mhurhangee/ep-ind-claims huggingface dataset:
A prosthetic socket sealing system (300, 550, 600, 750, 800, 855), including: a rigid prosthetic socket (305, 555, 605, 755, 805, 860); a prosthetic liner (310, 570, 620, 765, 815, 875) for donning over a residual limb, the liner (310, 570, 620, 765, 815, 875) having a polymeric interior (315, 575, 625, 770, 820, 880) and at least a partial fabric exterior (320, 580, 630, 775, 825, 885); and a soft inner socket (325, 585, 635, 780, 830, 890) adapted to receive a residual limb of an amputee while covered with the prosthetic liner (310, 570, 620, 765, 815, 875) and to be at least substantially inserted into the rigid prosthetic socket (305, 555, 605, 755, 805, 860); wherein the prosthetic liner (310, 570, 620, 765, 815, 875) is also adapted to extend beyond the open ends of the soft inner socket and rigid prosthetic socket (305, 555, 605, 755, 805, 860); wherein the system (300, 550, 600, 750, 800, 855) further includes a polymeric sealing sleeve (330, 590, 640, 785, 835, 850) adapted to be donned over the soft inner socket (325, 585, 635, 780, 830, 890) prior to insertion of the soft inner socket (325, 585, 635, 780, 830, 890) into the rigid prosthetic socket (305, 555, 605, 755, 805, 860) and to extend beyond the open ends of the soft inner socket (325, 585, 635, 780, 830, 890) and rigid prosthetic socket (305, 555, 605, 755, 805, 860); wherein the exterior of the sealing sleeve (330, 590, 640, 785, 835, 850) is adapted to seal against the interior of the rigid prosthetic socket (305, 555, 605, 755, 805,_860) and the interior of the sealing sleeve (330, 590, 640, 785, 835, 850) is adapted to seal against a portion of the prosthetic liner (310,570, 620, 765, 815, 875) that resides outside of the rigid prosthetic socket (305, 555, 605, 755, 805, 860) and soft inner socket (325, 585, 635, 780, 830, 890). a rigid prosthetic socket (305, 555, 605, 755, 805, 860); a prosthetic liner (310, 570, 620, 765, 815, 875) for donning over a residual limb, the liner (310, 570, 620, 765, 815, 875) having a polymeric interior (315, 575, 625, 770, 820, 880) and at least a partial fabric exterior (320, 580, 630, 775, 825, 885); and a soft inner socket (325, 585, 635, 780, 830, 890) adapted to receive a residual limb of an amputee while covered with the prosthetic liner (310, 570, 620, 765, 815, 875) and to be at least substantially inserted into the rigid prosthetic socket (305, 555, 605, 755, 805, 860);
A wireless communication device (100, 100A) comprising: a plurality of antenna elements (ATx, APx); a modulation unit configured to modulate signals including data in a plurality of first orbital angular momentum, OAM, modes, where the plurality of first orbital angular momentum, OAM, modes are real values different from each other and intervals between each of the real values is less than one; a calculation unit (130, 130a) configured to calculate factors (w m) indicating weights corresponding to each of the signals in the plurality of first OAM modes modulated by the modulation unit for each of the plurality of antenna elements, based on information indicating a wireless environment of a counter wireless communication device that is a transmission destination of the data; and a transmission processing unit (140, 140a) configured to multiplex each of the signals in the plurality of first OAM modes for each of the plurality of antenna elements by using the factors, and output the signals obtained through multiplexing for each of the plurality of antenna elements to each of the plurality of antenna elements. a plurality of antenna elements (ATx, APx); a modulation unit configured to modulate signals including data in a plurality of first orbital angular momentum, OAM, modes, where the plurality of first orbital angular momentum, OAM, modes are real values different from each other and intervals between each of the real values is less than one; a calculation unit (130, 130a) configured to calculate factors (w m) indicating weights corresponding to each of the signals in the plurality of first OAM modes modulated by the modulation unit for each of the plurality of antenna elements, based on information indicating a wireless environment of a counter wireless communication device that is a transmission destination of the data; and a transmission processing unit (140, 140a) configured to multiplex each of the signals in the plurality of first OAM modes for each of the plurality of antenna elements by using the factors, and output the signals obtained through multiplexing for each of the plurality of antenna elements to each of the plurality of antenna elements.
Loading floor for a vehicle, comprising a plurality of profile members which are elongate in a longitudinal direction, which are arranged beside each other and which are connected to each other, in which the loading floor has at least one hollow space (13, 16) which is continuous in the longitudinal direction, characterized in that the hollow space (13, 16) has at least one lateral opening (12, 19), which is not continuous in the longitudinal direction, with respect to an outer space of the loading floor and which is further laterally closed, so that an air conditioning air stream which can be directed through the hollow space (13, 16) is discharged from the hollow space (13, 16) and thereby reaches an inner space of the vehicle, wherein at least one profile member has a longitudinal groove and wherein the lateral opening of the hollow space of the profile member that is continuous in the longitudinal direction opens in the longitudinal groove.
Electromagnetic waveguide, based on the inhibited-coupling mechanism, comprising a hollow central portion the contour of which is at least partially defined by a first set of at least seven primary hollow tubes (8,9,10,11,12,13,14), distributed annularly around the central hollow portion, said primary hollow tubes being substantially of the same size, distant from one another, said waveguide being characterized in that it also comprises a second set of tubes comprising at least one hollow secondary tube, when there are several thereof, these secondary tubes are positioned annularly around the primary tubes, the area of the at least one hollow secondary tube being comprised between 0.35 and 0.50 times the area of the central hollow portion.
A nanosecond pulser comprising: a plurality of switch modules, each of the plurality of switch modules include one or more solid state switches, a snubber resistor, a snubber capacitor, and a snubber diode, the snubber capacitor, and the snubber diode, being arranged in series with each other and together in parallel with the solid state switch and the snubber resistor being arranged in parallel with the snubber diode; a transformer electrically coupled with the plurality of switches comprising: at least one core; a primary winding wound at least partially around a portion of the at least one core, each of the plurality of switch modules are electrically coupled with the primary windings; and a plurality of secondary windings wound at least partially around a portion of the core; and an output electrically coupled with the plurality of secondary windings that outputs electrical pulses having a peak voltage greater than about 1 kilovolt and having a pulse width of less than about 1000 nanoseconds. a plurality of switch modules, each of the plurality of switch modules include one or more solid state switches, a snubber resistor, a snubber capacitor, and a snubber diode, the snubber capacitor, and the snubber diode, being arranged in series with each other and together in parallel with the solid state switch and the snubber resistor being arranged in parallel with the snubber diode; a transformer electrically coupled with the plurality of switches comprising: at least one core; a primary winding wound at least partially around a portion of the at least one core, each of the plurality of switch modules are electrically coupled with the primary windings; and a plurality of secondary windings wound at least partially around a portion of the core; and at least one core; a primary winding wound at least partially around a portion of the at least one core, each of the plurality of switch modules are electrically coupled with the primary windings; and a plurality of secondary windings wound at least partially around a portion of the core; and an output electrically coupled with the plurality of secondary windings that outputs electrical pulses having a peak voltage greater than about 1 kilovolt and having a pulse width of less than about 1000 nanoseconds.
A thermal analysis sensor (100, 1600) comprising: a support member (120, 620, 1620); a sample sensor coupled to the support member and comprising a sample support (140, 420, 610, 1610) for receiving a sample, the sensor being electrically coupled to a first set of interconnects; and a reference sensor (110, 430, 1630) comprising a cylindrical ring being coupled to the support member and coupled to a second set of interconnects, wherein the cylindrical ring is positioned adjacent to and surrounding at least a portion of the sample support of the sample sensor without the surfaces physically contacting each other, the thermal mass of the reference sensor is matched to the thermal mass of the sample support and/or any crucible containing a sample on the sample support, and the reference sensor configured to provide a reference signal without the addition of an external reference material. a support member (120, 620, 1620); a sample sensor coupled to the support member and comprising a sample support (140, 420, 610, 1610) for receiving a sample, the sensor being electrically coupled to a first set of interconnects; and a reference sensor (110, 430, 1630) comprising a cylindrical ring being coupled to the support member and coupled to a second set of interconnects, wherein the cylindrical ring is positioned adjacent to and surrounding at least a portion of the sample support of the sample sensor without the surfaces physically contacting each other, the thermal mass of the reference sensor is matched to the thermal mass of the sample support and/or any crucible containing a sample on the sample support, and the reference sensor configured to provide a reference signal without the addition of an external reference material.
An opposed-piston engine having a cylinder block with a plurality of cylinders aligned in one row, in which each cylinder includes an intake port longitudinally separated from an exhaust port, comprising: an open intake chamber in the cylinder block including at least one air inlet opening through the cylinder block; and, all of the cylinder intake ports being contained in the intake chamber to receive charge air therein; characterized by: an open exhaust chamber in the cylinder block including at least one exhaust outlet opening through the cylinder block; and, all of the cylinder exhaust ports being contained in the exhaust chamber to discharge exhaust thereinto. an open intake chamber in the cylinder block including at least one air inlet opening through the cylinder block; and, all of the cylinder intake ports being contained in the intake chamber to receive charge air therein; characterized by: an open exhaust chamber in the cylinder block including at least one exhaust outlet opening through the cylinder block; and, all of the cylinder exhaust ports being contained in the exhaust chamber to discharge exhaust thereinto. an open exhaust chamber in the cylinder block including at least one exhaust outlet opening through the cylinder block; and, all of the cylinder exhaust ports being contained in the exhaust chamber to discharge exhaust thereinto.
A flux for submerged arc welding, comprising an Fe-Si-Mn alloy in an amount of 0.5 to 15% by mass, and further comprising: CaF 2: 10 to 30% by mass; CaO: 1 to 10% by mass; MgO: 15 to 30% by mass; MnO: 1 to 10% by mass; SiO 2: 10 to 30% by mass; Al 2 O 3: 15 to 35% by mass; TiO 2: 0.5 to 3.0% by mass; and ZrO 2: 0.1 to 3% by mass, wherein the Fe-Si-Mn alloy consists of Mn: 40 to 75% by mass, Si: 15 to 45% by mass, and Fe: 0.4% by mass or more and 30% by mass or less with the remainder being unavoidable impurities.
A method for measuring a tear meniscus using fluorescein concentrated in the tear meniscus to make it fluorescent, based on an analysis of an image obtained by implementing operations of: - instilling fluorescein on the surface of a patient's eye to be examined, - illuminating the eye to be examined with blue light, characterized in that it comprises: - capturing an image of the eye to be examined, said image comprising non-fluorescent blue regions in the absence of fluorescein and fluorescent green regions in the presence of fluorescein, - identifying the tear meniscus and measuring its height in pixels (h), - identifying the iris and measuring its outer diameter in pixels (d), - calculating a ratio (R = D/d) of a physical outer diameter of the iris as estimated or else measured in millimeters to its measurement in pixels (d) and calculating the physical height (H = Rxh) of the tear meniscus based on this ratio. - instilling fluorescein on the surface of a patient's eye to be examined, - illuminating the eye to be examined with blue light, - capturing an image of the eye to be examined, said image comprising non-fluorescent blue regions in the absence of fluorescein and fluorescent green regions in the presence of fluorescein, - identifying the tear meniscus and measuring its height in pixels (h), - identifying the iris and measuring its outer diameter in pixels (d), - calculating a ratio (R = D/d) of a physical outer diameter of the iris as estimated or else measured in millimeters to its measurement in pixels (d) and calculating the physical height (H = Rxh) of the tear meniscus based on this ratio.
A powder formulation comprising particles of tolterodine or a tolterodine-related compound selected from -N, N-diisopropyl-3-(2-hydroxy-5-hydroxymethylphenyl)-3-phenylpropanamine, -N, N-diisopropyl-3-(2-hydroxy-5-methylphenyl)-3-phenylpropanamine, -N, N-diisopropyl-3-(2-hydroxy-5-hydroxymethylphenyl)-3-phenylpropanamine, (R, S)-N, N-diisopropyl-3-(2-hydroxy-5-methylphenyl)-3-phenylpropanamine, and (2-[ -3-(di(propan-2-yl)amino)-1-phenylpropyl]-4-(hydroxymethyl)phenyl] 2-methylpropanoate), or a pharmaceutically acceptable salt thereof, said particles being obtainable by supercritical anti-solvent precipitation and having a D 50 of 4 μm or less and a D 90 of 10 μm or less.
A method of managing a decoded picture buffer, DPB, for a video decoder using coding modes including an Inter prediction mode and an Intra Block Copy, IntraBC, mode, comprising: determining a total number of reference pictures allowed to be stored in the DPB, wherein the DPB comprises short-term and long-term reference pictures; allocating up to the total number of reference pictures in the DPB; and decoding a current picture using the reference pictures stored in the DPB; characterized in that if the IntraBC mode is enabled, and no loop filters are used for the current picture, marking the current decoded picture as being used for long-term reference at a beginning of and during a process of decoding the current picture, and marking the current decoded picture in the DPB as a short-term reference picture after decoding the current picture is completed. determining a total number of reference pictures allowed to be stored in the DPB, wherein the DPB comprises short-term and long-term reference pictures; allocating up to the total number of reference pictures in the DPB; and decoding a current picture using the reference pictures stored in the DPB; characterized in that if the IntraBC mode is enabled, and no loop filters are used for the current picture, marking the current decoded picture as being used for long-term reference at a beginning of and during a process of decoding the current picture, and marking the current decoded picture in the DPB as a short-term reference picture after decoding the current picture is completed.
An aircraft including a heating assembly, the heating assembly comprising: an internal combustion engine having a liquid coolant system distinct from any fuel and lubricating system of the engine, the liquid cooling system including cooling passages in the internal combustion engine for circulating a liquid coolant from a coolant inlet to a coolant outlet; a heat exchanger and a coolant circulation path outside of the internal combustion engine, the coolant circulation path in fluid communication with the coolant inlet and the coolant outlet, the coolant circulation path extending through the heat exchanger and the heat exchanger configured to remove a portion of a waste heat from the liquid coolant; and a heating element (76, 76') in heat exchange relationship with the coolant circulation path to receive another portion of the waste heat therefrom, the heating element (76, 76') in heat exchange relationship with a portion of the aircraft to be heated, wherein the portion of the aircraft to be heated includes a surface susceptible to icing; characterised in that: the heating element (76, 76') is in heat exchange relationship with the coolant circulation path through fluid communication with the coolant circulation path such that the liquid coolant is circulated directly through a fluid passage forming the heating element (76, 76'), and the surface susceptible to icing is in heat exchange relationship with the fluid passage, to prevent or limit ice formation on the surface. an internal combustion engine having a liquid coolant system distinct from any fuel and lubricating system of the engine, the liquid cooling system including cooling passages in the internal combustion engine for circulating a liquid coolant from a coolant inlet to a coolant outlet; a heat exchanger and a coolant circulation path outside of the internal combustion engine, the coolant circulation path in fluid communication with the coolant inlet and the coolant outlet, the coolant circulation path extending through the heat exchanger and the heat exchanger configured to remove a portion of a waste heat from the liquid coolant; and a heating element (76, 76') in heat exchange relationship with the coolant circulation path to receive another portion of the waste heat therefrom, the heating element (76, 76') in heat exchange relationship with a portion of the aircraft to be heated, wherein the portion of the aircraft to be heated includes a surface susceptible to icing;
A hand tool with connections, comprising: a working unit having a working end and a handle end opposite to the working end; a handle being mounted on the handle end of the working unit and having a working unit end and a knocking unit end; a knocking unit mounted on the knocking unit end of the handle; characterized in that a connecting part between the knocking unit and the handle end of the working unit is a contacting surface (35, 37), the handle end or the contacting surface being configured as a deformable contact, realizing the connection between the working unit and the knocking unit. a working unit having a working end and a handle end opposite to the working end; a handle being mounted on the handle end of the working unit and having a working unit end and a knocking unit end; a knocking unit mounted on the knocking unit end of the handle; characterized in that a connecting part between the knocking unit and the handle end of the working unit is a contacting surface (35, 37), the handle end or the contacting surface being configured as a deformable contact, realizing the connection between the working unit and the knocking unit.
Dispenser part, comprising at least two component parts (17, 18; 31, 32; 41 a, 42a; 41 b, 42b; 41c, 42c; 41d; 42d) each joined by a seam (21; 33; 43a; 43b; 43c; 43d), said dispenser part comprising a first injection moulded plastic component part (17; 31; 41a) having an associated first mating surface; a second injection moulded plastic component part (18; 32; 42a) having an associated second mating surface; and a seam (21; 33; 43a) formed by said first mating surface and said second mating surface during a two component injection moulding for joining said first component part and said second component part (17, 18; 31, 32; 41a, 42a; 41b, 42b; 41c, 42c; 41d; 42d) to define a dispenser part, characterized in that an edge portion (44b, 44c, 44d) on one dispenser part extends past a transverse extension of the seam (43b; 43c; 43d) such that the resulting seam (21; 33; 43a; 43b; 43d) has an impact strength equal to or greater than the strength of at least one of said first and second moulded plastic component parts (17, 18; 31, 32; 41a, 42a; 41b, 42b; 41c, 42c; 41d; 42d) adjacent the seam (21; 33; 43a; 43b; 43c).
An apparatus for concentrating and diluting a specific gas, comprising: a specific gas concentrating system including a gas chamber having filled therein a particle material for condensation and vaporization capable of selectively condensing the specific gas and a freezing machine arranged on the outer periphery of the gas chamber for cooling the specific gas fed to the chamber to a predetermined cool temperature, and a gas feeding and retrieving system having a feeding port arranged for feeding a gas containing plural gas species, a diluted gas retrieving port arranged for retrieving a gas containing the specific gas having been diluted, and a concentrated gas retrieving port arranged for retrieving a gas containing the specific gas having been concentrated, to form the gas containing the specific gas being diluted by selectively condensing the specific gas on a surface of the particle material in the chamber through cooling with the freezing machine and to form the gas containing the specific gas being concentrated by vaporizing the condensed gas on the surface of the particle material through heating a surrounding of the concentrated gas retrieving part, thereby to cause continuous retrieval of the gas containing the specific gas having been diluted through the diluted gas retrieving port of the chamber or continuous retrieval of the gas containing the specific gas having been concentrated through the concentrated gas retrieving port of the chamber. a specific gas concentrating system including a gas chamber having filled therein a particle material for condensation and vaporization capable of selectively condensing the specific gas and a freezing machine arranged on the outer periphery of the gas chamber for cooling the specific gas fed to the chamber to a predetermined cool temperature, and a gas feeding and retrieving system having a feeding port arranged for feeding a gas containing plural gas species, a diluted gas retrieving port arranged for retrieving a gas containing the specific gas having been diluted, and a concentrated gas retrieving port arranged for retrieving a gas containing the specific gas having been concentrated, to form the gas containing the specific gas being diluted by selectively condensing the specific gas on a surface of the particle material in the chamber through cooling with the freezing machine and to form the gas containing the specific gas being concentrated by vaporizing the condensed gas on the surface of the particle material through heating a surrounding of the concentrated gas retrieving part, thereby to cause continuous retrieval of the gas containing the specific gas having been diluted through the diluted gas retrieving port of the chamber or continuous retrieval of the gas containing the specific gas having been concentrated through the concentrated gas retrieving port of the chamber.