mhurhangee/patent-ind-claim-en huggingface dataset:
A negative electrode current collector , comprising a polymer material-based support layer and a copper-based conductive layer disposed on at least one surface of the support layer , wherein a thickness D 1 of the copper-based conductive layer , a tensile strength T of the support layer , and a thickness D 2 of the support layer satisfy a relational formula 1, 0 .1 ≤ 300 × D 1 / T × D 2 ≤ 0.3 in the formula 1, D 1 and D 2 are in the same unit, and T is in MPa; and in case of the negative electrode current collector where the copper-based conductive layers are disposed on two opposite surfaces of the support layer , the "thickness D 1 of the copper-based conductive layer " refers to average thickness of the copper-based conductive layers on both sides of the support layer ; and the tensile strength T of the support layer satisfies 150 MPa ≤ T ≤ 300 MPa; and the thickness D 2 of the support layer satisfies 1 μm ≤ D 2 ≤ 20 μm, the thickness D 1 of the copper-based conductive layer satisfies 300 nm ≤ D 1 ≤ 2 μm, and the negative electrode current collector further comprising a protective layer ; and the protective layer is disposed between the copper-based conductive layer and the support layer , and/or, the protective layer is disposed on a surface of the copper-based conductive layer away from the support layer . wherein a thickness D 1 of the copper-based conductive layer , a tensile strength T of the support layer , and a thickness D 2 of the support layer satisfy a relational formula 1, 0 .1 ≤ 300 × D 1 / T × D 2 ≤ 0.3 in the formula 1, D 1 and D 2 are in the same unit, and T is in MPa; and in case of the negative electrode current collector where the copper-based conductive layers are disposed on two opposite surfaces of the support layer , the "thickness D 1 of the copper-based conductive layer " refers to average thickness of the copper-based conductive layers on both sides of the support layer ; and the tensile strength T of the support layer satisfies 150 MPa ≤ T ≤ 300 MPa; and the thickness D 2 of the support layer satisfies 1 μm ≤ D 2 ≤ 20 μm, the thickness D 1 of the copper-based conductive layer satisfies 300 nm ≤ D 1 ≤ 2 μm, and the negative electrode current collector further comprising a protective layer ; and the protective layer is disposed between the copper-based conductive layer and the support layer , and/or, the protective layer is disposed on a surface of the copper-based conductive layer away from the support layer .
A power generation system comprising: a first fuel cell; a second fuel cell; and a controller configured to control the first fuel cell, wherein the controller is configured to supply heat generated from power generation by the first fuel cell to the second fuel cell; monitor the power generated by the second fuel cell; and control the amount of heat supplied from the first fuel cell to the second fuel cell based on the amount of power generated by the second fuel cell. a first fuel cell; a second fuel cell; and a controller configured to control the first fuel cell, wherein the controller is configured to supply heat generated from power generation by the first fuel cell to the second fuel cell; monitor the power generated by the second fuel cell; and control the amount of heat supplied from the first fuel cell to the second fuel cell based on the amount of power generated by the second fuel cell.
A method of operating a Vertical Take-Off and Landing, VTOL, aircraft (104; 900), the method comprising: deploying a retractable propulsor assembly from a compartment of a fuselage of the VTOL aircraft to provide lift for vertical flight, wherein the retractable propulsor assembly comprises: an arm having a first end rotatably coupled to the fuselage ; a propulsor disposed at a second end of the arm and a drive mechanism configured to deploy the arm ; transitioning the VTOL aircraft from the vertical flight to cruise flight; and stowing the retractable propulsor assembly in the compartment during the cruise flight to reduce aerodynamic drag on the VTOL aircraft, wherein deploying the retractable propulsor assembly comprises: in case where the drive mechanism configured to deploy the arm has failed or is inoperable, disengaging the first end of the arm from the drive mechanism ; and applying a torque to the first end of the arm to deploy the arm and the propulsor from the compartment independently of the drive mechanism . deploying a retractable propulsor assembly from a compartment of a fuselage of the VTOL aircraft to provide lift for vertical flight, wherein the retractable propulsor assembly comprises: an arm having a first end rotatably coupled to the fuselage ; a propulsor disposed at a second end of the arm and a drive mechanism configured to deploy the arm ; transitioning the VTOL aircraft from the vertical flight to cruise flight; and stowing the retractable propulsor assembly in the compartment during the cruise flight to reduce aerodynamic drag on the VTOL aircraft, wherein deploying the retractable propulsor assembly comprises: in case where the drive mechanism configured to deploy the arm has failed or is inoperable, disengaging the first end of the arm from the drive mechanism ; and applying a torque to the first end of the arm to deploy the arm and the propulsor from the compartment independently of the drive mechanism . in case where the drive mechanism configured to deploy the arm has failed or is inoperable, disengaging the first end of the arm from the drive mechanism ; and applying a torque to the first end of the arm to deploy the arm and the propulsor from the compartment independently of the drive mechanism .
A method of detecting disease in a mammal during milking, comprising positioning an electrical probe within milk to be tested, delivering current to said probe at a frequency of greater than 60 megahertz, measuring a shift in phase angle between voltage and current signals that results from the milk while AC current is applied to said probe.
Apparatus for ultrasonic welding of at least two material webs comprising a processing sonotrode which can be excited with an ultrasonic vibration, a processing counterpart tool and a material web guide which is so designed that the material web can be passed through between the processing sonotrode and the processing counterpart tool, in which there is provided a device for heating at least one material web prior to the welding operation, wherein the device for preheating at least one material web has a preheating sonotrode which can be excited with an ultrasonic vibration, characterized in that the processing sonotrode has a welding surface with a welding surface width a and the preheating sonotrode has a welding surface with a welding surface width b, wherein b is greater than a, wherein b is preferably greater by more than 50% and at best b is approximately twice as great as a.
A process for preparing a whey-protein coated substrate film for packaging, comprising the following steps: a) providing a coating composition comprising a water solution of whey protein, which has at least 40% in its native state, the whey protein being selected from the group consisting of a whey protein isolate, a whey protein concentrate, and a mixture thereof; and b) applying directly the coating composition of step a) onto a substrate film in order to obtain a coated substrate film wherein the coating has at least 40% of the whey protein in its native state; and c) drying it at a temperature between 60-160 °C. a) providing a coating composition comprising a water solution of whey protein, which has at least 40% in its native state, the whey protein being selected from the group consisting of a whey protein isolate, a whey protein concentrate, and a mixture thereof; and b) applying directly the coating composition of step a) onto a substrate film in order to obtain a coated substrate film wherein the coating has at least 40% of the whey protein in its native state; and c) drying it at a temperature between 60-160 °C.
A sensing device comprising: an output area having an output circuit comprising an integrator adapted to integrate a received current so as to generate an output voltage (Vout) corresponding to the received current; an electrode area for bio-sensing purposes comprising: an electrode comprising an exposed, electrically conductive, surface area and electrode circuitry connected to the exposed surface area, wherein the electrode circuitry comprises a voltage-to-current transducer adapted to produce a wire current (Iwire) corresponding to a voltage present at the exposed surface area; and a connecting wire electrically connecting the electrode circuitry to the output circuit, wherein the current received by the output circuit is the wire current. an output area having an output circuit comprising an integrator adapted to integrate a received current so as to generate an output voltage (Vout) corresponding to the received current; an electrode area for bio-sensing purposes comprising: an electrode comprising an exposed, electrically conductive, surface area and electrode circuitry connected to the exposed surface area, wherein the electrode circuitry comprises a voltage-to-current transducer adapted to produce a wire current (Iwire) corresponding to a voltage present at the exposed surface area; and a connecting wire electrically connecting the electrode circuitry to the output circuit, an electrode comprising an exposed, electrically conductive, surface area and electrode circuitry connected to the exposed surface area, wherein the electrode circuitry comprises a voltage-to-current transducer adapted to produce a wire current (Iwire) corresponding to a voltage present at the exposed surface area; and a connecting wire electrically connecting the electrode circuitry to the output circuit, wherein the current received by the output circuit is the wire current.
Method for transporting a commodity by means of a multidimensional drive which is configured with: - a stator with a first magnetic device for generating a first magnetic field and - a mover which comprises a second magnetic device for generating a second magnetic field for magnetic interaction with the first magnetic field to be generated by the stator and which comprises a carrier and/or a container for a commodity to be transported, and wherein by magnetic interaction the mover can be moved contactless and controllably in relation to the stator , wherein a controlled movement of the mover in an xy plane with a controllable distance to a reference surface is made possible, wherein in the method: - the carrier is used for receiving and carrying the commodity , - at least one parameter representing the state of motion of the carrier and thus the state of motion of the carrier with or without commodity is sensed, - before, during and/or after a transport process of the carrier the mass of the commodity is determined a) from a parameter representing a change of the state of motion of the carrier and/or b) from a parameter representative of a means for reaching and/or maintaining a state of motion of the carrier with or without commodity . - a stator with a first magnetic device for generating a first magnetic field and - a mover which comprises a second magnetic device for generating a second magnetic field for magnetic interaction with the first magnetic field to be generated by the stator and which comprises a carrier and/or a container for a commodity to be transported, - the carrier is used for receiving and carrying the commodity , - at least one parameter representing the state of motion of the carrier and thus the state of motion of the carrier with or without commodity is sensed, - before, during and/or after a transport process of the carrier the mass of the commodity is determined a) from a parameter representing a change of the state of motion of the carrier and/or b) from a parameter representative of a means for reaching and/or maintaining a state of motion of the carrier with or without commodity . a) from a parameter representing a change of the state of motion of the carrier and/or b) from a parameter representative of a means for reaching and/or maintaining a state of motion of the carrier with or without commodity .
A nose cone configured to be mounted to a hub in a turbo machine, said nose cone comprising: a flange extending radially around a central axis and axially from an apex portion of said nose cone to a base portion of said nose cone , said flange forming an annular hub mating surface at said base portion and having an outer surface defining an air flow path; and a plurality of hub mounting elements comprising: one or more flexible spring flanges disposed around the circumference of said base portion , each of said flexible spring flanges forming a flexible spring flange hub engaging surface parallel to and facing in the same direction as said hub mating surface , and configured to provide a biasing force in the axial direction when mounted to the hub; and one or more bayonet flanges disposed around the circumference of said base portion , each of said bayonet flanges forming a bayonet flange hub engaging surface parallel to and facing in the opposite direction as said hub mating surface . a flange extending radially around a central axis and axially from an apex portion of said nose cone to a base portion of said nose cone , said flange forming an annular hub mating surface at said base portion and having an outer surface defining an air flow path; and a plurality of hub mounting elements comprising: one or more flexible spring flanges disposed around the circumference of said base portion , each of said flexible spring flanges forming a flexible spring flange hub engaging surface parallel to and facing in the same direction as said hub mating surface , and configured to provide a biasing force in the axial direction when mounted to the hub; and one or more bayonet flanges disposed around the circumference of said base portion , each of said bayonet flanges forming a bayonet flange hub engaging surface parallel to and facing in the opposite direction as said hub mating surface . one or more flexible spring flanges disposed around the circumference of said base portion , each of said flexible spring flanges forming a flexible spring flange hub engaging surface parallel to and facing in the same direction as said hub mating surface , and configured to provide a biasing force in the axial direction when mounted to the hub; and one or more bayonet flanges disposed around the circumference of said base portion , each of said bayonet flanges forming a bayonet flange hub engaging surface parallel to and facing in the opposite direction as said hub mating surface .
A suture delivery device for percutaneously suturing tissue comprising: an elongated deployment member having a guide member coaxially disposed over a shaft member , the elongated deployment member having a proximal end, a distal end, a needle deployment member carried at a distal end of the elongated deployment member , characterised in that the needle deployment member comprises: a lower band serving as a guide for a plurality of needles and an upper band , in which the lower band is positioned at the distal end of the needle deployment member at a distance from the upper band positioned at the proximal end of the needle deployment member, the distance between the upper band and the lower band adjusting a piercing angle of a plurality of needles in a proximal direction, the plurality of needles being releasably secured to the needle deployment member , in which each needle is routed coaxially within the distal end of the needle deployment member , and a needle pusher configured to releasably secure a non-piercing end of each of the plurality of needles, the needle pusher being driven by a link coaxially disposed within the shaft member , in which the needle pusher is configured to advance each needle through the distal end of the needle deployment member and coaxially over the proximal end of the needle deployment member to position the plurality of needles at the piercing angle in a proximal direction. an elongated deployment member having a guide member coaxially disposed over a shaft member , the elongated deployment member having a proximal end, a distal end, a needle deployment member carried at a distal end of the elongated deployment member , a lower band serving as a guide for a plurality of needles and an upper band , in which the lower band is positioned at the distal end of the needle deployment member at a distance from the upper band positioned at the proximal end of the needle deployment member, the distance between the upper band and the lower band adjusting a piercing angle of a plurality of needles in a proximal direction, the plurality of needles being releasably secured to the needle deployment member , in which each needle is routed coaxially within the distal end of the needle deployment member , and a needle pusher configured to releasably secure a non-piercing end of each of the plurality of needles, the needle pusher being driven by a link coaxially disposed within the shaft member , in which the needle pusher is configured to advance each needle through the distal end of the needle deployment member and coaxially over the proximal end of the needle deployment member to position the plurality of needles at the piercing angle in a proximal direction.
A multidirectional hinged connection system between electrical boxes and their covers or frames comprising: - at least, one bridge connecting the box to its cover or frame, and - articulated anchors for the ends of the bridge , disposed on, at least, one side of the box and of the cover or frame, Where, at least, one of the anchors for each bridge comprises means allowing movement of the bridge in a direction perpendicular to the respective open edge of the box or the frame or cover from an internal position of the bridge during closure to another external opening position, to enable the outward removal of the bridge during the hinged opening of the cover or frame, said system characterised in that said anchors are disposed on the two lateral sides and on the bottom side of the box and of the cover or frame to configure lateral hinged openings in both directions and bottom. wherein the bridges are mounted in the desired hinged position namely right, left or bottom and disassembled for changing the hinging position. - at least, one bridge connecting the box to its cover or frame, and - articulated anchors for the ends of the bridge , disposed on, at least, one side of the box and of the cover or frame,
A method for concentrating, separating and/or isolating a plurality of charged analytes contained in a sample by depletion zone isotachophoresis, in an apparatus comprising at least a main separation channel (C) comprising an electrolyte, the channel (C) comprising a downstream end (D) and an upstream end (U), and a depletion zone formation means (N) placed in or connected to an intermediate region between the upstream end and the downstream end, the method comprising the steps of: (i) introducing the sample into the electrolyte at an upstream channel region adjacent to the upstream end (U), and (ii) forming and/or maintaining an ion depleted zone in the separation channel (C) and adjacent to the depletion zone formation means at a depletion rate (R) using the depletion zone formation means, and (iii) applying an electric field (Ê1) between the downstream end (D) and the upstream end (U) and applying a downstream fluid flow (F), thereby causing focussing and separation of the analytes forming respective focused analyte zones in the separation channel (C) and adjacent to the ion depleted zone, and (iv) optionally detecting the position and/or composition of the focused zones, and (v) adjusting depletion rate (R) and optionally fluid flow (F) to move at least one focussed analyte zone in a upstream and/or downstream direction and/or to position the one or more focussed analyte zones at a desired position in the separation channel (C). (i) introducing the sample into the electrolyte at an upstream channel region adjacent to the upstream end (U), and (ii) forming and/or maintaining an ion depleted zone in the separation channel (C) and adjacent to the depletion zone formation means at a depletion rate (R) using the depletion zone formation means, and (iii) applying an electric field (Ê1) between the downstream end (D) and the upstream end (U) and applying a downstream fluid flow (F), thereby causing focussing and separation of the analytes forming respective focused analyte zones in the separation channel (C) and adjacent to the ion depleted zone, and (iv) optionally detecting the position and/or composition of the focused zones, and (v) adjusting depletion rate (R) and optionally fluid flow (F) to move at least one focussed analyte zone in a upstream and/or downstream direction and/or to position the one or more focussed analyte zones at a desired position in the separation channel (C).
An ophthalmic surgical laser system for creating a corneal flap on a subject's eye (E), comprising: a laser delivery system ; a suction ring configured to overlay an anterior surface of the subject's eye, the suction ring operatively coupled to a patient interface , wherein the patient interface is coupled to the laser delivery system; an imaging system operatively coupled to the laser delivery system and configured to capture a digital image of the subject's eye with the suction ring overlaying the anterior surface of the eye; a computer-readable medium having a set of instructions that, when executed by a processor , identifies an optimum location for creating the corneal flap, wherein the set of instructions comprise: identifying one or more anatomical reference points in digital image captured by the imaging system; generating an overlay on the image that identifies the central location on the cornea to place the suction ring coupled to the patient interface based on the one or more reference points on the cornea; calculating the location of the suction ring coupled to the patient interface relative to the reference points; and identifying a location on the cornea to create the flap based on the location of the suction ring coupled to the patient interface relative to the reference points on the cornea. a laser delivery system ; a suction ring configured to overlay an anterior surface of the subject's eye, the suction ring operatively coupled to a patient interface , wherein the patient interface is coupled to the laser delivery system; an imaging system operatively coupled to the laser delivery system and configured to capture a digital image of the subject's eye with the suction ring overlaying the anterior surface of the eye; a computer-readable medium having a set of instructions that, when executed by a processor , identifies an optimum location for creating the corneal flap, wherein the set of instructions comprise: identifying one or more anatomical reference points in digital image captured by the imaging system; generating an overlay on the image that identifies the central location on the cornea to place the suction ring coupled to the patient interface based on the one or more reference points on the cornea; calculating the location of the suction ring coupled to the patient interface relative to the reference points; and identifying a location on the cornea to create the flap based on the location of the suction ring coupled to the patient interface relative to the reference points on the cornea. identifying one or more anatomical reference points in digital image captured by the imaging system; generating an overlay on the image that identifies the central location on the cornea to place the suction ring coupled to the patient interface based on the one or more reference points on the cornea; calculating the location of the suction ring coupled to the patient interface relative to the reference points; and identifying a location on the cornea to create the flap based on the location of the suction ring coupled to the patient interface relative to the reference points on the cornea.