mhurhangee/ep-ind-claims huggingface dataset:
An implantable medical device, comprising: an electronic circuit; a shield member defining a first portion of an interior cavity of the implantable medical device; a feedthrough assembly comprising: a shield extender having a top face and a sidewall that extends from the top face so that the top face and the sidewall are a single continuous component, at least one feedthrough aperture extending through the top face, an insulated feedthrough pin extending through the feedthrough aperture, the sidewall having a bottom edge that defines an open side of the shield extender, the bottom edge coupled to the shield member, the sidewall defining a second portion of the interior cavity, the second portion in communication with the first portion, the electronic circuit residing in the interior cavity, the feedthrough pin being electrically coupled to the electronic circuit, the electronic circuit enclosed in the interior cavity, characterized in that the shield extender sidewall defines a channel, the shield extender further comprising a coupling member extending interiorly from the sidewall and accessible through the channel, wherein the electronic circuit is coupled to the coupling member. an electronic circuit; a shield member defining a first portion of an interior cavity of the implantable medical device; a feedthrough assembly comprising: a shield extender having a top face and a sidewall that extends from the top face so that the top face and the sidewall are a single continuous component, at least one feedthrough aperture extending through the top face, an insulated feedthrough pin extending through the feedthrough aperture, the sidewall having a bottom edge that defines an open side of the shield extender, the bottom edge coupled to the shield member, the sidewall defining a second portion of the interior cavity, the second portion in communication with the first portion, the electronic circuit residing in the interior cavity, the feedthrough pin being electrically coupled to the electronic circuit, the electronic circuit enclosed in the interior cavity, a shield extender having a top face and a sidewall that extends from the top face so that the top face and the sidewall are a single continuous component, at least one feedthrough aperture extending through the top face, an insulated feedthrough pin extending through the feedthrough aperture, the sidewall having a bottom edge that defines an open side of the shield extender, the bottom edge coupled to the shield member, the sidewall defining a second portion of the interior cavity, the second portion in communication with the first portion, the electronic circuit residing in the interior cavity, the feedthrough pin being electrically coupled to the electronic circuit, the electronic circuit enclosed in the interior cavity,
Polymer composition, comprising or consisting of a) a matrix made of at least one crystallisable, thermoplastic polymer, b) at least one azine dye, and also c) at least one mono-, bi-, tri- and/or tetravalent metal salt, selected from the group consisting of metal chlorides, metal bromides and metal pseudohalogenides and also mixtures or combinations hereof. a) a matrix made of at least one crystallisable, thermoplastic polymer, b) at least one azine dye, and also c) at least one mono-, bi-, tri- and/or tetravalent metal salt, selected from the group consisting of metal chlorides, metal bromides and metal pseudohalogenides and also mixtures or combinations hereof.
A barium titanate semiconductor ceramic comprising, as its main constituent, a perovskite-type compound containing Ba, Ca, Sr, and Ti, and further comprising R (R represents at least one selected from Y, La, Ce, Pr, Nd, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb, and Lu), Mn, and Si as a sintering aid, wherein Pb is not contained except in a case of containing Pb as an impurity, wherein when the barium titanate semiconductor ceramic is dissolved, the Ca content x in parts by mol, the Sr content y in parts by mol, and the Mn content z in parts by mol in a case of Ti regarded as 100 parts by mol respectively meet: 20 ≤ x ≤ 25; 19 ≤ y ≤ 25; and 0.01 ≤ z ≤ 0.03, and meet: y ≥ -0.8x + 37 in a case of 0.01 ≤ z<0.019; and y ≤ -x + 48 in a case of 0.021 < z ≤ 0.03, wherein the resistivity of the barium titanate semiconductor at 25°C, ρ 25, meets ρ 25 ≤ 70 Ω·cm, a temperature TR100 at which the resistivity of the barium titanate semiconductor grows to 100 times the resistivity ρ 25 meets TR100 ≤ 75°C, and a slope α 10-100 of the resistivity of the barium titanate semiconductor with respect to temperature in the case of growing from 10 times to 100 times the resistivity ρ 25 meets { (α 10-100) /log (ρ 25)} ≤ 10. 20 ≤ x ≤ 25; 19 ≤ y ≤ 25; and 0.01 ≤ z ≤ 0.03, and meet: y ≥ -0.8x + 37 in a case of 0.01 ≤ z<0.019; and y ≤ -x + 48 in a case of 0.021 < z ≤ 0.03, y ≥ -0.8x + 37 in a case of 0.01 ≤ z<0.019; and y ≤ -x + 48 in a case of 0.021 < z ≤ 0.03, the resistivity of the barium titanate semiconductor at 25°C, ρ 25, meets ρ 25 ≤ 70 Ω·cm, a temperature TR100 at which the resistivity of the barium titanate semiconductor grows to 100 times the resistivity ρ 25 meets TR100 ≤ 75°C, and a slope α 10-100 of the resistivity of the barium titanate semiconductor with respect to temperature in the case of growing from 10 times to 100 times the resistivity ρ 25 meets { (α 10-100) /log (ρ 25)} ≤ 10.
A battery module, comprising: two or more battery groups, wherein each battery group comprises two or more battery cells; a module frame, comprising end plates and side plates, wherein the end plates and the side plates enclose an accommodating cavity for fixing the battery groups; a middle plate, wherein the middle plate is disposed between two of the battery groups, and is provided with an accommodating groove inside, wherein the accommodating groove is recessed from a top to a bottom of the middle plate; and a cell management unit, disposed in the accommodating groove of the middle plate and connected to a sampling line of the battery cells to collect data of the battery cells, wherein the sampling line of the battery cells is connected to a top of the cell management unit; characterized in that the battery module further comprises a separator, wherein the separator is disposed at a top of the battery groups, and wherein the sampling line of the battery cells is a flexible circuit board, and disposed on an upper surface of the separator at the top of the battery groups. two or more battery groups, wherein each battery group comprises two or more battery cells; a module frame, comprising end plates and side plates, wherein the end plates and the side plates enclose an accommodating cavity for fixing the battery groups; a middle plate, wherein the middle plate is disposed between two of the battery groups, and is provided with an accommodating groove inside, wherein the accommodating groove is recessed from a top to a bottom of the middle plate; and a cell management unit, disposed in the accommodating groove of the middle plate and connected to a sampling line of the battery cells to collect data of the battery cells, wherein the sampling line of the battery cells is connected to a top of the cell management unit; characterized in that the battery module further comprises a separator, wherein the separator is disposed at a top of the battery groups, and wherein the sampling line of the battery cells is a flexible circuit board, and disposed on an upper surface of the separator at the top of the battery groups.
A seal assembly comprising: a rotating shaft; a seal segment situated on and reciprocatable with the rotating shaft, the seal segment having an axially facing seal surface terminating at a first inner radial extent (d step), wherein the seal segment is a gas turbine engine bearing seal; a seal housing situated adjacent the seal segment and around the rotating shaft, the seal housing comprising: a substrate terminating at a second inner radial extent (d shaft) inboard of the first inner radial extent (d step); and a coated surface deposited atop the substrate, abutting the axially facing seal surface and terminating at the second inner radial extent (d shaft); characterised in that the substrate has an annular notch at a corner adjacent the seal segment, the annular notch extending radially outward from the second inner radial extent (d shaft), inboard and axially forward of a corner chamfer; and in that the coated surface covers the annular notch and the corner chamfer. a rotating shaft; a seal segment situated on and reciprocatable with the rotating shaft, the seal segment having an axially facing seal surface terminating at a first inner radial extent (d step), wherein the seal segment is a gas turbine engine bearing seal; a seal housing situated adjacent the seal segment and around the rotating shaft, the seal housing comprising: a substrate terminating at a second inner radial extent (d shaft) inboard of the first inner radial extent (d step); and a coated surface deposited atop the substrate, abutting the axially facing seal surface and terminating at the second inner radial extent (d shaft); characterised in that the substrate has an annular notch at a corner adjacent the seal segment, the annular notch extending radially outward from the second inner radial extent (d shaft), inboard and axially forward of a corner chamfer; and in that the coated surface covers the annular notch and the corner chamfer. a substrate terminating at a second inner radial extent (d shaft) inboard of the first inner radial extent (d step); and a coated surface deposited atop the substrate, abutting the axially facing seal surface and terminating at the second inner radial extent (d shaft); characterised in that the substrate has an annular notch at a corner adjacent the seal segment, the annular notch extending radially outward from the second inner radial extent (d shaft), inboard and axially forward of a corner chamfer; and in that the coated surface covers the annular notch and the corner chamfer.
A stabilizer material for superconductor used for a superconducting wire, the stabilizer material for superconductor comprising a copper material, wherein the copper material contains one kind or two kinds or more of additive elements selected from Ca, La, and Ce for a total amount of 3 ppm by mass or more and 400 ppm by mass or less, with the remainder being Cu and unavoidable impurities, the total concentration of the unavoidable impurities other than O, H, C, N, and S, which are gas components, is 5 ppm by mass or more and 100 ppm by mass or less, the total concentration of the unavoidable impurities including O, H, C, N and S, which are the gas components, is 20 ppm by mass or more and 110 ppm by mass or less, the concentration of O is 20 ppm by mass or less, the total amount of S, Se and Te which are included in the unavoidable impurities is more than 0 ppm by mass and 25 ppm by mass or less, a ratio Y/X of the total amount of one kind or two kinds or more of the additive elements selected from Ca, La, and Ce (Y ppm by mass) to the total amount of S, Se, and Te (X ppm by mass) is in the range of 0.5≤Y/X≤100, and compounds including one kind or two kinds or more selected from CaS, CaSO 4, LaS, La 2 SO 2, CeS, and Ce 2 SO 2, wherein a part of S may be substituted with Te or Se, are present in the matrix. wherein the copper material contains one kind or two kinds or more of additive elements selected from Ca, La, and Ce for a total amount of 3 ppm by mass or more and 400 ppm by mass or less, with the remainder being Cu and unavoidable impurities, the total concentration of the unavoidable impurities other than O, H, C, N, and S, which are gas components, is 5 ppm by mass or more and 100 ppm by mass or less, the total concentration of the unavoidable impurities including O, H, C, N and S, which are the gas components, is 20 ppm by mass or more and 110 ppm by mass or less, the concentration of O is 20 ppm by mass or less, the total amount of S, Se and Te which are included in the unavoidable impurities is more than 0 ppm by mass and 25 ppm by mass or less, a ratio Y/X of the total amount of one kind or two kinds or more of the additive elements selected from Ca, La, and Ce (Y ppm by mass) to the total amount of S, Se, and Te (X ppm by mass) is in the range of 0.5≤Y/X≤100, and compounds including one kind or two kinds or more selected from CaS, CaSO 4, LaS, La 2 SO 2, CeS, and Ce 2 SO 2, wherein a part of S may be substituted with Te or Se, are present in the matrix.
A method of calibrating light output of a plurality of LEDs, comprising: determining a distance value for each of a plurality of distance sensors, each of said distance sensors associated with at least one LED of a plurality of LEDs; grouping each of a plurality of said distance values into one of at least a first distribution and a second distribution, said distance values of said first distribution indicative of larger distances than said distance values of said second distribution; setting light output characteristics of a first LED group of said LEDs in accordance with floor lighting characteristics, based on said first LED group being associated with said distance sensors having said distance values in said first distribution; and setting light output characteristics of a second LED group of said LEDs in accordance with workplace lighting characteristics, based on said second LED group being associated with said distance sensors having said distance values in said second distribution. determining a distance value for each of a plurality of distance sensors, each of said distance sensors associated with at least one LED of a plurality of LEDs; grouping each of a plurality of said distance values into one of at least a first distribution and a second distribution, said distance values of said first distribution indicative of larger distances than said distance values of said second distribution; setting light output characteristics of a first LED group of said LEDs in accordance with floor lighting characteristics, based on said first LED group being associated with said distance sensors having said distance values in said first distribution; and setting light output characteristics of a second LED group of said LEDs in accordance with workplace lighting characteristics, based on said second LED group being associated with said distance sensors having said distance values in said second distribution.
A printing device for printing on an object, the printing device comprising: a base part (6, 6A, 6B) which has an opening on a side and has a plurality of engaging parts disposed side by side in an up-down direction; a support member for supporting the object, wherein the support member is slidably engaged with any engaging part among the plurality of engaging parts in a lateral direction from the side of the opening and is slidable through the opening between a pull-out position pulled out from the base part (6, 6A, 6B) and a storage position stored in the base part (6, 6A, 6B); and a head part which is disposed above the support member located at the storage position and ejects ink toward the object supported by the support member. a base part (6, 6A, 6B) which has an opening on a side and has a plurality of engaging parts disposed side by side in an up-down direction; a support member for supporting the object, wherein the support member is slidably engaged with any engaging part among the plurality of engaging parts in a lateral direction from the side of the opening and is slidable through the opening between a pull-out position pulled out from the base part (6, 6A, 6B) and a storage position stored in the base part (6, 6A, 6B); and a head part which is disposed above the support member located at the storage position and ejects ink toward the object supported by the support member.
A plate fin heat exchanger configured to perform heat exchange between plural fluids, comprising: a heat exchange part main body including layers of flow passages (30a, 30b) for carrying each of the plural fluids (F1, F2) arranged with partition walls each of which is arranged between each of two adjacent said flow passages (30a, 30b) respectively; heat transfer members each of which is disposed within each of said flow passages (30a, 30b) of said heat exchange part main body respectively, each of said heat transfer member connecting said partition walls opposed across each of said flow passages (30a, 30b) to transfer the heat of the fluid (F1, F2) flowing in each of said flow passages (30a, 30b) to said opposed partition walls; sensing parts connected to both outer sides of said heat exchange part main body in the arrangement direction of said flow passages (30a, 30b) respectively, characterized in that each of said sensing parts includes a plurality of sealed spaces arranged in the arrangement direction of said flow passages (30a, 30b), and a sensor wall disposed to separate an outermost sealed space of said plural sealed spaces from a sealed space on the inner side of said outermost sealed space; and a detection means for detecting damage of said sensor wall. a heat exchange part main body including layers of flow passages (30a, 30b) for carrying each of the plural fluids (F1, F2) arranged with partition walls each of which is arranged between each of two adjacent said flow passages (30a, 30b) respectively; heat transfer members each of which is disposed within each of said flow passages (30a, 30b) of said heat exchange part main body respectively, each of said heat transfer member connecting said partition walls opposed across each of said flow passages (30a, 30b) to transfer the heat of the fluid (F1, F2) flowing in each of said flow passages (30a, 30b) to said opposed partition walls; sensing parts connected to both outer sides of said heat exchange part main body in the arrangement direction of said flow passages (30a, 30b) respectively, characterized in that each of said sensing parts includes a plurality of sealed spaces arranged in the arrangement direction of said flow passages (30a, 30b), and a sensor wall disposed to separate an outermost sealed space of said plural sealed spaces from a sealed space on the inner side of said outermost sealed space; and a detection means for detecting damage of said sensor wall.
An emergency power supply apparatus comprising: a switch unit; a plurality of load bars (208, 209) adapted to convey power to a load, each of the plurality of load bars (208, 209) adapted to be connectable in parallel to a primary power source via the switch unit, which is adapted to selectively connect one or more of the plurality of load bars (208, 209) to the primary power source; a DC bus arranged to receive DC power from a secondary power source (218, 224); a plurality of power conversion modules (212, 214), each power conversion module (212, 214) adapted to be connectable between the DC bus and each of the load bars (208, 209) and when active being selectively configurable in use either: in a rectifier mode, in which the power conversion module (212, 214) is connected to one of the load bars (208, 209) to transfer power therefrom to the DC bus; or in an inverter mode, in which the power conversion module (212, 214) is connected to one of the load bars (208, 209) to transfer power thereto from the DC bus; and a controller, in communication with the plurality of power conversion modules (212, 214), and adapted to set a power transfer direction between each load bar (208, 209) and the DC bus thereby to control an operational state for each load bar (208, 209). a switch unit; a plurality of load bars (208, 209) adapted to convey power to a load, each of the plurality of load bars (208, 209) adapted to be connectable in parallel to a primary power source via the switch unit, which is adapted to selectively connect one or more of the plurality of load bars (208, 209) to the primary power source; a DC bus arranged to receive DC power from a secondary power source (218, 224); a plurality of power conversion modules (212, 214), each power conversion module (212, 214) adapted to be connectable between the DC bus and each of the load bars (208, 209) and when active being selectively configurable in use either: in a rectifier mode, in which the power conversion module (212, 214) is connected to one of the load bars (208, 209) to transfer power therefrom to the DC bus; or in an inverter mode, in which the power conversion module (212, 214) is connected to one of the load bars (208, 209) to transfer power thereto from the DC bus; in a rectifier mode, in which the power conversion module (212, 214) is connected to one of the load bars (208, 209) to transfer power therefrom to the DC bus; or in an inverter mode, in which the power conversion module (212, 214) is connected to one of the load bars (208, 209) to transfer power thereto from the DC bus; and a controller, in communication with the plurality of power conversion modules (212, 214), and adapted to set a power transfer direction between each load bar (208, 209) and the DC bus thereby to control an operational state for each load bar (208, 209).
A system comprising: a passenger area of a vehicle, wherein the vehicle is an aircraft; an air distribution system arranged in fluid communication with the passenger area; a fluid movable through the air distribution system to the passenger area, the fluid having a cleaning agent entrained therein; characterized by: a support system comprising ground support equipment configured to be located remotely from the aircraft, wherein the ground support equipment is configured to connect to the aircraft when the aircraft is parked, and wherein the ground support equipment is operable to provide power and conditioned air to the aircraft; and wherein a cleaning source is integrated into the ground support equipment such that the conditioned air provided to the aircraft from the ground support equipment has the cleaning agent entrained therein. a passenger area of a vehicle, wherein the vehicle is an aircraft; an air distribution system arranged in fluid communication with the passenger area; a fluid movable through the air distribution system to the passenger area, the fluid having a cleaning agent entrained therein; characterized by: a support system comprising ground support equipment configured to be located remotely from the aircraft, wherein the ground support equipment is configured to connect to the aircraft when the aircraft is parked, and wherein the ground support equipment is operable to provide power and conditioned air to the aircraft; and wherein a cleaning source is integrated into the ground support equipment such that the conditioned air provided to the aircraft from the ground support equipment has the cleaning agent entrained therein. a support system comprising ground support equipment configured to be located remotely from the aircraft, wherein the ground support equipment is configured to connect to the aircraft when the aircraft is parked, and wherein the ground support equipment is operable to provide power and conditioned air to the aircraft; and wherein a cleaning source is integrated into the ground support equipment such that the conditioned air provided to the aircraft from the ground support equipment has the cleaning agent entrained therein.