mhurhangee/ep-ind-claims huggingface dataset:
An antimicrobial and anti-biofouling coating formulation, comprising: a hollow round colloidal structure, comprising: an active polymer shell; and an active or inert core; wherein the active polymer shell comprises two or more polymers with antimicrobial and anti-biofouling activities selected from the group consisting of polyethylenimine, poly(diallyldimethylammonium chloride) (PDDA) and polyhexamethylene biguanide (PHMB); wherein either the core is active and contains one or more disinfectants, biocides and fragrances; or the core is inert and contains water or an inert solvent; and wherein the hollow round colloidal structure further comprises stabilizers and is stable for at least 3 months, and wherein the stabilizers are present in concentrations of 0.01-20% (w/v) of polyvinyl alcohol having a mw of 31,000-186,000 g/mol; 0.01-20% (w/v) of poly(ethylene glycol) methacrylate (PEGMA) having a Mn of 200-1000; and 0.01-20% (w/v) of methoxypoly(ethylene glycol) methacrylate (MPEGMA) having a Mn of 200-5000. an active polymer shell; and an active or inert core; wherein the active polymer shell comprises two or more polymers with antimicrobial and anti-biofouling activities selected from the group consisting of polyethylenimine, poly(diallyldimethylammonium chloride) (PDDA) and polyhexamethylene biguanide (PHMB); wherein either the core is active and contains one or more disinfectants, biocides and fragrances; or the core is inert and contains water or an inert solvent; and wherein the hollow round colloidal structure further comprises stabilizers and is stable for at least 3 months, and wherein the stabilizers are present in concentrations of 0.01-20% (w/v) of polyvinyl alcohol having a mw of 31,000-186,000 g/mol; 0.01-20% (w/v) of poly(ethylene glycol) methacrylate (PEGMA) having a Mn of 200-1000; and 0.01-20% (w/v) of methoxypoly(ethylene glycol) methacrylate (MPEGMA) having a Mn of 200-5000.
Polymer having end groups of the formula where R 1a is a monovalent hydrocarbyl radical having 1 to 12 carbon atoms; R 1b is a hydrogen atom or a monovalent hydrocarbyl radical having 1 to 12 carbon atoms; R 2 is a hydrogen atom or a monovalent hydrocarbyl radical which has 1 to 12 carbon atoms and optionally contains ether groups, ester groups, nitrile groups, amino groups or silane groups; R 3 is a linear or branched alkylene or cycloalkylene radical having 1 to 20 carbon atoms, optionally having aromatic moieties, and optionally having one or more heteroatoms, especially nitrogen atoms; R 4 is an alkyl radical having 1 to 8 carbon atoms; R 5 is an alkyl radical which has 1 to 10 carbon atoms and optionally contains ether groups; and x is 0, 1 or 2. R 1a is a monovalent hydrocarbyl radical having 1 to 12 carbon atoms; R 1b is a hydrogen atom or a monovalent hydrocarbyl radical having 1 to 12 carbon atoms; R 2 is a hydrogen atom or a monovalent hydrocarbyl radical which has 1 to 12 carbon atoms and optionally contains ether groups, ester groups, nitrile groups, amino groups or silane groups; R 3 is a linear or branched alkylene or cycloalkylene radical having 1 to 20 carbon atoms, optionally having aromatic moieties, and optionally having one or more heteroatoms, especially nitrogen atoms; R 4 is an alkyl radical having 1 to 8 carbon atoms; R 5 is an alkyl radical which has 1 to 10 carbon atoms and optionally contains ether groups; and x is 0, 1 or 2.
An electroacoustic driver, comprising: a diaphragm; a diaphragm drive system configured to subject the diaphragm to a motion; and a diaphragm suspension configured to guide the diaphragm; wherein the diaphragm suspension comprises an option taken from i) a spider and a surround or ii) the surround; the surround comprising one or more active elements being integrated into the surround and configured to actively influence the motion of the diaphragm in accordance to a control signal by changing a restoring force in accordance to the control signal and/or by applying a force to the diaphragm in accordance to the control signal, wherein the electroacoustic driver comprises a basket, wherein the surround is arranged between the basket and the diaphragm such that the surround guides and seals the diaphragm against the basket; wherein the one or more active elements comprise electrical devices or piezo electrical devices; characterized in that the electroacoustic driver comprises a controller configured to output the control signal to the one or more active elements of the diaphragm suspension based on detected non-linearities and/or based on an audio signal via which the diaphragm drive system is controlled; the electroacoustic driver also comprising a sensor attached to the diaphragm and/or to the diaphragm suspension configured for detecting non-linearities in the piston-like motion of the diaphragm; and/or wherein the sensor is formed by one of the active elements. a diaphragm; a diaphragm drive system configured to subject the diaphragm to a motion; and a diaphragm suspension configured to guide the diaphragm; wherein the diaphragm suspension comprises an option taken from i) a spider and a surround or ii) the surround; the surround comprising one or more active elements being integrated into the surround and configured to actively influence the motion of the diaphragm in accordance to a control signal by changing a restoring force in accordance to the control signal and/or by applying a force to the diaphragm in accordance to the control signal, wherein the electroacoustic driver comprises a basket, wherein the surround is arranged between the basket and the diaphragm such that the surround guides and seals the diaphragm against the basket; wherein the one or more active elements comprise electrical devices or piezo electrical devices; characterized in that the electroacoustic driver comprises a controller configured to output the control signal to the one or more active elements of the diaphragm suspension based on detected non-linearities and/or based on an audio signal via which the diaphragm drive system is controlled; the electroacoustic driver also comprising a sensor attached to the diaphragm and/or to the diaphragm suspension configured for detecting non-linearities in the piston-like motion of the diaphragm; and/or wherein the sensor is formed by one of the active elements.
Method for dampening sound in water, wherein a bubble curtain is generated by means of a bubble curtain generation device with (a) a pressure line for conducting compressed air - that has a wall which encloses an interior space, - the wall comprising a number of openings, each of which has an opening cross-section, characterised by the fact that the bubble curtain generation device (b) has a membrane that - comprises a multitude of pores, each of a particular pore size, and - that is designed such that compressed air can be passed through the membrane into the surrounding water in the form of small bubbles through the pores, (c) wherein the wall is enclosed by a membrane, at least in the area surrounding the openings, that is designed such that compressed air can be passed out of the interior space through the openings, then through the membrane in the form of small bubbles and then through the pores into the surrounding water, (d) wherein the opening cross-sections and the pore sizes are selected in such a way that an air pressure (p 26) forms in the interior space and an applied pressure (p 32) forms in a space between the pressure line and the membrane for which the following applies: p 32 − p Umgebung p 26 − p Umgebung ≤ 0, 3, wherein p Umgebung represents the ambient pressure. (a) a pressure line for conducting compressed air - that has a wall which encloses an interior space, - the wall comprising a number of openings, each of which has an opening cross-section, characterised by the fact that the bubble curtain generation device - that has a wall which encloses an interior space, - the wall comprising a number of openings, each of which has an opening cross-section, characterised by the fact that the bubble curtain generation device (b) has a membrane that - comprises a multitude of pores, each of a particular pore size, and - that is designed such that compressed air can be passed through the membrane into the surrounding water in the form of small bubbles through the pores, - comprises a multitude of pores, each of a particular pore size, and - that is designed such that compressed air can be passed through the membrane into the surrounding water in the form of small bubbles through the pores, (c) wherein the wall is enclosed by a membrane, at least in the area surrounding the openings, that is designed such that compressed air can be passed out of the interior space through the openings, then through the membrane in the form of small bubbles and then through the pores into the surrounding water, (d) wherein the opening cross-sections and the pore sizes are selected in such a way that an air pressure (p 26) forms in the interior space and an applied pressure (p 32) forms in a space between the pressure line and the membrane for which the following applies: p 32 − p Umgebung p 26 − p Umgebung ≤ 0, 3, wherein p Umgebung represents the ambient pressure.
A safety evaluation method comprising: preparing a sample for secondary battery electrode evaluation in which a short circuit occurs when components included in the sample contact each other; applying a predetermined pressure which causes the contact between the components to an area of the sample set as a secondary battery internal short circuit simulation contact area; applying a current between I probes in contact with the sample, obtaining resistance by measuring a potential difference between V probes which are separate from the I probes, obtaining a graph of a change in resistance with a change in distance between the V probes, and calculating a short circuit resistance of the area from y-intercept of the graph; and predicting a heat generation amount of the area from the short circuit resistance. preparing a sample for secondary battery electrode evaluation in which a short circuit occurs when components included in the sample contact each other; applying a predetermined pressure which causes the contact between the components to an area of the sample set as a secondary battery internal short circuit simulation contact area; applying a current between I probes in contact with the sample, obtaining resistance by measuring a potential difference between V probes which are separate from the I probes, obtaining a graph of a change in resistance with a change in distance between the V probes, and calculating a short circuit resistance of the area from y-intercept of the graph; and predicting a heat generation amount of the area from the short circuit resistance.
A method, comprising: determining, by a communication apparatus, whether a length of channel state information,CSI, is less than a preset length; adding, by the communication apparatus, one or more padding bits to the CSI when determining that the length of the CSI is less than the preset length, wherein a length of CSI obtained by adding the one or more padding bits is consistent with the preset length; and sending, by the communication apparatus, the CSI obtained by adding the one or more padding bits; wherein the preset length is determined based on a quantity of CSI-reference signal RS ports, characterized in that: when the quantity of CSI-RS ports is 2 or 4, the preset length is 16; or when the quantity of CSI-RS ports is greater than 4, the preset length is 27; wherein the CSI comprises one or more of the following indication information: a channel quality indicator, CQI, a precoding matrix indicator, PMI, a rank indication, RI, a layer indicator, LI, and a CSI-reference signal resource indicator, CRI; wherein a maximum total length of the CQI, the PMI, the RI, the LI and the CRI is consistent with the preset length. determining, by a communication apparatus, whether a length of channel state information,CSI, is less than a preset length; adding, by the communication apparatus, one or more padding bits to the CSI when determining that the length of the CSI is less than the preset length, wherein a length of CSI obtained by adding the one or more padding bits is consistent with the preset length; and sending, by the communication apparatus, the CSI obtained by adding the one or more padding bits; wherein the preset length is determined based on a quantity of CSI-reference signal RS ports, characterized in that: when the quantity of CSI-RS ports is 2 or 4, the preset length is 16; or when the quantity of CSI-RS ports is greater than 4, the preset length is 27; wherein the CSI comprises one or more of the following indication information: a channel quality indicator, CQI, a precoding matrix indicator, PMI, a rank indication, RI, a layer indicator, LI, and a CSI-reference signal resource indicator, CRI; wherein a maximum total length of the CQI, the PMI, the RI, the LI and the CRI is consistent with the preset length.
A computer-implemented method, comprising: receiving a plurality of depth images of an environment via an imaging device, each depth image associated with a local coordinate system (135, 140, 145); for each local coordinate system (135, 140, 145), fusing each associated depth image to generate a local volume (403, 407, 413); fusing each local volume into a global volume having a global coordinate system; extracting a surface mesh for the global volume; determining one or more regions of inconsistency within the global volume, wherein a region of inconsistency comprises voxels associated with two or more adjacent local volumes, in which the voxels have assigned values that are unfusable; localizing the one or more determined regions of inconsistency to one or more erroneous local volumes; unfusing the one or more erroneous local volumes from the global volume; and re-fusing non-erroneous local volumes into a corrected global volume. receiving a plurality of depth images of an environment via an imaging device, each depth image associated with a local coordinate system (135, 140, 145); for each local coordinate system (135, 140, 145), fusing each associated depth image to generate a local volume (403, 407, 413); fusing each local volume into a global volume having a global coordinate system; extracting a surface mesh for the global volume; determining one or more regions of inconsistency within the global volume, wherein a region of inconsistency comprises voxels associated with two or more adjacent local volumes, in which the voxels have assigned values that are unfusable; localizing the one or more determined regions of inconsistency to one or more erroneous local volumes; unfusing the one or more erroneous local volumes from the global volume; and re-fusing non-erroneous local volumes into a corrected global volume.
A user equipment comprising: at least one processor; and at least one memory storing instructions that, when executed by the at least one processor, cause the user equipment at least to perform: - receiving conditional handover information from a first network node; and - retaining at least a part of the conditional handover information during a re-establishment procedure following a failure affecting a radio link of the user equipment; - receiving, from a second network node, renewed conditional handover information during the re-establishment procedure. at least one processor; and at least one memory storing instructions that, when executed by the at least one processor, cause the user equipment at least to perform: - receiving conditional handover information from a first network node; and - retaining at least a part of the conditional handover information during a re-establishment procedure following a failure affecting a radio link of the user equipment; - receiving, from a second network node, renewed conditional handover information during the re-establishment procedure. - receiving conditional handover information from a first network node; and - retaining at least a part of the conditional handover information during a re-establishment procedure following a failure affecting a radio link of the user equipment; - receiving, from a second network node, renewed conditional handover information during the re-establishment procedure.
A medical-topical composition for wound treatment comprising 0.001 to 3% by weight of fatty acid extracts of natural oils based on the total weight of the medical-topical composition, characterized in that the natural oils are linseed oil or rapeseed oil, wherein medical-topical compositions containing a combination of active ingredients that consist of the following components a) 0.01 to 20% by weight of almond oil, b) 0.01 to 1.5% by weight of linseed oil fatty acids, c) 0.001 to 0.5% by weight of amino acids; and d) 0.01 to 1.5% by weight of creatine are excluded. a) 0.01 to 20% by weight of almond oil, b) 0.01 to 1.5% by weight of linseed oil fatty acids, c) 0.001 to 0.5% by weight of amino acids; and d) 0.01 to 1.5% by weight of creatine
Elevator for caps, comprising a closed-loop conveyor belt including a plurality of projections extending from an outer face of the conveyor belt, characterized in that it comprises an inspection and selection system, comprising: - at least one camera (62, 64, 66) arranged to visually inspect the caps while they move along an ascending branch of the conveyor belt, and - an ejection device which ejects noncompliant caps from the elevator according to information provided by said at least one camera (62, 64, 66). - at least one camera (62, 64, 66) arranged to visually inspect the caps while they move along an ascending branch of the conveyor belt, and - an ejection device which ejects noncompliant caps from the elevator according to information provided by said at least one camera (62, 64, 66).
A bone anchoring device, comprising: a receiving part for coupling a rod to a bone anchoring element, the receiving part comprising a first end, a second end, and a central axis extending between the first end and the second end, and an end surface provided at the first end, a recess at the first end for receiving a rod, and a head receiving portion at the second end for pivotably holding a head of a bone anchoring element, the head receiving portion being at least partially flexible; a clamping ring configured to be arranged around the head receiving portion, wherein when the clamping ring is around the head receiving portion, the clamping ring can assume a locking position wherein the clamping ring exerts a force onto the head receiving portion such that an inserted head is locked and a non-locking position wherein an inserted head is pivotable relative to the receiving part (5, 5'); wherein the receiving part further comprises at least one first engagement structure (54a, 54b) arranged at an outer circumferential surface of the receiving part and configured to be engaged by an engagement portion of an instrument, characterized in that the engagement structure (54a, 54b) is positioned directly at or adjacent to the end surface at the first end, and extends farther radially outward than the outer circumferential surface of the receiving part, wherein the first engagement structure (54a, 54b) is arranged asymmetric with respect to a plane extending through the central axis of the receiving part and through a longitudinal axis of the recess for receiving the rod. a receiving part for coupling a rod to a bone anchoring element, the receiving part comprising a first end, a second end, and a central axis extending between the first end and the second end, and an end surface provided at the first end, a recess at the first end for receiving a rod, and a head receiving portion at the second end for pivotably holding a head of a bone anchoring element, the head receiving portion being at least partially flexible; a clamping ring configured to be arranged around the head receiving portion, wherein when the clamping ring is around the head receiving portion, the clamping ring can assume a locking position wherein the clamping ring exerts a force onto the head receiving portion such that an inserted head is locked and a non-locking position wherein an inserted head is pivotable relative to the receiving part (5, 5'); wherein the receiving part further comprises at least one first engagement structure (54a, 54b) arranged at an outer circumferential surface of the receiving part and configured to be engaged by an engagement portion of an instrument, characterized in that the engagement structure (54a, 54b) is positioned directly at or adjacent to the end surface at the first end, and extends farther radially outward than the outer circumferential surface of the receiving part, wherein the first engagement structure (54a, 54b) is arranged asymmetric with respect to a plane extending through the central axis of the receiving part and through a longitudinal axis of the recess for receiving the rod.
A thermosetting resin composition containing a flame retardant for thermosetting resin containing an aromatic phosphoric acid ester represented by the general formula: wherein R 1 to R 4 each independently represent a hydrogen atom, a C 1-4 alkyl group, or a C 1-4 alkoxy group; R 5, R 6, and R 9 each independently represent a C 1-10 alkyl group or a C 1-10 alkoxy group; R 7 and R 8 each independently represent a C 1-4 alkyl group or a C 1-4 alkoxy group; n represents an integer of 1 to 10; n 1 and n 2 each independently represent an integer of 0 to 3; m 1 and m 2 each independently represent an integer of 0 to 4; p represents an integer of 0 to 26; and k represents an integer of 1 to 12; and when p is 2 or more, any two substituents R 9 may be bonded to each other, and may be bonded to a carbon atom(s) of a ring to which the above substituents R 9 are bonded, forming another ring.
Computer implemented method for modeling aircraft performance through adaptive aircraft performance models using aircraft performance data; the aircraft performance data comprising recorded trajectory data of the aircraft, weather data faced during trajectory of the aircraft, aircraft configuration data and an aircraft intent characterized in that the method comprises the following stages: a) introducing aircraft degradation coefficients in a nominal aircraft performance model of the aircraft, obtaining a degraded aircraft performance model; b) calculating computed trajectory data in a trajectory computation infrastructure using as inputs the aircraft intent which represents the trajectory data, the weather data and the degraded aircraft performance model; c) comparing the recorded trajectory data with the computed trajectory data; d) obtaining an enhanced aircraft performance model by considering the degraded aircraft performance model as the enhanced aircraft performance model, when the result of the comparison is less than a previously established threshold; and e) modifying, when the result of the comparison is higher than the previously established threshold, the aircraft degradation coefficients and executing steps a) to e) of the method, until the result of the comparison is less than the previously established threshold. a) introducing aircraft degradation coefficients in a nominal aircraft performance model of the aircraft, obtaining a degraded aircraft performance model; b) calculating computed trajectory data in a trajectory computation infrastructure using as inputs the aircraft intent which represents the trajectory data, the weather data and the degraded aircraft performance model; c) comparing the recorded trajectory data with the computed trajectory data; d) obtaining an enhanced aircraft performance model by considering the degraded aircraft performance model as the enhanced aircraft performance model, when the result of the comparison is less than a previously established threshold; and e) modifying, when the result of the comparison is higher than the previously established threshold, the aircraft degradation coefficients and executing steps a) to e) of the method, until the result of the comparison is less than the previously established threshold.