mhurhangee/ep-ind-claims huggingface dataset:
A nozzle for blowing pressurized gas, the nozzle comprising: an elongate nozzle body having a supply end for receiving a supply of compressed gas and a substantially parabolic blowing end for blowing compressed gas along a blowing axis, the blowing end converging at an apex coaxial with the blowing axis; the blowing end comprising: a central outlet for generating a core stream of gas at the apex; at least three first outlets disposed at a first radius from the blowing axis, wherein: the first outlets are substantially parallel to the blowing axis and surround the core stream of gas, and the diameter of the first outlets is less than the diameter of the central outlet; at least three second outlets disposed at a second radius from the blowing axis, wherein: the second outlets are angled inward toward the blowing axis, the diameter of the second outlets is less than the diameter of the first outlets, and the second radius is greater than the first radius. an elongate nozzle body having a supply end for receiving a supply of compressed gas and a substantially parabolic blowing end for blowing compressed gas along a blowing axis, the blowing end converging at an apex coaxial with the blowing axis; the blowing end comprising: a central outlet for generating a core stream of gas at the apex; at least three first outlets disposed at a first radius from the blowing axis, wherein: the first outlets are substantially parallel to the blowing axis and surround the core stream of gas, and the diameter of the first outlets is less than the diameter of the central outlet; at least three second outlets disposed at a second radius from the blowing axis, wherein: the second outlets are angled inward toward the blowing axis, the diameter of the second outlets is less than the diameter of the first outlets, and the second radius is greater than the first radius. a central outlet for generating a core stream of gas at the apex; at least three first outlets disposed at a first radius from the blowing axis, wherein: the first outlets are substantially parallel to the blowing axis and surround the core stream of gas, and the diameter of the first outlets is less than the diameter of the central outlet; the first outlets are substantially parallel to the blowing axis and surround the core stream of gas, and the diameter of the first outlets is less than the diameter of the central outlet; at least three second outlets disposed at a second radius from the blowing axis, wherein: the second outlets are angled inward toward the blowing axis, the diameter of the second outlets is less than the diameter of the first outlets, and the second radius is greater than the first radius. the second outlets are angled inward toward the blowing axis, the diameter of the second outlets is less than the diameter of the first outlets, and the second radius is greater than the first radius.
A method for manufacturing luminescent crystals of 3-500nm size; said luminescent crystals being selected from compounds of formula [M 1 A 1] a M 2 b X c, wherein: A 1 represents one or more organic cations selected from the group consisting of ammonium, formamidinium, guanidinium, imidazolium, pyridinium, pyrrolidinium, protonated thiourea, M 1 represents one or more alkaline metals selected from Cs, Rb, K, Na, Li, M 2 represents one or more metals selected from the group consisting of Ge, Sn, Pb, Sb, and Bi, X represents one or more anions selected from the group consisting of chloride, bromide, iodide, cyanide, thiocyanate, isothiocyanate and sulfide, a represents 1-4, b represents 1-2, c represents 3-9; said method comprising the steps of: (a) providing a solid material, said solid material (i) having a stoichiometric composition of a moles (A 1 +M 1), b moles M 2 and c moles X and (ii) having an average particle size of at least 100nm and a poly-disperse size distribution, typically 50nm - 100μm; (b) dispersing said material in the presence of a liquid, whereby said liquid being selected from (i) liquid surfactants, (ii) a combination of surfactant and solvent, (iii) a combination of surfactant, solvent and pre-polymer or polymer and (iv) a combination of surfactant and liquid pre-polymer; and whereby said dispersing is effected by agitated milling balls, by ultrasound, by high shear mixing or by high pressure dispersion. A 1 represents one or more organic cations selected from the group consisting of ammonium, formamidinium, guanidinium, imidazolium, pyridinium, pyrrolidinium, protonated thiourea, M 1 represents one or more alkaline metals selected from Cs, Rb, K, Na, Li, M 2 represents one or more metals selected from the group consisting of Ge, Sn, Pb, Sb, and Bi, X represents one or more anions selected from the group consisting of chloride, bromide, iodide, cyanide, thiocyanate, isothiocyanate and sulfide, a represents 1-4, b represents 1-2, c represents 3-9; (a) providing a solid material, said solid material (i) having a stoichiometric composition of a moles (A 1 +M 1), b moles M 2 and c moles X and (ii) having an average particle size of at least 100nm and a poly-disperse size distribution, typically 50nm - 100μm; (b) dispersing said material in the presence of a liquid, whereby said liquid being selected from (i) liquid surfactants, (ii) a combination of surfactant and solvent, (iii) a combination of surfactant, solvent and pre-polymer or polymer and (iv) a combination of surfactant and liquid pre-polymer; and whereby said dispersing is effected by agitated milling balls, by ultrasound, by high shear mixing or by high pressure dispersion.
A turbine vane of a steam turbine comprising: a vane member (17,18) that has a space formed therein; and a plate spring member (19;191;192;193;194;195;196) that is disposed inside the space of the vane member (17,18) and slidably contacts an inner surface (21,22) of the vane member (17,18), wherein the plate spring member (19;191;192;193;194;195;196) includes a positioning portion which is positioned on the inner surface (21,22) of the vane member (17,18), a plurality of elastic contact portions arranged in the length direction of the vane member (17,18) which slidably contact the inner surface (21,22) of the vane member (17,18), and connection portions which connect the positioning portion to the elastic contact portion, and wherein the elastic contact portions of the plate spring member (19;191;192;193;194;195;196) are areas in which the elastic contact portions slidably contact the inner surface (21,22) of the vane member (17,18) to allow generation of friction between the elastic contact portions and the inner surface (21,22), and the contact area of an elastic contact portion at the center in the length direction of the vane member (17,18) is wider than the contact area of elastic contact portions at both ends in the length direction of the vane member (17,18). a vane member (17,18) that has a space formed therein; and a plate spring member (19;191;192;193;194;195;196) that is disposed inside the space of the vane member (17,18) and slidably contacts an inner surface (21,22) of the vane member (17,18), wherein the plate spring member (19;191;192;193;194;195;196) includes a positioning portion which is positioned on the inner surface (21,22) of the vane member (17,18), a plurality of elastic contact portions arranged in the length direction of the vane member (17,18) which slidably contact the inner surface (21,22) of the vane member (17,18), and connection portions which connect the positioning portion to the elastic contact portion, and wherein the elastic contact portions of the plate spring member (19;191;192;193;194;195;196) are areas in which the elastic contact portions slidably contact the inner surface (21,22) of the vane member (17,18) to allow generation of friction between the elastic contact portions and the inner surface (21,22), and the contact area of an elastic contact portion at the center in the length direction of the vane member (17,18) is wider than the contact area of elastic contact portions at both ends in the length direction of the vane member (17,18).
A remote controller comprising: a remote controller body including a control device for a user to input a remote-control command; a holding mechanism; a connecting mechanism connected between the remote controller body and the holding mechanism; and a first antenna and a second antenna provided at a side of the remote controller body and rotatably connected to the remote controller body, wherein the holding mechanism is movably connected to the remote controller body via the connecting mechanism and the holding mechanism is configured to move with respect to the remote controller body, such that the holding mechanism is either in an extended state or in a contracted state, and wherein each of the first antenna and the second antenna is configured to rotate relative to the remote controller body to cause the antenna to be extended or folded, and wherein the first antenna and the second antenna are stacked when folded, and wherein an anti-collision groove is provided at each of the first antenna and the second antenna in a thickness direction, and the anti-collision grooves of the first antenna and the second antenna overlap with each other when the first antenna and the second antenna are folded to cause a stacked thickness of the first antenna and the second antenna to be equal to a maximum thickness of one of the first antenna and the second antenna. a remote controller body including a control device for a user to input a remote-control command; a holding mechanism; a connecting mechanism connected between the remote controller body and the holding mechanism; and a first antenna and a second antenna provided at a side of the remote controller body and rotatably connected to the remote controller body, wherein the holding mechanism is movably connected to the remote controller body via the connecting mechanism and the holding mechanism is configured to move with respect to the remote controller body, such that the holding mechanism is either in an extended state or in a contracted state, and wherein each of the first antenna and the second antenna is configured to rotate relative to the remote controller body to cause the antenna to be extended or folded, and wherein the first antenna and the second antenna are stacked when folded, and wherein an anti-collision groove is provided at each of the first antenna and the second antenna in a thickness direction, and the anti-collision grooves of the first antenna and the second antenna overlap with each other when the first antenna and the second antenna are folded to cause a stacked thickness of the first antenna and the second antenna to be equal to a maximum thickness of one of the first antenna and the second antenna.
System for incubating microfluidic droplets, comprising a droplet incubator, a gas exchanger and a conveyer characterized in that, the droplet incubator comprises a container configured for the incubation of microfluidic droplets in a carrier fluid, wherein in the droplet incubator, microfluidic droplets are present, which comprise cell suspensions and/or dissolved reagents, wherein said microfluidic droplets are aqueous droplets in the carrier fluid, which is an oily phase wherein the droplet incubator is connected by flow-through means to a gas exchanger configured to allow for an exchange of gas between the carrier fluid and a gas source, wherein the flow-through means form a closed circuit for the carrier fluid which comprises gas or gas mixtures, and wherein the conveyer is a pump that leads the carrier fluid continuously through the closed circuit of the flow-through conduit, the droplet incubator and the gas exchanger, wherein the gas exchanger comprises a reservoir which is connected to a gas source, wherein the carrier fluid upon passing through the gas exchanger for the gas exchange resides in the reservoir, which is partially filled by the carrier fluid and partially filled by gas provided by the gas source and/or wherein the gas exchanger is formed at least partially by flow-through means, wherein the flow-through means consist of gas-permeable materials.
A computer-executable method for analyzing a motion, the method comprising: obtaining acceleration data associated with the motion, wherein the acceleration data comprises three components corresponding to three spatially orthogonal directions; for each orthogonal direction, computing an amount of oscillatory energy included in the motion in the orthogonal direction based on a corresponding acceleration component; for at least one orthogonal direction, obtaining an energy fraction factor by computing a ratio between the amount of the oscillatory energy in the orthogonal direction and a total amount of the oscillatory energy; and generating a motion-analysis output based at least on the energy fraction factor, wherein oscillatory energy is used to maintain balance and/or control a body part during the motion and does not contribute to the forward motion, and wherein computing the amount of the oscillatory energy comprises performing a frequency-domain analysis on the acceleration data, wherein performing the frequency-domain analysis comprises: performing a Fourier transform on the acceleration data to obtain a plurality of frequency components of the acceleration; computing, for each frequency of a predetermined set of frequencies, a frequency component of the oscillatory energy; and summing the computed frequency components of the oscillatory energy. obtaining acceleration data associated with the motion, wherein the acceleration data comprises three components corresponding to three spatially orthogonal directions; for each orthogonal direction, computing an amount of oscillatory energy included in the motion in the orthogonal direction based on a corresponding acceleration component; for at least one orthogonal direction, obtaining an energy fraction factor by computing a ratio between the amount of the oscillatory energy in the orthogonal direction and a total amount of the oscillatory energy; and generating a motion-analysis output based at least on the energy fraction factor, wherein oscillatory energy is used to maintain balance and/or control a body part during the motion and does not contribute to the forward motion, and wherein computing the amount of the oscillatory energy comprises performing a frequency-domain analysis on the acceleration data, wherein performing the frequency-domain analysis comprises: performing a Fourier transform on the acceleration data to obtain a plurality of frequency components of the acceleration; computing, for each frequency of a predetermined set of frequencies, a frequency component of the oscillatory energy; and summing the computed frequency components of the oscillatory energy. performing a Fourier transform on the acceleration data to obtain a plurality of frequency components of the acceleration; computing, for each frequency of a predetermined set of frequencies, a frequency component of the oscillatory energy; and summing the computed frequency components of the oscillatory energy.
A wound dressing comprising a perforated material having a top face and a bottom face and having plural through-holes, and an absorbent material disposed on the top face of the perforated material; wherein at least the bottom face of the perforated material is coated with a low-adhesive resin except leaving at least a part of the through-holes so as not to block up all the through-holes, at least a part of the absorbent material facing the through-holes of the perforated material is coated with the low-adhesive resin, and allowing fluid penetration from the bottom face side of the perforated material into the inside of the absorbent material. wherein at least the bottom face of the perforated material is coated with a low-adhesive resin except leaving at least a part of the through-holes so as not to block up all the through-holes, at least a part of the absorbent material facing the through-holes of the perforated material is coated with the low-adhesive resin, and allowing fluid penetration from the bottom face side of the perforated material into the inside of the absorbent material.
Method for equalizing the gas pressure in a mass flow hopper for discharging a fine-grained, fluidizable bulk material from a silo, wherein the mass flow hopper has at least one at least partially downwardly open pressure relief fitting or at least one internal hopper which is supported against the wall of the mass flow hopper by at least one vertical, upwardly closed and downwardly open channel, characterized by - reducing the relative negative gas pressure within the bulk material which is present in a state of flow with respect to the gas pressure in the external surroundings or in the upper space of the silo by means of at least one pressure equalization line, wherein the at least one pressure equalization line is arranged such that its lower open end extends into the internal region of the pressure relief fitting or into the at least one vertical channel, and in that its upper end leads into the external surroundings or into the upper space of the silo, - injecting pressurized gas, preferably pressurized air, into the interior of the mass flow hopper, and by - measuring the gas pressure using at least one pressure measurement device in at least one separate line, which is largely free of bulk material and which opens out into the internal region of the at least one at least partially downwardly open pressure relief fitting, or using at least one pressure measurement device in the at least one vertical, upwardly closed and downwardly open channel. - reducing the relative negative gas pressure within the bulk material which is present in a state of flow with respect to the gas pressure in the external surroundings or in the upper space of the silo by means of at least one pressure equalization line, wherein the at least one pressure equalization line is arranged such that its lower open end extends into the internal region of the pressure relief fitting or into the at least one vertical channel, and in that its upper end leads into the external surroundings or into the upper space of the silo, - injecting pressurized gas, preferably pressurized air, into the interior of the mass flow hopper, and by - measuring the gas pressure using at least one pressure measurement device in at least one separate line, which is largely free of bulk material and which opens out into the internal region of the at least one at least partially downwardly open pressure relief fitting, or using at least one pressure measurement device in the at least one vertical, upwardly closed and downwardly open channel.
A method for providing metallization upon a semiconductor substrate, the method comprising: providing a semiconductor substrate having a surface suitable for printing; placing a stencil having a contact side, a fill side, and at least one aperture extending from the contact side to the fill side over the semiconductor substrate with the contact side of the stencil in contact with the semiconductor substrate, the contact side of the stencil being substantially flat and forming a sharp edge with a wall of the at least one aperture, a cross- section of the at least one aperture at the contact side having a predetermined width, and the at least one aperture being tapered such that an area of a cross-section of the at least one aperture at the fill side is larger than an area of the cross-section of the at least one aperture at the contact side; and printing conductive ink through the at least one aperture and onto the semiconductor substrate, the conductive ink being printed in direct contact with the semiconductor substrate, wherein the conductive ink has a Malcom viscosity of less than about Mx 15, which corresponds to a viscosity of about 150 Pa ·s at 10RPM at 25°Celsius in a Malcom viscometer. providing a semiconductor substrate having a surface suitable for printing; placing a stencil having a contact side, a fill side, and at least one aperture extending from the contact side to the fill side over the semiconductor substrate with the contact side of the stencil in contact with the semiconductor substrate, the contact side of the stencil being substantially flat and forming a sharp edge with a wall of the at least one aperture, a cross- section of the at least one aperture at the contact side having a predetermined width, and the at least one aperture being tapered such that an area of a cross-section of the at least one aperture at the fill side is larger than an area of the cross-section of the at least one aperture at the contact side; and printing conductive ink through the at least one aperture and onto the semiconductor substrate, the conductive ink being printed in direct contact with the semiconductor substrate, wherein the conductive ink has a Malcom viscosity of less than about Mx 15, which corresponds to a viscosity of about 150 Pa ·s at 10RPM at 25°Celsius in a Malcom viscometer.
Water-conducting domestic appliance, in particular a dishwasher, comprising a treatment chamber, comprising a softening means for fresh water, which means is associated with a regeneration means that has a brine reservoir, and comprising a storage container for storing fresh water and cleaning liquor, the storage container being arranged thermally conductively with respect to the treatment chamber and containing at least one liquor volume, and comprising at least one means (29, 30) for transferring cleaning liquor out of the treatment chamber into the liquor volume, characterised in that the storage container additionally contains a regeneration volume which is used to produce the brine reservoir, and in that the storage container has at least one delimitation means for separating the liquor volume from the regeneration volume, which means prevents liquid being transferred out of the liquor volume and into the regeneration volume.
Composition comprising: - 0.003 to 0.02% by weight of an alkylethercarboxylic acid of formula or of a water-soluble salt of said acid: R-O(CH 2 -CH 2 O) n -CH 2 COOH Formula wherein R is an alkyl chain with 3 to 9 carbon atoms and n is an integer from 1 to 9, - 0.05 to 0.1% by weight of a alkali metal citrate, and - more than 98% by weight of an alkali metal chloride, with the percentages by weight being given in relation to the weight of the composition. - 0.003 to 0.02% by weight of an alkylethercarboxylic acid of formula or of a water-soluble salt of said acid: R-O(CH 2 -CH 2 O) n -CH 2 COOH Formula wherein R is an alkyl chain with 3 to 9 carbon atoms and n is an integer from 1 to 9, - 0.05 to 0.1% by weight of a alkali metal citrate, and - more than 98% by weight of an alkali metal chloride, with the percentages by weight being given in relation to the weight of the composition.