mhurhangee/patent-ind-claim-en huggingface dataset:
A quick hitch for mounting an implement on a machine, the quick hitch including an enclosure, the enclosure including at least one mounting means for connection to a machine, the enclosure accommodating a securing means for securing the quick hitch to an implement, the securing means having a first position in which the quick hitch is secured to an implement and a second position in which the quick hitch is not secured to an implement, the enclosure further including a first aperture through which a portion of the securing means extends when the securing means is in the first position, wherein the securing means includes a signal means , the signal means having a first position for signalling that the quick hitch is secured to an implement when the securing means is in the first position and a second position for signalling that the quick hitch is not secured to an implement when the securing means is in the second position; wherein the enclosure further includes an upper surface having an opening through which a portion of the signal means extends when the signal means is in either the first position or the second position; and wherein the opening includes a cover for preventing the ingress of dirt or debris into the enclosure and through which the portion of the signal means may extend. wherein the securing means includes a signal means , the signal means having a first position for signalling that the quick hitch is secured to an implement when the securing means is in the first position and a second position for signalling that the quick hitch is not secured to an implement when the securing means is in the second position; wherein the enclosure further includes an upper surface having an opening through which a portion of the signal means extends when the signal means is in either the first position or the second position; and wherein the opening includes a cover for preventing the ingress of dirt or debris into the enclosure and through which the portion of the signal means may extend.
A method for determining orientation of a vehicle relative to a surface, the vehicle having: - a first chassis section ; - a second chassis section ; - a hinge joint connecting the first and second chassis sections such that the first and second chassis sections are capable of rotation with respect to each other in at least a first direction; and - a wheel configuration provided by - a first wheel provided as a drive wheel and mounted to one of the first and second chassis sections ; and - a second wheel provided as an omni-wheel and mounted to the other of the first and second chassis sections ; the method comprising: - providing vehicle geometric data defining at least a distance between the hinge joint and a center of the first and second wheels , respectively, and a diameter of each of the first and second wheels ; - providing surface geometric data defining a curvature of the surface; - measuring an angle of rotation about the hinge joint ; and - determining an orientation of the vehicle relative to the surface based on the vehicle geometric data, the surface geometric data, and the measured angle of rotation. - a first chassis section ; - a second chassis section ; - a hinge joint connecting the first and second chassis sections such that the first and second chassis sections are capable of rotation with respect to each other in at least a first direction; and - a wheel configuration provided by - a first wheel provided as a drive wheel and mounted to one of the first and second chassis sections ; and - a second wheel provided as an omni-wheel and mounted to the other of the first and second chassis sections ; - a first wheel provided as a drive wheel and mounted to one of the first and second chassis sections ; and - a second wheel provided as an omni-wheel and mounted to the other of the first and second chassis sections ; - providing vehicle geometric data defining at least a distance between the hinge joint and a center of the first and second wheels , respectively, and a diameter of each of the first and second wheels ; - providing surface geometric data defining a curvature of the surface; - measuring an angle of rotation about the hinge joint ; and - determining an orientation of the vehicle relative to the surface based on the vehicle geometric data, the surface geometric data, and the measured angle of rotation.
Process of making pig iron in a blast furnace, said process comprising the steps of: a) charging the blast furnace with an iron ore and coke; b) injecting a reducing agent into the blast furnace at the level of one or more tuyeres in the raceway of the blast furnace; c) feeding hot air in the raceway of the blast furnace, wherein the blast furnace is furthermore charged with pellets in unground form as a reducing and energy supply agent, said pellets comprising: - one or more thermoplastic material(s) of more than 40 weight %, based on the total dry weight of the pellets; and - one or more cellulosic material(s) of more than 20 weight %, based on the total dry weight of the pellets d) and obtaining pig iron at the bottom of the blast furnace. a) charging the blast furnace with an iron ore and coke; b) injecting a reducing agent into the blast furnace at the level of one or more tuyeres in the raceway of the blast furnace; c) feeding hot air in the raceway of the blast furnace, wherein the blast furnace is furthermore charged with pellets in unground form as a reducing and energy supply agent, said pellets comprising: - one or more thermoplastic material(s) of more than 40 weight %, based on the total dry weight of the pellets; and - one or more cellulosic material(s) of more than 20 weight %, based on the total dry weight of the pellets - one or more thermoplastic material(s) of more than 40 weight %, based on the total dry weight of the pellets; and - one or more cellulosic material(s) of more than 20 weight %, based on the total dry weight of the pellets d) and obtaining pig iron at the bottom of the blast furnace.
A method of fabricating a formed structure comprising: forming a first mixture and a second mixture by mixing heat expanded polymeric shell microspheres with an epoxy resin and unexpanded polymeric shell microspheres, wherein the first and second mixtures are different to one another; forming the core mixtures into a shape to create a preform , wherein the differing core mixtures are used to create zones of varying density and stiffness; wrapping the preform with fiber tape to create a wrapped preform; placing the wrapped preform in a mold; heating the mold and expanding the unexpanded microspheres from an unexpanded state to an expanded state; cooling the mold; and removing the formed structure from the mold. forming a first mixture and a second mixture by mixing heat expanded polymeric shell microspheres with an epoxy resin and unexpanded polymeric shell microspheres, wherein the first and second mixtures are different to one another; forming the core mixtures into a shape to create a preform , wherein the differing core mixtures are used to create zones of varying density and stiffness; wrapping the preform with fiber tape to create a wrapped preform; placing the wrapped preform in a mold; heating the mold and expanding the unexpanded microspheres from an unexpanded state to an expanded state; cooling the mold; and removing the formed structure from the mold.
An anchoring system for securing soft tissue to bone, the system comprising an implant having a body for securement into a bone tunnel , pre-loaded sutures extending from the implant body and an insert comprising a nanofiber material attached to the implant body and having an extended surface for contacting the soft tissue.
Procedure to determine a remaining operating time (Δt B,r ) of a detector unit for a radiometric density or level transmitter , wherein the detector unit comprises at least a photomultiplier with a controllable amplification factor (A) and a control/evaluation unit , and wherein the control/evaluation unit controls the photomultiplier using a control voltage (V a ) in such a way that the amplification factor (A) is approximately constant, wherein said procedure is characterized by the following procedural steps: - Recording of the control voltage (V a ) over at least a predefined period of time (dt), - Determination of a temporal change function (dV a /dt) using the control voltage (V a ) recorded over the predetermined period of time (dt), - Calculation of the remaining operation time (Δt B,r ) until a maximum control voltage (V a,max ) is reached using the temporal change function (dV a /dt) and the current control voltage (V a,a ) that is present at the current operating time (t B,a ). - Recording of the control voltage (V a ) over at least a predefined period of time (dt), - Determination of a temporal change function (dV a /dt) using the control voltage (V a ) recorded over the predetermined period of time (dt), - Calculation of the remaining operation time (Δt B,r ) until a maximum control voltage (V a,max ) is reached using the temporal change function (dV a /dt) and the current control voltage (V a,a ) that is present at the current operating time (t B,a ).
A pharmaceutical composition for use in the prevention or treatment of flavivirus infection, the composition comprising: at least one of gentamicin sulfate, netilmicin, tobramycin, amikacin, capreomycin, trifluoroperazine, dihydrostreptomycin, thioridazine HCl, efavirenz, miltefosine, bleomycin, resminostat, norfloxacin, nedaplatin and cephalothin; or at least one of pharmaceutically acceptable salts of the above compounds.
Rotor (R) for an electric motor (EM), in particular a separately excited synchronous motor, having a rotor body (K); and an even number n of poles which are arranged on the rotor body (K) with in each case one rotor winding (L1,...,L6), the rotor windings of the poles being connected in series between two electric connectors (A1, A2) of the rotor (R) which serve to feed in and dissipate an electric field current through the rotor windings; the series circuit having a first section, to which the n/2 rotor windings (L1,...,L3) which are arranged first of all in the series circuit from a first one of the connectors belong, and a second section, to which the further n/2 rotor windings (L4,...,L6) which remain in the series circuit and are arranged upstream of the second one of the connectors belong; characterized in that the rotor windings (L1,...,L6) and the series circuit are configured in such a way that, in the case of the application of a DC voltage between the two connectors (A1, A2), in each of the rotor windings of the first section, the radial component, oriented in the direction of the winding height of the respective rotor winding, of the direct current flow which occurs in the series circuit runs through the respective rotor winding (L1,...,L3) overall from an inner side to an outer side of the rotor winding (L1,...,L3), and, in each of the rotor windings (L4,...,L6) of the second section, runs conversely overall from an outer side to an inner side of the rotor winding (L4,...,L6).
A computer-implemented image-based position detection method, comprising: acquiring (S11) first depth images captured at a same time by a plurality of photographing devices mounted in different orientations, wherein the plurality of photographing devices are synchronous in time, and the first depth images comprise a target object; acquiring (S32) second depth images captured by the plurality of photographing devices when the target object is not in an actual space as reference images; detecting (S12) a two-dimensional position of a target object in each of the first depth images, wherein the detecting (S12) a two-dimensional position of a target object in each of the first depth images comprises: determining (S33), for each of the photographing devices, the two-dimensional position of the target object in each of the first depth images based on a difference between depth information of the corresponding first depth image and depth information of a corresponding reference image; determining (S13) a three-dimensional position of the target object in the actual space based on the two-dimensional position of the target object in each of the first depth images and an internal parameter and an external parameter of each of the plurality of photographing devices; and correcting the two-dimensional position of the target object in each of the first depth images captured by each of the photographing devices based on the three-dimensional position of the target object in the actual space and the external parameter and the internal parameter of the each of the photographing devices using a geometric theory. acquiring (S11) first depth images captured at a same time by a plurality of photographing devices mounted in different orientations, wherein the plurality of photographing devices are synchronous in time, and the first depth images comprise a target object; acquiring (S32) second depth images captured by the plurality of photographing devices when the target object is not in an actual space as reference images; detecting (S12) a two-dimensional position of a target object in each of the first depth images, wherein the detecting (S12) a two-dimensional position of a target object in each of the first depth images comprises: determining (S33), for each of the photographing devices, the two-dimensional position of the target object in each of the first depth images based on a difference between depth information of the corresponding first depth image and depth information of a corresponding reference image; determining (S13) a three-dimensional position of the target object in the actual space based on the two-dimensional position of the target object in each of the first depth images and an internal parameter and an external parameter of each of the plurality of photographing devices; and correcting the two-dimensional position of the target object in each of the first depth images captured by each of the photographing devices based on the three-dimensional position of the target object in the actual space and the external parameter and the internal parameter of the each of the photographing devices using a geometric theory.
A composition comprising: (A) an ethylene/α-olefin copolymer comprising (i) ethylene and (ii) from 20 wt% to 35 wt% C 6 -C 8 α-olefin comonomer, the ethylene/α-olefin copolymer having a density from 0.880 g/cc to 0.895 g/cc; a melt viscosity, at 177°C, from 4,000 mPa•s to 20,000 mPa•s; a glass transition temperature from -55°C to -20°C; wherein the glass transition temperature is measured by Differential Scanning Calorimetry (DSC); (B) a tackifier; and (C) a wax. (A) an ethylene/α-olefin copolymer comprising (i) ethylene and (ii) from 20 wt% to 35 wt% C 6 -C 8 α-olefin comonomer, the ethylene/α-olefin copolymer having a density from 0.880 g/cc to 0.895 g/cc; a melt viscosity, at 177°C, from 4,000 mPa•s to 20,000 mPa•s; a glass transition temperature from -55°C to -20°C; wherein the glass transition temperature is measured by Differential Scanning Calorimetry (DSC); a density from 0.880 g/cc to 0.895 g/cc; a melt viscosity, at 177°C, from 4,000 mPa•s to 20,000 mPa•s; a glass transition temperature from -55°C to -20°C; wherein the glass transition temperature is measured by Differential Scanning Calorimetry (DSC); (B) a tackifier; and (C) a wax.
A compound represented by the following General Formula [V], wherein A, B, C, and D are the following groups: A = -N(R a )R b -Si(R c ) n (OR d ) 3-n , or -N{R b -Si(R c ) n (OR d ) 3-n } 2 , B = -N(R e )R f (NH 2 ) m , or -N{R f (NH 2 ) m } 2 , C = A, B, or -N(R g )R h , and D=R i ; each of R a , R e , and R g is H or a hydrocarbon group; R b , R c , R d , R f , R h , and R i are hydrocarbon groups; n is 0, 1 or 2; and m is 1 or 2; wherein the hydrocarbon group consists of H and C atoms. A, B, C, and D are the following groups: A = -N(R a )R b -Si(R c ) n (OR d ) 3-n , or -N{R b -Si(R c ) n (OR d ) 3-n } 2 , B = -N(R e )R f (NH 2 ) m , or -N{R f (NH 2 ) m } 2 , C = A, B, or -N(R g )R h , and D=R i ; A = -N(R a )R b -Si(R c ) n (OR d ) 3-n , or -N{R b -Si(R c ) n (OR d ) 3-n } 2 , B = -N(R e )R f (NH 2 ) m , or -N{R f (NH 2 ) m } 2 , C = A, B, or -N(R g )R h , and D=R i ; each of R a , R e , and R g is H or a hydrocarbon group; R b , R c , R d , R f , R h , and R i are hydrocarbon groups; n is 0, 1 or 2; and m is 1 or 2; wherein the hydrocarbon group consists of H and C atoms.
A fuel injector for a turbomachine , comprising an inner heat shield , said inner heat shield comprising: an air cavity wall defining an air cavity for allowing air to flow therethrough, wherein the inner heat shield includes an integral air swirler forming a downstream end thereof, wherein the air cavity wall and/or the integral air swirler are configured to extend in an axially downstream direction at least as far as a fuel distribution channel defined on or in a fuel distributor of the injector to direct airflow at an outlet of the fuel distributor ; wherein the integral air swirler includes an angled or curved wall extending from the downstream end of the air cavity wall such that the angled or curved wall extends both axially downstream and radially inward; wherein the angled or curved wall includes a plurality of swirling channels defined therethrough and configured to effuse swirling air; characterized in that the air swirler includes an upstream extending wall that extends from a downstream end of the angled or curved wall in the axially upstream direction; wherein the upstream extending wall extends both axially upstream and radially inward. an air cavity wall defining an air cavity for allowing air to flow therethrough, wherein the inner heat shield includes an integral air swirler forming a downstream end thereof, wherein the air cavity wall and/or the integral air swirler are configured to extend in an axially downstream direction at least as far as a fuel distribution channel defined on or in a fuel distributor of the injector to direct airflow at an outlet of the fuel distributor ; wherein the integral air swirler includes an angled or curved wall extending from the downstream end of the air cavity wall such that the angled or curved wall extends both axially downstream and radially inward;
A damper unit having a hydraulic cylinder with a hydraulic piston which is mounted displacably therein and which is coupled to a piston rod and divides the hydraulic cylinder into two hydraulic chambers which are fluidically interconnected via at least one hydraulic channel , and having a pneumatic cylinder with a pneumatic piston which is mounted displacably therein and which is coupled to the piston rod and divides the pneumatic cylinder into two pneumatic chambers which are fluidically interconnected via at least one pneumatic channel , wherein the value of the volume change of the hydraulic chambers during a movement of the hydraulic piston differs and the hydraulic chambers are fluidically coupled to a compensating volume , characterized in that the value of the volume change of the pneumatic chambers during a movement of the pneumatic piston is identical.
A casing of an electronic device, comprising: a metallic housing , having an inner surface (S1) and an outer surface (S2) opposite to the inner surface (S1), and also having a back area and at least one side area, wherein the inner surface (S1), the outer surface (S2), the back area and the at least one side area form at least part of the metallic housing , the inner surface (S1) being substantially a recessed structure covering the entire back area and side area, and the outer surface (S2) covering the back area and the side area on the opposite side from the inner surface (S1), and the metallic housing having a first gap communicating the inner surface (S1) and the outer surface (S2), wherein a first area (R1) of the metallic housing next to the first gap at a side area of the metallic housing is formed as one piece; and a first non-conductive spacer , at least partially disposed in the first gap of the metallic housing and extended from the back area to the at least one side area. a metallic housing , having an inner surface (S1) and an outer surface (S2) opposite to the inner surface (S1), and also having a back area and at least one side area, wherein the inner surface (S1), the outer surface (S2), the back area and the at least one side area form at least part of the metallic housing , the inner surface (S1) being substantially a recessed structure covering the entire back area and side area, and the outer surface (S2) covering the back area and the side area on the opposite side from the inner surface (S1), and the metallic housing having a first gap communicating the inner surface (S1) and the outer surface (S2), wherein a first area (R1) of the metallic housing next to the first gap at a side area of the metallic housing is formed as one piece; and a first non-conductive spacer , at least partially disposed in the first gap of the metallic housing and extended from the back area to the at least one side area.
A recombinant alpha galactosidase A and/or biologically active recombinant alpha galactosidase A fragment comprising an amino acid sequence comprising at least about 90%, at least about 91%, at least about 92%, at least about 93%, at least about 94%, at least about 95%, at least about 96%, at least about 97%, at least about 98%, or at least about 99% sequence identity to SEQ ID NO:5, wherein said alpha galactosidase A comprises a mutation at position 206 where the position is numbered with reference to SEQ ID NO:5.
A hydraulic machine having at least two stages comprising a shaft and impellers , wherein each stage comprises an impeller , and wherein each impeller comprises a plurality of impeller blades , is connected to the shaft and is of the radial type, and wherein the hydraulic machine has a low and a high pressure side, and wherein a first stage is located adjacent to the low pressure side of the hydraulic machine, and wherein an uppermost stage is located adjacent to the high pressure side of the hydraulic machine, and wherein the number of impeller blades of the first stage impeller is less than the number of impeller blades of any one impeller of the remaining stages, characterised in that each stage comprises a plurality of stationary blades , the distance between the stationary blades and the impeller blades of the uppermost stage being greater than the distance between the stationary blades and the impeller blades of the remaining stages.