mhurhangee/ep-ind-claims huggingface dataset:
A lid attachment member comprising: a metal plate that is equipped with an attachment hole to which a lid of a container is to be attached; a raised or recessed seal portion that is formed at, and continuously all the way around, an outer peripheral portion of the metal plat; and a resin member that is integrally formed on the outer peripheral portion of the metal plate, covers the seal portion, and has a back surface side that is configured to be welded to an open portion of the container, wherein the seal portion is an annular groove formed at at least one of a front surface or a back surface of the metal plate, and wherein an angle between a groove bottom surface of the annular groove and a groove wall surface at an outer peripheral side of the annular groove is equal to or less than 90 degrees. a metal plate that is equipped with an attachment hole to which a lid of a container is to be attached; a raised or recessed seal portion that is formed at, and continuously all the way around, an outer peripheral portion of the metal plat; and a resin member that is integrally formed on the outer peripheral portion of the metal plate, covers the seal portion, and has a back surface side that is configured to be welded to an open portion of the container, wherein the seal portion is an annular groove formed at at least one of a front surface or a back surface of the metal plate, and wherein an angle between a groove bottom surface of the annular groove and a groove wall surface at an outer peripheral side of the annular groove is equal to or less than 90 degrees.
A control system comprising: a plurality of field devices (FD1 - FD9); a host computer adapted to send control messages to and to recieve response messages from the field devices (FD1 -FD9); a plurality of wireless nodes (20, 22, 24, 26, 28, 30) adapted to cycle between a sleep state and an active state according to a wireless network power cycle, at least one of the field devices (FD1 - FD9) being associated with each node (20, 22, 24, 26, 28, 30); and a gateway between the host computer and the wireless nodes (20, 22, 24, 26, 28, 30); characterized in that the gateway is adapted to provide the host computer, in response to a message addressed to one of the field devices (20, 22, 24, 26, 28, 30), a predicted time value of when the field device (FD1 - FD9) will respond to the message. a plurality of field devices (FD1 - FD9); a host computer adapted to send control messages to and to recieve response messages from the field devices (FD1 -FD9); a plurality of wireless nodes (20, 22, 24, 26, 28, 30) adapted to cycle between a sleep state and an active state according to a wireless network power cycle, at least one of the field devices (FD1 - FD9) being associated with each node (20, 22, 24, 26, 28, 30); and a gateway between the host computer and the wireless nodes (20, 22, 24, 26, 28, 30); characterized in that the gateway is adapted to provide the host computer, in response to a message addressed to one of the field devices (20, 22, 24, 26, 28, 30), a predicted time value of when the field device (FD1 - FD9) will respond to the message.
A sensor for sensing pressure, the sensor comprising at least one VCSEL on a substrate, a compressible sensor layer and a reflecting element covering a top surface of the sensor layer, characterized in that the compressible sensor layer comprising sensor layer material is covering a top surface of the at least one VCSEL, wherein the at least one VCSEL is embedded in the compressible sensor layer or in a solid and/or liquid encapsulation material in direct contact with the compressible sensor layer, the sensor further comprising a processing means for deriving a pressure based on a self-mixing interference effect caused by reflection of radiation of the VCSEL at the reflecting element and on the mechanical characteristics of the compressible sensor layer.
A method for long term preservation of anatomical or surgical material, comprising the following steps: a. pretreatment of the material available and previously fixed in formalin; b. dehydration of the material by treatment with ethyl alcohol at different gradations; c. clarification of the material by using D-limonene and an acrylic polymer; d. dripping of the material fragments taken from the previous clarification step and giving the desired shape; e. drying of the material and obtaining the dehydrated final product; f. taking off a small quantity of material from the dehydrated final product; g. arrangement of the taken material in sampling little cells for surgical pieces; h. immersion of the little cells containing the material in D-limonene according to a volume ratio 10:1; i. reiteration of step h. for three consecutive days by changing said D-limonene for 3 times; j. realization of a paraffin block from which the material, which can be analyzed in anatomical pathology labs, is obtained. said method being characterized in that: said clarification step c) of the material comprises the following steps: i. a first treatment of the material in a stirrer with D-Limonene for a time interval of 10 minutes; ii. a second treatment of the material in a hermetic container at ambient temperature by means of D-Limonene overnight. iii. a third treatment of the material in a 1:10 solution of an acrylic polymer for a whole day. a. pretreatment of the material available and previously fixed in formalin; b. dehydration of the material by treatment with ethyl alcohol at different gradations; c. clarification of the material by using D-limonene and an acrylic polymer; d. dripping of the material fragments taken from the previous clarification step and giving the desired shape; e. drying of the material and obtaining the dehydrated final product; f. taking off a small quantity of material from the dehydrated final product; g. arrangement of the taken material in sampling little cells for surgical pieces; h. immersion of the little cells containing the material in D-limonene according to a volume ratio 10:1; i. reiteration of step h. for three consecutive days by changing said D-limonene for 3 times; j. realization of a paraffin block from which the material, which can be analyzed in anatomical pathology labs, is obtained. i. a first treatment of the material in a stirrer with D-Limonene for a time interval of 10 minutes; ii. a second treatment of the material in a hermetic container at ambient temperature by means of D-Limonene overnight. iii. a third treatment of the material in a 1:10 solution of an acrylic polymer for a whole day.
A pharmaceutical composition, comprising: a plurality of metal nanoparticles, each of the metal nanoparticles comprising: a core; and a stabilizing agent coated on a surface of the core; and at least one therapeutic agent attached to the stabilizing agent of the metal nanoparticles, wherein each of the therapeutic agent is an amphiphilic compound having at least one hydrophobic chain that interacts with the stabilizing agent, wherein the at least one therapeutic agent comprises 2-amino-2-[2-(4-octylphenyl)ethyl]-1,3-propanediol. a core; and a stabilizing agent coated on a surface of the core; and at least one therapeutic agent attached to the stabilizing agent of the metal nanoparticles, wherein each of the therapeutic agent is an amphiphilic compound having at least one hydrophobic chain that interacts with the stabilizing agent, wherein the at least one therapeutic agent comprises 2-amino-2-[2-(4-octylphenyl)ethyl]-1,3-propanediol.
A method of determining in an aircraft comprising a refuelled aircraft fuel tank and an aircraft fuel tank inerting system whether it is necessary to inert the refuelled aircraft fuel tank containing fuel, the method comprising providing a temperature value indicative of a temperature of the fuel after refuelling, characterised in that based on said temperature value, determining (102, 302) before take-off whether or not it is necessary to inert the aircraft fuel tank, wherein determining whether or not it is necessary to inert the fuel tank comprises determining whether or not to disable the aircraft fuel tank inerting system for substantially all of the immediately forthcoming flight. based on said temperature value, determining (102, 302) before take-off whether or not it is necessary to inert the aircraft fuel tank, wherein determining whether or not it is necessary to inert the fuel tank comprises determining whether or not to disable the aircraft fuel tank inerting system for substantially all of the immediately forthcoming flight.
A bait box maintenance tool comprising a hub and a plurality of bait box keys attached around a periphery of the hub, wherein each key is rotatable from a stowed position to a deployed position, wherein the hub comprises a plurality of bosses, each adapted to support the rotation of a respective key, wherein the bosses each comprise a substantially circular aperture operable to receive a substantially cylindrical portion of the respective key, wherein the cylindrical portion is rotatable relative to the boss, wherein the bait box maintenance tool further comprises an indexing means (118, 125) operable to retain each key in the deployed position, and wherein the indexing means comprise one or more projections extending parallel to a longitudinal axis of the boss on an interior face of the substantially circular aperture of the respective boss, wherein that the cylindrical portion comprises retaining means to retain the cylindrical portion in the aperture, charac terised in that the retaining means comprise a retaining region of the cylindrical portion having an increased diameter with respect to the remainder of the cylindrical portion, thereby preventing withdrawal of the cylindrical portion from the aperture, wherein the retaining region of each key is resiliently radially compressible, wherein the compression reduces the diameter of the retaining region to allow insertion or withdrawal of the cylindrical portion to or from the aperture, wherein the cylindrical portion comprises one or more slits, so as to allow compression in the retaining region and in that the or each projection is receivable in one of the slits on the respective cylindrical portion.
Aircraft fuselage section subjected to impacts of external bodies, the aircraft fuselage having a curved shape with at least a vertical symmetry plane (A-A) and a central longitudinal axis and comprising a skin and a plurality of frames arranged perpendicularly to said longitudinal axis, the fuselage section also comprising at least an inner reticular structure (51, 53) mounted on a supporting structure (41, 43) comprising longitudinal beams attached to the skin and interconnected with said frames, said inner reticular structure (51, 53) being arranged for creating at least one closed cell with the skin for improving its resistance and its damage tolerance to said impacts characterized in that the supporting structure is formed by two longitudinal beams and a set of transversal elements between them, said transversal elements being located transversal to said beams.
An intramedullary nail extending along a longitudinal axis from a proximal end to a distal end, comprising: a cavity extending from an opening at the proximal end along the longitudinal axis; a first locking hole extending transversely through the nail sized and shaped to receive a locking screw therethrough; a first insert sized and shaped for insertion into the cavity including a first transverse bore arranged so that, when the first insert is in the desired position within the cavity, the first transverse bore is aligned with the first locking hole so that a locking screw inserted through the first locking hole passes through the first insert via the first bore, whereby the first insert is adapted and configured to firmly secure a locking screw to the intramedullary nail; and a second insert sized and shaped to be received within the cavity proximal of the first insert to lock the first insert at the desired position in the cavity, characterized in that the first insert includes an eccentric projection shaped to be received in a correspondingly shaped eccentric portion of the cavity thereby forming an anti-rotation mechanism, which prevents the first insert from rotating relative to the cavity in the intramedullary nail. a cavity extending from an opening at the proximal end along the longitudinal axis; a first locking hole extending transversely through the nail sized and shaped to receive a locking screw therethrough; a first insert sized and shaped for insertion into the cavity including a first transverse bore arranged so that, when the first insert is in the desired position within the cavity, the first transverse bore is aligned with the first locking hole so that a locking screw inserted through the first locking hole passes through the first insert via the first bore, whereby the first insert is adapted and configured to firmly secure a locking screw to the intramedullary nail; and a second insert sized and shaped to be received within the cavity proximal of the first insert to lock the first insert at the desired position in the cavity, characterized in that the first insert includes an eccentric projection shaped to be received in a correspondingly shaped eccentric portion of the cavity thereby forming an anti-rotation mechanism, which prevents the first insert from rotating relative to the cavity in the intramedullary nail.
A molding product inspection device used for an injection molding machine that manufactures a molding product by injecting a molding material into a mold unit, the molding product inspection device comprising: an acquisition unit configured to acquire target appearance information relating to an appearance (Pe) of the molding product serving as an inspection target; and a processing unit configured to divide the appearance (Pe) in the target appearance information into a plurality of divided regions (Rd), and determine importance of each of the divided regions (Rd) by weighting, characterized in that the processing unit performs more machine learning on one or more divided regions (Rd) determined to be of relatively higher importance out of the plurality of divided regions (Rd), than at least one of other divided regions (Rd). an acquisition unit configured to acquire target appearance information relating to an appearance (Pe) of the molding product serving as an inspection target; and a processing unit configured to divide the appearance (Pe) in the target appearance information into a plurality of divided regions (Rd), and determine importance of each of the divided regions (Rd) by weighting, characterized in that the processing unit performs more machine learning on one or more divided regions (Rd) determined to be of relatively higher importance out of the plurality of divided regions (Rd), than at least one of other divided regions (Rd).
A heat pump type vehicle air-conditioning device provided with an external heat exchanger performing heat exchange between refrigerant flowing inside thereof and outside air, comprising: a temperature-difference calculation unit configured to calculate a temperature difference (ΔT) between exit-side refrigerant in the external heat exchanger and the outside air; and a frost formation determination unit configured to determine that frost formation is caused on the external heat exchanger based on an elapsed time (tn) of a state in which the temperature difference (ΔT) at time of heating operation is equal to or larger than a frost-formation temperature difference at which the frost formation may be caused on the external heat exchanger; and a frost-formation time estimation unit configured to estimate a frost-formation time (tf) at which the frost formation that may affect heat exchangeability at the external heat exchanger is caused, wherein the frost formation determination unit determines that, in a case in which the elapsed time (tn) is equal to or longer than the frost-formation time (tf), the frost formation that may affect the heat exchangeability at the external heat exchanger is caused, characterized in that the frost-formation time (tf) is changed depending on the temperature difference (ΔT) between the exit-side refrigerant and the outside air; and the frost-formation time (tf) is estimated to be shorter when the temperature difference (ΔT) is larger. a temperature-difference calculation unit configured to calculate a temperature difference (ΔT) between exit-side refrigerant in the external heat exchanger and the outside air; and a frost formation determination unit configured to determine that frost formation is caused on the external heat exchanger based on an elapsed time (tn) of a state in which the temperature difference (ΔT) at time of heating operation is equal to or larger than a frost-formation temperature difference at which the frost formation may be caused on the external heat exchanger; and a frost-formation time estimation unit configured to estimate a frost-formation time (tf) at which the frost formation that may affect heat exchangeability at the external heat exchanger is caused, wherein the frost formation determination unit determines that, in a case in which the elapsed time (tn) is equal to or longer than the frost-formation time (tf), the frost formation that may affect the heat exchangeability at the external heat exchanger is caused, characterized in that the frost-formation time (tf) is changed depending on the temperature difference (ΔT) between the exit-side refrigerant and the outside air; and the frost-formation time (tf) is estimated to be shorter when the temperature difference (ΔT) is larger.
An access control and mobility management function, AMF, node, comprising: a processor configured to: receive a N2 session management, SM, information from a session management function, SMF, node, wherein the N2 SM information indicates an available area for N2 information; receive a service request from a wireless transmit receive unit, WTRU; determine whether to update the N2 SM information based on a location of the WTRU and the available area for N2 information, wherein if the WTRU is outside of the available area for N2 information, the processor is configured to request a second N2 SM information from the SMF node and update the N2 SM information with the second N2 SM information; and send an N2 request with the N2 SM information to an access network associated with the WTRU. receive a N2 session management, SM, information from a session management function, SMF, node, wherein the N2 SM information indicates an available area for N2 information; receive a service request from a wireless transmit receive unit, WTRU; determine whether to update the N2 SM information based on a location of the WTRU and the available area for N2 information, wherein if the WTRU is outside of the available area for N2 information, the processor is configured to request a second N2 SM information from the SMF node and update the N2 SM information with the second N2 SM information; and send an N2 request with the N2 SM information to an access network associated with the WTRU.
A guiding element (28; 228; 326) of gaseous flow (44; 244; 344) of a turbomachine, in particular a compressor (4; 6), the element including a plasma generator, comprising: - a layer of dielectric material (32; 232; 332) with a guiding surface (46; 146; 246) in contact with the gaseous flow of the turbomachine, - a first electrode (34; 234; 334) arranged in the guiding surface, - a second electrode (36; 236; 336) electrically isolated from the first electrode by means of the dielectric layer (32; 232; 332), the plasma generator being configured so as to drive the gaseous flow (44; 244; 344) along the guiding surface from the first electrode towards the second electrode, the plasma generator further comprising a third electrode (38; 238; 338) covered by the dielectric layer (32; 232; 332) and electrically connected to the second electrode (36; 236; 336) so as to participate in the generation of the plasma in combination with the first electrode and the second electrode, the second electrode (36; 236; 336) being closer to the guiding surface than the third electrode (38; 238; 338), characterized in that the dielectric layer (32; 232; 332) comprises an opposite surface, opposite the guiding surface (46; 246) in the direction of the thickness of the dielectric layer, the third electrode (38; 238; 338) being disposed on said opposite surface. - a layer of dielectric material (32; 232; 332) with a guiding surface (46; 146; 246) in contact with the gaseous flow of the turbomachine, - a first electrode (34; 234; 334) arranged in the guiding surface, - a second electrode (36; 236; 336) electrically isolated from the first electrode by means of the dielectric layer (32; 232; 332), the plasma generator being configured so as to drive the gaseous flow (44; 244; 344) along the guiding surface from the first electrode towards the second electrode,
A method for producing pigments of defined size and shape, comprising the steps of: a) producing a three-dimensional surface structure (10; 30; 40) on a substrate, surface regions (12; 120; 500, 501, 502; 600; 700) being formed which are arranged in columns (14, 15; 140, 150) and are each bordered by a defined by a plurality of three-dimensional structural elements (20; 22; 24; 26; 32; 300; 504; 601; 701); b) applying a pigment material layer to the surface structure (10; 30; 40); c) detaching the pigment material layer from the surface structure (10; 30; 40) and producing pigments, characterized in that in step a) adjacent surface regions are only partially separated from each other by the three-dimensional structural elements and otherwise remain connected to each other. a) producing a three-dimensional surface structure (10; 30; 40) on a substrate, surface regions (12; 120; 500, 501, 502; 600; 700) being formed which are arranged in columns (14, 15; 140, 150) and are each bordered by a defined by a plurality of three-dimensional structural elements (20; 22; 24; 26; 32; 300; 504; 601; 701); b) applying a pigment material layer to the surface structure (10; 30; 40); c) detaching the pigment material layer from the surface structure (10; 30; 40) and producing pigments,
A T cell receptor having the property of specifically binding to SLLMWITQC (SEQ ID NO: 1) HLA-A*02 complex and comprising a TCR alpha chain variable domain and a TCR beta chain variable domain, wherein the alpha chain variable domain comprises an amino acid sequence that has at least 90% identity, such as 90%, 91%, 92%, 93%, 94%, 95%, 96%, 97%, 98%, 99% or 100% identity, to SEQ ID NO: 12, the beta chain variable domain comprises an amino acid sequence that has at least 90% identity, such as 90%, 91%, 92%, 93%, 94%, 95%, 96%, 97%, 98%, 99% or 100% identity, to SEQ ID NO: 15, and the alpha chain variable domain sequence of amino acids residues 27-32, 50-57 and 91-107 and the beta chain variable domain sequence of amino acid residues 27-31, 49-55 and 93-106 are selected from the following: Alpha chain Beta Chain 27-32 50-57 91-107 27-31 49-55 93-106 VSGNPY YLGDSALV CAVRDINSGAGSYQLTF KRLAL AWTGGEA CSVGGSGAADTQYF VSGNPY YLGDSALV CAVRDINSGAGSYQLTF KRLAL AWTGSEA CSVGGSGGADTQYF VSGNPY YLGDSALV CAVRDIRSGAGSYQLTF KRLAL AWTGGEA CSVGGSGAADTQYF VSGNPY YLGDSALV CAVRDIRSGAGSYQLTF KRLAL AWTGSEA CSVGGSGGADTQYF the alpha chain variable domain comprises an amino acid sequence that has at least 90% identity, such as 90%, 91%, 92%, 93%, 94%, 95%, 96%, 97%, 98%, 99% or 100% identity, to SEQ ID NO: 12, the beta chain variable domain comprises an amino acid sequence that has at least 90% identity, such as 90%, 91%, 92%, 93%, 94%, 95%, 96%, 97%, 98%, 99% or 100% identity, to SEQ ID NO: 15, and the alpha chain variable domain sequence of amino acids residues 27-32, 50-57 and 91-107 and the beta chain variable domain sequence of amino acid residues 27-31, 49-55 and 93-106 are selected from the following: Alpha chain Beta Chain 27-32 50-57 91-107 27-31 49-55 93-106 VSGNPY YLGDSALV CAVRDINSGAGSYQLTF KRLAL AWTGGEA CSVGGSGAADTQYF VSGNPY YLGDSALV CAVRDINSGAGSYQLTF KRLAL AWTGSEA CSVGGSGGADTQYF VSGNPY YLGDSALV CAVRDIRSGAGSYQLTF KRLAL AWTGGEA CSVGGSGAADTQYF VSGNPY YLGDSALV CAVRDIRSGAGSYQLTF KRLAL AWTGSEA CSVGGSGGADTQYF