mhurhangee/patent-ind-claim-en huggingface dataset:
A proximity wireless communication device comprising: a first communication block and a second communication block , wherein the first communication block has a first surface defining a first plane, and a projection equipped in a part of the first surface, and a first antenna is disposed in an upper surface of the projection which defines a second plane and a second antenna is disposed in the first surface, the second communication block has a second surface and a recess equipped in a part of the second surface, and a third antenna is disposed in a bottom surface of the recess and a fourth antenna is disposed in the second surface, the first surface and the second surface face in proximity, the projection and the recess fit, and the upper surface of the projection and the bottom surface of the recess face in proximity, and non-contact near-field wireless communication is carried out between the first antenna and the third antenna through the second plane, and between the second antenna and the fourth antenna through the first plane, wherein the first plane and the second plane are apart by a predetermined distance in a direction in which the projection and the recess extend. a first communication block and a second communication block , wherein the first communication block has a first surface defining a first plane, and a projection equipped in a part of the first surface, and a first antenna is disposed in an upper surface of the projection which defines a second plane and a second antenna is disposed in the first surface, the second communication block has a second surface and a recess equipped in a part of the second surface, and a third antenna is disposed in a bottom surface of the recess and a fourth antenna is disposed in the second surface, the first surface and the second surface face in proximity, the projection and the recess fit, and the upper surface of the projection and the bottom surface of the recess face in proximity, and non-contact near-field wireless communication is carried out between the first antenna and the third antenna through the second plane, and between the second antenna and the fourth antenna through the first plane, wherein the first plane and the second plane are apart by a predetermined distance in a direction in which the projection and the recess extend.
Valve housing for a pinch valve, comprising - a housing body with an upper opening and two opposing side walls laterally bounding the opening with their upper edges, the inner sides of which walls each carry a longitudinally extending lid guide groove proximate to the respective upper edge, and - a plate-like lid with lateral, longitudinally extending guide edges , the lid being slidingly mounted on the housing body by engagement of the guide edges in the lid guide grooves of the housing body, wherein the housing body carries on the outer side of one of the side walls a bolt aligned parallel to the lid guide grooves , and the lid carries a guide fixed to a tab projecting over the corresponding side wall upper edge of the housing body and aligned coaxially with the bolt , the guide engaging around the bolt to form a rotationally movable sliding bearing, wherein the bolt is detachably fixed axially to the housing body and the guide is formed as a sleeve which engages around the bolt to form an additional, axially movable sliding bearing. - a housing body with an upper opening and two opposing side walls laterally bounding the opening with their upper edges, the inner sides of which walls each carry a longitudinally extending lid guide groove proximate to the respective upper edge, and - a plate-like lid with lateral, longitudinally extending guide edges , the lid being slidingly mounted on the housing body by engagement of the guide edges in the lid guide grooves of the housing body, wherein the housing body carries on the outer side of one of the side walls a bolt aligned parallel to the lid guide grooves , and the lid carries a guide fixed to a tab projecting over the corresponding side wall upper edge of the housing body and aligned coaxially with the bolt , the guide engaging around the bolt to form a rotationally movable sliding bearing, wherein the bolt is detachably fixed axially to the housing body and the guide is formed as a sleeve which engages around the bolt to form an additional, axially movable sliding bearing.
An oral care composition comprising a phosphate/acrylate co-polymer and an orally acceptable carrier, wherein the phosphate/acrylate co-polymer is a co-polymerized product of a mixture of acrylic acid, methacrylic acid, and 2-hydroxyethyl methacrylate phosphates of Formula 1 comprising acrylic acid in a molar percentage of 70-90%; methacrylic acid in a molar percentage of 5-20%, and a mixture of hydroxyethyl methacrylate phosphates of Formula 1 in a molar percentage of 1-10%: wherein n is 0, 1 or 2.
An integrated service design center comprising: a plan/catalog design engine and subscriber management engine providing a sandboxed design environment , the plan/catalog design engine is configured to generate a catalog descriptor in response to input from one or more service designers, the catalog descriptor including definitions of service plans, service plan objects, and prioritization information, the subscriber management engine , in response to input from a plurality of subscriber managers, is configured to define respective end-user device groups and to associate each end-user device group with a respective catalog specified by the catalog descriptor, the subscriber management engine is configured to output a set of end-user device identifiers and/or credentials for each association, the sandboxed design environment is configured to associate a user credential with each service designer and subscriber manager, and to limit the design and management functions available to each service designer and subscriber manager according to design permissions and subscriber groups for a respective user credential; and a provisioning instruction translator configured to combine network implementation and configuration information with each association from the plan/catalog design engine and the subscriber management engine in order to determine one or more network elements and one or more end-user devices , and to provide provisioning instructions to the determined network elements and end-user devices to effectuate the respective catalog associated with each end-user device group. a plan/catalog design engine and subscriber management engine providing a sandboxed design environment , the plan/catalog design engine is configured to generate a catalog descriptor in response to input from one or more service designers, the catalog descriptor including definitions of service plans, service plan objects, and prioritization information, the subscriber management engine , in response to input from a plurality of subscriber managers, is configured to define respective end-user device groups and to associate each end-user device group with a respective catalog specified by the catalog descriptor, the subscriber management engine is configured to output a set of end-user device identifiers and/or credentials for each association, the sandboxed design environment is configured to associate a user credential with each service designer and subscriber manager, and to limit the design and management functions available to each service designer and subscriber manager according to design permissions and subscriber groups for a respective user credential; and a provisioning instruction translator configured to combine network implementation and configuration information with each association from the plan/catalog design engine and the subscriber management engine in order to determine one or more network elements and one or more end-user devices , and to provide provisioning instructions to the determined network elements and end-user devices to effectuate the respective catalog associated with each end-user device group.
Air conditioning system for a cabin of an air or rail transport vehicle, comprising: - a pneumatic turbine engine that comprises at least one compressor and at least one turbine and is connected by a mechanical shaft extending along an axis, referred to as the turbine engine axis , said turbine comprising an air inlet and an air outlet, and - a water extraction loop that comprises a heater , a condenser , and a water separator , is arranged fluidically between an air outlet of the compressor and the air inlet of said turbine , and is configured to be able to dry the air supplied to said turbine , - said heater , said condenser , and said water separator being arranged in series, forming the air inlet of said turbine ; - said heater is arranged on the turbine engine axis or around said axis; - said condenser being arranged on the turbine engine axis or around said axis; - said water separator being arranged on the turbine engine axis or around said axis, characterized in that - said heater is cylindrical and surrounds the axis of the turbine engine and the turbine , so that the outlet of the cold pass of the heater opens directly into the air inlet of the turbine. - a pneumatic turbine engine that comprises at least one compressor and at least one turbine and is connected by a mechanical shaft extending along an axis, referred to as the turbine engine axis , said turbine comprising an air inlet and an air outlet, and - a water extraction loop that comprises a heater , a condenser , and a water separator , is arranged fluidically between an air outlet of the compressor and the air inlet of said turbine , and is configured to be able to dry the air supplied to said turbine , - said heater , said condenser , and said water separator being arranged in series, forming the air inlet of said turbine ; - said heater is arranged on the turbine engine axis or around said axis; - said condenser being arranged on the turbine engine axis or around said axis; - said water separator being arranged on the turbine engine axis or around said axis, characterized in that - said heater is cylindrical and surrounds the axis of the turbine engine and the turbine , so that the outlet of the cold pass of the heater opens directly into the air inlet of the turbine. - said heater , said condenser , and said water separator being arranged in series, forming the air inlet of said turbine ; - said heater is arranged on the turbine engine axis or around said axis; - said condenser being arranged on the turbine engine axis or around said axis; - said water separator being arranged on the turbine engine axis or around said axis, characterized in that - said heater is cylindrical and surrounds the axis of the turbine engine and the turbine , so that the outlet of the cold pass of the heater opens directly into the air inlet of the turbine.
Double fabric comprising an upper fabric G H and a lower fabric G L , wherein the fabrics G H and G L each comprise a plurality of warp threads K, K R , K H and K L and a plurality of weft threads S, S H and S L and the fabrics G H and G L are woven with the warp threads K R in the end region of the weft threads S to a common edge R, R', wherein between the two edges R and R' the upper fabric G H is divided into a segment A H and a segment B H , wherein the lower fabric G L is divided into a segment A L and a segment B L as a mirror images to the segments A H and B H , wherein - the segment A H has the same length as the segment B L and the segment A L has the same length as the segment B H and - at least one weft thread S connects the segment A H of the upper fabric G H to the segment B L of the lower fabric G L and thus forms the weft thread S(A H B L ) and at least one weft thread S connects the segment A L of the lower fabric G L to the segment B H of the upper fabric G H and thus forms the weft thread S(A L B H ), wherein the weft thread S(A H B L ) is preferably arranged parallel to the segment B H and the weft thread S(A L B H ) is preferably arranged parallel to the segment A H , characterized in that the weft threads S H are woven with the warp threads K H to the upper fabric G H and extend from the edge R along the entire upper fabric G H , which comprises the warp threads K H as far as the edge R' and that the weft threads S L are woven with the warp threads K L to the lower fabric G L and extend from the edge R along the entire lower fabric G L comprising the warp threads K L as far as the edge R'. - the segment A H has the same length as the segment B L and the segment A L has the same length as the segment B H and - at least one weft thread S connects the segment A H of the upper fabric G H to the segment B L of the lower fabric G L and thus forms the weft thread S(A H B L ) and at least one weft thread S connects the segment A L of the lower fabric G L to the segment B H of the upper fabric G H and thus forms the weft thread S(A L B H ), wherein the weft thread S(A H B L ) is preferably arranged parallel to the segment B H and the weft thread S(A L B H ) is preferably arranged parallel to the segment A H ,
A textile sleeve (10;11;34;50;70) for protecting elongate members, comprising: a substrate (12;52;72) having filamentary members (14,18;36) interlaced with one another, at least some of said filamentary members (18;36) having a core of heat-settable polymeric material and an outer sheath of heat-fusible polymeric material and at least some of said outer sheaths being heat-fused to other ones of said filamentary members (14,18;36), characterised in that said filamentary members (18;36) have a core of heat-settable polymeric material and an outer sheath of heat-fusible polymeric material are monofilaments. a substrate (12;52;72) having filamentary members (14,18;36) interlaced with one another, at least some of said filamentary members (18;36) having a core of heat-settable polymeric material and an outer sheath of heat-fusible polymeric material and at least some of said outer sheaths being heat-fused to other ones of said filamentary members (14,18;36), characterised in that said filamentary members (18;36) have a core of heat-settable polymeric material and an outer sheath of heat-fusible polymeric material are monofilaments.
Oscillatingly drivable machine tool, with a tool spindle pivotably mounted about its longitudinal axis , with a drive motor , wherein the machine tool is configured to drive the tool spindle in a rotationally oscillating manner at a frequency of 5000 to 30000 oscillations per minute and with a pivoting angle of ± 1° to ± 5° from reversal point to reversal point, wherein the machine tool is characterized in that the drive motor is coupled to a hydraulic generator for generating an oscillating fluid flow, which drives a hydraulic motor in the form of a rotary vane motor in order to drive the tool spindle in a oscillating manner about its longitudinal axis .
A droplet deposition apparatus comprising a droplet deposition head , a fluid supply , a controller , and drive signal generating circuitry , wherein: the droplet deposition head comprises one or more fluid chambers each having a nozzle , a fluid inlet path having a fluid inlet into the droplet deposition head , and ending in the one or more nozzles , and a fluid return path starting at the one or more nozzles and ending in a fluid return of the droplet deposition head ; each fluid chamber comprises two opposing chamber walls comprising piezoelectric material and deformable upon application of an electric drive signal so as to eject a fluid droplet from the nozzle in use; and the fluid supply is configured to supply, in use, a fluid to the fluid inlet at a differential pressure as measured between the fluid inlet and the fluid return ; wherein the controller is configured to apply drive signals to the piezoelectric chamber walls such that, in use, the nozzle or nozzles deposit droplets of fluid having a viscosity in the range from 45 mPa·s to 130 mPa·s at a predefined jetting temperature between 20°C and 90°C; wherein the drive signal generating circuitry is configured to modify the drive signals to control droplet velocity during changes in chamber wall actuation rate so as to keep the droplet velocity of the ejected droplets substantially equal to a predefined droplet velocity in use; and wherein, in use, the differential pressure applied by the fluid supply causes a fluid return flow into the fluid return at a rate of between 50 ml/min and 200 ml/min. the droplet deposition head comprises one or more fluid chambers each having a nozzle , a fluid inlet path having a fluid inlet into the droplet deposition head , and ending in the one or more nozzles , and a fluid return path starting at the one or more nozzles and ending in a fluid return of the droplet deposition head ; each fluid chamber comprises two opposing chamber walls comprising piezoelectric material and deformable upon application of an electric drive signal so as to eject a fluid droplet from the nozzle in use; and the fluid supply is configured to supply, in use, a fluid to the fluid inlet at a differential pressure as measured between the fluid inlet and the fluid return ; wherein the controller is configured to apply drive signals to the piezoelectric chamber walls such that, in use, the nozzle or nozzles deposit droplets of fluid having a viscosity in the range from 45 mPa·s to 130 mPa·s at a predefined jetting temperature between 20°C and 90°C; wherein the drive signal generating circuitry is configured to modify the drive signals to control droplet velocity during changes in chamber wall actuation rate so as to keep the droplet velocity of the ejected droplets substantially equal to a predefined droplet velocity in use; and wherein, in use, the differential pressure applied by the fluid supply causes a fluid return flow into the fluid return at a rate of between 50 ml/min and 200 ml/min.
An aircraft engine comprising an inertial particle separator (IPS) communicating with an engine inlet of the aircraft engine , the IPS comprising: an inlet duct defining an intake communicating with an environment (E) of the aircraft engine ; an intermediate duct extending from the inlet duct to the engine inlet ; a bypass duct in fluid communication with and extending downstream from the inlet duct , the bypass duct defining an outlet communicating with the environment (E) of the aircraft engine , a splitter defined at an intersection of a wall of the bypass duct and a wall of the intermediate duct ; a splitter vane within the intermediate duct and having a leading edge located upstream of the splitter relative to a flow (F) circulating through the IPS , the splitter vane and the wall of the intermediate duct defining a channel therebetween; and characterised by a porous plate extending across the channel and defining openings sized so as to aggregate ice and be blocked by ice under icing conditions, such that in icing conditions the channel becomes ice-blocked, and in non-icing conditions, the channel is open. an inlet duct defining an intake communicating with an environment (E) of the aircraft engine ; an intermediate duct extending from the inlet duct to the engine inlet ; a bypass duct in fluid communication with and extending downstream from the inlet duct , the bypass duct defining an outlet communicating with the environment (E) of the aircraft engine , a splitter defined at an intersection of a wall of the bypass duct and a wall of the intermediate duct ; a splitter vane within the intermediate duct and having a leading edge located upstream of the splitter relative to a flow (F) circulating through the IPS , the splitter vane and the wall of the intermediate duct defining a channel therebetween; and characterised by a porous plate extending across the channel and defining openings sized so as to aggregate ice and be blocked by ice under icing conditions, such that in icing conditions the channel becomes ice-blocked, and in non-icing conditions, the channel is open.
A computer-implemented method for providing single sign-on to remote or cloud-based computing resources, comprising: requesting, via a local network computer, access to a cloud-based resource; passing a request from the local network computer to a local directory services system for a service ticket associated with a cloud-based directory services system through which access may be granted to the cloud-based resource; passing the service ticket associated with the cloud-based directory services system from the local network computer to a cloud-based authentication endpoint associated with the cloud-based directory services system for validating a requesting user associated with the requesting local network computer for access to the requested cloud-based resource; receiving from the cloud-based directory services system validation of the service ticket by the cloud-based directory services system for authenticating the requesting user for access to the requested cloud-based resource; and receiving at the requesting local network computer authorization to access the requested cloud-based resource, and prior to passing the service ticket to the cloud-based authentication endpoint, registering the cloud-based authentication endpoint with the local directory services system as a local device, service or resource for allowing the service ticket to be passed to the cloud-based authentication endpoint as a local endpoint. requesting, via a local network computer, access to a cloud-based resource; passing a request from the local network computer to a local directory services system for a service ticket associated with a cloud-based directory services system through which access may be granted to the cloud-based resource; passing the service ticket associated with the cloud-based directory services system from the local network computer to a cloud-based authentication endpoint associated with the cloud-based directory services system for validating a requesting user associated with the requesting local network computer for access to the requested cloud-based resource; receiving from the cloud-based directory services system validation of the service ticket by the cloud-based directory services system for authenticating the requesting user for access to the requested cloud-based resource; and receiving at the requesting local network computer authorization to access the requested cloud-based resource, and prior to passing the service ticket to the cloud-based authentication endpoint, registering the cloud-based authentication endpoint with the local directory services system as a local device, service or resource for allowing the service ticket to be passed to the cloud-based authentication endpoint as a local endpoint.