mhurhangee/patent-ind-claim-en huggingface dataset:
A method of enabling measurements for handling of a device-to-device, D2D, side link in a cellular system , the method being performed in a first D2D capable device and comprising: - providing , to a second D2D device , information relating to a first transmission power of a first transmission between the first D2D device and the second D2D device , wherein the first transmission power is used by the first D2D capable device , wherein the information relating to the first transmission power comprises an indication of a power change of the first transmission power of the first transmission, and - receiving , from the second D2D device , a measurement report based on the provided information relating to the first transmission power. - providing , to a second D2D device , information relating to a first transmission power of a first transmission between the first D2D device and the second D2D device , wherein the first transmission power is used by the first D2D capable device , wherein the information relating to the first transmission power comprises an indication of a power change of the first transmission power of the first transmission, and - receiving , from the second D2D device , a measurement report based on the provided information relating to the first transmission power.
A mutant strain of bacterial strain DD1 as deposited with DSMZ having the deposit number DSM 18541, having the ability to produce succinic acid from glycerol and wherein said mutant strain has a 16S rDNA of SEQ ID NO: 1; or a sequence, which shows a sequence homology of at least 99.9% to SEQ ID NO: 1.
A security sheet including an iridescent security mark observable on the surface of the sheet , characterized by the fact that said mark includes at least two zones , each presenting an iridescent effect, said zones being colored in normal observation with the naked eye and at least one of said zones including iridescent pigments that are practically colorless in normal observation and that present an iridescent effect that is visible only in oblique observation, each of said zones including firstly a dye, said dye being such that said zones have the same hue, and secondly iridescent pigments, said pigments presenting in oblique observation iridescent effects that differ from one zone to the other.
A base component, comprising: a base and an overflow cover , wherein the base has a side plate and an upper surface, the side plate has a mounting surface perpendicular to the upper surface, the overflow cover includes an overflow cover body , the overflow cover body is provided with an overflow port and a mounting portion , and the overflow cover body has an overflow chamber , the base has an overflow hole and a connection portion engaged with the mounting portion for fixing, the overflow hole and the connection portion are both provided on the mounting surface, and the overflow port and the overflow hole are both in communication with the overflow chamber to form an overflow channel between the overflow cover body and the base, characterized in that one side of the overflow cover, adjacent to the upper surface of the base, is arranged with a water inlet plate communicating with the overflow port, and the water inlet plate is provided with a plurality of filter holes , wherein the water inlet plate is arranged obliquely to the upper surface.
Use of a phytase variant in animal feed to enhance phosphate digestion; wherein said phytase variant has improved thermal activity of at least about 5°C as compared to wild type Buttiauxella sp. phytase (SEQ ID NO: 1); further wherein said phytase variant shares at least 80% sequence identity with SEQ ID NO: 1, further wherein said phytase variant comprises a phytase that contains a substitution at one, two or three positions selected from the group consisting of S75, Q76 and A374; at one or more positions selected from the group consisting of A89, D92, T134, F164, T176, A178, K207, A209, S248, Q256, A261 and/or N270; and at one or more positions selected from the group consisting of: N37, G77, H160, F164, T171, S188, G192, K198, A235, Q256 and/or P367, wherein each position corresponds to the amino acid sequence of SEQ ID NO: 1.
A vehicle control method, comprising: step 1, acquiring (S10) position information of a vehicle in real time to determine a current position of the vehicle; step 2, acquiring (S20) data of first road anomalies within a first predetermined range of the current position from a local road anomalies database of the vehicle; step 3, screening (S30) the data of the first road anomalies to obtain data of second road anomalies within a second predetermined range of the current position, wherein the first predetermined range is larger than the second predetermined range; and step 4, controlling (S40) the vehicle to perform road anomalies processing based on the obtained data of the second road anomalies; characterised in that : said step 2 comprises acquiring (S201) the data of the first road anomalies at first predetermined time intervals based on the position information. step 1, acquiring (S10) position information of a vehicle in real time to determine a current position of the vehicle; step 2, acquiring (S20) data of first road anomalies within a first predetermined range of the current position from a local road anomalies database of the vehicle; step 3, screening (S30) the data of the first road anomalies to obtain data of second road anomalies within a second predetermined range of the current position, wherein the first predetermined range is larger than the second predetermined range; and step 4, controlling (S40) the vehicle to perform road anomalies processing based on the obtained data of the second road anomalies; characterised in that : said step 2 comprises acquiring (S201) the data of the first road anomalies at first predetermined time intervals based on the position information.
A spacecraft servicing system , comprising: a spacecraft servicing device ; and characterized by a plurality of pods comprising at least one spacecraft servicing component , the plurality of pods carried by the spacecraft servicing device , wherein the spacecraft servicing device is configured to transfer at least one pod of the plurality of pods to a target spacecraft using propulsion of the spacecraft servicing device while any maneuvering devices on the at least one pod are not utilized, in order to service the target spacecraft with the at least one spacecraft servicing component of the at least one pod to provide one or more life-extending services to the target spacecraft , wherein the spacecraft servicing device is configured to remain in at least partial physical contact with the at least one pod until the at least one pod is secured to the target spacecraft , and wherein the spacecraft servicing device is configured to cease physical contact with the at least one pod after the at least one pod is secured to the target spacecraft , wherein the at least one spacecraft servicing component of the at least one pod comprises a thruster assembly configured to alter at least one of an orbit or a velocity of the target spacecraft . a spacecraft servicing device ; and characterized by a plurality of pods comprising at least one spacecraft servicing component , the plurality of pods carried by the spacecraft servicing device , wherein the spacecraft servicing device is configured to transfer at least one pod of the plurality of pods to a target spacecraft using propulsion of the spacecraft servicing device while any maneuvering devices on the at least one pod are not utilized, in order to service the target spacecraft with the at least one spacecraft servicing component of the at least one pod to provide one or more life-extending services to the target spacecraft , wherein the spacecraft servicing device is configured to remain in at least partial physical contact with the at least one pod until the at least one pod is secured to the target spacecraft , and wherein the spacecraft servicing device is configured to cease physical contact with the at least one pod after the at least one pod is secured to the target spacecraft , wherein the at least one spacecraft servicing component of the at least one pod comprises a thruster assembly configured to alter at least one of an orbit or a velocity of the target spacecraft .
A method of entropy coding for source symbols in an encoder comprising: receiving a current source symbol, determining a prefix part and any suffix part for the current symbol, deriving a first binary string by binarizing a first prefix part related to the prefix part using a first variable length code, if a test value related to the prefix part is greater than or equal to a threshold , otherwise deriving a second binary string by binarizing a second prefix part related to the prefix part using a second variable length code or a first fixed-length code; deriving a third binary string by binarizing the suffix part using a second fixed-length code or a first truncated binary code if any suffix exists; encoding a syntax structure, comprising at least one flag, indicating whether the first prefix part or the second prefix part is to be used for reconstruction during decoding; and encoding exclusively either the first binary string or the second binary string using context-adaptive binary arithmetic coding, CABAC, mode in accordance with the indication of the syntax structure. receiving a current source symbol, determining a prefix part and any suffix part for the current symbol, deriving a first binary string by binarizing a first prefix part related to the prefix part using a first variable length code, if a test value related to the prefix part is greater than or equal to a threshold , otherwise deriving a second binary string by binarizing a second prefix part related to the prefix part using a second variable length code or a first fixed-length code; deriving a third binary string by binarizing the suffix part using a second fixed-length code or a first truncated binary code if any suffix exists; encoding a syntax structure, comprising at least one flag, indicating whether the first prefix part or the second prefix part is to be used for reconstruction during decoding; and encoding exclusively either the first binary string or the second binary string using context-adaptive binary arithmetic coding, CABAC, mode in accordance with the indication of the syntax structure.
A packaging machine for producing packages of a pourable product from a web of packaging material advancing along a web advancement path (P), the packaging machine comprises: - a conveying device for advancing the web of packaging material along the web advancement path (P) to a tube forming station at which the web of packaging material is formed, in use, into a tube and for advancing the tube along a tube advancement path (Q); - an isolation housing having a main chamber and an auxiliary chamber arranged downstream form the main chamber along the tube advancement path (Q) ; - a tube forming and sealing device at least partially arranged within the main chamber and being configured to form and longitudinally seal the tube , in use, within the main chamber , the tube having a longitudinal seal portion ; - a filling device for filling the tube with the pourable product; - a pressure control device configured to control a first pressure (p1) within the main chamber and a second pressure (p2) within the auxiliary chamber , the second pressure (p2) being different from the first pressure (p1); - a pressure measuring device configured to measure a pressure difference (Δp) between the first pressure (p1) and the second pressure (p2); and - an analysis unit operatively connected to the pressure measuring device and configured to monitor a time-dependent course of the pressure difference (Δp); wherein the analysis unit is configured to determine a collapse of the longitudinal seal portion in dependence of the time-dependent course of the pressure difference (Δp). - a conveying device for advancing the web of packaging material along the web advancement path (P) to a tube forming station at which the web of packaging material is formed, in use, into a tube and for advancing the tube along a tube advancement path (Q); - an isolation housing having a main chamber and an auxiliary chamber arranged downstream form the main chamber along the tube advancement path (Q) ; - a tube forming and sealing device at least partially arranged within the main chamber and being configured to form and longitudinally seal the tube , in use, within the main chamber , the tube having a longitudinal seal portion ; - a filling device for filling the tube with the pourable product; - a pressure control device configured to control a first pressure (p1) within the main chamber and a second pressure (p2) within the auxiliary chamber , the second pressure (p2) being different from the first pressure (p1); - a pressure measuring device configured to measure a pressure difference (Δp) between the first pressure (p1) and the second pressure (p2); and - an analysis unit operatively connected to the pressure measuring device and configured to monitor a time-dependent course of the pressure difference (Δp);
A locking joint device, comprising: a center body connector having an interior surface forming a cavity extending axially therethrough, wherein the center body connector includes a center flange extending radially inwardly from the center body connector interior surface ; at least one retaining cap having an inner surface forming a retaining cap opening extending axially therethrough, wherein the retaining cap has a body with an axially inner portion having a notch and a ledge formed therein, and wherein the ledge is adapted to slidingly engage the interior surface of the center body connector ; and a first packing arrangement secured between the axially inner portion of the at least one retaining cap and the body connector interior surface , wherein the first packing arrangement includes a shoe gland having an outer sloped edge in sliding engagement with the retaining cap axially inner portion , and wherein the shoe gland further includes an intermediate surface in sliding engagement with the center body connector interior surface , and wherein the first packing arrangement further includes at least one sealing member secured between the shoe gland and the center flange . a center body connector having an interior surface forming a cavity extending axially therethrough, wherein the center body connector includes a center flange extending radially inwardly from the center body connector interior surface ; at least one retaining cap having an inner surface forming a retaining cap opening extending axially therethrough, wherein the retaining cap has a body with an axially inner portion having a notch and a ledge formed therein, and wherein the ledge is adapted to slidingly engage the interior surface of the center body connector ; and a first packing arrangement secured between the axially inner portion of the at least one retaining cap and the body connector interior surface , wherein the first packing arrangement includes a shoe gland having an outer sloped edge in sliding engagement with the retaining cap axially inner portion , and wherein the shoe gland further includes an intermediate surface in sliding engagement with the center body connector interior surface , and wherein the first packing arrangement further includes at least one sealing member secured between the shoe gland and the center flange .
A method for upgrading hydrocarbons using C4, C5 and C6 streams, comprising: preparing C4, C5 and C6 streams; oligomerizing the C4, C5 and C6 streams with a catalyst to produce branched unsaturated hydrocarbons; and fractional distillating the branched unsaturated hydrocarbons to separate into C14-18 products and C32-40 products, wherein the C4, C5 and C6 streams are the product of naphtha catalytic cracking (NCC) process, heavy oil upgrading process, thermal cracking process, or fluidized catalytic cracking (FCC or RFCC) process, and wherein to obtain the C32-40 products the oligomerization reaction is carried out using a solvent, at a temperature of 200 to 300°C and under pressure of 10 to 90 bars, and wherein the C32-40 products are subjected to an aromatic alkylation reaction, wherein the aromatic alkylation reaction of the C32-40 products is carried out at a temperature of 150 to 350 °C under N 2 and 1 to 20 bars for 0.5 to 48 hrs at 200 to 7000 rpm using an acid catalyst, such as zeolite, in a batch reactor. preparing C4, C5 and C6 streams; oligomerizing the C4, C5 and C6 streams with a catalyst to produce branched unsaturated hydrocarbons; and fractional distillating the branched unsaturated hydrocarbons to separate into C14-18 products and C32-40 products, wherein the C4, C5 and C6 streams are the product of naphtha catalytic cracking (NCC) process, heavy oil upgrading process, thermal cracking process, or fluidized catalytic cracking (FCC or RFCC) process, and wherein to obtain the C32-40 products the oligomerization reaction is carried out using a solvent, at a temperature of 200 to 300°C and under pressure of 10 to 90 bars, and wherein the C32-40 products are subjected to an aromatic alkylation reaction, wherein the aromatic alkylation reaction of the C32-40 products is carried out at a temperature of 150 to 350 °C under N 2 and 1 to 20 bars for 0.5 to 48 hrs at 200 to 7000 rpm using an acid catalyst, such as zeolite, in a batch reactor.
Docking system for spacecraft, comprising an end ring and a docking assembly , the docking assembly comprising a support ring connected to a plurality of linear actuators for deployment and retracting, the support ring and the end ring being connected, such that in a stowed position the docking assembly is placed inside the end ring and in a deployed position the docking assembly is placed out of the end ring , characterized in that the docking assembly comprises at least three docking platforms hinged to the support ring , each docking platform comprising: - a main body , - a guide member , - initial engagement means , and - a docking mechanism fixed to the main body and articulated to the end ring , the support ring and the end ring being connected by elastic means . characterized in that the docking assembly comprises at least three docking platforms hinged to the support ring , each docking platform comprising: - a main body , - a guide member , - initial engagement means , and - a docking mechanism fixed to the main body and articulated to the end ring , - a main body , - a guide member , - initial engagement means , and - a docking mechanism fixed to the main body and articulated to the end ring , the support ring and the end ring being connected by elastic means .
A method of making snack bars comprising: extruding a primary filling, constituted by a non-flowable material, onto a base; co-extruding a secondary filling with the primary filling, wherein the secondary filling is embedded in, yet externally exposed from, the primary filling; and cutting the primary filling, secondary filling and base into individual snack bars. extruding a primary filling, constituted by a non-flowable material, onto a base; co-extruding a secondary filling with the primary filling, wherein the secondary filling is embedded in, yet externally exposed from, the primary filling; and cutting the primary filling, secondary filling and base into individual snack bars.
A brake disc for a two-wheeled motor vehicle, the brake disc comprising a plurality of weight reduction holes for weight reduction, the weight reduction holes being formed in a slide section in use making sliding contact with a brake pad , wherein a plurality of grooves is formed at predetermined intervals in a circumferential direction so as to pass through a plurality of adjacent ones of the weight reduction holes , the grooves being formed on at least one of slide surfaces of the slide section , and wherein, among regions each between adjacent ones of the weight reduction holes , the grooves are formed so as to pass through a region between adjacent ones of the weight reduction holes in which a distance therebetween is shorter than a distance between other adjacent ones of the weight reduction holes and weight reduction holes arranged on both sides of the region. wherein a plurality of grooves is formed at predetermined intervals in a circumferential direction so as to pass through a plurality of adjacent ones of the weight reduction holes , the grooves being formed on at least one of slide surfaces of the slide section , and wherein, among regions each between adjacent ones of the weight reduction holes , the grooves are formed so as to pass through a region between adjacent ones of the weight reduction holes in which a distance therebetween is shorter than a distance between other adjacent ones of the weight reduction holes and weight reduction holes arranged on both sides of the region.
Industrial truck having a driver's workstation which comprises a driver's standing platform for a standing operating person (P) and which is arranged on a drive part (A) of the industrial truck , between a battery compartment of a traction battery and a vertical rear wall of the drive part (A) in a longitudinal direction (L) of the industrial truck , wherein the driver's workstation is arranged on the drive part (A) so as to be raisable and lowerable by means of a lifting drive , characterized in that the lifting drive is arranged, so as to be movable in a vertical direction (V) by means of a linear guide , on the drive part (A), and the lifting drive is supported in the vertical direction (V) on the drive part (A) with the interposition of a spring element .
A silicone composition comprising: (A') 70 to 98 parts by weight of an organopolysiloxane having, at an end of the molecule or on a side chain, a group of general formula below [wherein R x is a divalent hydrocarbon group of 1 to 8 carbon atoms; the letter "a" is an integer from 0 to 4; and each R z is independently a hydrogen atom, a monovalent hydrocarbon group of 1 to 10 carbon atoms, an acyl group or the polyoxyalkylene-containing organic group -CH 2 -CH(OH)CH 2 O-(C 2 H 4 O) b -(C 3 H 6 O) c -Z (Z being a hydrogen atom, a substituted or unsubstituted monovalent hydrocarbon group of 1 to 12 carbon atoms or an acyl group, b being an integer from 2 to 30, c being an integer from 0 to 20, and the oxyethylene and oxypropylene units optionally forming a block polymer or a random polymer), with the proviso that at least 90% of the total number of R z groups are -CH 2 -CH(OH)CH 2 O-(C 2 H 4 O) b -(C 3 H 6 O) c -Z groups]; and (B) 2 to 30 parts by weight of a blocked polyisocyanate which has at least two isocyanate groups per molecule, at least 50 mol% of the isocyanate groups being capped with a thermally labile blocking agent. (A') 70 to 98 parts by weight of an organopolysiloxane having, at an end of the molecule or on a side chain, a group of general formula below [wherein R x is a divalent hydrocarbon group of 1 to 8 carbon atoms; the letter "a" is an integer from 0 to 4; and each R z is independently a hydrogen atom, a monovalent hydrocarbon group of 1 to 10 carbon atoms, an acyl group or the polyoxyalkylene-containing organic group -CH 2 -CH(OH)CH 2 O-(C 2 H 4 O) b -(C 3 H 6 O) c -Z (Z being a hydrogen atom, a substituted or unsubstituted monovalent hydrocarbon group of 1 to 12 carbon atoms or an acyl group, b being an integer from 2 to 30, c being an integer from 0 to 20, and the oxyethylene and oxypropylene units optionally forming a block polymer or a random polymer), with the proviso that at least 90% of the total number of R z groups are -CH 2 -CH(OH)CH 2 O-(C 2 H 4 O) b -(C 3 H 6 O) c -Z groups]; and (B) 2 to 30 parts by weight of a blocked polyisocyanate which has at least two isocyanate groups per molecule, at least 50 mol% of the isocyanate groups being capped with a thermally labile blocking agent.