mhurhangee/ep-ind-claims huggingface dataset:
A wearable article continuous in a longitudinal direction and a transverse direction comprising a front elastic belt region, a back elastic belt region, a crotch region, a waist opening, and a pair of leg openings; the crotch region extending longitudinally between the front elastic belt region and the back elastic belt region; wherein each of the front and back elastic belt (84, 86) is a laminate comprising an inner sheet, an outer sheet, and a plurality of elastic members running in the transverse direction, wherein the laminate further comprising an elastic adhesive bonding which continuously bonds the elastic member for at least about 10mm in the direction of stretch in a region adjacent the side edges of the front and back elastic belts (84, 86), and a discrete patterned adhesive bonding applied to at least one of the inner sheet and the outer sheet with intervals in the transverse direction and the longitudinal direction to intermittently bond the inner sheet and the outer sheet, wherein the discrete patterned adhesive bonding at least extends substantially along the transverse dimension between the elastic adhesive bonding, and substantially along the longitudinal dimension between the distal edge and proximal edge of the front and back elastic belts (84, 86), wherein the elastic adhesive bonding and the discrete patterned adhesive bonding are provided by the same adhesive agent; wherein the laminate is bonded by heat at the side edges to form side seams, the side seams existing no distant than about 20mm from the side edges, and the remainder of the laminate is free of heat bonds. wherein each of the front and back elastic belt (84, 86) is a laminate comprising an inner sheet, an outer sheet, and a plurality of elastic members running in the transverse direction, wherein the laminate further comprising an elastic adhesive bonding which continuously bonds the elastic member for at least about 10mm in the direction of stretch in a region adjacent the side edges of the front and back elastic belts (84, 86), and a discrete patterned adhesive bonding applied to at least one of the inner sheet and the outer sheet with intervals in the transverse direction and the longitudinal direction to intermittently bond the inner sheet and the outer sheet, wherein the discrete patterned adhesive bonding at least extends substantially along the transverse dimension between the elastic adhesive bonding, and substantially along the longitudinal dimension between the distal edge and proximal edge of the front and back elastic belts (84, 86), wherein the elastic adhesive bonding and the discrete patterned adhesive bonding are provided by the same adhesive agent; wherein the laminate is bonded by heat at the side edges to form side seams, the side seams existing no distant than about 20mm from the side edges, and the remainder of the laminate is free of heat bonds.
A method for preparing a resin comprising the steps of a) providing an aqueous medium having a pH of 1 to 7; b) adding lignin to the aqueous medium; c) mixing at a temperature of from 41°C to 95°C until a dispersion of lignin in the aqueous medium has been obtained; d) adding alkali, phenol and formaldehyde to the dispersion and e) maintaining the mixture at a temperature of from 30°C to 95°C for at least 30 minutes. a) providing an aqueous medium having a pH of 1 to 7; b) adding lignin to the aqueous medium; c) mixing at a temperature of from 41°C to 95°C until a dispersion of lignin in the aqueous medium has been obtained; d) adding alkali, phenol and formaldehyde to the dispersion and e) maintaining the mixture at a temperature of from 30°C to 95°C for at least 30 minutes.
An ethylene copolymer composition comprising a copolymer blend of: an ethylene copolymer fraction having Mooney Viscosity within the range from 14 to 40 MU (MST, 5+4 @ 200°C), measured as described in the description, and corrected Mooney Small-Thin Relaxation Area (cMSTRA, normalized to 50 MU (MST, 5+4 @ 200°C) reference) of at least 600 MU-sec, measured as described in the description, wherein the ethylene copolymer fraction comprises 30 to 80 wt% ethylene-derived units, units derived from one or more C 3 to C 20 α-olefins, and 0 to 10 wt% polyene-derived units, said wt%s based on the weight of the ethylene copolymer fraction; and a linear ethylene copolymer fraction having Mooney Viscosity within the range from 5 to 100 MU (ML, 1+4 @ 125°C), measured as described in the description, and corrected Mooney Large Relaxation Area (cMLRA, normalized to 80 MU (ML, 1+4 @ 125°C) reference) within the range from 15 to 350 MU-sec, measured as described in the description, wherein the linear ethylene copolymer fraction comprises 30 to 80 wt% ethylene-derived units, units derived from one or more C 3 to C 20 α-olefins, and 0 to 10 wt% polyene-derived units, said wt%s based on the weight of the ethylene copolymer fraction. an ethylene copolymer fraction having Mooney Viscosity within the range from 14 to 40 MU (MST, 5+4 @ 200°C), measured as described in the description, and corrected Mooney Small-Thin Relaxation Area (cMSTRA, normalized to 50 MU (MST, 5+4 @ 200°C) reference) of at least 600 MU-sec, measured as described in the description, wherein the ethylene copolymer fraction comprises 30 to 80 wt% ethylene-derived units, units derived from one or more C 3 to C 20 α-olefins, and 0 to 10 wt% polyene-derived units, said wt%s based on the weight of the ethylene copolymer fraction; and a linear ethylene copolymer fraction having Mooney Viscosity within the range from 5 to 100 MU (ML, 1+4 @ 125°C), measured as described in the description, and corrected Mooney Large Relaxation Area (cMLRA, normalized to 80 MU (ML, 1+4 @ 125°C) reference) within the range from 15 to 350 MU-sec, measured as described in the description, wherein the linear ethylene copolymer fraction comprises 30 to 80 wt% ethylene-derived units, units derived from one or more C 3 to C 20 α-olefins, and 0 to 10 wt% polyene-derived units, said wt%s based on the weight of the ethylene copolymer fraction.
A method for monitoring and controlling deflection of rotor blades of a wind turbine, the method comprising: operating the wind turbine at standard pitch angle settings for the rotor blades; monitoring a loading condition of the wind turbine over a predetermined time period; tracking a number of wind condition deviations comprising at least a wind direction deviation or a wind speed deviation of a certain magnitude occurring during the predetermined time period; and, if the number of wind condition deviations exceed a wind deviation threshold and the loading condition exceed a loading threshold, wherein an exceedance above the wind deviation threshold and the loading threshold is indicative of a certain magnitude of a rotor blade deflection occurring in one or more of the rotor blades, altering one or more of the standard pitch angle settings of the rotor blades; and performing one or more corrective actions so as to reduce the probability of a rotor blade tower strike by reducing blade deflection by altering a blade pitch angle of at least one of the rotor blades. operating the wind turbine at standard pitch angle settings for the rotor blades; monitoring a loading condition of the wind turbine over a predetermined time period; tracking a number of wind condition deviations comprising at least a wind direction deviation or a wind speed deviation of a certain magnitude occurring during the predetermined time period; and, if the number of wind condition deviations exceed a wind deviation threshold and the loading condition exceed a loading threshold, wherein an exceedance above the wind deviation threshold and the loading threshold is indicative of a certain magnitude of a rotor blade deflection occurring in one or more of the rotor blades, altering one or more of the standard pitch angle settings of the rotor blades; and performing one or more corrective actions so as to reduce the probability of a rotor blade tower strike by reducing blade deflection by altering a blade pitch angle of at least one of the rotor blades.
A medical antimicrobial composition characterized in that an ammonium group-containing polymer compound is dispersed in a siloxanyl structure-containing polymer, wherein the polymer compound is constituted of a monomer having a radical polymerizable group and an ammonium group in the molecule.
A three-dimensional molding machine comprising: a three-dimensional molding device configured to mold a three-dimensional object (Fr) on a molding pallet (Pm); a circuit forming device configured to form a circuit pattern on the molded object (Fr) during or after molding; a component mounting device configured to mount an electronic component on the circuit pattern formed on the molded object (Fr); a pallet conveyance device configured to convey the molded object (Fr) together with the molding pallet (Pm) between the three-dimensional molding device, the circuit forming device, and the component mounting device; and a component conveyance device configured to convey the electronic components into the component mounting device from an outside of the machine characterized in that: the three-dimensional molding machine is configured by integrating a molding block and a mounting block on two different sides, wherein the pallet conveyance device is disposed in the molding block, wherein the component conveyance device is disposed at a position ahead of the pallet conveyance device in the mounting block so as to be parallel to it. a three-dimensional molding device configured to mold a three-dimensional object (Fr) on a molding pallet (Pm); a circuit forming device configured to form a circuit pattern on the molded object (Fr) during or after molding; a component mounting device configured to mount an electronic component on the circuit pattern formed on the molded object (Fr); a pallet conveyance device configured to convey the molded object (Fr) together with the molding pallet (Pm) between the three-dimensional molding device, the circuit forming device, and the component mounting device; and a component conveyance device configured to convey the electronic components into the component mounting device from an outside of the machine characterized in that: the three-dimensional molding machine is configured by integrating a molding block and a mounting block on two different sides, wherein the pallet conveyance device is disposed in the molding block, wherein the component conveyance device is disposed at a position ahead of the pallet conveyance device in the mounting block so as to be parallel to it. the three-dimensional molding machine is configured by integrating a molding block and a mounting block on two different sides, wherein the pallet conveyance device is disposed in the molding block, wherein the component conveyance device is disposed at a position ahead of the pallet conveyance device in the mounting block so as to be parallel to it.
Method for producing a superconductive conductor, comprising the following steps: - providing a plurality of conductive strips (1, 2) by means of a strip provision device, wherein the plurality of conductive strips comprises at least one superconductor strip; - applying liquid solder to the plurality of conductive strips (1, 2) by immersing the conductive strips (1, 2) in a solder bath; - forming a strip stack by stacking the conductive strips (1, 2) wetted with solder in the solder bath; - forming a superconductor body by processing the strip stack with a roll system; wherein the solder bath comprises an inlet with a plurality of individual inlets arranged in a comb-like manner for the plurality of conductive strips (1, 2), a passage for stacking the plurality of conductive strips (1, 2), and an outlet. - providing a plurality of conductive strips (1, 2) by means of a strip provision device, wherein the plurality of conductive strips comprises at least one superconductor strip; - applying liquid solder to the plurality of conductive strips (1, 2) by immersing the conductive strips (1, 2) in a solder bath; - forming a strip stack by stacking the conductive strips (1, 2) wetted with solder in the solder bath; - forming a superconductor body by processing the strip stack with a roll system;
A method of assessing a sample from a transplant subject who is a heart transplant recipient, the method comprising: (a) determining an amount of total cf-DNA in a blood, plasma or serum sample from the subject, wherein the subject has, is suspected of having, has had, or is at risk of having a transplant complication; and (b) reporting and/or recording the amount of total cf-DNA; (c) comparing the amount of total cf-DNA to a threshold total cf-DNA value; and (d) determining that the subject has, or as being at increased risk of having, a transplant complication when the amount of total cf-DNA is equal to or greater than the threshold, wherein the threshold is 8 ng/mL. (a) determining an amount of total cf-DNA in a blood, plasma or serum sample from the subject, wherein the subject has, is suspected of having, has had, or is at risk of having a transplant complication; and (b) reporting and/or recording the amount of total cf-DNA; (c) comparing the amount of total cf-DNA to a threshold total cf-DNA value; and (d) determining that the subject has, or as being at increased risk of having, a transplant complication when the amount of total cf-DNA is equal to or greater than the threshold,
A powdery composition based on silica for ceramic welding, comprising (a) from 10% to 90% of a phase of siliceous particles based on the total weight of the composition comprising at least 80% by weight of cristobalite and at most 20% by weight, preferably at most 17% by weight of residual tridymite based on the total weight of the composition; and (b) from 90% to 10% by weight based on the total weight of the composition of conventional additives forming a binding phase, which comprises at least one of the following elements or compounds: Al, Si, Mg, Ca, Fe, Cr, Zr, oxide Al 2 O 3, SiO 2, MgO, CaO, Fe 2 O 3, Cr 2 O 3, ZrO 2, BaO, SrO, peroxides CaO 2, MgO 2, BaO 2, and SrO 2, and said siliceous particles having an average particle size by sifting d 50 comprised between 350 and 800 μm, preferably between 400 and 500 μm. (a) from 10% to 90% of a phase of siliceous particles based on the total weight of the composition comprising at least 80% by weight of cristobalite and at most 20% by weight, preferably at most 17% by weight of residual tridymite based on the total weight of the composition; and (b) from 90% to 10% by weight based on the total weight of the composition of conventional additives forming a binding phase, which comprises at least one of the following elements or compounds: Al, Si, Mg, Ca, Fe, Cr, Zr, oxide Al 2 O 3, SiO 2, MgO, CaO, Fe 2 O 3, Cr 2 O 3, ZrO 2, BaO, SrO, peroxides CaO 2, MgO 2, BaO 2, and SrO 2, and
A compound of the formula: wherein X is: R is H, methyl, or ethyl; R 1 is methyl, when R 2 is H, and R 1 is H when R 2 is methyl; R 3 is H or F; R 4 is H, F, or methyl; R 5 is OH, methyl, methoxy, or F; R 6 is H when R 7 is OH, and R 6 is F when R 7 is F; and R 8 and R 9 are each independently H or F; or a pharmaceutically acceptable salt thereof. wherein X is: R is H, methyl, or ethyl; R 1 is methyl, when R 2 is H, and R 1 is H when R 2 is methyl; R 3 is H or F; R 4 is H, F, or methyl; R 5 is OH, methyl, methoxy, or F; R 6 is H when R 7 is OH, and R 6 is F when R 7 is F; and R 8 and R 9 are each independently H or F;
A portable attitude test stand (PATS) (50; 150; 250) for an aircraft engine (10; 10a), comprising: a support frame (60; 160; 260) mountable on a trailer of a road vehicle; a test cell supported by the support frame (60; 160; 260) and sized to receive the aircraft engine (10; 10a), the test cell operable to rotate the aircraft engine (10; 10a) about a pitch axis and a roll axis of the aircraft engine (10; 10a); characterised in that it further comprises an actuator (71; 171) operatively connected to the test cell and to the support frame (60; 160; 260), the actuator (71; 171) operable to lower and raise the test cell relative to the support frame (60; 160; 260) between a transport configuration in which the test cell has a transport height and a test configuration in which the test cell has a test height, the test height being greater than the transport height, wherein the support frame (60; 160; 260) includes a base (62; 262) and vertical members (64; 164; 264) protruding from the base (62; 262), two carriages (70, 70'; 170; 270) movably engaged to the vertical members (64; 164; 264) of the support frame (60; 160; 260), the test cell supported by the support frame (60; 160; 260) via the carriages (70, 70'; 170; 270), the carriages (70, 70'; 170; 270) movable relative to the vertical members (64; 164; 264) to vary the height of the test cell between the test height and the transport height. a support frame (60; 160; 260) mountable on a trailer of a road vehicle; a test cell supported by the support frame (60; 160; 260) and sized to receive the aircraft engine (10; 10a), the test cell operable to rotate the aircraft engine (10; 10a) about a pitch axis and a roll axis of the aircraft engine (10; 10a); characterised in that it further comprises an actuator (71; 171) operatively connected to the test cell and to the support frame (60; 160; 260), the actuator (71; 171) operable to lower and raise the test cell relative to the support frame (60; 160; 260) between a transport configuration in which the test cell has a transport height and a test configuration in which the test cell has a test height, the test height being greater than the transport height, wherein the support frame (60; 160; 260) includes a base (62; 262) and vertical members (64; 164; 264) protruding from the base (62; 262), two carriages (70, 70'; 170; 270) movably engaged to the vertical members (64; 164; 264) of the support frame (60; 160; 260), the test cell supported by the support frame (60; 160; 260) via the carriages (70, 70'; 170; 270), the carriages (70, 70'; 170; 270) movable relative to the vertical members (64; 164; 264) to vary the height of the test cell between the test height and the transport height.
A system for adapting a wireless transmission rate, comprising; a transmitter; a processor adapted to perform the following for a transmission of each of a plurality of sequential wireless local area network, WLAN, frames by said transmitter: estimate a packet Error Rate, PER, for each of a plurality of physical layer, PHY, rate values; estimate a plurality of data transmit times each according to respective said PER and one of said PHY rate values; and select one of said PHY rate values for adaption of a wireless transmission rate of said transmitter in a following frame according to an analysis of said plurality of data transmit times, characterised in that, when at least some WLAN frames are fragmented, each of said data transmit times are calculated using the equation below: Tx time = PHY + P + F + MAC ⋅ 8 PHY Rate ⋅ 1 + PER + CW min ⋅ S 2 ⋅ 2 ⋅ PER r − 1 2 ⋅ PER − 1 Wherein: PHY denotes PLCP time; PHY rate denotes the PHY rate; P denotes protocol overheads; S denotes Slot time; MAC denotes MAC headers and/or trailers; F denotes Data frame size; CW min denotes initial contention window size; and r denotes the maximum number of frame or fragment re-transmissions. estimate a packet Error Rate, PER, for each of a plurality of physical layer, PHY, rate values; estimate a plurality of data transmit times each according to respective said PER and one of said PHY rate values; and select one of said PHY rate values for adaption of a wireless transmission rate of said transmitter in a following frame according to an analysis of said plurality of data transmit times, characterised in that, when at least some WLAN frames are fragmented, each of said data transmit times are calculated using the equation below: Tx time = PHY + P + F + MAC ⋅ 8 PHY Rate ⋅ 1 + PER + CW min ⋅ S 2 ⋅ 2 ⋅ PER r − 1 2 ⋅ PER − 1 Wherein: PHY denotes PLCP time; PHY rate denotes the PHY rate; P denotes protocol overheads; S denotes Slot time; MAC denotes MAC headers and/or trailers; F denotes Data frame size; CW min denotes initial contention window size; and r denotes the maximum number of frame or fragment re-transmissions. PHY denotes PLCP time; PHY rate denotes the PHY rate; P denotes protocol overheads; S denotes Slot time; MAC denotes MAC headers and/or trailers; F denotes Data frame size; CW min denotes initial contention window size; and r denotes the maximum number of frame or fragment re-transmissions.
A method for locating probes within a gas turbine engine, the method comprising: positioning a plurality of location transmitters relative to the gas turbine engine, each location transmitter having a known location relative to the gas turbine engine; inserting a probe through an access port of the gas turbine engine, the probe including a probe tip and a location signal receiver, the location signal receiver being configured to receive location-related signals transmitted from the plurality of location transmitters; receiving the location-related signals at a computing device communicatively coupled to the probe; determining, by the computing device, a current location of the probe tip within the gas turbine engine based on the location-related signals and the known locations of the plurality of location transmitters; identifying, with the computing device, a virtual location of the probe tip within a three-dimensional model of the gas turbine engine corresponding to the current location of the probe tip within the gas turbine engine; and providing for display, by the computing device, the three-dimensional model of the gas turbine engine, wherein the virtual location of the probe tip is displayed as a visual indicator within the three-dimensional model; characterized in that said positioning a plurality of location transmitters relative to the gas turbine engine comprises positioning the plurality of location transmitters within a plurality of access ports of the gas turbine engine, the plurality of access ports differing from the access port through which the probe is inserted. positioning a plurality of location transmitters relative to the gas turbine engine, each location transmitter having a known location relative to the gas turbine engine; inserting a probe through an access port of the gas turbine engine, the probe including a probe tip and a location signal receiver, the location signal receiver being configured to receive location-related signals transmitted from the plurality of location transmitters; receiving the location-related signals at a computing device communicatively coupled to the probe; determining, by the computing device, a current location of the probe tip within the gas turbine engine based on the location-related signals and the known locations of the plurality of location transmitters; identifying, with the computing device, a virtual location of the probe tip within a three-dimensional model of the gas turbine engine corresponding to the current location of the probe tip within the gas turbine engine; and providing for display, by the computing device, the three-dimensional model of the gas turbine engine, wherein the virtual location of the probe tip is displayed as a visual indicator within the three-dimensional model; characterized in that said positioning a plurality of location transmitters relative to the gas turbine engine comprises positioning the plurality of location transmitters within a plurality of access ports of the gas turbine engine, the plurality of access ports differing from the access port through which the probe is inserted.