mhurhangee/ep-ind-claims huggingface dataset:
A film (10, 11) comprising a first and second exterior layer (1, 2) and a third layer arranged between the first and second layer (1, 2), where the first, second, and third layer (1, 2, 3) is mutually independently respectively composed of a proportion of more than 30 % by weight, based on the total weight of the layer, of a first, second, and third copolyester (1A, 2A, 3A), and optionally of one or more other polymers and additives, wherein - the first copolyester is composed of diacid moieties and of diol moieties, at least 80 mol % of the diacid moieties are terephthalic acid moieties, and the diol moieties comprise from 70 to 90 mol % of ethylene glycol moieties and from 5 to 20 mol % of neopentyl glycol moieties; - the second copolyester is composed of diacid moieties and of diol moieties, at least 80 mol % of the diacid moieties are terephthalic acid moieties, and the diol moieties comprise from 70 to 90 mol % of ethylene glycol moieties and from 5 to 20 mol % of neopentyl glycol moieties; and - the third copolyester is composed of diacid moieties and of diol moieties, at least 80 mol % of the diacid moieties are terephthalic acid moieties, and the diol moieties comprise from 60 to 90 mol % of ethylene glycol moieties and from 10 to 35 mol % of 1,4-cyclohexanedimethanol moieties. - the first copolyester is composed of diacid moieties and of diol moieties, at least 80 mol % of the diacid moieties are terephthalic acid moieties, and the diol moieties comprise from 70 to 90 mol % of ethylene glycol moieties and from 5 to 20 mol % of neopentyl glycol moieties; - the second copolyester is composed of diacid moieties and of diol moieties, at least 80 mol % of the diacid moieties are terephthalic acid moieties, and the diol moieties comprise from 70 to 90 mol % of ethylene glycol moieties and from 5 to 20 mol % of neopentyl glycol moieties; and - the third copolyester is composed of diacid moieties and of diol moieties, at least 80 mol % of the diacid moieties are terephthalic acid moieties, and the diol moieties comprise from 60 to 90 mol % of ethylene glycol moieties and from 10 to 35 mol % of 1,4-cyclohexanedimethanol moieties.
A high yield ratio-type high strength steel sheet comprising: in weight%, 0.04 to 0.09% of C, 0.2% or less excluding 0% of Si, 2.0 to 3.5% of Mn, 0.3 to 1.2% of Cr, 0.03 to 0.08% of Ti, 0.01 to 0.05% of Nb, 0.0010 to 0.0050% of B, 0.01 to 0.10% of Sol.Al, 0.001 to 0.10% of P, 0.010% or less including 0% of S, 0.010% or less excluding 0% of N, a remainder of Fe and unavoidable impurities, the contents of Si, Cr and C satisfying the following relationship 1, Si + Cr / 2 C ≥ 5, where each component indicates a weight content; and as a microstructure, in an area fraction, 50% or more of bainite, 20 to 40% of tempered martensite, and residual ferrite, in which a hardness ratio of a bainite phase and a tempered martensite phase at a 1/4t point of a thickness of a steel sheet measured as detailed in the description, represented by the following relationship 2, is 1.3 or less, where t is the thickness of the steel sheet in millimeter, the tempered martensite has an average particle diameter of 2 μm or less, the bainite has an average particle diameter of 3 μm or less, measured as detailed in the description, HB / HTM ≤ 1.3, where HB is a bainite hardness, and HTM is a tempered martensite hardness. in weight%, 0.04 to 0.09% of C, 0.2% or less excluding 0% of Si, 2.0 to 3.5% of Mn, 0.3 to 1.2% of Cr, 0.03 to 0.08% of Ti, 0.01 to 0.05% of Nb, 0.0010 to 0.0050% of B, 0.01 to 0.10% of Sol.Al, 0.001 to 0.10% of P, 0.010% or less including 0% of S, 0.010% or less excluding 0% of N, a remainder of Fe and unavoidable impurities, the contents of Si, Cr and C satisfying the following relationship 1, Si + Cr / 2 C ≥ 5, where each component indicates a weight content; and as a microstructure, in an area fraction, 50% or more of bainite, 20 to 40% of tempered martensite, and residual ferrite, in which a hardness ratio of a bainite phase and a tempered martensite phase at a 1/4t point of a thickness of a steel sheet measured as detailed in the description, represented by the following relationship 2, is 1.3 or less, where t is the thickness of the steel sheet in millimeter, the tempered martensite has an average particle diameter of 2 μm or less, the bainite has an average particle diameter of 3 μm or less, measured as detailed in the description, HB / HTM ≤ 1.3, where HB is a bainite hardness, and HTM is a tempered martensite hardness.
Fluid filter having a fluid filter medium through which a fluid can flow, wherein the fluid filter medium comprises: - a fine filter medium, - a first coarse filter medium which is arranged parallel to the fine filter medium such that fluid can flow through it, wherein the coarse filter medium is incorporated into the fine filter medium and, under normal and high operating temperatures of the fluid in the fluid filter, the coarse filter medium is arranged in a region which is situated outside a main throughflow area of the fluid filter, wherein the fluid filter medium additionally comprises an ultrafine filter medium which is arranged parallel to the fine filter medium and to the coarse filter medium such that fluid can flow through it, with the result that a fluid flow of the fluid is subdivided by the fine filter medium, the coarse filter medium and the ultrafine filter medium, that the ultrafine filter medium is incorporated into the fine filter medium, characterized in that the fine filter medium used is a polyester needle felt which retains particles in a range from 5 μm to 50 μm, and the fine filter medium is a carrier material in which the coarse filter medium and the ultrafine filter medium are introduced, wherein the fine filter medium is cut out at points at which the coarse filter medium and the ultrafine filter medium are provided, with the result that no series connection of a fine filter medium with a coarse filter medium or an ultrafine filter medium is present. - a fine filter medium, - a first coarse filter medium which is arranged parallel to the fine filter medium such that fluid can flow through it, wherein the coarse filter medium is incorporated into the fine filter medium and, under normal and high operating temperatures of the fluid in the fluid filter, the coarse filter medium is arranged in a region which is situated outside a main throughflow area of the fluid filter,
A graphite article comprising graphitized polymer having a thickness of at least 100 microns and up to 500 microns, the graphite having a density of less than 1.00 g/cc, a compressibility of at least 3% at a contact pressure of 100 kPa and a generally sheet like shape, wherein the graphite article has a resistivity of less than 0.019 °C/W at a contact pressure of 200 kPa, as measured on an apparatus that meets the requirements of ASTM D5470 Standard Test Method.
An insulating glass including two or more glass sheets arranged to face each other via a spacer sandwiched between the glass sheets so as to form an air space layer between the glass sheets, the spacer being made from a thermoplastic resin composition having a JIS A hardness of 10 to 90 at 25 °C, the thermoplastic resin composition containing a butyl-type rubber, a crystalline polyolefin, a desiccant and an inorganic filler, characterized in that a percentage of the butyl-type rubber is 50 to 98% by weight, and a percentage of the crystalline polyolefin is 2 to 50% by weight with respect to a total amount of the butyl-type rubber and the crystalline polyolefin, a ratio of the inorganic filler is 200 parts by weight or less to a total of 100 parts by weight of the butyl-type rubber and the crystalline polyolefin, melt viscosity at 120 °C is not less than 0.6 kPa·s and not more than 7.0 kPa·s, and storage elastic modulus at 25 °C is not less than 15 MPa and not more than 60 MPa, wherein the butyl-type rubber contains a high molecular weight butyl-type rubber and a low molecular weight butyl-type rubber, a number average molecular weight of the high molecular weight butyl-type rubber is not less than 55000 and not more than 150000, and a number average molecular weight of the low molecular weight butyl-type rubber is not less than 35000 and not more than 50000. characterized in that a percentage of the butyl-type rubber is 50 to 98% by weight, and a percentage of the crystalline polyolefin is 2 to 50% by weight with respect to a total amount of the butyl-type rubber and the crystalline polyolefin, a ratio of the inorganic filler is 200 parts by weight or less to a total of 100 parts by weight of the butyl-type rubber and the crystalline polyolefin, melt viscosity at 120 °C is not less than 0.6 kPa·s and not more than 7.0 kPa·s, and storage elastic modulus at 25 °C is not less than 15 MPa and not more than 60 MPa, wherein the butyl-type rubber contains a high molecular weight butyl-type rubber and a low molecular weight butyl-type rubber, a number average molecular weight of the high molecular weight butyl-type rubber is not less than 55000 and not more than 150000, and a number average molecular weight of the low molecular weight butyl-type rubber is not less than 35000 and not more than 50000.
A method for tactile presentation of threat information to a pilot of an aircraft, the method comprising: tactually presenting the threat information to the pilot by controlling a plurality of tactors (212, 214, 216, 218, 220, 222) to produce one or more tactile stimuli based on situational awareness information, wherein tactors in the plurality of tactors are physically coupled to a pilot seat in the aircraft and the threat information is indicative of a threat to the aircraft, wherein tactually presenting the threat information to the pilot comprises tactually presenting information indicative of a location of the threat to the aircraft, and wherein controlling the plurality of tactors comprises controlling the plurality of tactors to produce the one or more tactile stimuli such that the one or more produced stimuli are indicative of the location of the threat. tactually presenting the threat information to the pilot by controlling a plurality of tactors (212, 214, 216, 218, 220, 222) to produce one or more tactile stimuli based on situational awareness information, wherein tactors in the plurality of tactors are physically coupled to a pilot seat in the aircraft and the threat information is indicative of a threat to the aircraft, wherein tactually presenting the threat information to the pilot comprises tactually presenting information indicative of a location of the threat to the aircraft, and wherein controlling the plurality of tactors comprises controlling the plurality of tactors to produce the one or more tactile stimuli such that the one or more produced stimuli are indicative of the location of the threat.
An induction heating type cooktop, comprising: a case (25, 1025); an upper plate (15, 1110, 1015) coupled to a top of the case (25, 1025) and configured to support a target heating object; a working coil disposed inside the case (25, 1025) and configured to heat the target heating object; a thin film (1120, 1200, 1220) disposed at a top surface of the upper plate (15, 1110, 1015) or a bottom surface of the upper plate (15, 1110, 1015); and an insulator (35, 1035) disposed between the bottom surface of the upper plate (15, 1110, 1015) and the working coil, wherein the thin film (1120, 1200,1300) comprises: a plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320) that are arranged about a central portion of the working coil, each of the plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320) defining a closed loop surrounding the central portion of the working coil, characterised by a heat conduction member (1120c, 1120d, 1124, 1330) that is arranged in a predetermined pattern and contacts at least one of the plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320). a case (25, 1025); an upper plate (15, 1110, 1015) coupled to a top of the case (25, 1025) and configured to support a target heating object; a working coil disposed inside the case (25, 1025) and configured to heat the target heating object; a thin film (1120, 1200, 1220) disposed at a top surface of the upper plate (15, 1110, 1015) or a bottom surface of the upper plate (15, 1110, 1015); and an insulator (35, 1035) disposed between the bottom surface of the upper plate (15, 1110, 1015) and the working coil, wherein the thin film (1120, 1200,1300) comprises: a plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320) that are arranged about a central portion of the working coil, each of the plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320) defining a closed loop surrounding the central portion of the working coil, characterised by a heat conduction member (1120c, 1120d, 1124, 1330) that is arranged in a predetermined pattern and contacts at least one of the plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320). a plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320) that are arranged about a central portion of the working coil, each of the plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320) defining a closed loop surrounding the central portion of the working coil, characterised by a heat conduction member (1120c, 1120d, 1124, 1330) that is arranged in a predetermined pattern and contacts at least one of the plurality of sub-thin films (1120a, 1120b, 1210, 1220, 1310, 1320).
An induction heating type cooktop comprising: a case; a cover plate coupled to a top of the case and having an upper plate that is configured to support a target object; a thin film (1020, 1420) disposed on at least one of a top of the upper plate or a bottom of the upper plate, characterised by a working coil (1050, 1450) provided in the case and configured to inductively heat the thin film (1020, 1420); a memory (1030, 1430) configured to store information on one or more correlations between a temperature of the thin film (1020, 1420) and a plurality of components of an equivalent circuit associated with the thin film (1020, 1420), the plurality of components including an inductor component and a resistor component; and a controller (1040, 1440) configured to operate the working coil (1050, 1450) and determine estimated temperature information corresponding to the inductor component and the resistor component of the equivalent circuit, wherein the controller (1040, 1440) is configured to determine an estimated temperature associated with the determined estimated temperature information as a current temperature of the thin film (1020, 1420) based on the information on the one or more correlations. a case; a cover plate coupled to a top of the case and having an upper plate that is configured to support a target object; a thin film (1020, 1420) disposed on at least one of a top of the upper plate or a bottom of the upper plate, characterised by a working coil (1050, 1450) provided in the case and configured to inductively heat the thin film (1020, 1420); a memory (1030, 1430) configured to store information on one or more correlations between a temperature of the thin film (1020, 1420) and a plurality of components of an equivalent circuit associated with the thin film (1020, 1420), the plurality of components including an inductor component and a resistor component; and a controller (1040, 1440) configured to operate the working coil (1050, 1450) and determine estimated temperature information corresponding to the inductor component and the resistor component of the equivalent circuit, wherein the controller (1040, 1440) is configured to determine an estimated temperature associated with the determined estimated temperature information as a current temperature of the thin film (1020, 1420) based on the information on the one or more correlations.
An electronic vapour provision system comprising first and second units which when connected define a longitudinal axis, wherein the first and second units are mechanically and electrically connectable via a bayonet fitting, the bayonet fitting providing co-axial and radial mechanical bias relative to the longitudinal axis; wherein the first unit is arranged to: receive insertion of the second unit along said longitudinal axis to a first engagement position of the bayonet fitting; and allow the second unit to rotate about the longitudinal axis from the first engagement position to a final engagement position that prevents both (i) relative movement of the first and second units along said longitudinal axis, and (ii) rotation of the second unit past the final engagement position further away from the first engagement position; characterized in that the first unit further includes in the bayonet fitting a biasing means that applies a rotational bias against rotation of the second unit from the final engagement position back to the first engagement position, wherein a transition point is located between the first engagement position and the final engagement position, and when the second unit is located between the first engagement position and the transition point, the biasing means applies a rotational bias in favour of rotation of the second unit in a rotational direction from the final engagement position towards the first engagement position, and when the second unit is located between the final engagement position and the transition point, the biasing means applies a rotational bias in favour of rotation of the second unit in a rotational direction from the first engagement position towards the final engagement position. receive insertion of the second unit along said longitudinal axis to a first engagement position of the bayonet fitting; and allow the second unit to rotate about the longitudinal axis from the first engagement position to a final engagement position that prevents both (i) relative movement of the first and second units along said longitudinal axis, and (ii) rotation of the second unit past the final engagement position further away from the first engagement position; characterized in that the first unit further includes in the bayonet fitting a biasing means that applies a rotational bias against rotation of the second unit from the final engagement position back to the first engagement position, wherein a transition point is located between the first engagement position and the final engagement position, and when the second unit is located between the first engagement position and the transition point, the biasing means applies a rotational bias in favour of rotation of the second unit in a rotational direction from the final engagement position towards the first engagement position, and when the second unit is located between the final engagement position and the transition point, the biasing means applies a rotational bias in favour of rotation of the second unit in a rotational direction from the first engagement position towards the final engagement position.
A nitride semiconductor light-emitting device, comprising: a first nitride semiconductor layer; an active layer formed on the first nitride semiconductor layer; a second nitride semiconductor layer formed on the active layer; and a third nitride semiconductor layer having Alln, which is formed on the second nitride semiconductor layer, wherein the first nitride semiconductor layer has a n-type nitride semiconductor layer; and wherein the second nitride semiconductor layer is p-type; characterized in that Alln of the third nitride semiconductor layer is n-AlIn. a first nitride semiconductor layer; an active layer formed on the first nitride semiconductor layer; a second nitride semiconductor layer formed on the active layer; and a third nitride semiconductor layer having Alln, which is formed on the second nitride semiconductor layer, wherein the first nitride semiconductor layer has a n-type nitride semiconductor layer; and wherein the second nitride semiconductor layer is p-type; characterized in that Alln of the third nitride semiconductor layer is n-AlIn.
Yankee dryer cylinder comprising: - a cylindrical shell made of steel having a first end and a second end opposite to said first end, said cylindrical shell having a longitudinal axis and being, furthermore, provided with a plurality of circumferential grooves; - a first head, or end wall, fixed to said first end of said cylindrical shell made of steel, said first head being made of cast iron; - a second head, or end wall, fixed to said second end of said cylindrical shell made of steel, also said second head being made of cast iron; - a hollow shaft mounted inside said cylindrical shell and connected to said first and a said second head (20,30) at a first and a second end (41,42), respectively; - a first bearing journal fixed to said hollow shaft at said first end; - a second bearing journal fixed to said hollow shaft at said second end; said Yankee dryer cylinder being characterised in that said cast iron in which said first and said second head (20,30) are made has the following composition by weight %: - C: between 3,0 and 3,5%; - Si: between 1,5 and 2,7%; - Mn: between 0,3 and 0,7%; - P: between 0,05 and 0,10%; - V: between 0,20 and 0,50%; - S: between 0,05 and 0,10%; - Mg: between 0,06 and 0,20%; - Cu: between 0,10 and 0,80%; - Cr: between 0,05 and 0,10%. - a cylindrical shell made of steel having a first end and a second end opposite to said first end, said cylindrical shell having a longitudinal axis and being, furthermore, provided with a plurality of circumferential grooves; - a first head, or end wall, fixed to said first end of said cylindrical shell made of steel, said first head being made of cast iron; - a second head, or end wall, fixed to said second end of said cylindrical shell made of steel, also said second head being made of cast iron; - a hollow shaft mounted inside said cylindrical shell and connected to said first and a said second head (20,30) at a first and a second end (41,42), respectively; - a first bearing journal fixed to said hollow shaft at said first end; - a second bearing journal fixed to said hollow shaft at said second end; - C: between 3,0 and 3,5%; - Si: between 1,5 and 2,7%; - Mn: between 0,3 and 0,7%; - P: between 0,05 and 0,10%; - V: between 0,20 and 0,50%; - S: between 0,05 and 0,10%; - Mg: between 0,06 and 0,20%; - Cu: between 0,10 and 0,80%; - Cr: between 0,05 and 0,10%.
A blade (11,12,13) for a turbine or, more generally a turbomachine, having at a top end a shroud segment (11-2, 12-2, 13-2) designed to engage with shroud segments (11-2, 12-2, 13-2) of adjacent blades (11,12,13) in an ring-shaped assembly with the shroud segment (11-2, 12-2, 13-2) having an indentation along an engaging face characterized in that the indentation is forming a capital H shape.