mhurhangee/ep-ind-claims huggingface dataset:
A protective shield (100; 200; 300) comprising: a body for protecting a user from a projectile or impact, the body comprising a front strike face (110; 210) and an opposing rear face (115; 310); and a connector arrangement (125, 126; 225; 325) provided on the body adapted so as to allow the shield (100; 200; 300) to connect to an adjacent protective shield, wherein the body comprises a composite structure (170; 470) comprising at least one layer comprising graphene (172a-l; 472) and a second layer (173a-l; 473) comprising an aerogel, and wherein the composite structure (170; 470) is arranged: (i) between the strike face (110; 210) and rear face (115; 310); and/or (ii) so as to at least partly define the strike face (110; 210) and/or the rear face (115; 310). a body for protecting a user from a projectile or impact, the body comprising a front strike face (110; 210) and an opposing rear face (115; 310); and a connector arrangement (125, 126; 225; 325) provided on the body adapted so as to allow the shield (100; 200; 300) to connect to an adjacent protective shield, wherein the body comprises a composite structure (170; 470) comprising at least one layer comprising graphene (172a-l; 472) and a second layer (173a-l; 473) comprising an aerogel, and wherein the composite structure (170; 470) is arranged: (i) between the strike face (110; 210) and rear face (115; 310); and/or (ii) so as to at least partly define the strike face (110; 210) and/or the rear face (115; 310). (i) between the strike face (110; 210) and rear face (115; 310); and/or (ii) so as to at least partly define the strike face (110; 210) and/or the rear face (115; 310).
A joining structure for an interior panel for an aircraft (12, 14), comprising: two interior panels for an aircraft (12, 14) each including a plate-shaped core having a uniform thickness and a first surface plate and a second surface plate attached to both sides of the core, the two interior panels for an aircraft (12, 14) being joined so that the first surface plates intersect with each other or the second surface plates intersect with each other; wherein the first surface plate and the second surface plate have a flat surface portion (2002, 2202), the flat surface portions (2002, 2202) being parallel with each other; the second surface plate has an end surface portion that protrudes from an end portion of the flat surface portion and is connected with an end portion of the flat surface portion of the first surface plate as well as the flat surface portion; a corner portion is provided by the end portion of the flat surface portion of the first surface plate and an end portion of the end surface portion of the second surface plate being attached, the corner portion extending in a direction the end portions extend; a plurality of strip-shaped connection pieces are provided, the connection pieces being formed across an entire length of the corner portion of the two interior panels for an aircraft (12, 14) by portions of the end portion of the flat surface portion of the first surface plate protruding from the corner portion and continuously protruding from the flat surface portion of the first surface plate or by portions of the end portion of the end surface portion of the second surface plate continuously protruding from the end surface portion, and the connection pieces having gaps therebetween in a direction the corner portion extends; wherein the plurality of strip-shaped connection pieces are provided throughout the corner portion extending across the surface plates; and the two interior panels for an aircraft (12, 14) are joined by the corner portions of the two interior panels for an aircraft (12, 14) being brought together, and the connection pieces of the two interior panels for an aircraft (12, 14) passing through the gaps between the connection pieces of the other interior panels for an aircraft (12, 14) to be joined, and being adhered to one of the second surface plate and the first surface plate of the other interior panels for an aircraft (12, 14). two interior panels for an aircraft (12, 14) each including a plate-shaped core having a uniform thickness and a first surface plate and a second surface plate attached to both sides of the core, the two interior panels for an aircraft (12, 14) being joined so that the first surface plates intersect with each other or the second surface plates intersect with each other; wherein
A control head for a flow valve, the control head comprising: a housing provided with a threaded tube portion, the housing mounted within a corresponding thread provided in the head such that by rotation of the housing the axial position of the housing relative to a flow valve can be varied; a sensing element operable to expand or contract axially in response to temperature variations, the sensing element provided within the housing and having an abutting pin projecting axially of the housing to contact an operating pin of the flow valve; and a spring retained within the housing and biasing the sensing element towards the operating pin of the flow valve by engagement with the housing wherein the sensing element and the spring are free to expand within the threaded tube portion of the housing.
A squeegee having a pair of spaced apart blades extending in a widthwise direction, each of said blades extending from a proximal end to a distal end, said proximal ends of said blades being joined to a head, said head having an inner surface and an outer surface opposed thereto, said head having a tucker bar joined thereto, said tucker bar being axially rotatable to longitudinally advance a sheet between said tucker bar and said outer surface of said head.
A method for updating a configuration of a user equipment, UE, by an access and mobility management function, AMF, in a wireless communication system, the method comprising: determining (S2401, S2402) whether at least one UE parameter related to the configuration of the UE needs to be updated; transmitting (S2403, S2404) a UE configuration update command message to the UE based on that the AMF determines that the at least one UE parameter needs to be updated; and receiving a UE configuration update complete message from the UE based on that acknowledgement for the UE configuration update command message is requested, characterized in that the UE configuration update command message includes i) a UE parameter to be updated and ii) indication information for whether the UE needs to perform the registration procedure for the UE parameter to be updated, wherein, based on the indication information and a kind of the UE parameter to be updated, the registration procedure is configured to be initiated based on that the UE is in i) a CONNECTED mode or ii) an idle mode, and wherein the registration procedure is configured to be initiated while the UE is in the CONNECTED mode based on the UE parameter to be updated being a Mobile Initiated Connected Only, MICO, parameter. determining (S2401, S2402) whether at least one UE parameter related to the configuration of the UE needs to be updated; transmitting (S2403, S2404) a UE configuration update command message to the UE based on that the AMF determines that the at least one UE parameter needs to be updated; and receiving a UE configuration update complete message from the UE based on that acknowledgement for the UE configuration update command message is requested, characterized in that the UE configuration update command message includes i) a UE parameter to be updated and ii) indication information for whether the UE needs to perform the registration procedure for the UE parameter to be updated, wherein, based on the indication information and a kind of the UE parameter to be updated, the registration procedure is configured to be initiated based on that the UE is in i) a CONNECTED mode or ii) an idle mode, and wherein the registration procedure is configured to be initiated while the UE is in the CONNECTED mode based on the UE parameter to be updated being a Mobile Initiated Connected Only, MICO, parameter.
A flexible display apparatus comprising: a flexible substrate, and a TFT structure, a display device, a film packaging layer, and a curing material layer laminated successively on the flexible substrate, wherein the TFT structure comprises a polysilicon layer region, the curing material layer comprises a pair of specific regions, a projection of one of the specific regions on the flexible substrate coinciding with a projection of the polysilicon layer region on the flexible substrate, and a projection of the another specific region on the flexible substrate coinciding with a projection of the display device on the flexible substrate; the curing material layer is patterned, and each of the specific regions of the curing material layer has a thickness greater than a thickness of other regions of the curing material layer other than the specific region, wherein the specific regions of the curing material layer corresponding to the polysilicon region and the display device have a thickness twice of a thickness of other regions of the curing material layer other than the polysilicon region and the display device.
Reinforcing element comprising a single strand of high-modulus textile monofilaments and a single strand of low-modulus textile monofilaments which are wound one around the other in a direction D3 with a twist R3, by a high-modulus strand of textile monofilaments is a strand having a so-called final modulus strictly higher than 25 cN/tex and by a low-modulus strand of textile monofilaments is a strand having a so-called final modulus less than or equal to 25 cN/tex, the strand of high-modulus textile monofilaments having a residual twist R1 in the direction D1, the strand of low-modulus textile monofilaments having a residual twist R2 in the direction D2, the residual twists R1 and R2 being such that: - R1>R2 when R2 is greater than or equal to 2.5% of the twist R3; - R1 is greater than or equal to 2.5% of the twist R3 when R2 is strictly below 2.5% of the twist R3; in which R3 ranges from 200 to 450 twists per metre and the ratio R1/R3 ranges from 0.05 to 0.45. - R1>R2 when R2 is greater than or equal to 2.5% of the twist R3; - R1 is greater than or equal to 2.5% of the twist R3 when R2 is strictly below 2.5% of the twist R3;
A method for operating a combustion device comprising the steps of: producing a gaseous fuel stream that is resistant to autoignition by mixing a vaporized liquid fuel with an inert gas stream having an oxygen content less than that of ambient air, the inert gas stream being supplied by an air separator, or vaporizing a liquid fuel using an inert gas stream having an oxygen content less than that of ambient air, the inert gas stream being supplied by the air separator; premixing the gaseous fuel stream with a oxygenated gas to produce a gas mixture at a location upstream of a combustion zone of the combustion device; combusting the gas mixture in the combustion zone of the combustion device, whereby auto-ignition of the gaseous fuel stream or of the gas mixture upstream of the combustion zone is substantially suppressed; and supplying an oxygen enriched stream from the air separator to the combustion device downstream of the combustion zone. producing a gaseous fuel stream that is resistant to autoignition by mixing a vaporized liquid fuel with an inert gas stream having an oxygen content less than that of ambient air, the inert gas stream being supplied by an air separator, or vaporizing a liquid fuel using an inert gas stream having an oxygen content less than that of ambient air, the inert gas stream being supplied by the air separator; premixing the gaseous fuel stream with a oxygenated gas to produce a gas mixture at a location upstream of a combustion zone of the combustion device; combusting the gas mixture in the combustion zone of the combustion device, whereby auto-ignition of the gaseous fuel stream or of the gas mixture upstream of the combustion zone is substantially suppressed; and supplying an oxygen enriched stream from the air separator to the combustion device downstream of the combustion zone.
A method for manufacturing an object, the method comprising the steps of: obtaining a preform of the object, the preform comprising a first panel and at least one second panel (4, 6, 8, 10) having an orientation different from that of the first panel, then thermoforming a planar portion of the first panel of the preform into a protruding element in a selective manner such that the at least one second panel is not thermoformed; and wherein said thermoforming comprises the steps of placing the preform in a position wherein the first panel is between a heater and above a mold, said mold including side walls (40, 42, 44, 46) and a bottom surface defining a molding cavity, and wherein a molding element protrudes from the bottom surface, and wherein the at least one second panel (4, 6, 8, 10) of the preform extends outside the mold, and wherein the planar portion of the first panel is above the molding element, heating the planar portion with the heater, such that as the planar portion is deformed, it falls towards the molding element and is thereby thermoformed by the molding element; and characterized in that the mold further comprises a vacuum insulation seal arranged on the side walls (40, 42, 44, 46) of the mold to seal the molding cavity when the preform is in said position. obtaining a preform of the object, the preform comprising a first panel and at least one second panel (4, 6, 8, 10) having an orientation different from that of the first panel, then thermoforming a planar portion of the first panel of the preform into a protruding element in a selective manner such that the at least one second panel is not thermoformed; and wherein said thermoforming comprises the steps of placing the preform in a position wherein the first panel is between a heater and above a mold, said mold including side walls (40, 42, 44, 46) and a bottom surface defining a molding cavity, and wherein a molding element protrudes from the bottom surface, and wherein the at least one second panel (4, 6, 8, 10) of the preform extends outside the mold, and wherein the planar portion of the first panel is above the molding element, heating the planar portion with the heater, such that as the planar portion is deformed, it falls towards the molding element and is thereby thermoformed by the molding element; and placing the preform in a position wherein the first panel is between a heater and above a mold, said mold including side walls (40, 42, 44, 46) and a bottom surface defining a molding cavity, and wherein a molding element protrudes from the bottom surface, and wherein the at least one second panel (4, 6, 8, 10) of the preform extends outside the mold, and wherein the planar portion of the first panel is above the molding element, heating the planar portion with the heater, such that as the planar portion is deformed, it falls towards the molding element and is thereby thermoformed by the molding element; and characterized in that the mold further comprises a vacuum insulation seal arranged on the side walls (40, 42, 44, 46) of the mold to seal the molding cavity when the preform is in said position.
A wireless power transmitter apparatus, the apparatus comprising: means for wirelessly transmitting power at a transmit frequency to a first means for receiving; and characterised by means for controlling configured to reduce a level of emission generated at a determined frequency for a period of time by the means for wirelessly transmitting, the period of time for reducing the level of emission being based on information about the frequency of an information signal transmitted to a second means for receiving to be received within the period of time, the level of emissions reduced to avoid interfering with the transmission of the information signal. means for wirelessly transmitting power at a transmit frequency to a first means for receiving; and characterised by means for controlling configured to reduce a level of emission generated at a determined frequency for a period of time by the means for wirelessly transmitting, the period of time for reducing the level of emission being based on information about the frequency of an information signal transmitted to a second means for receiving to be received within the period of time, the level of emissions reduced to avoid interfering with the transmission of the information signal.
An oxygen concentration system, the system comprising: a patient portable unit having an oxygen concentrator configured to deliver gaseous oxygen to a patient, the patient portable unit being portable by the patient, wherein the patient portable unit is configured to deliver gaseous oxygen to a patient up to a first maximum flow rate when in a standalone mode and not attached to a docking station, the portable unit including a rechargeable battery; a docking station configured to be at least electrically and fluidly connected to the patient portable unit, wherein the patient portable unit is configured to deliver gaseous oxygen to a patient up to a second maximum flow rate that is greater than the first maximum flow rate when the patient portable unit is at least electrically and fluidly connected to the docking station, and wherein the patient portable unit includes a compressor that is configured to draw power and fluid from the docking station when the patient portable unit is attached to the docking station. a patient portable unit having an oxygen concentrator configured to deliver gaseous oxygen to a patient, the patient portable unit being portable by the patient, wherein the patient portable unit is configured to deliver gaseous oxygen to a patient up to a first maximum flow rate when in a standalone mode and not attached to a docking station, the portable unit including a rechargeable battery; a docking station configured to be at least electrically and fluidly connected to the patient portable unit, wherein the patient portable unit is configured to deliver gaseous oxygen to a patient up to a second maximum flow rate that is greater than the first maximum flow rate when the patient portable unit is at least electrically and fluidly connected to the docking station, and wherein the patient portable unit includes a compressor that is configured to draw power and fluid from the docking station when the patient portable unit is attached to the docking station.
A radiation therapy system comprising: a particle therapy delivery system for delivery of radiation therapy to a patient via a particle beam; a magnetic resonance imaging system configured to obtain patient magnetic resonance imaging, MRI, data during radiation therapy; a controller configured to receive the patient MRI data during radiation therapy and utilize the patient MRI data to perform real-time calculations of a location of dose deposition for the particle beam, taking into account interaction properties of soft tissues through which the particle beam passes; a dosimetry system for monitoring the radiation therapy to the patient; and a magnetic shielding structure surrounding at least a portion of the dosimetry system. a particle therapy delivery system for delivery of radiation therapy to a patient via a particle beam; a magnetic resonance imaging system configured to obtain patient magnetic resonance imaging, MRI, data during radiation therapy; a controller configured to receive the patient MRI data during radiation therapy and utilize the patient MRI data to perform real-time calculations of a location of dose deposition for the particle beam, taking into account interaction properties of soft tissues through which the particle beam passes; a dosimetry system for monitoring the radiation therapy to the patient; and a magnetic shielding structure surrounding at least a portion of the dosimetry system.
A crystalline diethylamine tetrathiomolybdate salt, characterized by: (a) an XRPD pattern having at least three peaks selected from the peaks at 7.9, 11.4, 12.5, 13.9, 14.9, 20.8 and 21.5 ± 0.5°2θ, wherein (i) the XRPD pattern has peaks at 11.4 and 14.9 ± 0.2°2θ, wherein the peak at 11.4 ± 0.2°2θ is at least one and a half times as intense as the peak at 14.9 ± 0.2°2θ; or (ii) the XRPD pattern has peaks at 11.4 and 21.5 ± 0.2°2θ, wherein the peak at 11.4 ± 0.2°2θ is at least three times as intense as the peak at 21.5 ± 0.2°2θ; (b) an XRPD pattern substantially similar to Fig. 1; (c) a P 2 1 space group at a temperature of about 100 K; (d) unit cell dimensions of a=7.1433 Å, b=10.7328 Å, c=10.7485 Å, α=90.00°, β=93.902 °, and γ=90.00° at a temperature of about 100 K; or (e) a combination thereof. (a) an XRPD pattern having at least three peaks selected from the peaks at 7.9, 11.4, 12.5, 13.9, 14.9, 20.8 and 21.5 ± 0.5°2θ, wherein (i) the XRPD pattern has peaks at 11.4 and 14.9 ± 0.2°2θ, wherein the peak at 11.4 ± 0.2°2θ is at least one and a half times as intense as the peak at 14.9 ± 0.2°2θ; or (ii) the XRPD pattern has peaks at 11.4 and 21.5 ± 0.2°2θ, wherein the peak at 11.4 ± 0.2°2θ is at least three times as intense as the peak at 21.5 ± 0.2°2θ; (i) the XRPD pattern has peaks at 11.4 and 14.9 ± 0.2°2θ, wherein the peak at 11.4 ± 0.2°2θ is at least one and a half times as intense as the peak at 14.9 ± 0.2°2θ; or (ii) the XRPD pattern has peaks at 11.4 and 21.5 ± 0.2°2θ, wherein the peak at 11.4 ± 0.2°2θ is at least three times as intense as the peak at 21.5 ± 0.2°2θ; (b) an XRPD pattern substantially similar to Fig. 1; (c) a P 2 1 space group at a temperature of about 100 K; (d) unit cell dimensions of a=7.1433 Å, b=10.7328 Å, c=10.7485 Å, α=90.00°, β=93.902 °, and γ=90.00° at a temperature of about 100 K; or (e) a combination thereof.
A drive shaft for a motorized, surgical handpiece comprising: a first prong and a second prong, wherein a slot is located between the first prong and the second prong, characterised in that the first prong is longer than the second prong, the first prong is tapered at a first angle and rounded at a first radius, and wherein the first prong is engagable with a drive tang of a cutting tool such that the first prong causes rotation and subsequent insertion of the drive tang into the slot located between the first prong and the second prong. a first prong and a second prong, wherein a slot is located between the first prong and the second prong, characterised in that the first prong is longer than the second prong, the first prong is tapered at a first angle and rounded at a first radius, and wherein the first prong is engagable with a drive tang of a cutting tool such that the first prong causes rotation and subsequent insertion of the drive tang into the slot located between the first prong and the second prong.