mhurhangee/patent-ind-claim-en huggingface dataset:
A resin molded body comprising: a resin structure; an intermediate layer comprising an inorganic filler and an organic resin binder and provided on a surface of at least a part of the resin structure; and a thermal sprayed ceramic coating provided on the intermediate layer, wherein the inorganic filler is amorphous in shape and has a central particle diameter of 20 μm or more and 100 μm or less, wherein the inorganic filler is a crushed inorganic filler and the central particle diameter of the inorganic filler is the particle diameter d50 defined by the median diameter, wherein the particle diameter d50 refers to the volume average particle diameter at which the cumulative volume calculated from the small diameter side is 50% in the particle diameter distribution on a volume basis measured by the laser diffraction method, and wherein the intermediate layer has a thickness of 50 μm or more and 250 μm or less, the central particle diameter a of the inorganic filler and the thickness b of the intermediate layer satisfy the relationship of b ≥ 2 a , the inorganic filler is contained in the intermediate layer in an amount of 40% to 60% as a volume ratio, and the surface of the intermediate layer on which the thermal sprayed ceramic coating is formed has irregularities capable of effectively exerting an anchor effect on the thermal sprayed ceramic coating. a resin structure; an intermediate layer comprising an inorganic filler and an organic resin binder and provided on a surface of at least a part of the resin structure; and a thermal sprayed ceramic coating provided on the intermediate layer, wherein the inorganic filler is amorphous in shape and has a central particle diameter of 20 μm or more and 100 μm or less, wherein the inorganic filler is a crushed inorganic filler and the central particle diameter of the inorganic filler is the particle diameter d50 defined by the median diameter, wherein the particle diameter d50 refers to the volume average particle diameter at which the cumulative volume calculated from the small diameter side is 50% in the particle diameter distribution on a volume basis measured by the laser diffraction method, and wherein the intermediate layer has a thickness of 50 μm or more and 250 μm or less, the central particle diameter a of the inorganic filler and the thickness b of the intermediate layer satisfy the relationship of b ≥ 2 a , the inorganic filler is contained in the intermediate layer in an amount of 40% to 60% as a volume ratio, and the surface of the intermediate layer on which the thermal sprayed ceramic coating is formed has irregularities capable of effectively exerting an anchor effect on the thermal sprayed ceramic coating.
A computer-implemented method for estimating a load at executing a predetermined program, comprising: collecting, by a collection driver , run information that includes execution addresses sampled during execution of the predetermined program by a processor; specifying, by an aggregation unit , execution status based on the collected run information, wherein the execution status includes a feature related to the number of samples of the sampled execution addresses for each predetermined block range of addresses; calculating, by an estimation unit , for each load level of a plurality of load levels, a degree of similarity between the specified execution status and reference execution characteristic of the load level, which includes a reference feature prepared in advance for each predetermined block range of addresses; selecting, by the estimation unit , at least one of the plurality of load levels based on the calculated degrees of similarity from among the plurality of load levels, wherein at least one of the plurality of load levels having the highest similarity from among the plurality of load levels is selected; and estimating, by the estimation unit , a load based on the selected load levels as the load of the predetermined program. collecting, by a collection driver , run information that includes execution addresses sampled during execution of the predetermined program by a processor; specifying, by an aggregation unit , execution status based on the collected run information, wherein the execution status includes a feature related to the number of samples of the sampled execution addresses for each predetermined block range of addresses; calculating, by an estimation unit , for each load level of a plurality of load levels, a degree of similarity between the specified execution status and reference execution characteristic of the load level, which includes a reference feature prepared in advance for each predetermined block range of addresses; selecting, by the estimation unit , at least one of the plurality of load levels based on the calculated degrees of similarity from among the plurality of load levels, wherein at least one of the plurality of load levels having the highest similarity from among the plurality of load levels is selected; and estimating, by the estimation unit , a load based on the selected load levels as the load of the predetermined program.
Dynamic transaction card comprising: an outer protective layer having an outer edge; a core layer containing components of the dynamic transaction card ; wherein the components of the core layer of the dynamic transaction card (120, ...) include: a EuroPay-Mastercard-Visa (EMVTM) chip comprising an EMVTM plate accessible from the outer protective layer and an EMVTM processor ; a printed circuit board (PCB, 232) to provide integration between the components of the dynamic transaction card (120, ...); the dynamic transaction card further comprising: a card backing having an outer edge, wherein the card backing outer edge and the outer protective layer are connected to one another along the respective outer edges to form a casing for the core layer ; the dynamic transaction card being characterized by : a top outer layer comprising a film covering, the top outer layer covering the outer protective layer ; and an antenna incorporated into the top outer layer ; wherein the antenna is connected to the core layer onto the PCB via a conductive path. an outer protective layer having an outer edge; a core layer containing components of the dynamic transaction card ; wherein the components of the core layer of the dynamic transaction card (120, ...) include: a EuroPay-Mastercard-Visa (EMVTM) chip comprising an EMVTM plate accessible from the outer protective layer and an EMVTM processor ; a printed circuit board (PCB, 232) to provide integration between the components of the dynamic transaction card (120, ...); a EuroPay-Mastercard-Visa (EMVTM) chip comprising an EMVTM plate accessible from the outer protective layer and an EMVTM processor ; a printed circuit board (PCB, 232) to provide integration between the components of the dynamic transaction card (120, ...); the dynamic transaction card further comprising: a card backing having an outer edge, wherein the card backing outer edge and the outer protective layer are connected to one another along the respective outer edges to form a casing for the core layer ; the dynamic transaction card being characterized by : a top outer layer comprising a film covering, the top outer layer covering the outer protective layer ; and an antenna incorporated into the top outer layer ; wherein the antenna is connected to the core layer onto the PCB via a conductive path. a top outer layer comprising a film covering, the top outer layer covering the outer protective layer ; and an antenna incorporated into the top outer layer ; wherein the antenna is connected to the core layer onto the PCB via a conductive path.
A method of manufacturing an ice panel segment (310; 430) comprising: wrapping an ice panel material around a mandrel ; curing the ice panel material ; and cutting the ice panel material into ice panel cylinders ; characterised in that the wrapping the ice panel material around the mandrel comprises wrapping an inner fiberglass layer around the mandrel ; the wrapping the ice panel material around the mandrel further comprises wrapping a para-aramid synthetic fiber and epoxy pre-preg layer around the inner fiberglass layer; the wrapping the ice panel material around the mandrel further comprises wrapping an outer fiberglass layer around the para-aramid synthetic fiber and epoxy pre-preg layer; and the fibers in the inner fiberglass layer are wrapped in an orthogonal direction to the fibers in the outer fiberglass layer. wrapping an ice panel material around a mandrel ; curing the ice panel material ; and cutting the ice panel material into ice panel cylinders ; characterised in that the wrapping the ice panel material around the mandrel comprises wrapping an inner fiberglass layer around the mandrel ; the wrapping the ice panel material around the mandrel further comprises wrapping a para-aramid synthetic fiber and epoxy pre-preg layer around the inner fiberglass layer; the wrapping the ice panel material around the mandrel further comprises wrapping an outer fiberglass layer around the para-aramid synthetic fiber and epoxy pre-preg layer; and the fibers in the inner fiberglass layer are wrapped in an orthogonal direction to the fibers in the outer fiberglass layer.
Method of manufacturing a cover nonwoven for an interior lining for a vehicle, said cover nonwoven comprising a nonwoven fabric having at least two nonwoven layers , said at least two nonwoven layers comprising a first nonwoven layer and a second nonwoven layer , wherein a first outer surface of said nonwoven fabric is formed by a surface of said first nonwoven layer and a second outer surface of said nonwoven fabric is formed by a surface of said second nonwoven layer , and wherein the first nonwoven layer and the second nonwoven layer are inseparably bonded over the entire surface, characterized in that the first nonwoven layer is formed from a rough polypropylene spunlaced nonwoven, wherein a ratio (p/v) of an entangling pressure (p) applied to solidify the first nonwoven layer and a production speed (v) does not exceed a value of 9.0 bar/(m/min), wherein the first outer surface of the nonwoven fabric is suitable for applying a pressure-sensitive adhesive, and the second nonwoven layer is formed from a dense polypropylene spun-bonded nonwoven, wherein the second outer surface of the nonwoven fabric has hydrophobic properties and the second nonwoven layer has an air permeability of at most 400 l/(m 2 ·s) at a pressure difference of 1 mbar between the first outer surface of the second nonwoven layer and the second outer surface of the second nonwoven layer .
Filter element featuring an oval cross section defined by a filter body made of a filter media having two first opposing curvature sections with stronger curvature connected to one another by two second sections with a straight progression, the filter element further featuring an oval circumferential sealing means only with curvature sections for in particular radially sealing the filter element against a filter seat , wherein the sealing means features two oppositely disposed first curvature sections which are more strongly curved and two oppositely disposed second curvature sections which are less curved compared to the first curvature sections.
A vertical axis wind turbine comprising: a vertical rotation shaft ; and a plurality of vertical blades arranged around the rotation shaft and attached to the rotation shaft through an arm , wherein each of the blades includes a blade main part extending in a vertical direction and a pair of blade-tip inclined parts extending from upper and lower ends of the blade main part toward the rotation shaft , and each of the blade-tip inclined parts has a smaller thickness than a thickness of the blade main part , characterized in that the thickness of each of the blade-tip inclined parts is constant from a base end to a tip end of the blade-tip inclined part and a ratio of the thickness (t) of the blade-tip inclined part to the thickness (L) of the blade main part is 1/10 or smaller. a vertical rotation shaft ; and a plurality of vertical blades arranged around the rotation shaft and attached to the rotation shaft through an arm , wherein each of the blades includes a blade main part extending in a vertical direction and a pair of blade-tip inclined parts extending from upper and lower ends of the blade main part toward the rotation shaft , and each of the blade-tip inclined parts has a smaller thickness than a thickness of the blade main part , characterized in that the thickness of each of the blade-tip inclined parts is constant from a base end to a tip end of the blade-tip inclined part and a ratio of the thickness (t) of the blade-tip inclined part to the thickness (L) of the blade main part is 1/10 or smaller.
Attachment element for a turbine wheel of an air handling unit , the air handling unit comprising: - a motor which drives a shaft in rotation about an axis (X), - the attachment element for attaching the turbine wheel to the shaft , wherein there passes through the fixing element a passage provided to cooperate with the driving shaft , the passage and the shaft each being provided with a flat region for blocking the rotation of the attachment element relative to the shaft , characterised - in that , inside the attachment element , a cylindrical wall which delimits the passage comprises ribs for blocking the rotation of the attachment element relative to the turbine wheel , the ribs being provided to cooperate with slots of the turbine wheel , - in that the attachment element comprises a screw-shaft provided to cooperate with a fixing screw in order to block the translation of the attachment element relative to the driving shaft . - a motor which drives a shaft in rotation about an axis (X), - the attachment element for attaching the turbine wheel to the shaft , - in that , inside the attachment element , a cylindrical wall which delimits the passage comprises ribs for blocking the rotation of the attachment element relative to the turbine wheel , the ribs being provided to cooperate with slots of the turbine wheel , - in that the attachment element comprises a screw-shaft provided to cooperate with a fixing screw in order to block the translation of the attachment element relative to the driving shaft .
A combination of a modified T cell that expresses a BCMA-specific binding protein, wherein the BCMA-specific binding protein is a chimeric antigen receptor (CAR) or a tagged chimeric antigen receptor molecule (T-ChARM) and a γ-secretase inhibitor, for use in a method of treating a proliferative disease or disorder associated with BCMA expression, such as a cancer, in a subject having the proliferative disease or disorder, wherein the method comprises administering to the subject a therapeutically effective amount of the modified T cell and a therapeutically effective amount of the γ-secretase inhibitor.
A waveguide assembly for waveguides , the waveguide assembly comprises: a first waveguide comprising a first flange surrounding an end opening of the first waveguide ; a second waveguide comprising a second flange surrounding an end opening of the second waveguide ; wherein each flange comprises at least two holes which are periodically distributed around the respective end opening ; and wherein the first and second waveguides are arranged to be connected to each other by connecting the first flange to the second flange such that the end openings face each other and such that the holes in the first flange are at least partly glide symmetrically positioned with respect to the holes in the second flange , wherein the at least two holes in the first flange at least partly overlap with the at least two holes in the second flange such that the holes in the first flange are glided a certain period with respect to the at least two holes in the second flange when the first and second flanges are connected, the at least partly glide symmetric holes being configured to prevent leakage of signals guided through the first and second waveguides at the joint between the first and second flanges , wherein all of the at least two holes in each flange are periodically distributed around the respective end opening in one row, wherein the at least partly glide symmetrically positioned comprises completely glide symmetrically positioned or quasi glide symmetrically positioned, and wherein the quasi glide symmetrically positioned comprises a small deviation from ar exact glide symmetric structure. a first waveguide comprising a first flange surrounding an end opening of the first waveguide ; a second waveguide comprising a second flange surrounding an end opening of the second waveguide ; wherein each flange comprises at least two holes which are periodically distributed around the respective end opening ; and wherein the first and second waveguides are arranged to be connected to each other by connecting the first flange to the second flange such that the end openings face each other and such that the holes in the first flange are at least partly glide symmetrically positioned with respect to the holes in the second flange , wherein the at least two holes in the first flange at least partly overlap with the at least two holes in the second flange such that the holes in the first flange are glided a certain period with respect to the at least two holes in the second flange when the first and second flanges are connected, the at least partly glide symmetric holes being configured to prevent leakage of signals guided through the first and second waveguides at the joint between the first and second flanges , wherein all of the at least two holes in each flange are periodically distributed around the respective end opening in one row, wherein the at least partly glide symmetrically positioned comprises completely glide symmetrically positioned or quasi glide symmetrically positioned, and wherein the quasi glide symmetrically positioned comprises a small deviation from ar exact glide symmetric structure.
A method of manufacturing a hollow stabilizer , which is provided in a vehicle and comprises: a torsion portion extending in a vehicle width direction; an arm extending in a vehicle front-rear direction; and a bent portion connecting the torsion portion and the arm , wherein a ratio (t/D) of a thickness (t) to an outer diameter (D) of the element pipe is 0.10 or more, and wherein the method comprises: a forming step (S10) of subjecting an element pipe as a material of the hollow stabilizer to a bending process, to form a product shape including the bent portion ; and a quenching step (S20) of quenching the element pipe subjected to the bending process, wherein in the quenching step (S20), a cooling process is performed by immersing the element pipe in coolant and by spraying the coolant in the form of jet flow to an outer surface of the bent portion of the element pipe immersed in the coolant. a forming step (S10) of subjecting an element pipe as a material of the hollow stabilizer to a bending process, to form a product shape including the bent portion ; and a quenching step (S20) of quenching the element pipe subjected to the bending process, wherein
A receptacle unit for a first contact element of an electrical device, wherein the receptacle unit comprises: a holding element ; and one or more first clamping units, wherein each first clamping unit comprises: two separate clamping jaws , between which the first contact element can be clamped; and a first spring element , which is formed as a single piece, wherein the first spring element is designed such that it fits at least partially around the two clamping jaws and preloads them towards one another, and wherein the two clamping jaws are designed such that they define a receiving region for the first contact element , characterised in that the two clamping jaws are fastened to the holding element by means of the first spring element . a holding element ; and one or more first clamping units, wherein each first clamping unit comprises: two separate clamping jaws , between which the first contact element can be clamped; and a first spring element , which is formed as a single piece, wherein the first spring element is designed such that it fits at least partially around the two clamping jaws and preloads them towards one another, and wherein the two clamping jaws are designed such that they define a receiving region for the first contact element , characterised in that the two clamping jaws are fastened to the holding element by means of the first spring element . two separate clamping jaws , between which the first contact element can be clamped; and a first spring element , which is formed as a single piece, wherein the first spring element is designed such that it fits at least partially around the two clamping jaws and preloads them towards one another, and wherein the two clamping jaws are designed such that they define a receiving region for the first contact element , characterised in that the two clamping jaws are fastened to the holding element by means of the first spring element .
A subsea unit (1A; 1B) comprising: an external housing , a passive pressure compensator arranged to reduce a pressure difference between ambient subsea pressure and pressure inside the external housing , a subsea unit liquid for counteracting deformation of the external housing , and a first subunit (3A; 3B; 3C; 3D; 3E; 3F; 3G) arranged inside the external housing , and which first subunit (3A; 3B; 3C; 3D; 3E; 3F; 3G) comprises: a subunit housing , a passive pressure compensator arranged to reduce a pressure difference between the pressure inside the subunit housing and the pressure inside the external housing , a first electronic or electric device arranged inside the subunit housing , a first type of liquid for counteracting deformation of the subunit housing , characterised by an absorber arranged to absorb a pollutant in the first subunit (3A; 3B; 3C; 3D; 3E; 3F; 3G), wherein the absorber comprises one of a silicone gel, active coal and magnetic material. an external housing , a passive pressure compensator arranged to reduce a pressure difference between ambient subsea pressure and pressure inside the external housing , a subsea unit liquid for counteracting deformation of the external housing , and a first subunit (3A; 3B; 3C; 3D; 3E; 3F; 3G) arranged inside the external housing , and which first subunit (3A; 3B; 3C; 3D; 3E; 3F; 3G) comprises: a subunit housing , a passive pressure compensator arranged to reduce a pressure difference between the pressure inside the subunit housing and the pressure inside the external housing , a first electronic or electric device arranged inside the subunit housing , a first type of liquid for counteracting deformation of the subunit housing , characterised by an absorber arranged to absorb a pollutant in the first subunit (3A; 3B; 3C; 3D; 3E; 3F; 3G), wherein the absorber comprises one of a silicone gel, active coal and magnetic material. a subunit housing , a passive pressure compensator arranged to reduce a pressure difference between the pressure inside the subunit housing and the pressure inside the external housing , a first electronic or electric device arranged inside the subunit housing , a first type of liquid for counteracting deformation of the subunit housing , characterised by an absorber arranged to absorb a pollutant in the first subunit (3A; 3B; 3C; 3D; 3E; 3F; 3G), wherein the absorber comprises one of a silicone gel, active coal and magnetic material.