mhurhangee/ep-ind-claims huggingface dataset:
A method for transmitting a medium access control, MAC, protocol data unit, PDU, comprising: identifying, by a hybrid automatic repeat request, HARQ, entity, for an uplink grant, a HARQ process associated with the uplink grant; and obtaining, by the HARQ entity, a MAC PDU to transmit from a HARQ buffer of the identified HARQ process when a following condition is satisfied: a MAC entity of the HARQ entity is configured with priority based prioritization, the uplink grant is a configured grant, and a previous uplink grant for the HARQ process was de-prioritized and the MAC PDU had already been obtained for the HARQ process; the method further comprising: after obtaining the MAC PDU to transmit, delivering, by the HARQ entity, the MAC PDU and the uplink grant and HARQ information of a transport block, TB, to the identified HARQ process; and instructing, by the HARQ entity, the identified HARQ process to trigger a new transmission; wherein when the HARQ process is configured with a configured grant timer, the configured grant timer is not started or restarted when a following condition is satisfied: the MAC entity is configured with priority based prioritization, the uplink grant is a configured uplink grant and the uplink grant is a deprioritized uplink grant. identifying, by a hybrid automatic repeat request, HARQ, entity, for an uplink grant, a HARQ process associated with the uplink grant; and obtaining, by the HARQ entity, a MAC PDU to transmit from a HARQ buffer of the identified HARQ process when a following condition is satisfied: a MAC entity of the HARQ entity is configured with priority based prioritization, the uplink grant is a configured grant, and a previous uplink grant for the HARQ process was de-prioritized and the MAC PDU had already been obtained for the HARQ process; the method further comprising: after obtaining the MAC PDU to transmit, delivering, by the HARQ entity, the MAC PDU and the uplink grant and HARQ information of a transport block, TB, to the identified HARQ process; and instructing, by the HARQ entity, the identified HARQ process to trigger a new transmission; wherein when the HARQ process is configured with a configured grant timer, the configured grant timer is not started or restarted when a following condition is satisfied: the MAC entity is configured with priority based prioritization, the uplink grant is a configured uplink grant and the uplink grant is a deprioritized uplink grant. after obtaining the MAC PDU to transmit, delivering, by the HARQ entity, the MAC PDU and the uplink grant and HARQ information of a transport block, TB, to the identified HARQ process; and instructing, by the HARQ entity, the identified HARQ process to trigger a new transmission; wherein when the HARQ process is configured with a configured grant timer, the configured grant timer is not started or restarted when a following condition is satisfied: the MAC entity is configured with priority based prioritization, the uplink grant is a configured uplink grant and the uplink grant is a deprioritized uplink grant.
Optical fiber comprising a core and optionally a cladding, covering or coating surrounding said core, the core comprising at least one Bragg grating and at least one internal closed cavity, characterized in that said at least one Bragg grating is associated with said cavity so that the internal cavity will allow the grating to change its physical form by means of a pressure difference between the pressure inside the cavity and the pressure surrounding the fibre when the pressure surrounding the fibre changes, wherein the Bragg grating completely surrounds the cavity or wherein the Bragg grating has a longitudinal extension in the longitudinal direction of the core at least along the entire longitudinal extension of the internal closed cavity.
A method for identifying an extremum value, comprising: determining a location of an extremum value of a set of N data values stored as vectors in a memory array (130, 330), wherein each of the set of N data values is stored in memory cells coupled to a corresponding sense line, and the location of the extremum value is determined by: determining if the sensed data includes a target binary value by: transferring data stored in a group of memory cells coupled to a particular access line to an input/output (I/O) line (266, 366) in parallel; and determining that the sensed data includes a target binary value based on whether a level of the I/O line (266, 366) changes responsive to transferring the sense data in parallel such that a number of operations to determine the location of the extremum value remains constant with respect to a value of N; comparing, responsive to the sensed data including the target binary value, the data stored in the group of memory cells coupled to the particular access line to data stored in a group of the memory cells coupled to another access line, wherein the another access line corresponds to a lower index of the vectors than the particular access line; and repeating the determination and the comparison for each access line corresponding to a lower index of the vectors than the particular access line. determining if the sensed data includes a target binary value by: transferring data stored in a group of memory cells coupled to a particular access line to an input/output (I/O) line (266, 366) in parallel; and determining that the sensed data includes a target binary value based on whether a level of the I/O line (266, 366) changes responsive to transferring the sense data in parallel such that a number of operations to determine the location of the extremum value remains constant with respect to a value of N; transferring data stored in a group of memory cells coupled to a particular access line to an input/output (I/O) line (266, 366) in parallel; and determining that the sensed data includes a target binary value based on whether a level of the I/O line (266, 366) changes responsive to transferring the sense data in parallel such that a number of operations to determine the location of the extremum value remains constant with respect to a value of N; comparing, responsive to the sensed data including the target binary value, the data stored in the group of memory cells coupled to the particular access line to data stored in a group of the memory cells coupled to another access line, wherein the another access line corresponds to a lower index of the vectors than the particular access line; and repeating the determination and the comparison for each access line corresponding to a lower index of the vectors than the particular access line.
A flame retardant composition comprising: 10 to 90 weight percent of a linear polycarbonate; a branched polycarbonate; 10 to 70 weight percent of a polysiloxane-polycarbonate copolymer where the polysiloxane-polycarbonate copolymer comprises 10 weight percent or less of polysiloxane having a weight average molecular weight of less than 30,000 Daltons; and 1 to 20 weight percent of a phosphazene compound; where all weight percents are based on the total weight of the composition, and where the composition does not contain a flame retardant other than the phosphazene compound. 10 to 90 weight percent of a linear polycarbonate; a branched polycarbonate; 10 to 70 weight percent of a polysiloxane-polycarbonate copolymer where the polysiloxane-polycarbonate copolymer comprises 10 weight percent or less of polysiloxane having a weight average molecular weight of less than 30,000 Daltons; and 1 to 20 weight percent of a phosphazene compound; where all weight percents are based on the total weight of the composition, and where the composition does not contain a flame retardant other than the phosphazene compound.
A cam assembly (123, 124) for an archery bow, the cam assembly (123, 124) comprising: a cam body defining a pivot axis and a groove circumferentially routed at least partially around the pivot axis; and an anchoring lug for attaching a bow cord to the cam body, the anchoring lug being coupled with the cam body and comprising a force sensor, the anchoring lug being offset from the pivot axis, and the force sensor being configured to detect a tension on the bow cord. a cam body defining a pivot axis and a groove circumferentially routed at least partially around the pivot axis; and an anchoring lug for attaching a bow cord to the cam body, the anchoring lug being coupled with the cam body and comprising a force sensor, the anchoring lug being offset from the pivot axis, and the force sensor being configured to detect a tension on the bow cord.
A decoupler comprising: a drive member; a hub (32, 32a,); and an isolator that is configured to transmit rotary power between the drive member and the hub (32, 32a) in a predetermined rotational direction, the isolator comprising a wrap spring, a plurality of helical coil springs, and a carrier assembly (80, 80a), the wrap spring comprising a plurality of helical coils and a proximal end, the helical coil springs being disposed between the hub (32, 32a) and the carrier assembly (80, 80a), the carrier assembly (80, 80a) comprising a spring shell (402, 402a), the spring shell (402, 402a) having a toric inner surface into which the helical coil springs are received, characterized in that the carrier assembly (80, 80a) comprises a carrier plate (400, 400A), wherein the spring shell (402, 402a) being assembled to the carrier plate (400, 400a), wherein the carrier plate (400, 400a) having a plate member with a rim, whereby the plate member can comprise a first reaction block; and wherein a spring groove is provided in the plate member or the first reaction clock, wherein the rim abutting an axial end of the wrap spring, and wherein the proximal end of the wrap spring is received in the spring groove. a drive member; a hub (32, 32a,); and an isolator that is configured to transmit rotary power between the drive member and the hub (32, 32a) in a predetermined rotational direction, the isolator comprising a wrap spring, a plurality of helical coil springs, and a carrier assembly (80, 80a), the wrap spring comprising a plurality of helical coils and a proximal end, the helical coil springs being disposed between the hub (32, 32a) and the carrier assembly (80, 80a), the carrier assembly (80, 80a) comprising a spring shell (402, 402a), the spring shell (402, 402a) having a toric inner surface into which the helical coil springs are received, characterized in that the carrier assembly (80, 80a) comprises a carrier plate (400, 400A), wherein the spring shell (402, 402a) being assembled to the carrier plate (400, 400a), wherein the carrier plate (400, 400a) having a plate member with a rim, whereby the plate member can comprise a first reaction block; and wherein a spring groove is provided in the plate member or the first reaction clock, wherein the rim abutting an axial end of the wrap spring, and wherein the proximal end of the wrap spring is received in the spring groove.
A fabric softener active composition, comprising a) as component A at least 50 % by weight of a bis-(2-hydroxypropyl)-dimethylammonium methylsulphate fatty acid ester having a molar ratio of fatty acid moieties to amine moieties of from 1.5 to 1.99, an average chain length of the fatty acid moieties of from 16 to 18 carbon atoms and an iodine value of the fatty acid moieties, calculated for the free fatty acid, of from 0.5 to 50, and b) as component B a (2-hydroxypropyl)-(1-methyl-2-hydroxyethyl)-dimethylammonium methylsulphate fatty acid ester having the same fatty acid moieties as component A, wherein the molar ratio of component B to component A is from 0.05 to 0.20. a) as component A at least 50 % by weight of a bis-(2-hydroxypropyl)-dimethylammonium methylsulphate fatty acid ester having a molar ratio of fatty acid moieties to amine moieties of from 1.5 to 1.99, an average chain length of the fatty acid moieties of from 16 to 18 carbon atoms and an iodine value of the fatty acid moieties, calculated for the free fatty acid, of from 0.5 to 50, and b) as component B a (2-hydroxypropyl)-(1-methyl-2-hydroxyethyl)-dimethylammonium methylsulphate fatty acid ester having the same fatty acid moieties as component A,
A gas turbine engine fan case, comprising: a plurality of wound layers that form a laminate and have a nominal radial fan case thickness, where the laminate includes a plurality of discrete fan case radial locations comprising a discrete filler material (604; 702) sandwiched between radially adjacent layers of the plurality of wound layers to form a radial integral build up in comparison to the nominal radial fan case thickness, characterized in that the radial integral build up comprises a radially extending machined cavity into which is mounted a metallic insert with a threaded hole configured to receive attachment hardware. a plurality of wound layers that form a laminate and have a nominal radial fan case thickness, where the laminate includes a plurality of discrete fan case radial locations comprising a discrete filler material (604; 702) sandwiched between radially adjacent layers of the plurality of wound layers to form a radial integral build up in comparison to the nominal radial fan case thickness, characterized in that the radial integral build up comprises a radially extending machined cavity into which is mounted a metallic insert with a threaded hole configured to receive attachment hardware.
An unleaded aviation fuel composition having a MON of at least 99.6, sulfur content of less than 0.05wt%, a T10 of at most 75°C, T40 of at least 75° C, a T50 of at most 105° C, a T90 of at most 135°C, a final boiling point of less than 210°C, an adjusted heat of combustion of at least 43.5 MJ/kg, a vapor pressure in the range of 38 to 49 kPa, comprising: from 5 vol.% to 20 vol.% of toluene having a MON of at least 107; from 2 vol.% to 10 vol.% of toluidine; from 35 vol.% to 65 vol.% of at least one alkylate or alkylate blend having an initial boiling range of from 32°C to 60°C and a final boiling range of from 105°C to 140°C, having T40 of less than 99°C, T50 of less than 100°C, T90 of less than 110°C, the alkylate or alkylate blend comprising isoparaffins from 4 to 9 carbon atoms, 3-20 vol.% of C5 isoparaffins, 3-15 vol.% of C7 isoparaffins, and 60-90 vol.% of C8 isoparaffins, based on the alkylate or alkylate blend, and less than 1 vol.% of C10+, based on the alkylate or alkylate blend; from 5 vol.% to 20 vol.% of a diethyl carbonate with the proviso that the combined toluene and diethyl carbonate content is at least 20 vol.%; and from 8 vol.% to 26 vol.% of isopentane in an amount sufficient to reach a vapor pressure in the range of 38 to 49 kPa; wherein the fuel composition contains less than 1 vol.% of C8 aromatics and wherein the adjusted heat of combustion is calculated as follows: HOC * = HOC v / density + % range increase / % playload increase + 1 where HOC* is the adjusted Heat of Combustion (MJ/kg), HOC v is the volumetric energy density (MJ/L) obtained from actual Heat of Combustion measurement, density is the fuel density (g/L), % range increase is the percentage increase in aircraft range compared to 100 LL(HOC LL) calculated using HOC v and HOC LL for a fixed fuel volume, and % payload increase is the corresponding percentage increase in payload capacity due to the mass of the fuel. from 5 vol.% to 20 vol.% of toluene having a MON of at least 107; from 2 vol.% to 10 vol.% of toluidine; from 35 vol.% to 65 vol.% of at least one alkylate or alkylate blend having an initial boiling range of from 32°C to 60°C and a final boiling range of from 105°C to 140°C, having T40 of less than 99°C, T50 of less than 100°C, T90 of less than 110°C, the alkylate or alkylate blend comprising isoparaffins from 4 to 9 carbon atoms, 3-20 vol.% of C5 isoparaffins, 3-15 vol.% of C7 isoparaffins, and 60-90 vol.% of C8 isoparaffins, based on the alkylate or alkylate blend, and less than 1 vol.% of C10+, based on the alkylate or alkylate blend; from 5 vol.% to 20 vol.% of a diethyl carbonate with the proviso that the combined toluene and diethyl carbonate content is at least 20 vol.%; and from 8 vol.% to 26 vol.% of isopentane in an amount sufficient to reach a vapor pressure in the range of 38 to 49 kPa;
Optical diode comprising an optical waveguide for conducting light, preferably a light mode, having a vacuum wavelength λ 0, where the optical waveguide has a waveguide core (2, 3, 14) having a first refractive index n 1 and the waveguide core (2, 3, 14) is surrounded by at least one second optical medium, which has at least one second refractive index n 2, where n 1 > n 2, where the waveguide core (2, 3, 14) has, at least in segments, a smallest lateral dimension, which is a smallest dimension of a cross section perpendicular to a direction of propagation of the light in the waveguide core (2, 3, 14), where the smallest lateral dimension is greater than or equal to λ 0 /(5*n 1) and is less than or equal to 20*λ 0 /n 1, where the optical diode additionally comprises at least one absorber element (10, 11, 15, 16), which is disposed in a near field, where the near field consists of the electromagnetic field of the light of the vacuum wavelength λ 0 in the waveguide core (2, 3, 14) and outside of the waveguide core (2, 3, 14) up to a standard distance of 5*λ 0, where the standard distance is measured from a surface of the waveguide core (2, 3, 14) that forms an optical interface and in a direction perpendicular to the surface, characterized in that the at least one absorber element (10, 11, 15, 16) exhibits a differently strong absorption for the light having the vacuum wavelength λ 0 when it has left-circular polarization (σ -) on the one hand and when it has right-circular polarization (σ +) on the other.
A gas turbine engine comprising a secondary flow path and a primary flow path and a valve system intermediate the secondary flow path and the primary flow path, the valve system comprising: a valve seat; and a valve member rotatable relative to said valve seat between an open position and a closed position, said valve member defining a cylindrical surface which defines said closed position and a sculpted surface which defines said open position and intermediate positions; characterised in that said sculpted surface defines paired wave surfaces which twist from parallel surfaces at one end of said valve member to generally perpendicular or angularly acute surfaces at the opposite end of said valve member. a valve seat; and a valve member rotatable relative to said valve seat between an open position and a closed position, said valve member defining a cylindrical surface which defines said closed position and a sculpted surface which defines said open position and intermediate positions; characterised in that said sculpted surface defines paired wave surfaces which twist from parallel surfaces at one end of said valve member to generally perpendicular or angularly acute surfaces at the opposite end of said valve member.
Sound-absorbing textile composite comprising a) at least one open-pore carrier ply comprising coarse staple fibres having a linear density of 3 dtex to 12 dtex in a proportion of - 10% by weight to 90% by weight if the carrier ply does not contain any binder fibres, or in a proportion of - 10% by weight to 85% by weight if the carrier ply does contain binder fibres as further fibres, and fine staple fibres having a linear density of 0.5 dtex to 2.5 dtex as scaffold fibres in a proportion of - 10% by weight to 90% by weight if the carrier ply does not contain any binder fibres, or in a proportion of - 10% by weight to 80% by weight if the carrier ply does contain binder fibres as further fibres, and b) a microporous flow ply which is disposed on the carrier ply and comprises microfibres having a fibre diameter below 10 μm, where the flow resistance of the sound-absorbing textile composite is from 250 Ns/m 3 to 5000 Ns/m 3, especially from 250 Ns/m 3 to 2000 Ns/m 3, characterized in that the carrier ply has a volume ratio of air to fibre of 75:1 to 250:1. a) at least one open-pore carrier ply comprising coarse staple fibres having a linear density of 3 dtex to 12 dtex in a proportion of - 10% by weight to 90% by weight if the carrier ply does not contain any binder fibres, or in a proportion of - 10% by weight to 85% by weight if the carrier ply does contain binder fibres as further fibres, and fine staple fibres having a linear density of 0.5 dtex to 2.5 dtex as scaffold fibres in a proportion of - 10% by weight to 90% by weight if the carrier ply does not contain any binder fibres, or in a proportion of - 10% by weight to 80% by weight if the carrier ply does contain binder fibres as further fibres, and - 10% by weight to 90% by weight if the carrier ply does not contain any binder fibres, or in a proportion of - 10% by weight to 85% by weight if the carrier ply does contain binder fibres as further fibres, and - 10% by weight to 90% by weight if the carrier ply does not contain any binder fibres, or in a proportion of - 10% by weight to 80% by weight if the carrier ply does contain binder fibres as further fibres, and b) a microporous flow ply which is disposed on the carrier ply and comprises microfibres having a fibre diameter below 10 μm, where
Aircraft gas-turbine engine having a fan mounted on a fan shaft and including several fan blades, where the fan shaft is mounted on an engine structure by means of an upstream fan bearing, when seen in the flow direction, and a downstream bearing, where at least one predetermined breaking point is provided in the area of the upstream fan bearing, where at least one shock-absorbing element designed as metal fabric damper is arranged to have a parallel effect relative to the predetermined breaking point, characterized in that the shock-absorbing element is arranged at a radial gap, - where means for the supply of oil for cooling the shock-absorbing element are assigned to the shock-absorbing element, and - where the means for the supply of overflow oil from the fan bearing or of spray oil are provided. - where means for the supply of oil for cooling the shock-absorbing element are assigned to the shock-absorbing element, and - where the means for the supply of overflow oil from the fan bearing or of spray oil are provided.