mhurhangee/patent-ind-claim-en huggingface dataset:
An article comprising: a first member consisting of a first carbon composite; and a second member disposed on the first member and consisting of a second carbon composite and a reinforcing agent , wherein the second member has a gradient in the weight ratio of the second carbon composite to the reinforcing agent , wherein the first member has one or more of the following properties different than those of the second member : elasticity; corrosion resistance; erosion resistance; or hardness; and wherein each of the first carbon composite and the second carbon composite independently comprises a carbon and a binder containing one or more of the following: SiO 2 ; Si; B; B 2 O 3 ; a metal; or an alloy of the metal; and wherein the metal is one or more of the following: aluminum; copper; titanium; nickel; tungsten; chromium; iron; manganese; zirconium; hafnium; vanadium; niobium; molybdenum; tin; bismuth; antimony; lead; cadmium; or selenium; and wherein the carbon in the first carbon composite and the carbon in the second carbon composite independently comprise one or more of the following: expanded graphite; expandable graphite; natural graphite; or synthetic graphite. a first member consisting of a first carbon composite; and a second member disposed on the first member and consisting of a second carbon composite and a reinforcing agent , wherein the second member has a gradient in the weight ratio of the second carbon composite to the reinforcing agent , wherein the first member has one or more of the following properties different than those of the second member : elasticity; corrosion resistance; erosion resistance; or hardness; and wherein each of the first carbon composite and the second carbon composite independently comprises a carbon and a binder containing one or more of the following: SiO 2 ; Si; B; B 2 O 3 ; a metal; or an alloy of the metal; and wherein the metal is one or more of the following: aluminum; copper; titanium; nickel; tungsten; chromium; iron; manganese; zirconium; hafnium; vanadium; niobium; molybdenum; tin; bismuth; antimony; lead; cadmium; or selenium; and wherein the carbon in the first carbon composite and the carbon in the second carbon composite independently comprise one or more of the following: expanded graphite; expandable graphite; natural graphite; or synthetic graphite.
Fluid-connection adapter which, for the fluid connection of a pipe to a hose nozzle , has an elastomer body which can be pushed onto the hose nozzle , the elastomer body comprising an inner ring configured to be pushed onto the hose nozzle , an outer ring arranged concentrically with respect to the inner ring , and a connecting web connecting the inner ring and the outer ring to one another, wherein the inner ring , the outer ring and the connecting web jointly delimit a pipe receptacle for receiving a pipe end of the pipe , characterised in that , for the equalisation of pressure when the pipe is introduced into the pipe receptacle , an air passage opening closed at the rim extends completely through the outer ring and/or the connecting web and/or at least one pressure equalisation channel is formed in the outer ring and/or the inner ring , the pressure equalisation channel extending in the axial direction and extending through an end face of the outer ring or of the inner ring on the side facing away from the connecting web .
A method of dispensing a liquid or aerosol to maintain a clog free capillary system , comprising: supplying a liquid formulation from a pumping unit to a capillary of an aerosol generator unit at a flow rate; vaporizing at least a portion of the liquid formulation within the capillary of the aerosol generator unit ; and periodically increasing the flow rate from a first flow rate to a second flow rate. supplying a liquid formulation from a pumping unit to a capillary of an aerosol generator unit at a flow rate; vaporizing at least a portion of the liquid formulation within the capillary of the aerosol generator unit ; and periodically increasing the flow rate from a first flow rate to a second flow rate.
A method for operating a receiverless device positioning, the method comprising: receiving, by a processor , a first request corresponding to a first location ; registering data associated with the first request; receiving a second request at a second location , the first location is different than the second location; characterised by : comparing the first and second location, and time between the first request and the second request; and allowing the second request based at least in part on the comparison. receiving, by a processor , a first request corresponding to a first location ; registering data associated with the first request; receiving a second request at a second location , the first location is different than the second location; characterised by : comparing the first and second location, and time between the first request and the second request; and allowing the second request based at least in part on the comparison. comparing the first and second location, and time between the first request and the second request; and allowing the second request based at least in part on the comparison.
A composition for use in protecting bicycle or motorbike chains from dirt comprising from 30 to 90% by weight of water; from 5 to 65% by weight of wax selected from microcrystalline wax, paraffin and mixtures thereof; and from 0.005 to 10% by weight of graphene.
A thermoplastic resin composition, comprising: 100 parts by weight of a base resin comprising 10 to 50 % by weight of an acrylate-aromatic vinyl compound-vinyl cyanide compound graft copolymer (A-1) containing acrylate rubber having an average particle diameter of 0.3 to 0.5 μm, 5 to 40 % by weight of an acrylate-aromatic vinyl compound-vinyl cyanide compound graft copolymer (A-2) containing acrylate rubber having an average particle diameter of 0.05 μm or more and less than 0.3 μm, and 20 to 65 % by weight of an aromatic vinyl polymer (B); and 6 to 12 parts by weight of a polyamide (C), wherein the thermoplastic resin composition has a solvent resistance of 15 days or more, wherein the solvent resistance is measured as time when a crack occurs in a solvent consisting of 98 % by weight of water, 1 % by weight of citric acid, and 1 % by weight of malic acid, wherein the weight content of the general-diameter ASA resin (A-1) is greater than that of the small-diameter ASA resin (A-2), and wherein the average particle diameter is measured by dynamic light scattering. 100 parts by weight of a base resin comprising 10 to 50 % by weight of an acrylate-aromatic vinyl compound-vinyl cyanide compound graft copolymer (A-1) containing acrylate rubber having an average particle diameter of 0.3 to 0.5 μm, 5 to 40 % by weight of an acrylate-aromatic vinyl compound-vinyl cyanide compound graft copolymer (A-2) containing acrylate rubber having an average particle diameter of 0.05 μm or more and less than 0.3 μm, and 20 to 65 % by weight of an aromatic vinyl polymer (B); and 6 to 12 parts by weight of a polyamide (C), wherein the thermoplastic resin composition has a solvent resistance of 15 days or more, wherein the solvent resistance is measured as time when a crack occurs in a solvent consisting of 98 % by weight of water, 1 % by weight of citric acid, and 1 % by weight of malic acid, wherein the weight content of the general-diameter ASA resin (A-1) is greater than that of the small-diameter ASA resin (A-2), and wherein the average particle diameter is measured by dynamic light scattering.
A turbomachine liner manufacturing method characterised by : scanning a second surface of a liner to help determining appropriate areas of the liner for machining apertures ; machining apertures in the liner from a first, opposite surface of the liner ; with positioning the apertures within the liner based on the scanning. scanning a second surface of a liner to help determining appropriate areas of the liner for machining apertures ; machining apertures in the liner from a first, opposite surface of the liner ; with positioning the apertures within the liner based on the scanning.
A heater member comprising: a support that is made of an organic polymer and has a sheet shape; a heating element that is a transparent conductive film made of a polycrystalline material containing indium oxide as a main component, the heating element being in contact with one principal surface of the support; and at least one pair of power supply electrodes in contact with one principal surface of the heating element, wherein the heating element has a sheet resistance in a range from 10 to 150 Ω/sq, the heating element has a thickness of more than 20 nm and not more than 200 nm, and an internal stress of the heating element as measured by an X-ray stress measurement method is 500 MPa or less. a support that is made of an organic polymer and has a sheet shape; a heating element that is a transparent conductive film made of a polycrystalline material containing indium oxide as a main component, the heating element being in contact with one principal surface of the support; and at least one pair of power supply electrodes in contact with one principal surface of the heating element, wherein the heating element has a sheet resistance in a range from 10 to 150 Ω/sq, the heating element has a thickness of more than 20 nm and not more than 200 nm, and an internal stress of the heating element as measured by an X-ray stress measurement method is 500 MPa or less.
A double wrap spring having a helical inner winding region and a helical outer winding region , as well as a transition region mechanically connecting the inner winding region to the outer winding region , characterised in that , in the relaxed, non-installed state of the double wrap spring, the winding regions are arranged eccentrically with respect to one another.
Robot lawnmower comprising a base frame , two driving wheels and at least one directional idler wheel , wherein each driving wheel is driven by a respective electric motor , each motor comprises a pinion , wherein the rotation axis (X1) of the pinion coincides with the rotation axis of the crankshaft of the motor , wherein the motor is fixed to a bracket to which the driving wheel is rotatably fixed, wherein the rotation axis (X1) of the pinion is parallel to the rotation axis (X2) of the driving wheel , characterized in that the pinion meshes with a crown gear of the driving wheel , the rotation axis (X1) of the pinion is distinct from the rotation axis (X2) of the driving wheel , the motor being off-axis with respect to the driving wheel . wherein the bracket extends upwards so that the motor is mounted in a high position of the bracket , extending inwards, above the base frame , above a recess of the base frame in which a cutting deck is housed. each motor comprises a pinion , wherein the rotation axis (X1) of the pinion coincides with the rotation axis of the crankshaft of the motor , wherein the motor is fixed to a bracket to which the driving wheel is rotatably fixed, wherein the rotation axis (X1) of the pinion is parallel to the rotation axis (X2) of the driving wheel , characterized in that the pinion meshes with a crown gear of the driving wheel , the rotation axis (X1) of the pinion is distinct from the rotation axis (X2) of the driving wheel , the motor being off-axis with respect to the driving wheel . wherein the bracket extends upwards so that the motor is mounted in a high position of the bracket , extending inwards, above the base frame , above a recess of the base frame in which a cutting deck is housed.
A secondary filter element for a filter assembly , comprising a central tube comprising a grid-shaped, fluid-permeable, oval-shaped cross-sectional support section that carries a filter medium and a circumferential sealing means for sealing the secondary filter element with respect to a filter seat for the secondary filter element , wherein the sealing means completely surrounds the secondary filter element ; and wherein the sealing means comprises an outer surface and an inner surface opposing the outer surface ; and wherein the secondary element comprises a radial direction (R) perpendicular to a central axis (MA24) and oriented away from it; and wherein the central axis (MA24) extends parallel to a longitudinal direction (LR24) of the filter element ; wherein the sealing means , when viewed in the longitudinal direction (LR24), features an oval geometry having a center point and two symmetry axes intersecting therein, in particular a long side as the principal axis and a short side as the secondary axis, and wherein the outer surface of the sealing means , when viewed along the short side , projects radially further beyond the filter medium than when viewed along the long side , and wherein the inner surface of the sealing means , when viewed along the short side , projects radially further beyond the inner contour of the central tube than when viewed along the long side . a circumferential sealing means for sealing the secondary filter element with respect to a filter seat for the secondary filter element , wherein the sealing means completely surrounds the secondary filter element ; and wherein the sealing means comprises an outer surface and an inner surface opposing the outer surface ; and wherein the secondary element comprises a radial direction (R) perpendicular to a central axis (MA24) and oriented away from it; and wherein the central axis (MA24) extends parallel to a longitudinal direction (LR24) of the filter element ; wherein the sealing means , when viewed in the longitudinal direction (LR24), features an oval geometry having a center point and two symmetry axes intersecting therein, in particular a long side as the principal axis and a short side as the secondary axis, and wherein the outer surface of the sealing means , when viewed along the short side , projects radially further beyond the filter medium than when viewed along the long side , and wherein the inner surface of the sealing means , when viewed along the short side , projects radially further beyond the inner contour of the central tube than when viewed along the long side .
A payload system releasable from an aircraft, the payload system comprising: a payload having a forward portion releasably coupled to the aircraft and an aft portion releasably coupled to the aircraft; a pivot assembly secured to the aft portion of the payload to facilitate release of the payload from an aircraft, the pivot assembly comprising: a mount device secured to an aft portion of the payload; a shaft rotationally coupled to the mount device, and rotatable about multiple shaft axes relative to the mount device; and a release component interfaced with the shaft and removably coupleable to the aircraft, wherein, in response to release of the forward portion of the payload from the aircraft, the shaft is arranged to move in multiple degrees of freedom about multiple axes and along a longitudinal axis of the shaft as the payload transitions from a carriage phase to a jettison phase, whereby the assembly is configured to either minimize or eliminate carriage loads about the aft portion of the payload. a payload having a forward portion releasably coupled to the aircraft and an aft portion releasably coupled to the aircraft; a pivot assembly secured to the aft portion of the payload to facilitate release of the payload from an aircraft, the pivot assembly comprising: a mount device secured to an aft portion of the payload; a shaft rotationally coupled to the mount device, and rotatable about multiple shaft axes relative to the mount device; and a release component interfaced with the shaft and removably coupleable to the aircraft, wherein, in response to release of the forward portion of the payload from the aircraft, the shaft is arranged to move in multiple degrees of freedom about multiple axes and along a longitudinal axis of the shaft as the payload transitions from a carriage phase to a jettison phase, whereby the assembly is configured to either minimize or eliminate carriage loads about the aft portion of the payload. a mount device secured to an aft portion of the payload; a shaft rotationally coupled to the mount device, and rotatable about multiple shaft axes relative to the mount device; and a release component interfaced with the shaft and removably coupleable to the aircraft, wherein, in response to release of the forward portion of the payload from the aircraft, the shaft is arranged to move in multiple degrees of freedom about multiple axes and along a longitudinal axis of the shaft as the payload transitions from a carriage phase to a jettison phase, whereby the assembly is configured to either minimize or eliminate carriage loads about the aft portion of the payload.
Charge changing control device for a reciprocating engine, comprising at least one cam follower configured for being pivotably actuated around a pivot axis (P) upon rotational movement of a camshaft , and an adjustment unit configured for setting at least three different charge-changing modes of the device by translationally displacing the pivot axis (P) relative to a rotational axis (R) of the camshaft , characterized in that the device is configured to set the different charge-changing modes as a function of a knocking characteristic or an exhaust gas temperature of the engine such that the device switches a charge-changing mode when the knocking characteristic or the exhaust gas temperature has reached a predefined threshold value.
An apparatus , comprising: a polymer spray head configured to direct a plurality of polymeric fibers in an upward direction and levitate a product portion in a polymer enrobing zone above said polymer spray head ; and at least one guide configured to help retain the levitated product portion in the polymer enrobing zone, the guide including, a first air knife and a second air knife , the first air knife and the second air knife being located on opposite sides of the polymer enrobing zone , and a first guide structure and a second guide structure , the first guide structure and the second guide structure being located on opposite sides of the polymer enrobing zone . a polymer spray head configured to direct a plurality of polymeric fibers in an upward direction and levitate a product portion in a polymer enrobing zone above said polymer spray head ; and at least one guide configured to help retain the levitated product portion in the polymer enrobing zone, the guide including, a first air knife and a second air knife , the first air knife and the second air knife being located on opposite sides of the polymer enrobing zone , and a first guide structure and a second guide structure , the first guide structure and the second guide structure being located on opposite sides of the polymer enrobing zone . a first air knife and a second air knife , the first air knife and the second air knife being located on opposite sides of the polymer enrobing zone , and a first guide structure and a second guide structure , the first guide structure and the second guide structure being located on opposite sides of the polymer enrobing zone .
A method for remotely controlling a function of a slave portable terminal , the method comprising: receiving , by a slave portable terminal , a message from a master terminal ; determining, by the slave portable terminal , whether the received message is a message for a remote control function; identifying, if the received message is the message for the remote control function, information which is included in the received message, the information comprising an authentication password and information regarding a type of the remote control function; authenticating the received message by comparing a password stored in the slave portable terminal with the authentication password included in the received message; setting up the remote control function to make the slave portable terminal be remotely controlled by the master terminal after an authentication of the received message is successful; detecting an event associated with the remote control function; and performing the remote control function in response to the detecting of the event, wherein the type of the remote control function comprises at least one of a call barring function and a forwarding function. receiving , by a slave portable terminal , a message from a master terminal ; determining, by the slave portable terminal , whether the received message is a message for a remote control function; identifying, if the received message is the message for the remote control function, information which is included in the received message, the information comprising an authentication password and information regarding a type of the remote control function; authenticating the received message by comparing a password stored in the slave portable terminal with the authentication password included in the received message; setting up the remote control function to make the slave portable terminal be remotely controlled by the master terminal after an authentication of the received message is successful; detecting an event associated with the remote control function; and performing the remote control function in response to the detecting of the event, wherein the type of the remote control function comprises at least one of a call barring function and a forwarding function.
A printing control method, comprising: acquiring first scan times, which is the printing times of shuttle scan when the inkjet head ejects a first ink to print a thc unit area on the printing medium; acquiring second scan times, which is the printing times of shuttle scan when the inkjet head ejects a the second ink to print the unit area on the printing medium; comparing the first scan times with the second scan times; according to the comparison result, controlling the printer to eject the first ink or/and the second ink in each scan in the main scan direction, comprising: according to the comparison result, performing filtering process on image data corresponding to the first ink or/and image data corresponding to the second ink to obtain first printing data corresponding to the first ink and second printing data corresponding to the second ink, making the same of the scan times of printing a unit area according to the first printing data and the scan times of printing a unit area according to the second printing data; according to the first printing data and the second printing data, controlling the printer to eject first ink and second ink in each scan in the main scan direction; wherein one of the first ink and the second ink is white ink. acquiring first scan times, which is the printing times of shuttle scan when the inkjet head ejects a first ink to print a thc unit area on the printing medium; acquiring second scan times, which is the printing times of shuttle scan when the inkjet head ejects a the second ink to print the unit area on the printing medium; comparing the first scan times with the second scan times; according to the comparison result, controlling the printer to eject the first ink or/and the second ink in each scan in the main scan direction, comprising: according to the comparison result, performing filtering process on image data corresponding to the first ink or/and image data corresponding to the second ink to obtain first printing data corresponding to the first ink and second printing data corresponding to the second ink, making the same of the scan times of printing a unit area according to the first printing data and the scan times of printing a unit area according to the second printing data; according to the first printing data and the second printing data, controlling the printer to eject first ink and second ink in each scan in the main scan direction; wherein one of the first ink and the second ink is white ink.