mhurhangee/patent-ind-claim-en huggingface dataset:
A saddle tree comprising a back engaging element for engaging the back of an animal, a seat forming element resiliently mounted on the back engaging element and being resiliently moveable relative to the back engaging element , and a limit means connected between the seat forming element and the back engaging element for limiting upward travel of the seat forming element relative to the back engaging element , the limit means being adjustable for adjusting the limit of upward travel of the seat forming element relative to the back engaging element , the limit means being adjustably coupled to the one of the back engaging element and the seat forming element by an adjusting means , characterised in that the adjusting means comprises a ratchet mechanism .
Security element for a security paper or value document, comprising a carrier having a reflective areal region divided into a multiplicity of reflective pixels , the area of each pixel being smaller than the area of the reflective areal region by at least one order of magnitude, each pixel having at least one reflective facet formed in a surface of the carrier , the at least one reflective facet reflecting light incident along a predetermined direction on the areal region directionally in a reflection direction predefined by the orientation of said facet, characterized in that the orientations of the facets of different pixels have a substantially random variation over the reflective areal region , and in that the orientations of the facets of different pixels have a substantially random variation only in one of the parameters determining the orientation of the facets. the area of each pixel being smaller than the area of the reflective areal region by at least one order of magnitude, each pixel having at least one reflective facet formed in a surface of the carrier , the at least one reflective facet reflecting light incident along a predetermined direction on the areal region directionally in a reflection direction predefined by the orientation of said facet, characterized in that the orientations of the facets of different pixels have a substantially random variation over the reflective areal region , and in that the orientations of the facets of different pixels have a substantially random variation only in one of the parameters determining the orientation of the facets.
An apparel item comprising: an exterior shell layer , an inner liner layer , a sleeve and a gusset for coupling the exterior shell layer of the apparel item , the inner liner layer of the apparel item , and the sleeve of the apparel item , the gusset being a textile material comprising: an interior facing that has a body edge and a sleeve edge ; and an exterior facing that has a body edge and a sleeve edge ; wherein at least a portion of the sleeve edge of the exterior facing is coupled to the exterior shell layer of the apparel item , at least a portion of the body edge of the interior facing is coupled to at least a portion of the body edge of the exterior facing to form a bi-fold pleat , at least a portion of the body edge of the interior facing is coupled to the inner liner layer of the apparel item , and at least a portion of the sleeve edge of the interior facing is coupled to the sleeve .
The use of an organic material as a barocaloric cooling or heating agent wherein the organic material is selected from: a plastic crystal comprising a cycloalkyl group; a liquid crystal comprising one or more groups selected from alkyl, cycloalkyl and aryl; or an alkyl carboxylic acid or an alkyl carboxylate salt. a plastic crystal comprising a cycloalkyl group; a liquid crystal comprising one or more groups selected from alkyl, cycloalkyl and aryl; or an alkyl carboxylic acid or an alkyl carboxylate salt.
An LTE base station, comprising: a processing module , configured to: determine a first direct current component DC subcarrier on a carrier, wherein the first DC subcarrier is located, in a frequency domain, at a non-center frequency location on the carrier, and a center frequency of the first DC subcarrier is an integer multiple of 100 KHz; and determine a second DC subcarrier on the carrier, wherein the second DC subcarrier is located, in the frequency domain, at a center frequency location at which the base station transmits the carrier, and the first DC subcarrier does not overlap the second DC subcarrier; characterised in that the first DC subcarrier is located on a central subcarrier of an access bandwidth of the carrier, the access bandwidth is used to send at least a synchronization channel and a physical broadcast channel PBCH, and the synchronization channel comprises a primary synchronization signal PSS and a secondary synchronization signal SSS; wherein the first DC subcarrier does not belong to any Physical Resource Block, PRB, on the carrier, and the second DC subcarrier belongs to a PRB on the carrier. a processing module , configured to: determine a first direct current component DC subcarrier on a carrier, wherein the first DC subcarrier is located, in a frequency domain, at a non-center frequency location on the carrier, and a center frequency of the first DC subcarrier is an integer multiple of 100 KHz; and determine a second DC subcarrier on the carrier, wherein the second DC subcarrier is located, in the frequency domain, at a center frequency location at which the base station transmits the carrier, and the first DC subcarrier does not overlap the second DC subcarrier; characterised in that the first DC subcarrier is located on a central subcarrier of an access bandwidth of the carrier, the access bandwidth is used to send at least a synchronization channel and a physical broadcast channel PBCH, and the synchronization channel comprises a primary synchronization signal PSS and a secondary synchronization signal SSS; wherein the first DC subcarrier does not belong to any Physical Resource Block, PRB, on the carrier, and the second DC subcarrier belongs to a PRB on the carrier.
A gas turbine engine defined along a central longitudinal engine axis (A), comprising: a turbine section ; and an exhaust section located axially aft of the turbine section , the exhaust section including an exhaust case , wherein the exhaust case includes a first case ; a second case that is co-axial with the first case and radially inward of the first case , wherein the second case includes a flange and a bracket ; a strut coupled to the first case and the second case ; and a fastener that fastens the flange and the strut , wherein the strut radially contacts the bracket due to a difference in temperature of the strut relative to the bracket when the gas turbine engine is powered-on, wherein the second case transfers a load to the strut as part of a load path when the gas turbine engine is powered-on, and wherein the load path bypasses the fastener . a turbine section ; and an exhaust section located axially aft of the turbine section , the exhaust section including an exhaust case , wherein the exhaust case includes a first case ; a second case that is co-axial with the first case and radially inward of the first case , wherein the second case includes a flange and a bracket ; a strut coupled to the first case and the second case ; and a fastener that fastens the flange and the strut , wherein the strut radially contacts the bracket due to a difference in temperature of the strut relative to the bracket when the gas turbine engine is powered-on, a first case ; a second case that is co-axial with the first case and radially inward of the first case , wherein the second case includes a flange and a bracket ; a strut coupled to the first case and the second case ; and a fastener that fastens the flange and the strut , wherein the strut radially contacts the bracket due to a difference in temperature of the strut relative to the bracket when the gas turbine engine is powered-on, wherein the second case transfers a load to the strut as part of a load path when the gas turbine engine is powered-on, and wherein the load path bypasses the fastener .
A rotor (60C; 60T) for a gas turbine engine comprising: a rotor disk (66; 124) defined along an axis of rotation (A), said rotor disk (66; 124) including a rim (70; 128); and a plurality of blades (64; 102) which extend from said rotor disk (66; 124), wherein each blade (64;124) includes an attachment section (74; 132), a platform section (76; 134) and an airfoil section (78; 136) extending out from said platform section (76; 134), and wherein each of said plurality of blades (64; 102) extends from said rotor disk (66; 124) at an interface (801; 1361) between said rim (70; 128) and said attachment section (74; 132), said interface (801; 1361) defined along a spoke (80; 136) that comprises a circumferentially reduced section defined by interruptions which produce axial or semi-axial slots which flank each spoke (80;136), said platform section (76; 134) comprises at least one recess extending along an entire edge of the platform section (76; 134) for defining with an adjacent recess a teardrop shaped cavity that receives a first wire seal that extends axially, characterised in that a second wire seal extends circumferentially and is received in another teardrop shaped cavity , wherein the second wire seal is configured to be located between the rotor (60C; 60T) and an adjacent spacer (62C; 62T). a rotor disk (66; 124) defined along an axis of rotation (A), said rotor disk (66; 124) including a rim (70; 128); and a plurality of blades (64; 102) which extend from said rotor disk (66; 124), wherein each blade (64;124) includes an attachment section (74; 132), a platform section (76; 134) and an airfoil section (78; 136) extending out from said platform section (76; 134), and wherein each of said plurality of blades (64; 102) extends from said rotor disk (66; 124) at an interface (801; 1361) between said rim (70; 128) and said attachment section (74; 132), said interface (801; 1361) defined along a spoke (80; 136) that comprises a circumferentially reduced section defined by interruptions which produce axial or semi-axial slots which flank each spoke (80;136), said platform section (76; 134) comprises at least one recess extending along an entire edge of the platform section (76; 134) for defining with an adjacent recess a teardrop shaped cavity that receives a first wire seal that extends axially, characterised in that a second wire seal extends circumferentially and is received in another teardrop shaped cavity , wherein the second wire seal is configured to be located between the rotor (60C; 60T) and an adjacent spacer (62C; 62T).
A method of administering biocide to industrial water in an industrial water process, the method comprising: diverting a portion of industrial water to a side stream at a water level; filtering the industrial water side stream, wherein suspended solids having an average particle size of from 1 micron to 50 microns that are present in the industrial water side stream are removed via the filtering; adding to a biocide-forming reactor a first reactant and a second reactant at a ratio sufficient to form biocide, wherein the biocide-forming reactor is located at least partially below the industrial water level; treating the filtered industrial water side stream with biocide from the biocide-forming reactor; and returning the biocide-treated industrial water side stream to the industrial water in the industrial water process, wherein the method has a flow-residence factor of from 0.0001 to 0.1; wherein the flow-residence factor (FRF) is calculated as demonstrated by formula : FRF = VVS / Σ RVF * SS / VOL wherein the volumetric void space of the reaction chamber (WS) is divided by the sum total volumetric flow rate of reactants (ΣRVF) and then multiplying the quotient by the volumetric flow rate of the industrial water side stream (SS) divided by the total industrial water in the industrial water system (VOL), ΣRVF and SS having like units and VOL and WS having like units, leaving unitless FRF. diverting a portion of industrial water to a side stream at a water level; filtering the industrial water side stream, wherein suspended solids having an average particle size of from 1 micron to 50 microns that are present in the industrial water side stream are removed via the filtering; adding to a biocide-forming reactor a first reactant and a second reactant at a ratio sufficient to form biocide, wherein the biocide-forming reactor is located at least partially below the industrial water level; treating the filtered industrial water side stream with biocide from the biocide-forming reactor; and returning the biocide-treated industrial water side stream to the industrial water in the industrial water process, wherein the method has a flow-residence factor of from 0.0001 to 0.1; wherein the flow-residence factor (FRF) is calculated as demonstrated by formula : FRF = VVS / Σ RVF * SS / VOL wherein the volumetric void space of the reaction chamber (WS) is divided by the sum total volumetric flow rate of reactants (ΣRVF) and then multiplying the quotient by the volumetric flow rate of the industrial water side stream (SS) divided by the total industrial water in the industrial water system (VOL), ΣRVF and SS having like units and VOL and WS having like units, leaving unitless FRF.
A method for determining a tridimensional location of a camera for a self-calibrated monitoring system , in which a plurality of N tridimensional sensors respectively monitor at least a part of the monitored volume (V) and respectively communicate with a central processing unit , - providing a camera comprising at least one reflective pattern such that a data point of said reflective pattern acquired by a tridimensional sensor of the self-calibrated monitoring system can be associated to said camera , - positioning the camera in the monitored volume (V), in a field of view of at least one sensor of the plurality of N tridimensional sensors so that said sensor acquire a local point cloud (C) comprising at least one tridimensional data point (D) of the reflective pattern of the camera , - receiving a local point cloud (C) from said at least one tridimensional sensor and computing an aligned local point cloud (A) by aligning said local point cloud (C) with the global tridimensional map (M) of the self-calibrated monitoring system, - identifying, in the aligned local point cloud (A) at least one data point (D) corresponding to the reflective pattern of the camera , and - determining at least a tridimensional location of the camera in a global coordinate system (G) of the global tridimensional map (M) on the basis of the coordinates of said identified data point (D) of the aligned local point cloud (A) corresponding to the reflective pattern of the camera. - providing a camera comprising at least one reflective pattern such that a data point of said reflective pattern acquired by a tridimensional sensor of the self-calibrated monitoring system can be associated to said camera , - positioning the camera in the monitored volume (V), in a field of view of at least one sensor of the plurality of N tridimensional sensors so that said sensor acquire a local point cloud (C) comprising at least one tridimensional data point (D) of the reflective pattern of the camera , - receiving a local point cloud (C) from said at least one tridimensional sensor and computing an aligned local point cloud (A) by aligning said local point cloud (C) with the global tridimensional map (M) of the self-calibrated monitoring system, - identifying, in the aligned local point cloud (A) at least one data point (D) corresponding to the reflective pattern of the camera , and - determining at least a tridimensional location of the camera in a global coordinate system (G) of the global tridimensional map (M) on the basis of the coordinates of said identified data point (D) of the aligned local point cloud (A) corresponding to the reflective pattern of the camera.
A display system for displaying image data, wherein the display system comprises: a light source ; a spatial light modulator including a plurality of controllable elements; a light source controller , configured to control the light source to emit, in each of a plurality of N time intervals, light with a different illumination power level, wherein the time intervals have the same length; a spatial light modulator controller , configured to activate, based on received image data, the plurality of controllable elements for at least one of the time intervals for directing the light from the light source for displaying the image data; wherein the light source controller is configured to control the light source by performing pulse count modulation of the light source, wherein each time interval is subdivided into 2 (N-1) pulse sectors, wherein each illumination power level in each time interval is obtained by activating at least one pulse, in at least one corresponding pulse sector among the pulse sectors, wherein the N time intervals are used to compose a 2 N grey-level pixel and N indicates the color-depth of the image data; characterized in that the time interval indicates the shortest time duration for the controllable elements after which the controllable elements may change their state. a light source ; a spatial light modulator including a plurality of controllable elements; a light source controller , configured to control the light source to emit, in each of a plurality of N time intervals, light with a different illumination power level, wherein the time intervals have the same length; a spatial light modulator controller , configured to activate, based on received image data, the plurality of controllable elements for at least one of the time intervals for directing the light from the light source for displaying the image data; wherein the light source controller is configured to control the light source by performing pulse count modulation of the light source, wherein each time interval is subdivided into 2 (N-1) pulse sectors, wherein each illumination power level in each time interval is obtained by activating at least one pulse, in at least one corresponding pulse sector among the pulse sectors, wherein the N time intervals are used to compose a 2 N grey-level pixel and N indicates the color-depth of the image data; characterized in that the time interval indicates the shortest time duration for the controllable elements after which the controllable elements may change their state.
A method of selecting a beam-forming weighting vector said method comprising: receiving from user equipment a radio frequency fingerprint comprising indications of characteristics of radio signals received from a network node and at least one neighbouring network node within a wireless communication network; accessing a data base associating a plurality of radio frequency fingerprints comprising said indications of characteristics of radio signals from said network node and from neighbouring network nodes with a plurality of beam-forming weighting vectors; and comparing said received radio frequency fingerprint with said radio frequency fingerprints within said data base and selecting one of said beam-forming weighting vectors in dependence upon said comparison. receiving from user equipment a radio frequency fingerprint comprising indications of characteristics of radio signals received from a network node and at least one neighbouring network node within a wireless communication network; accessing a data base associating a plurality of radio frequency fingerprints comprising said indications of characteristics of radio signals from said network node and from neighbouring network nodes with a plurality of beam-forming weighting vectors; and comparing said received radio frequency fingerprint with said radio frequency fingerprints within said data base and selecting one of said beam-forming weighting vectors in dependence upon said comparison.
A three-dimensional-object inkjet printing apparatus comprising: a base ; an arm supported by the base; a liquid ejecting head that is fixed to a tip end of the arm and ejects a liquid onto a work piece; a liquid accumulation section that accumulates the liquid; a supply channel which communicates the liquid accumulation section and the liquid ejecting head with each other and along which the liquid is supplied from the liquid accumulation section to the liquid ejecting head; and a pressure control valve that is provided halfway in the supply channel and controls a pressure of the liquid supplied to the liquid ejecting head, wherein the arm includes N movable sections (231-236) that change an angle of the liquid ejecting head with respect to a horizontal plane, N being 1 or more, the pressure control valve is fixed to the arm, and K pieces of the movable sections are provided between the pressure control valve and the base, K being 1 or more and N or less. a base ; an arm supported by the base; a liquid ejecting head that is fixed to a tip end of the arm and ejects a liquid onto a work piece; a liquid accumulation section that accumulates the liquid; a supply channel which communicates the liquid accumulation section and the liquid ejecting head with each other and along which the liquid is supplied from the liquid accumulation section to the liquid ejecting head; and a pressure control valve that is provided halfway in the supply channel and controls a pressure of the liquid supplied to the liquid ejecting head, wherein the arm includes N movable sections (231-236) that change an angle of the liquid ejecting head with respect to a horizontal plane, N being 1 or more, the pressure control valve is fixed to the arm, and K pieces of the movable sections are provided between the pressure control valve and the base, K being 1 or more and N or less.