mhurhangee/ep-ind-claims huggingface dataset:
A method of loading a therapeutic substance within a lumenal space of a hollow wire having a plurality of side openings that forms a hollow stent, the method comprising the steps of: submerging the hollow stent within a solution of a therapeutic substance and a solvent; vibrating the hollow stent and the solution to assist in moving the solution through the plurality of side openings into the lumenal space of the hollow stent; removing the hollow stent from the solution when the lumenal space is substantially full of the solution and thereby creating a filled hollow stent; precipitating the therapeutic substance out of solution within the lumenal space of the filled hollow stent; cooling the filled hollow stent to a temperature below the melting point of the solvent such that the solvent freezes; and sublimating the frozen solvent to extract substantially all residual solvent from the lumenal space of the filled hollow stent while the precipitated therapeutic substance remains therein to thereby load the hollow stent with the therapeutic substance for subsequent delivery within a body lumen. submerging the hollow stent within a solution of a therapeutic substance and a solvent; vibrating the hollow stent and the solution to assist in moving the solution through the plurality of side openings into the lumenal space of the hollow stent; removing the hollow stent from the solution when the lumenal space is substantially full of the solution and thereby creating a filled hollow stent; precipitating the therapeutic substance out of solution within the lumenal space of the filled hollow stent; cooling the filled hollow stent to a temperature below the melting point of the solvent such that the solvent freezes; and sublimating the frozen solvent to extract substantially all residual solvent from the lumenal space of the filled hollow stent while the precipitated therapeutic substance remains therein to thereby load the hollow stent with the therapeutic substance for subsequent delivery within a body lumen.
A wind deflector arrangement comprising a wind deflector configured to reduce air resistance, said wind deflector being arranged on a cab roof of a vehicle, said wind deflector being pivotable around a substantially transversal axis of said vehicle, wherein the wind deflector arrangement further comprises at least one air pressure sensor for measuring an air pressure during traveling of said vehicle, characterized in that the at least one air pressure sensor is arranged within a space formed by said wind deflector and said cab roof of the vehicle.
A method for producing an yttrium oxide material, comprising the step of: firing a mixture of Y 2 O 3, SiC, and inorganic particles at a temperature in the range of 1500°C to 1850°C in an argon atmosphere, the inorganic particles being converted into a compound that contains a rare-earth element, Si, 0, and N; wherein the mixture of Y 2 O 3, SiC and inorganic particles comprises 80 vol% or more Y 2 O 3, 3.0 to 7.5 vol% Si 3 N 4 and 5.0 to 13 vol% SiC. firing a mixture of Y 2 O 3, SiC, and inorganic particles at a temperature in the range of 1500°C to 1850°C in an argon atmosphere, the inorganic particles being converted into a compound that contains a rare-earth element, Si, 0, and N; wherein the mixture of Y 2 O 3, SiC and inorganic particles comprises 80 vol% or more Y 2 O 3, 3.0 to 7.5 vol% Si 3 N 4 and 5.0 to 13 vol% SiC.
A transfer apparatus comprising: a first transfer module configured to hold an object to be transferred on the top thereof and transfer the object to be transferred at a first speed in a longitudinal direction; a second transfer module disposed in parallel with the first transfer module and configured to hold the object to be transferred on the top thereof and transfer the object to be transferred at a second speed in the longitudinal direction; and a blowing module, below at least one of the first transfer module and the second transfer module, for causing air to flow upward or downward; characterized in that the transfer apparatus further comprises: a third transfer module disposed in parallel with the first transfer module and the second transfer module and configured to transfer the object to be transferred in the longitudinal direction, wherein the third transfer module is provided between the first transfer module and the second transfer module, and wherein the third transfer module includes: a lower transfer unit for transferring the object to be transferred by contacting the bottom of the object to be transferred, and an upper transfer unit for transferring the object to be transferred by contacting the top of the object to be transferred. a first transfer module configured to hold an object to be transferred on the top thereof and transfer the object to be transferred at a first speed in a longitudinal direction; a second transfer module disposed in parallel with the first transfer module and configured to hold the object to be transferred on the top thereof and transfer the object to be transferred at a second speed in the longitudinal direction; and a blowing module, below at least one of the first transfer module and the second transfer module, for causing air to flow upward or downward; a third transfer module disposed in parallel with the first transfer module and the second transfer module and configured to transfer the object to be transferred in the longitudinal direction, wherein the third transfer module is provided between the first transfer module and the second transfer module, and wherein the third transfer module includes: a lower transfer unit for transferring the object to be transferred by contacting the bottom of the object to be transferred, and an upper transfer unit for transferring the object to be transferred by contacting the top of the object to be transferred. a lower transfer unit for transferring the object to be transferred by contacting the bottom of the object to be transferred, and an upper transfer unit for transferring the object to be transferred by contacting the top of the object to be transferred.
A temperature control method comprising: setting a plurality of control durations which are time durations for controlling a setting temperature of a specific space; there being a number of control durations, each of the control durations having a length; collecting predicted weather information and user's setting temperature information according to weather information for each control duration; determining setting temperature control information for each control duration, based on the collected setting temperature information; and controlling the setting temperature of the specific space, based on the setting temperature control information determined for each control duration and the predicted weather information, the method characterized in that the number of the plurality of control durations and the length of each control duration are changed, based on at least one of a highest weather information value during a day or a discomfort frequency counted by a time zone, and the discomfort frequency is calculated based on a state in which temperature measured by a sensor located in the specific space is below or above a threshold value. setting a plurality of control durations which are time durations for controlling a setting temperature of a specific space; there being a number of control durations, each of the control durations having a length; collecting predicted weather information and user's setting temperature information according to weather information for each control duration; determining setting temperature control information for each control duration, based on the collected setting temperature information; and controlling the setting temperature of the specific space, based on the setting temperature control information determined for each control duration and the predicted weather information, the method characterized in that the number of the plurality of control durations and the length of each control duration are changed, based on at least one of a highest weather information value during a day or a discomfort frequency counted by a time zone, and the discomfort frequency is calculated based on a state in which temperature measured by a sensor located in the specific space is below or above a threshold value.
A bolt having a chemical composition consisting of, in mass%: C: 0.32 to 0.39%, Si: 0.15% or less, Mn: 0.40 to 0.65%, P: 0.020% or less, S: 0.020% or less, Cr: 0.85 to 1.25%, Al: 0.005 to 0.060%, Ti: 0.010 to 0.050%, B: 0.0010 to 0.0030%, N: 0.0015 to 0.0080%, O: 0.0015% or less, Mo: 0 to 0.05%, V: 0 to 0.05%, Cu: 0 to 0.50%, Ni: 0 to 0.30%, and Nb: 0 to 0.05%, with a balance being Fe and impurities, and satisfying Formula and Formula, wherein the bolt: has a tensile strength of 1000 to 1300 MPa, measured in accordance with JIS B1051, and satisfies Formula; 4.9 ≤ 10 C + Si + 2 Mn + Cr + 4 Mo + 5 V ≤ 6.1 Mn / Cr ≤ 0.55 dissolved Cr / Cr ≥ 0.70 where, a content in mass% of a corresponding element is substituted for each symbol of an element in Formulae to; in a case where a corresponding element is at an impurity level, "0" is substituted for the symbol of the corresponding element in Formula; and a dissolved Cr amount in mass% in the bolt is substituted for [dissolved Cr] in Formula, the amount of dissolved Cr being measured by the method indicated in the description, and wherein a matrix micro-structure of the bolt is a tempered martensite single-phase structure. C: 0.32 to 0.39%, Si: 0.15% or less, Mn: 0.40 to 0.65%, P: 0.020% or less, S: 0.020% or less, Cr: 0.85 to 1.25%, Al: 0.005 to 0.060%, Ti: 0.010 to 0.050%, B: 0.0010 to 0.0030%, N: 0.0015 to 0.0080%, O: 0.0015% or less, Mo: 0 to 0.05%, V: 0 to 0.05%, Cu: 0 to 0.50%, Ni: 0 to 0.30%, and Nb: 0 to 0.05%, with a balance being Fe and impurities, and satisfying Formula and Formula, wherein the bolt: has a tensile strength of 1000 to 1300 MPa, measured in accordance with JIS B1051, and satisfies Formula; 4.9 ≤ 10 C + Si + 2 Mn + Cr + 4 Mo + 5 V ≤ 6.1 Mn / Cr ≤ 0.55 dissolved Cr / Cr ≥ 0.70 where, a content in mass% of a corresponding element is substituted for each symbol of an element in Formulae to; in a case where a corresponding element is at an impurity level, "0" is substituted for the symbol of the corresponding element in Formula; and a dissolved Cr amount in mass% in the bolt is substituted for [dissolved Cr] in Formula, the amount of dissolved Cr being measured by the method indicated in the description, and wherein a matrix micro-structure of the bolt is a tempered martensite single-phase structure. has a tensile strength of 1000 to 1300 MPa, measured in accordance with JIS B1051, and satisfies Formula; 4.9 ≤ 10 C + Si + 2 Mn + Cr + 4 Mo + 5 V ≤ 6.1 Mn / Cr ≤ 0.55 dissolved Cr / Cr ≥ 0.70 where, a content in mass% of a corresponding element is substituted for each symbol of an element in Formulae to; in a case where a corresponding element is at an impurity level, "0" is substituted for the symbol of the corresponding element in Formula; and a dissolved Cr amount in mass% in the bolt is substituted for [dissolved Cr] in Formula, the amount of dissolved Cr being measured by the method indicated in the description, and wherein a matrix micro-structure of the bolt is a tempered martensite single-phase structure.
Tread profile of a vehicle tyre - in particular a pneumatic vehicle tyre - with profile elements (1, 2, 3, 4) separated from one another by grooves (5, 6, 7), wherein the grooves (5, 6, 7) are delimited inwards in the radial direction R by a groove base and the profile elements (1, 2, 3, 4) are delimited outwards in the radial direction R by a radially outer surface, forming the ground contact surface, with grooves, in which at least one abrasion indicator is formed, wherein the abrasion indicator is formed by a rubber block, which extends from the groove base outwards in the radial direction R and has a surface delimiting the rubber block radially outwards in the radial direction R and an X-shaped line which is formed in the surface and indicates an abrasion threshold, wherein the X-shaped line of the abrasion indicator is a notch-shaped depression (17, 18) formed in the surface delimiting the rubber block, characterized in that the rubber block is delimited in the circumferential direction U of the vehicle tyre by block flanks (19, 20), which in the sectional planes formed perpendicularly to the axial direction A respectively extend from the groove base outwards in the radial direction R up to the surface, while forming an angle of inclination β in relation to the radial direction R, where 10°≤β≤30°, and form there the peripheral line delimiting the surface in the circumferential direction U, and in that the angle of inclination of the two block flanks (19, 20) is oriented outwards along their radial extent R respectively towards the rubber block.
A gas sparger which is operative for supplying an oxidation gas containing oxygen to a tank of a wet scrubber which is operative for removing sulphur dioxide from a process gas by means of a slurry comprising at least one compound chosen from the group of compounds comprising calcium sulphite and calcium sulphate, said gas sparger comprising an oxidation gas supply duct and at least a first oxidation gas supply nozzle, which is operative for distributing the oxidation gas in the slurry of said tank, said gas sparger being provided with at least a first liquid supply nozzle, which is located inside said oxidation gas supply duct and is operative for spraying a liquid containing water towards said first oxidation gas supply nozzle, said oxidation gas supply duct having a characteristic cross-sectional measure at said first oxidation gas supply nozzle, said first liquid supply nozzle being located a distance of maximum 5 times said characteristic cross-sectional measure from said first oxidation gas supply nozzle, wherein the oxidation gas supply duct is substantially straight between the location of said first liquid supply nozzle and the location of said first oxidation gas supply nozzle, characterised in that said gas sparger comprises a drain pipe for draining liquid from said gas supply duct.
An aircraft insulation system for providing fire penetration resistance and thermal protection, the aircraft insulation system comprising: two or more insulation blankets (24,26) comprising one or more bay blankets and one or more cap blankets, wherein the bay blankets have a greater thickness than the cap blankets, each insulation blanket (24, 26) having an inboard side and an outboard side; a continuous fire penetration resistant cover material having a heat seal adhesive, wherein the fire penetration resistant cover material covers the outboard side of the one or more bay blankets and the one or more cap blankets to provide a continuous fire barrier; a continuous insulation cover film having a heat seal adhesive, wherein the insulation cover film covers the inboard side of the two or more insulation blankets (24, 26) and is continous between the one or more bay blankets and the one or more cap blankets; and, a thermal heat seal that joins the fire penetration resistant cover material and the insulation cover film together between the one or more bay blankets and the one or more cap blankets to form a continuous insulation blanket assembly. two or more insulation blankets (24,26) comprising one or more bay blankets and one or more cap blankets, wherein the bay blankets have a greater thickness than the cap blankets, each insulation blanket (24, 26) having an inboard side and an outboard side; a continuous fire penetration resistant cover material having a heat seal adhesive, wherein the fire penetration resistant cover material covers the outboard side of the one or more bay blankets and the one or more cap blankets to provide a continuous fire barrier; a continuous insulation cover film having a heat seal adhesive, wherein the insulation cover film covers the inboard side of the two or more insulation blankets (24, 26) and is continous between the one or more bay blankets and the one or more cap blankets; and, a thermal heat seal that joins the fire penetration resistant cover material and the insulation cover film together between the one or more bay blankets and the one or more cap blankets to form a continuous insulation blanket assembly.
A method of estimating characterized in that the method is for estimating a ratio real total discharge time divided by theoretical discharge time giving the state of health of a battery in a power supply device for powering a system, the power supply device having at least one main power source that nominally powers said system, the battery being coupled to said main power source and to said system so as to be capable of powering the system in the event of an interruption of the supply of power from said main power source, the method comprising the steps of: • voluntarily interrupting the supply of power to the system from the main power source, the battery remaining coupled to the external system in order to power said external system; • determining the power (P batt) delivered from the battery to said system and measuring the voltage (V syst) delivered by the battery to said system; • reestablishing the supply of power to the system from the main power source prior to total discharge of the battery; • from the delivered power, determining (200, 201) a theoretical total discharge time (t theoretical_total) for the battery; and • from the voltage measured during the partial discharge, determining a partial discharge curve for the battery and extrapolating said curve in order to deduce therefrom a total discharge curve for the battery and thus estimate the real total discharge time (t real_total) for the battery, the ratio of the real total discharge time divided by the theoretical discharge time giving the state of health of the battery. • voluntarily interrupting the supply of power to the system from the main power source, the battery remaining coupled to the external system in order to power said external system; • determining the power (P batt) delivered from the battery to said system and measuring the voltage (V syst) delivered by the battery to said system; • reestablishing the supply of power to the system from the main power source prior to total discharge of the battery; • from the delivered power, determining (200, 201) a theoretical total discharge time (t theoretical_total) for the battery; and • from the voltage measured during the partial discharge, determining a partial discharge curve for the battery and extrapolating said curve in order to deduce therefrom a total discharge curve for the battery and thus estimate the real total discharge time (t real_total) for the battery, the ratio of the real total discharge time divided by the theoretical discharge time giving the state of health of the battery.
A metallocene compound represented by Formula 1 below: wherein R 1 and R 2 are same as or different from each other, and are independently hydrogen, a C1∼C20 alkyl group, a C6∼C20 aryl group, a C7∼C20 alkylaryl group, a C7∼C20 arylalkyl group, or a C7∼C20 alkoxyaryl group; R 3 is a C1∼C20 alkylsilyl group; Q 1 and Q 2 are same as or different from each other, and are independently hydrogen, a C1∼C20 alkyl group, or halogen; and M is Zr, Ti, or Hf. wherein R 1 and R 2 are same as or different from each other, and are independently hydrogen, a C1∼C20 alkyl group, a C6∼C20 aryl group, a C7∼C20 alkylaryl group, a C7∼C20 arylalkyl group, or a C7∼C20 alkoxyaryl group; R 3 is a C1∼C20 alkylsilyl group; Q 1 and Q 2 are same as or different from each other, and are independently hydrogen, a C1∼C20 alkyl group, or halogen; and M is Zr, Ti, or Hf.
A light-emitting semiconductor apparatus comprising: a light-emitting semiconductor device; a heat dissipating member (7, 107) whereon the light-emitting semiconductor device is mounted; leads (2, 102, 3, 103) that are electrically connected to the light-emitting semiconductor device; a tab (5, 105), which is a metal piece having an O-shape, the tab (5, 105) having an aperture (6, 106) formed therein into which the heat dissipating member (7, 107) is inserted; and an insulating resin that allows one end of the leads (2, 102, 3, 103) to be exposed therefrom and fastens at least a part of the leads (2, 102, 3, 103) and the heat dissipating member (7, 107) therein; a protective Zener diode, the protective Zener diode and the leads (2, 102, 3, 103) being electrically connected to each other; wherein the heat dissipating member (7, 107) is mounted in the aperture (6, 106) of the tab (5, 105); characterized in that the protective Zener diode is mounted on the tab. a light-emitting semiconductor device; a heat dissipating member (7, 107) whereon the light-emitting semiconductor device is mounted; leads (2, 102, 3, 103) that are electrically connected to the light-emitting semiconductor device; a tab (5, 105), which is a metal piece having an O-shape, the tab (5, 105) having an aperture (6, 106) formed therein into which the heat dissipating member (7, 107) is inserted; and an insulating resin that allows one end of the leads (2, 102, 3, 103) to be exposed therefrom and fastens at least a part of the leads (2, 102, 3, 103) and the heat dissipating member (7, 107) therein; a protective Zener diode, the protective Zener diode and the leads (2, 102, 3, 103) being electrically connected to each other; wherein the heat dissipating member (7, 107) is mounted in the aperture (6, 106) of the tab (5, 105); characterized in that the protective Zener diode is mounted on the tab.
A surface-treated steel material comprising a coating film formed on a surface of a steel material through a base layer containing at least an aluminum-zinc alloy plating layer, the aluminum-zinc alloy plating layer containing Al, Zn, Si, Cr, and Mg as constituent elements thereof, wherein an Mg content is 0.1 to 10% by mass, a Cr content is 0.02 to 1.0% by mass, the aluminum-zinc alloy plating layer contains 0.2 to 15% by volume of an Si-Mg phase, a ratio of a mass of Mg in the Si-Mg phase to a total mass of Mg is 3% or more, the coating film contains a coating film-forming resin (a), a cross-linking agent (b), at least one type of vanadium compound (c) selected from the group consisting of an alkaline earth metal vanadate and magnesium vanadate, and trimagnesium phosphate (d), the vanadium compound (c) is a compound in which an electrical conductivity of 1% by mass aqueous solution thereof at a temperature of 25°C is 200 μS/cm to 2,000 μS/cm, a content of the vanadium compound (c) is more than 50% by mass and 150% by mass or less relative to 100% by mass of a total of the coating film-forming resin (a) and the cross-linking agent (b), a pH of 1% by mass aqueous solution of the vanadium compound (c) is 6.5 to 11, and a content of the trimagnesium phosphate (d) is 3 to 150% by mass relative to 100% by mass of the total of the coating film-forming resin (a) and the cross-linking agent (b).
An isolated IL-1β specific antigen binding protein comprising the following CDRs: - a heavy chain variable region that includes the CDRs H1 = DYYWS, H2 = EIDHSGSTNYNPSLKS, H3 = ASPSSGWTLDY; and - a light chain variable region that includes the CDRs L1 = GDKLGDKFAF, L2 = LDNKRPS, L3 = YAWADTYEV. - a heavy chain variable region that includes the CDRs H1 = DYYWS, H2 = EIDHSGSTNYNPSLKS, H3 = ASPSSGWTLDY; and - a light chain variable region that includes the CDRs L1 = GDKLGDKFAF, L2 = LDNKRPS, L3 = YAWADTYEV.