mhurhangee/patent-ind-claim-en huggingface dataset:
A method performed by a user equipment comprising, in Time Division Duplex, TDD: receiving a block of complex-valued symbols for narrowband physical broadcast channel, NPBCH, in subframe 9 during 64 consecutive radio frames; receiving a narrowband primary synchronization signal, NPSS; and receiving a narrowband secondary synchronization signal, NSSS, wherein the NPSS is mapped to resource elements in subframe 5 in every radio frame; and the NSSS is mapped to resource elements in subframe 0 in even radio frames, wherein the resource mapping of the NSSS and the NPBCH in the radio frames is exchanged compared to resource mapping of a NSSS and a NPBCH in the radio frames for Frequency Division Duplex, FDD, and in FDD, the NSSS is mapped to resource elements in subframe 9 in even radio frames, and the NPBCH is mapped to subframe 0 during 64 consecutive radio frames. receiving a block of complex-valued symbols for narrowband physical broadcast channel, NPBCH, in subframe 9 during 64 consecutive radio frames; receiving a narrowband primary synchronization signal, NPSS; and receiving a narrowband secondary synchronization signal, NSSS, wherein the NPSS is mapped to resource elements in subframe 5 in every radio frame; and the NSSS is mapped to resource elements in subframe 0 in even radio frames, wherein the resource mapping of the NSSS and the NPBCH in the radio frames is exchanged compared to resource mapping of a NSSS and a NPBCH in the radio frames for Frequency Division Duplex, FDD, and in FDD, the NSSS is mapped to resource elements in subframe 9 in even radio frames, and the NPBCH is mapped to subframe 0 during 64 consecutive radio frames.
Process for manufacturing a turbine part for aeronautics, comprising : - a substrate made of single-crystal nickel-based superalloy, comprising chromium and at least one element chosen from rhenium and ruthenium, having a γ-γ' phase, an average mass fraction of rhenium and ruthenium greater than or equal to 4% and an average mass fraction of chromium less than or equal to 5% and preferably less than or equal to 3%, - an underlayer covering at least part of a surface of the substrate , the sublayer having a γ-γ' phase and an average atomic fraction: - of chromium of between 5% and 10%, - of aluminium of between 10% and 20%, - of platinum of between 15% and 25%, this process comprising at least the steps of : a) deposition of an enrichment layer on the substrate , the enrichment layer having at least an average platinum atomic fraction of more than 90% and an average chromium atomic fraction of between 3% and 10%, b) heat treatment of the assembly formed by the substrate and the enrichment layer , at a temperature of between 1000°C and 1200°C, for more than one hour, preferably for more than 2 hours, so that the enrichment layer diffuses at least partially into the substrate . - an underlayer covering at least part of a surface of the substrate , the sublayer having a γ-γ' phase and an average atomic fraction: - of chromium of between 5% and 10%, - of aluminium of between 10% and 20%, - of platinum of between 15% and 25%, - of chromium of between 5% and 10%, - of aluminium of between 10% and 20%, - of platinum of between 15% and 25%, this process comprising at least the steps of : a) deposition of an enrichment layer on the substrate , the enrichment layer having at least an average platinum atomic fraction of more than 90% and an average chromium atomic fraction of between 3% and 10%, b) heat treatment of the assembly formed by the substrate and the enrichment layer , at a temperature of between 1000°C and 1200°C, for more than one hour, preferably for more than 2 hours, so that the enrichment layer diffuses at least partially into the substrate . a) deposition of an enrichment layer on the substrate , the enrichment layer having at least an average platinum atomic fraction of more than 90% and an average chromium atomic fraction of between 3% and 10%, b) heat treatment of the assembly formed by the substrate and the enrichment layer , at a temperature of between 1000°C and 1200°C, for more than one hour, preferably for more than 2 hours, so that the enrichment layer diffuses at least partially into the substrate .
A moisture barrier coated paper material, comprising: a base substrate comprising a paper-based substrate; a first polymer coating , a second polymer coating , a third polymer coating , and a hydraulic encapsulation layer of microencapsulated humectants formed by a semi-liquid microencapsulation process between the first polymer coating and the second polymer coating or between the second polymer coating and the third polymer coating , the first polymer coating , the second polymer coating , and the third polymer coating providing a barrier for moisture and air exchange through the paper material, the first polymer coating , the second polymer coating , and the third polymer coating providing heat and pressure sealability capabilities to the paper material, wherein each of the first polymer coating , the second polymer coating , and the third polymer coatings are mineral composite extrudates that include a polymer base with embedded minerals. a base substrate comprising a paper-based substrate; a first polymer coating , a second polymer coating , a third polymer coating , and a hydraulic encapsulation layer of microencapsulated humectants formed by a semi-liquid microencapsulation process between the first polymer coating and the second polymer coating or between the second polymer coating and the third polymer coating , the first polymer coating , the second polymer coating , and the third polymer coating providing a barrier for moisture and air exchange through the paper material, the first polymer coating , the second polymer coating , and the third polymer coating providing heat and pressure sealability capabilities to the paper material, wherein each of the first polymer coating , the second polymer coating , and the third polymer coatings are mineral composite extrudates that include a polymer base with embedded minerals.
A vehicle comprising a seat, the seat comprising: a seat base portion ; a seat back portion rotatable with respect to the seat base portion between a first position, in which the seat back portion is substantially upright, and a second position, in which a back surface of the seat back portion is substantially horizontal, and a projecting portion extending from an edge of the seat back portion that is at a lower end of the seat back portion when in the first position, the projecting portion having a surface that is contiguous with the back surface of the seat back portion , wherein the projecting portion is configured to rotate with the seat back portion such that in the second position the projecting portion extends rearwards of the seat base portion and the back surface of the seat back portion and the surface of the projecting portion together form a table surface , wherein the seat further comprises at least one selectively extending portion , the extending portion being configured to further extend the table surface , wherein the vehicle further comprises at least one further seat , the further seat being provided adjacent to the seat such that the seat and further seat are in a row, characterised in that the extending portion when deployed extends behind the further seat . a seat base portion ; a seat back portion rotatable with respect to the seat base portion between a first position, in which the seat back portion is substantially upright, and a second position, in which a back surface of the seat back portion is substantially horizontal, and a projecting portion extending from an edge of the seat back portion that is at a lower end of the seat back portion when in the first position, the projecting portion having a surface that is contiguous with the back surface of the seat back portion , wherein the projecting portion is configured to rotate with the seat back portion such that in the second position the projecting portion extends rearwards of the seat base portion and the back surface of the seat back portion and the surface of the projecting portion together form a table surface , wherein the seat further comprises at least one selectively extending portion , the extending portion being configured to further extend the table surface , wherein the vehicle further comprises at least one further seat , the further seat being provided adjacent to the seat such that the seat and further seat are in a row, characterised in that the extending portion when deployed extends behind the further seat .
A galleryless piston comprising: a body portion formed of steel, said body portion including an upper wall including an undercrown surface , said undercrown surface being exposed when viewed from an underside of said piston, said upper wall including an upper combustion surface opposite said undercrown surface, a ring belt depending from said upper wall and extending circumferentially around a central longitudinal axis of said piston, a pair of pin bosses depending from said upper wall, and a pair of skirt panels depending from said ring belt and coupled to said pin bosses, a thermal barrier layer applied to at least a portion of said upper combustion surface and/or at least a portion of said ring belt , said thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of said steel of said body portion, said thermal barrier layer includes a ceramic material, and the ceramic material of the thermal barrier layer includes ceria in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material, or ceria stabilized zirconia in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material, or a mixture of ceria stabilized zirconia and yttria stabilized zirconia in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material. a body portion formed of steel, said body portion including an upper wall including an undercrown surface , said undercrown surface being exposed when viewed from an underside of said piston, said upper wall including an upper combustion surface opposite said undercrown surface, a ring belt depending from said upper wall and extending circumferentially around a central longitudinal axis of said piston, a pair of pin bosses depending from said upper wall, and a pair of skirt panels depending from said ring belt and coupled to said pin bosses, a thermal barrier layer applied to at least a portion of said upper combustion surface and/or at least a portion of said ring belt , said thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of said steel of said body portion, said thermal barrier layer includes a ceramic material, and the ceramic material of the thermal barrier layer includes ceria in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material, or ceria stabilized zirconia in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material, or a mixture of ceria stabilized zirconia and yttria stabilized zirconia in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material.
A method of preparing wear and cut resistant UHMWPE fibers, comprising: the preparation of a mother liquor and a resin material, characterized in that the mother liquor is prepared by adding 0.1~5 parts of coupling agent A, 1~20 parts of nano additive B, 1~20 parts of additive C, 0.1~5 parts of sodium stearate, 0.1∼8 parts of nano dispersant, and 0.1~10 parts of antioxidant into 1000 parts of solvent oil, and processed by a 1000~20000r/min high-speed rotating emulsifier for 2-6 hours, and a mixing temperature being controlled at 25~100°C; and the resin material is an UHMWPE resin with a viscosity-average molecular weight of 2millions~8 millions, and 20~200 parts of the resin material are added into a ball grinder, and the temperature is controlled at 30~100°C, and then the mother liquor is added into the ball grinder at a speed of 2 parts/minute, and blended and mixed uniformly, and then the mixed solution is vacuumed in a sealed container for 2-6 hours, and then extruded by a twin screw extruder, a metering pump, a spin beam, and processed by drafting, and hot drawing and winding formation, wherein the additive C comprises one of a basalt staple fiber, a rockwool staple fiber, a slag cotton staple fiber, a glass staple fiber, an aluminum silicate cotton staple fiber, a polyester staple fiber, a carbon staple fiber, and an aramid staple fiber, or a combination thereof.
A composition comprising a refrigerant mixture consisting essentially of from 42 to 59 weight percent difluoromethane, 33 to 53 weight percent 2,3,3,3-tetrafluoropropene, and 1 to 9 weight percent carbon dioxide.
A thermal treatment process of a ferrous alloy sheet comprising the step of performing a thermal treatment on said sheet when running, by immersing it into at least one molten oxides bath , wherein said molten oxides bath has a viscosity lower than 3.10 -1 Pa.s, preferably lower than 2.10 -2 Pa.s, the surface of said bath being in contact with a non-oxidizing atmosphere, said molten oxides being inert towards iron, the difference (ΔT) between the temperature of said ferrous alloy sheet at the entry of the bath and the temperature of said bath being between 25°C and 900°C, and eliminating the residues of oxides remaining on the surfaces of said ferrous alloy sheet at the exit of said bath .
A method of manufacturing a moulded article comprising: a) providing a moulding material comprising a fibrous reinforcement material, a first resin material and a second resin material , the first resin material being at least partially cured; followed by b) providing the moulding material in relation to a mould to form a moulding; and c) in-mould processing the moulding to form the moulded article by heating to a cure temperature and maintaining the moulding at a dwell temperature in a dwell stage, characterised in that the dwell temperature is higher than the dwell temperature required for manufacturing the moulded article from a moulding comprising the same first and second resin material in which the first resin material is uncured, the dwell stage is shorter than the dwell stage required for manufacturing the moulded article from a moulding comprising the same first and second resin material in which the first resin material is uncured, and the energy input for processing the moulding to form the moulded article is less than the energy input required for manufacturing the moulded article from a moulding comprising the same first and second resin material in which the first resin material is uncured. a) providing a moulding material comprising a fibrous reinforcement material, a first resin material and a second resin material , the first resin material being at least partially cured; followed by b) providing the moulding material in relation to a mould to form a moulding; and c) in-mould processing the moulding to form the moulded article by heating to a cure temperature and maintaining the moulding at a dwell temperature in a dwell stage,
A fifth wheel plate for a fifth wheel coupling , the fifth wheel plate having an upper surface for receiving vertical forces and a recess for inserting a kingpin , the fifth wheel plate comprising a lightweight material, characterized in that the fifth wheel plate is made of a light metal in a casting process, wherein a reinforcement of a material having a higher strength than that of the light metal is cast into the fifth wheel plate .
Module for replacement of a sleeve to be slipped on a mandrel for a rotary printing press, comprising - a sleeve gripper - a mandrel gripper - a linear guide wherein, - in a replacement position a revolution axis of the sleeve coincides with a revolution axis of the mandrel defining an assembly axis ; and - the linear guide is engaged with at least one of the sleeve gripper and/or the mandrel gripper ; and - the linear guide is configured to translate the sleeve gripper and/or the mandrel gripper substantially along the assembly axis , wherein the orientation of the assembly axis is substantially perpendicular to a revolution axis of the sleeve in a printing mode and the sleeve gripper comprises a central stem for carrying the sleeve , a first clamp element , a second clamp element and a third clamp element , wherein at least one of the clamp elements is arranged to move toward the central stem up to a position where the sleeve is gripped by the first , second and third clamp element , whereby the revolution axis of the sleeve is in parallel to the axis of the stem . - a sleeve gripper - a mandrel gripper - a linear guide wherein, - in a replacement position a revolution axis of the sleeve coincides with a revolution axis of the mandrel defining an assembly axis ; and - the linear guide is engaged with at least one of the sleeve gripper and/or the mandrel gripper ; and - the linear guide is configured to translate the sleeve gripper and/or the mandrel gripper substantially along the assembly axis , wherein the orientation of the assembly axis is substantially perpendicular to a revolution axis of the sleeve in a printing mode and the sleeve gripper comprises a central stem for carrying the sleeve , a first clamp element , a second clamp element and a third clamp element , wherein at least one of the clamp elements is arranged to move toward the central stem up to a position where the sleeve is gripped by the first , second and third clamp element , whereby the revolution axis of the sleeve is in parallel to the axis of the stem .
A head-up display that is mounted on a vehicle , performs the projection on a transparent reflective member , and allows an observer (D) to visually recognize a virtual image (I), the head-up display comprising: a display device that displays an image ; and a projection optical system that has a refractive optical system , and projects the image displayed by the display device on an eye box of the observer (D), characterized in that <E> where an inner deflection angle (θ2i) is formed between a vector of a light beam incident on the refractive optical system and a vector of a light beam output from the refractive optical system on an reference inner side light beam (Li) that passes in a vicinity of an end of a vehicle inner side in a range from the display device to the refractive optical system and an outer deflection angle (θ2o) is formed between a vector of a light beam incident on the refractive optical system and a vector of a light beam output from the refractive optical system on an reference outer side light beam (Lo) that passes in a vicinity of an end of a vehicle outer side in the range from the display device to the refractive optical system . <E> = < the inner deflection angle (θ2i) is larger than the outer deflection angle (θ2o)> a display device that displays an image ; and a projection optical system that has a refractive optical system , and projects the image displayed by the display device on an eye box of the observer (D), characterized in that <E> where an inner deflection angle (θ2i) is formed between a vector of a light beam incident on the refractive optical system and a vector of a light beam output from the refractive optical system on an reference inner side light beam (Li) that passes in a vicinity of an end of a vehicle inner side in a range from the display device to the refractive optical system and an outer deflection angle (θ2o) is formed between a vector of a light beam incident on the refractive optical system and a vector of a light beam output from the refractive optical system on an reference outer side light beam (Lo) that passes in a vicinity of an end of a vehicle outer side in the range from the display device to the refractive optical system . <E> = < the inner deflection angle (θ2i) is larger than the outer deflection angle (θ2o)>
A burner module in an air stream comprising a feed pipe of substantially circular cross section and having an axis, fuel injection orifices situated on the pipe and intended to produce a flame, oxidant injection orifices and fins arranged symmetrically with espect to a plane P of flow of the fuel upstream of the burner module and laterally on the pipe on each side of the fuel injection orifices , at least two fuel injection orifices in a section of the pipe that have an axis that makes an angle α with the plane of flow P of the fuel, and fins making an angle β with the plane P of flow of the fuel, characterized in that the angle α is between 10° and 30° inclusive and in that the angle β is between 2α and 3α.
Granules consisting of natural, preferably purely plant-based ingredients comprising starch and plant-based natural fibers, characterized in that the granules have a solid composition consisting of Plant-based starch 75-90 wt% Natural fibers 1-10 wt% Thickener and/or gelling agent 0-10 wt% Optional additives 0-10 wt%, wherein the granules have a residual moisture content of 30-40%, preferably 35%.
Method for servicing a transformer, especially a transformer of a wind turbine, wherein a lifting device is used to lift a lid that closes a case of a transformer from the case to expose at least one electrical component of the transformer that is connected to the lid for exchanging or servicing the electrical component , wherein the lifting device comprises at least one fixed component that is fixed with respect to the case and at least one moveable component that is coupled to the lid , wherein the moveable component is moveable with respect to the fixed component by at least one actuator to lift the lid .