mhurhangee/ep-ind-claims huggingface dataset:
A light conversion device comprising: a phosphor wheel including: an optoceramic phosphor element comprising one or more phosphors embedded in a ceramic host; a metal heat sink which is a metal disk rotatable about a central axis of the metal disk; a solder bond disposed on the metal heat sink, attaching the optoceramic phosphor element to the metal heat sink; and a solderable metal stack including more than one metal layer disposed on a back side of the optoceramic phosphor element between the optoceramic phosphor element and the solder bond; wherein the metal heat sink is attached with the solderable metal stack by the solder bond on an outer rim of the metal heat sink. an optoceramic phosphor element comprising one or more phosphors embedded in a ceramic host; a metal heat sink which is a metal disk rotatable about a central axis of the metal disk; a solder bond disposed on the metal heat sink, attaching the optoceramic phosphor element to the metal heat sink; and a solderable metal stack including more than one metal layer disposed on a back side of the optoceramic phosphor element between the optoceramic phosphor element and the solder bond; wherein the metal heat sink is attached with the solderable metal stack by the solder bond on an outer rim of the metal heat sink.
A parenteral composition, comprising a therapeutically effective amount of an eprinomectin and a vehicle comprising dimethylsulfoxide, and optionally other excipients.
A flowmeter, comprising: a flow inlet; a flow outlet; a first conduit having an inlet leg, an outlet leg (212'A), and a central conduit portion disposed between the inlet leg and the outlet leg (212'A), the inlet leg being fluidly coupled to the central conduit portion, and the central conduit portion being fluidly coupled to the outlet leg (212'A); a second conduit having an inlet leg, an outlet leg (212'B), and a central conduit portion (212'C) disposed between the inlet leg and the outlet leg (212'B), the inlet leg being fluidly coupled to the central conduit portion (212'C), and the central conduit portion (212'C) being fluidly coupled to the outlet leg (212'B); wherein the flow inlet is fluidly coupled to a first end of the first conduit and a first end of the second conduit, and the flow outlet is fluidly coupled to a second end of the first conduit and a second end of the second conduit; a manifold fluidly coupled to the inlet legs (212A, 212B) and the outlet legs (212'A, 212'B); and a first driver coupled to the manifold, wherein the first driver is arranged to vibrate the first and second conduits (208A, 208B). a flow inlet; a flow outlet; a first conduit having an inlet leg, an outlet leg (212'A), and a central conduit portion disposed between the inlet leg and the outlet leg (212'A), the inlet leg being fluidly coupled to the central conduit portion, and the central conduit portion being fluidly coupled to the outlet leg (212'A); a second conduit having an inlet leg, an outlet leg (212'B), and a central conduit portion (212'C) disposed between the inlet leg and the outlet leg (212'B), the inlet leg being fluidly coupled to the central conduit portion (212'C), and the central conduit portion (212'C) being fluidly coupled to the outlet leg (212'B); wherein the flow inlet is fluidly coupled to a first end of the first conduit and a first end of the second conduit, and the flow outlet is fluidly coupled to a second end of the first conduit and a second end of the second conduit; a manifold fluidly coupled to the inlet legs (212A, 212B) and the outlet legs (212'A, 212'B); and a first driver coupled to the manifold, wherein the first driver is arranged to vibrate the first and second conduits (208A, 208B).
Fabric for use in a machine for producing and/or finishing a paper, board, tissue or pulp web, comprising a base structure which is formed as a piece of flat woven material, which flat woven material is formed by warp threads and weft threads crossing one another, wherein the piece of flat woven material has multiple sections (4a, 4b, 4c) which are formed in one piece with one another, wherein at least one property in one of the sections (4a, 4b, 4c) is different from the respective property of at least one adjacent section (4a, 4b, 4c), wherein the piece of flat woven material has three successive sections (4a, 4b, 4c) which, viewed in a machine direction of the fabric, extend one after another, wherein a first section is followed by a second section which is followed by a third section, wherein the length of the first and of the third section (4a, 4c) is the same, wherein the first and the third section (4a, 4c) are woven in one layer and the second section is woven in two layers, and wherein the first and the third section (4a, 4c) are arranged one above the other, by which means a two-layer fabric is also formed there.
A modifying agent for polyolefin resins, comprising a calcium-containing inorganic filler whose particle surface is treated with an alicyclic dicarboxylic acid represented by formula and/or formula: wherein R 1 is a C 1 -C 4 alkyl group, and R 1 binds to the carbon at position 3 or 4 of a cyclohexane ring; and wherein R 2 is a hydrogen atom or a C 1 -C 4 alkyl group, and R 2 binds to the carbon at position 3 or 4 of a cyclohexene ring.
An air-bag for use in a vehicle, the air-bag comprising: a first layer having a first edge and a second edge; and a second layer having a third edge and a fourth edge, wherein the layers (12, 13) are offset rotationally relative to one another such that the first edge is at an angle A relative to the third edge, and wherein a second part of the first layer is folded about a fold line that intersects the first edge and which is substantially at the angle A relative to the first edge so that a second part of the second layer is superimposed on the second part of the first layer to define a chamber therebetween, the layers (12, 13) being attached to one another along a seam which extends at least partly around a periphery of the chamber so that the chamber may be inflated by gas provided by a source of gas, characterised in that: a first part of the second layer is superimposed on a first part of the first layer to define a reinforced part and the superimposed parts (27, 27) of the first and second layers (12, 13) are attached to one another along a seam which extends at least partly around the reinforced part. a first layer having a first edge and a second edge; and a second layer having a third edge and a fourth edge, wherein the layers (12, 13) are offset rotationally relative to one another such that the first edge is at an angle A relative to the third edge, and wherein a second part of the first layer is folded about a fold line that intersects the first edge and which is substantially at the angle A relative to the first edge so that a second part of the second layer is superimposed on the second part of the first layer to define a chamber therebetween, the layers (12, 13) being attached to one another along a seam which extends at least partly around a periphery of the chamber so that the chamber may be inflated by gas provided by a source of gas, characterised in that: a first part of the second layer is superimposed on a first part of the first layer to define a reinforced part and the superimposed parts (27, 27) of the first and second layers (12, 13) are attached to one another along a seam which extends at least partly around the reinforced part.
A method of making a gas separation system, said method comprising the steps of: (a) providing a porous metal support having a first surface and a second surface with each said surface being opposed to the other to thereby define a support thickness, said first surface of said support having a first mean pore size; (b) contacting said first surface of said support with a first particulate material having a first mean particle size that is less than said first mean pore size to form a first coated surface on a coated support; (c) removing excess first particulate material from said first coated surface; (d) contacting said first coated surface with a second particulate material having a second mean particle size that is less than said first mean particle size to form a second coated surface on said coated support; (e) removing excess second particulate material from said second coated surface; (f) depositing at least one layer of a gas selective metal to overlie said first surface of said support; and (g) annealing said coated support and said at least one layer of gas selective metal wherein said annealing is conducted at a temperature that encourages grain growth of the gas selective metal, and wherein said annealing occurs in the absence of hydrogen until the annealing temperature reaches a set temperature, and in the presence of hydrogen when the temperature is above the set temperature, wherein the set temperature is at least 300° C. (a) providing a porous metal support having a first surface and a second surface with each said surface being opposed to the other to thereby define a support thickness, said first surface of said support having a first mean pore size; (b) contacting said first surface of said support with a first particulate material having a first mean particle size that is less than said first mean pore size to form a first coated surface on a coated support; (c) removing excess first particulate material from said first coated surface; (d) contacting said first coated surface with a second particulate material having a second mean particle size that is less than said first mean particle size to form a second coated surface on said coated support; (e) removing excess second particulate material from said second coated surface; (f) depositing at least one layer of a gas selective metal to overlie said first surface of said support; and (g) annealing said coated support and said at least one layer of gas selective metal wherein said annealing is conducted at a temperature that encourages grain growth of the gas selective metal, and wherein said annealing occurs in the absence of hydrogen until the annealing temperature reaches a set temperature, and in the presence of hydrogen when the temperature is above the set temperature, wherein the set temperature is at least 300° C.
A computer-implemented method of detecting one or more branches of a blood vessel comprising storing one or more intravascular image datasets of the blood vessel, each intravascular dataset comprising a plurality of A-lines; detecting a lumen boundary in a first A-line image generated from a set of A-lines from the plurality of A-lines, wherein the first A-line image has an r dimension and an A-line dimension; specifying a predetermined search distance T; defining a search region, the search region bounded by the detected lumen boundary and a boundary offset therefrom by the predetermined distance T; detecting edges in the search region; and identifying a candidate branching region in response to the detected edges. storing one or more intravascular image datasets of the blood vessel, each intravascular dataset comprising a plurality of A-lines; detecting a lumen boundary in a first A-line image generated from a set of A-lines from the plurality of A-lines, wherein the first A-line image has an r dimension and an A-line dimension; specifying a predetermined search distance T; defining a search region, the search region bounded by the detected lumen boundary and a boundary offset therefrom by the predetermined distance T; detecting edges in the search region; and identifying a candidate branching region in response to the detected edges.
Vibrating device for the treatment of adipose tissues comprising: at least one generator apparatus of alternating electric current, at least one probe connected to said generator apparatus and including: at least one piezoelectric element, suitable to transform said alternating electric current into mechanical vibrations, and at least one tip (31, 40), suitable to be introduced into said adipose tissue, to transmit said mechanical vibrations and to cause cavitation inside said adipose tissue, said probe presenting at least one resonance frequency variable according to said probe and to the environment surrounding said tip, a control system suitable to verify the resonance frequency of said probe immersed in the surrounding environment, and to regulate the emission frequency of the electrical current so as to supply to said probe frequencies prevalently in proximity of the resonance frequency of said probe when said tip is immersed in specific environments to be treated, so as to cause cavitation only if said tip is immersed in said specific environments, wherein said control system is suitable to indicate important variations of the resonance frequency of said probe and to avoid damaging of non-adipose tissues by not regulating, in this cases, the emission frequency of the electrical current.
A p-type thermoelectric conversion material having a full Heusler alloy having a composition represented by the following General Formula and having a relative density of 85% or more, Fe x Ti y MA a MB b... wherein in Formula, MA is one element selected from the group consisting of Si, Sn, and Ge, MB is one element selected from the group consisting of Al, Ga, and In, and x, y, a, and b are numbers set so that x + y + a + b = 100, a + b = z, 50 < x ≤ 52.5, 20 ≤ y ≤ 24.5, 24.5 ≤ z ≤ 29, a > 0, and b > 0 in atom%, respectively.
A computer-implemented method at an autonomous vehicle for signaling a refueling attendant, wherein the autonomous vehicle comprises a fuel door which while closed is configured by a layer of materials to prevent near-field communication, NFC, with an NFC enabled payment card located in proximity to a refueling port of the autonomous vehicle, the method comprising: in response to confirming that the autonomous vehicle is proximal to a refueling station (140, 142): a) providing a signal to the refueling attendant; b) waiting for refueling to commence; and c) determining whether refueling has commenced, said refuelling including opening the fuel door to allow NFC communications between a reader on a fuel nozzle and the NFC enabled payment card; if, after a threshold period, refueling has not commenced, repeating the steps a) to c) until refueling has commenced. in response to confirming that the autonomous vehicle is proximal to a refueling station (140, 142): a) providing a signal to the refueling attendant; b) waiting for refueling to commence; and c) determining whether refueling has commenced, said refuelling including opening the fuel door to allow NFC communications between a reader on a fuel nozzle and the NFC enabled payment card; a) providing a signal to the refueling attendant; b) waiting for refueling to commence; and c) determining whether refueling has commenced, said refuelling including opening the fuel door to allow NFC communications between a reader on a fuel nozzle and the NFC enabled payment card; if, after a threshold period, refueling has not commenced, repeating the steps a) to c) until refueling has commenced.
Electrical contact element for a single- or multipole plug housing having at least one contact element accommodation chamber, which is composed of electrically insulating material, for accommodating the at least one electrical contact element, wherein the contact element has a fastening section for fastening an electrical line, wherein the electrical contact element has a contact section for establishing an electrically conductive connection with a corresponding mating contact element, wherein the electrical contact element has at least one latching lance, wherein the latching lance can be moved from a first position to a second position and vice versa, wherein the latching lance protrudes obliquely outwards in the first position, wherein the latching lance latches with the contact element accommodation chamber in the first position when the electrical contact element is arranged in a predetermined position in the contact element accommodation chamber, wherein the latching lance further has a first locking element, wherein the electrical contact element has a second locking element which corresponds to the first locking element, wherein the first locking element and the second locking element are formed in such a way that when, in the first position, a force acts on the latching lance against a withdrawal direction of the electrical contact element out of the contact element accommodation chamber, the first locking element and the second locking element are connected to one another, wherein the first locking element has a first section, wherein the first section extends substantially transverse to a withdrawal direction of the electrical contact element from the contact element accommodation chamber, characterized in that the first locking element has a second section which is fixedly connected to the first section, wherein the second section is substantially in the form of a hook element, and in that the second locking element is in the form of a tab element, wherein the first locking element and the second locking element interact in the first position in such a way that the tab element and the hook element are connected in an interlocking manner; or in that the first locking element has an opening, and in that the second locking element has an angular element with a first limb and a second limb, wherein the first limb extends through the opening and the second limb extends substantially parallel in relation to the first locking element, wherein the first locking element and the second locking element are connected in an interlocking manner in the first position.
A radiation shielding material for shielding X-rays, gamma-rays and neutron-rays, the radiation shielding material comprises a complex containing a fibrous nanocarbon material, a primary radiation shielding particle, and a binder, the fibrous nanocarbon material and the primary radiation shielding particle being dispersed in the binder, wherein the complex has a density of 0.8 to 3.0 g/cm 3, and characterized in that the complex has nanosized holes outside the fibrous nanocarbon material. the fibrous nanocarbon material and the primary radiation shielding particle being dispersed in the binder, wherein the complex has a density of 0.8 to 3.0 g/cm 3, and characterized in that the complex has nanosized holes outside the fibrous nanocarbon material.
A surgical access assembly for use during a surgical procedure, comprising: a housing defining proximal and distal ends; an access member extending distally from the housing and being dimensioned for positioning within tissue, the housing and the access member defining a longitudinal axis; and a seal assembly disposed within the housing, the seal assembly including first and second seal components (102, 104) operatively coupled to each other for relative rotation, each of the first and second seal components including respective passages (112, 130) for passage of a surgical object, wherein the first seal component includes one of an annular recess and an annular rib, and the second seal component includes the other of the annular recess and the annular rib, the annular recess dimensioned to engage the annular rib when the first and second seal components are mounted relative to each other such that the first seal component is rotatably moveable about the longitudinal axis relative to the second seal component; and characterized in that the first seal component includes at least one manually operable member extending orthogonally from a proximal surface of the first seal component and beyond the proximal end of the housing, the manually operable member dimensioned and positioned to be manipulated by a clinician to effect rotational movement of the first seal component relative to the second seal component. a housing defining proximal and distal ends; an access member extending distally from the housing and being dimensioned for positioning within tissue, the housing and the access member defining a longitudinal axis; and a seal assembly disposed within the housing, the seal assembly including first and second seal components (102, 104) operatively coupled to each other for relative rotation, each of the first and second seal components including respective passages (112, 130) for passage of a surgical object, wherein the first seal component includes one of an annular recess and an annular rib, and the second seal component includes the other of the annular recess and the annular rib, the annular recess dimensioned to engage the annular rib when the first and second seal components are mounted relative to each other such that the first seal component is rotatably moveable about the longitudinal axis relative to the second seal component; and characterized in that the first seal component includes at least one manually operable member extending orthogonally from a proximal surface of the first seal component and beyond the proximal end of the housing, the manually operable member dimensioned and positioned to be manipulated by a clinician to effect rotational movement of the first seal component relative to the second seal component.