free end being located axially upstream of the first end , and, on said flexible tab , the second free end extends radially inwardly with respect to the first end , characterised in that the central element has a peripheral wall : - provided with an acoustic-attenuation structure , and - having, upstream of the acoustic-attenuation structure, an upstream end portion : -- which is located radially inwardly with respect to the flexible tabs , and -- where the central element is attached with said flexible tabs at said second free ends , so that the acoustic-attenuation structure is confined downstream of the upstream end portion through which the attachment with the flexible tabs takes place. - a metal gas outlet for the turbomachine, - a central element for ejecting gas, which is annular about an axis (X) and adapted to have gas ejected around it by the turbomachine, from upstream to downstream, and - a connecting flange interposed between, upstream, the metal gas outlet for the turbomachine, and downstream, the central element , to connect them together, the connecting flange comprising an annular portion , and, circumferentially, flexible tabs individually having, axially: -- a first end at which the tab is connected to said annular portion, and -- a second free end at which said tab is attached with the central element , the second free end being located axially upstream of the first end , and, -- a first end at which the tab is connected to said annular portion, and -- a second free end at which said tab is attached with the central element , the second free end being located axially upstream of the first end , and, - provided with an acoustic-attenuation structure , and - having, upstream of the acoustic-attenuation structure, an upstream end portion : -- which is located radially inwardly with respect to the flexible tabs , and -- where the central element is attached with said flexible tabs at said second free ends , so that the acoustic-attenuation structure is confined downstream of the upstream end portion through which the attachment with the flexible tabs takes place. -- which is located radially inwardly with respect to the flexible tabs , and -- where the central element is attached with said flexible tabs at said second free ends , so that the acoustic-attenuation structure is confined downstream of the upstream end portion through which the attachment with the flexible tabs takes place.
A system for measuring the focus state of an optical instrument , said system comprising: - at least one first optical element configured to form an image (P') of an exit pupil (P) of an objective of said optical instrument ; - at least one second optical element placed substantially where said image (P') of said exit pupil (P) is formed and configured to deviate at least part of the rays coming from said exit pupil so that, downstream said image (P') of said exit pupil (P), first rays (R1) coming from a first portion of said exit pupil (P) and second rays (R2) coming from a second portion of said exit pupil (P) follow separate optical paths, said first portion and said second portion of said exit pupil (P) being non overlapping, and are focused into two bidimensional images (IM1, IM2); and - a computer configured to determine a mutual distance (Y) between said two bidimensional images (IM1, IM2) as a mutual rigid lateral displacement between said bidimensional images (IM1, IM2) and, based on said mutual distance (Y), to determine a corresponding defocus of said optical instrument , wherein said computer is configured to apply to said two bidimensional images (IM1, IM2) a global merit function, providing a measurement of their similarity, and to determine said mutual distance (Y) as the mutual rigid lateral displacement between said two bidimensional images (IM1, IM2) which maximizes the value of said global merit function. - at least one first optical element configured to form an image (P') of an exit pupil (P) of an objective of said optical instrument ; - at least one second optical element placed substantially where said image (P') of said exit pupil (P) is formed and configured to deviate at least part of the rays coming from said exit pupil so that, downstream said image (P') of said exit pupil (P), first rays (R1) coming from a first portion of said exit pupil (P) and second rays (R2) coming from a second portion of said exit pupil (P) follow separate optical paths, said first portion and said second portion of said exit pupil (P) being non overlapping, and are focused into two bidimensional images (IM1, IM2); and - a computer configured to determine a mutual distance (Y) between said two bidimensional images (IM1, IM2) as a mutual rigid lateral displacement between said bidimensional images (IM1, IM2) and, based on said mutual distance (Y), to determine a corresponding defocus of said optical instrument ,
A method for wireless communications in a wireless network via an orthogonal frequency division multiplexed, OFDM radio access technology, comprising: determining dimensions of a matrix to be used in a row-column interleaver for performing interleaving of modulated symbols from a plurality of code blocks into bundles of resource elements, said modulated symbols carrying bits of said code blocks, based on a ratio of a code block size to a number of bits to be mapped into each resource element, given by ⌈ N CB Bits ∑ i = 1 N Layers N QAM i ⋅ k ⌉ , wherein N CB Bits is the number of bits in a code block, k is the resource element bundle size, N Layers is a number of transmission layers, and N QAM i is the QAM order for layer i, wherein determining the dimensions of the matrix comprises determining a number of rows N rows of the matrix based on N REs per CB = N CB Bits ∑ i = 1 N Layers N QAM i , and N rows = ⌈ N REs per CB 1 k ⌉ , and determining the number of columns N columns of the matrix based on a total number of bundles of resource elements N k-REs , given by N columns = ⌈ N k − REs N rows ⌉ ; performing the interleaving of the modulated symbols according to the matrix having the determined dimensions; and transmitting the interleaved modulated symbols in the wireless network via the radio access technology. determining dimensions of a matrix to be used in a row-column interleaver for performing interleaving of modulated symbols from a plurality of code blocks into bundles of resource elements, said modulated symbols carrying bits of said code blocks, based on a ratio of a code block size to a number of bits to be mapped into each resource element, given by ⌈ N CB Bits ∑ i = 1 N Layers N QAM i ⋅ k ⌉ , wherein N CB Bits is the number of bits in a code block, k is the resource element bundle size, N Layers is a number of transmission layers, and N QAM i is the QAM order for layer i, wherein determining the dimensions of the matrix comprises determining a number of rows N rows of the matrix based on N REs per CB = N CB Bits ∑ i = 1 N Layers N QAM i , and N rows = ⌈ N REs per CB 1 k ⌉ , and determining the number of columns N columns of the matrix based on a total number of bundles of resource elements N k-REs , given by N columns = ⌈ N k − REs N rows ⌉ ; performing the interleaving of the modulated symbols according to the matrix having the determined dimensions; and transmitting the interleaved modulated symbols in the wireless network via the radio access technology.
A motor comprising: a rotor that rotates about a rotation axis; and a stator facing the rotor while having a gap from the rotor , wherein the stator comprises: a ring-shaped connection core formed by connecting a plurality of divided cores ; an insulator formed by resin molding by an insertion forming as if surrounding the connection core ; and a reinforcement ring mounted on an outer circumferential portion of the connection core , and wherein an inner diameter (r) of the connection core is set smaller than an inner diameter (R) of the divided cores that are bent in a half moon shape when connected, characterised in that a penetration hole through which a slide pin (P) penetrates is formed at least at a coupling portion (A, B, C, D) or a neighboring portion thereof of the divided cores . a rotor that rotates about a rotation axis; and a stator facing the rotor while having a gap from the rotor , a ring-shaped connection core formed by connecting a plurality of divided cores ; an insulator formed by resin molding by an insertion forming as if surrounding the connection core ; and a reinforcement ring mounted on an outer circumferential portion of the connection core , and wherein an inner diameter (r) of the connection core is set smaller than an inner diameter (R) of the divided cores that are bent in a half moon shape when connected, characterised in that a penetration hole through which a slide pin (P) penetrates is formed at least at a coupling portion (A, B, C, D) or a neighboring portion thereof of the divided cores .
A control device for an automatic transmission , comprising: a friction engagement element (BR1, BR2, CL1, CL2, CL3); and a control unit : configured to control a gear change operation by supplying and/or discharging hydraulic fluid for forming a gear stage to and/or from the friction engagement element (BR1, BR2, CL1, CL2, CL3); and configured to control a switching operation to switch a supply amount of lubricant to the friction engagement element (BR1, BR2, CL1, CL2, CL3) according to an operating state of a vehicle, wherein the control unit is further configured to control the gear change operation and the switching operation to not overlap with one another, characterized in that the control unit is configured to prohibit the gear change operation when the control unit performs the switching operation. a friction engagement element (BR1, BR2, CL1, CL2, CL3); and a control unit : configured to control a gear change operation by supplying and/or discharging hydraulic fluid for forming a gear stage to and/or from the friction engagement element (BR1, BR2, CL1, CL2, CL3); and configured to control a switching operation to switch a supply amount of lubricant to the friction engagement element (BR1, BR2, CL1, CL2, CL3) according to an operating state of a vehicle, configured to control a gear change operation by supplying and/or discharging hydraulic fluid for forming a gear stage to and/or from the friction engagement element (BR1, BR2, CL1, CL2, CL3); and configured to control a switching operation to switch a supply amount of lubricant to the friction engagement element (BR1, BR2, CL1, CL2, CL3) according to an operating state of a vehicle, wherein the control unit is further configured to control the gear change operation and the switching operation to not overlap with one another, characterized in that the control unit is configured to prohibit the gear change operation when the control unit performs the switching operation.