mhurhangee/ep-ind-claims huggingface dataset:
Identity card, comprising: a card body (101, 121); a physical unclonable function (103, 123) arranged within the card body (101, 121), wherein the physical unclonable function (103, 123) comprises a first arrangement of light reflecting elements (105, 125) being arranged in a first card body area (107, 127), and a second arrangement of light reflecting elements (109, 129) being arranged in a second card body area (111, 131), and wherein the first arrangement of light reflecting elements (105, 125) has a higher light reflectivity than the second arrangement of light reflecting elements (109, 129); characterised in that the identity card further comprises: a light source for emitting light towards the first arrangement of light reflecting elements (105, 125) and the second arrangement of light reflecting elements (109, 129); and an optical sensor for sensing light reflected from the first arrangement of light reflecting elements (105, 125) and the second arrangement of light reflecting elements (109, 129). a card body (101, 121); a physical unclonable function (103, 123) arranged within the card body (101, 121), wherein the physical unclonable function (103, 123) comprises a first arrangement of light reflecting elements (105, 125) being arranged in a first card body area (107, 127), and a second arrangement of light reflecting elements (109, 129) being arranged in a second card body area (111, 131), and wherein the first arrangement of light reflecting elements (105, 125) has a higher light reflectivity than the second arrangement of light reflecting elements (109, 129); characterised in that the identity card further comprises: a light source for emitting light towards the first arrangement of light reflecting elements (105, 125) and the second arrangement of light reflecting elements (109, 129); and an optical sensor for sensing light reflected from the first arrangement of light reflecting elements (105, 125) and the second arrangement of light reflecting elements (109, 129). a light source for emitting light towards the first arrangement of light reflecting elements (105, 125) and the second arrangement of light reflecting elements (109, 129); and an optical sensor for sensing light reflected from the first arrangement of light reflecting elements (105, 125) and the second arrangement of light reflecting elements (109, 129).
Method for predictive determination of at least one characteristic power necessary for performing a predetermined manoeuvre of a rotary-wing aircraft, said aircraft comprising a power installation, a plurality of sensors, at least one calculator, at least one memory and at least one display device, said method comprising the following main steps: - a first measurement of a current atmospheric pressure Pc and a current temperature Tc outside said aircraft at a current altitude Zc of said aircraft, - a first determination of at least one parameter relating either to said current altitude Zc of said aircraft, or to a predictive altitude Zp for performing said predetermined manoeuvre of said aircraft, or to said current altitude Zc of said aircraft and to said predictive altitude Zp for performing said predetermined manoeuvre of said aircraft, - a second determination of a predictive atmospheric pressure Pp at said predictive altitude Zp, - a third determination of a predictive temperature Tp at said predictive altitude Zp, - a fourth determination of a maximum power available from said power installation at said predictive altitude Zp, taking into account said predictive atmospheric pressure Pp and said predictive temperature Tp, - a fifth determination of at least one characteristic power of said power installation necessary for performing said predetermined manoeuvre of said aircraft. - a first measurement of a current atmospheric pressure Pc and a current temperature Tc outside said aircraft at a current altitude Zc of said aircraft, - a first determination of at least one parameter relating either to said current altitude Zc of said aircraft, or to a predictive altitude Zp for performing said predetermined manoeuvre of said aircraft, or to said current altitude Zc of said aircraft and to said predictive altitude Zp for performing said predetermined manoeuvre of said aircraft, - a second determination of a predictive atmospheric pressure Pp at said predictive altitude Zp, - a third determination of a predictive temperature Tp at said predictive altitude Zp, - a fourth determination of a maximum power available from said power installation at said predictive altitude Zp, taking into account said predictive atmospheric pressure Pp and said predictive temperature Tp, - a fifth determination of at least one characteristic power of said power installation necessary for performing said predetermined manoeuvre of said aircraft.
A passive wireless transponder configured to communicate with a backscattering principle to provide radio frequency identification (RFID) features, comprising an antenna, a rectifier to convert a received radio frequency power into a direct current, an oscillator adapted to generate a modulation frequency and an internal clock, a demodulator adapted to demodulate a received RFID signal, a digital control part adapted to process a received RFID interrogating command and to output a digital response, a modulator adapted to generate a modulated backscattered signal carrying the digital response, and a sensing element for sensing a predetermined variable, wherein the modulated backscattered signal carries a digital response comprises sidebands that are offset from an interrogation frequency by a modulation frequency outputted from the oscillator, characterized in that the oscillator is based on a resonator, and the sensing element is connected to the oscillator to load the oscillator, and the modulation frequency outputted from the oscillator, namely the offset of the sidebands of the modulated backscattered signal from the oscillation frequency is dependent on and carry a sensed value of the predetermined variable.
Use of a composite component composed of a plastics-fibre composite material, having at least two plies of fibre-reinforced material, wherein, between the at least two plies of fibre-reinforced material, there is inlaid at least one electrical line, wherein the electrical line is part of a ply of metal cords that can be connected to electrical terminals, wherein the metal cords form a bidirectional metal laid fabric, such that the elasticity of the composite component is increased in at least two directions, characterized in that a part of the metal laid fabric is used not only for its reinforcement task but also as an electrical line, wherein the electrical terminals are integrated in the composite component, or the electrical terminals project in the form of electrical lines out of the composite component.
A high water oral care composition comprising an orally acceptable carrier, zinc phosphate, stannous fluoride, and an anionic polymer, wherein the amount of the water is 15% - 30% by weight and wherein the zinc phosphate is present in an amount of from 0.05 to 4% by weight, relative to the weight of the oral care composition, wherein the amount of the stannous fluoride is from 0.01% to 5% by weight; and wherein the anionic polymer is a methyl vinyl ether/maleic anhydride or acid copolymer having an average molecular weight (M.W.) of about 30,000 to about 1,000,000.
A method for establishing an inter-radio frequency subsystem interface, ISSI, group call through a hosted ISSI function, HIF, and between a home radio frequency subsystem, RFSS, and at least one serving radio frequency subsystem, the method comprising: maintaining, at the HIF, a list of affiliated RFSSs, wherein the list identifies the at least one serving RFSS; transmitting an affiliation request, from the HIF to the home RFSS, wherein the home RFSS is a home RFSS of a group; receiving, at the HIF from the serving RFSS, a request to initiate an inter-RFSS group call to the group using HIF addressing; transmitting, from the HIF to the home RFSS, a request to initiate the inter-RFSS group call using serving RFSS addressing; receiving, at the HIF, a data packet from the home RFSS or the serving RFSS; and transmitting, from the HIF to the serving RFSS, a copy of the data packet if the data packet was received from the home RFSS; otherwise, transmitting, from the HIF to the home RFSS, a copy of the data packet if the data packet was received from the serving RFSS. maintaining, at the HIF, a list of affiliated RFSSs, wherein the list identifies the at least one serving RFSS; transmitting an affiliation request, from the HIF to the home RFSS, wherein the home RFSS is a home RFSS of a group; receiving, at the HIF from the serving RFSS, a request to initiate an inter-RFSS group call to the group using HIF addressing; transmitting, from the HIF to the home RFSS, a request to initiate the inter-RFSS group call using serving RFSS addressing; receiving, at the HIF, a data packet from the home RFSS or the serving RFSS; and transmitting, from the HIF to the serving RFSS, a copy of the data packet if the data packet was received from the home RFSS; otherwise, transmitting, from the HIF to the home RFSS, a copy of the data packet if the data packet was received from the serving RFSS.
A drain fitting for a bath- or shower tub, which operates without sealing water, with a housing comprising an inlet opening and an outlet opening and with an odor trap formed as a mechanical valve with at least one sealing lip (12, 13), characterized in that an essentially annular drain channel is arranged after the inlet opening, which comprises a circumferential exit opening, which is sealed by the at least one sealing lip (12, 13), in that the exit opening opens in an annular space, which is open laterally towards an additional exit opening, and in that the at least one sealing lip (12, 13) is resiliently biased.
A payload including a gimbal assembly and associated gyro assembly, comprising a gyro assembly control associated with said gyro assembly and operable to trigger the gyro assembly to obtain deviation measurements in the azimuth plane and elevation plane and process the measurements in a first dynamic range corresponding to a first rotation rate range, for stabilizing the payload utilizing said gimbal assembly; characterised by the gyro assembly control being operable to trigger the gyro assembly to obtain instantaneous measurements from an elevation rate gyro and process the measurements in a second dynamic range corresponding to a second rotation rate range having more sensitivity than said first dynamic range, for finding deviation of the payload from the north of the earth.
A metallic-composite joint fitting, comprising: a frustoconical internal bearing having a bore; a conical sleeve configured to be disposed about the frustoconical internal bearing; a composite structure configured to couple between the frustoconical internal bearing and the conical sleeve; a metallic end fitting configured to be disposed within the bore and couple to the frustoconical internal bearing; and an external nut configured to couple to the metallic end fitting and the conical sleeve, wherein at least one of the frustoconical internal bearing or the conical sleeve comprises a flanged portion, and characterized by a locking ring; wherein the conical sleeve and the frustoconical internal bearing are coupled at the flanged portion via the locking ring. a frustoconical internal bearing having a bore; a conical sleeve configured to be disposed about the frustoconical internal bearing; a composite structure configured to couple between the frustoconical internal bearing and the conical sleeve; a metallic end fitting configured to be disposed within the bore and couple to the frustoconical internal bearing; and an external nut configured to couple to the metallic end fitting and the conical sleeve, wherein at least one of the frustoconical internal bearing or the conical sleeve comprises a flanged portion, and characterized by a locking ring; wherein the conical sleeve and the frustoconical internal bearing are coupled at the flanged portion via the locking ring.
A method of route directing performed in an unmanned aerial vehicle, the unmanned aerial vehicle comprising a communication module for wireless communication with an access node (2a, 2b) of a communications system, characterized by the method comprising: - receiving, from a network entity, warning signaling about a restricted area, and - withdrawing from the restricted area in response to receiving the warning signaling, by receiving, from the network entity, signaling comprising route directions to a destination along a route excluding the restricted area. - receiving, from a network entity, warning signaling about a restricted area, and - withdrawing from the restricted area in response to receiving the warning signaling, by receiving, from the network entity, signaling comprising route directions to a destination along a route excluding the restricted area.
Hardware part for windows or doors, consisting of at least one first and one second hardware part (8.3, 21), wherein each hardware part (8.3, 21) is made up of at least one cover rail (23, 24) and a drive bar (25, 26) displaceable relative to the cover rail (23, 24), wherein the drive bars (25, 26) are connected via a coupling device located at the drive bar ends (27, 28), and the coupling device consists of two coupling parts (30, 31), wherein the first coupling part consists of a toothed segment running along a part section, on the longitudinal narrow side of the one drive rod, and the second coupling part consists of a U-shaped coupling shoe of the other drive bar, engaging around the toothed segment with a complementary tooth arrangement, wherein one of the coupling parts (30, 31) recoils in a coupling position relative to the cover rail covering the drive bar, while the second coupling part protrudes over the cover rail, characterized in that the toothed segment has a spacer, dimensioned such that said spacer, supported by the second drive bar or the second coupling part, holds the coupling parts (30, 31) out of engagement, wherein the spacer has no effect in a potential coupling position.
A bispecific antigen-binding molecule comprising a first antigen-binding domain that specifically binds human CD3, and a second antigen-binding domain that specifically binds human CD20, wherein the first antigen-binding domain comprises a heavy chain variable region (HCVR) comprising complementarity determining regions A1-HCDR1, A1-HCDR2 and A1-HCDR3, and a light chain variable region (LCVR) comprising complementarity determining regions A1-LCDR1, A1-LCDR2 and A1-LCDR3, wherein the complementarity determining regions are contained within a HCVR/LCVR pair comprising the amino acid sequences selected from SEQ ID NOs: 1250/1258, 1266/1274 or 1282/1290, wherein the bispecific antigen-binding molecule induces proliferation of human and cynomolgous peripheral blood mononuclear cells in vitro.
A hub for a heavy-duty vehicle and for mounting a wheel for relative rotation, the hub comprising: a substantially cylindrical body having axially opposite end portions and a longitudinal central axis, the cylindrical body defining a lubrication chamber; a pair of bearing-receiving bores (124,126) formed in the cylindrical body, each one of the pair of bearing-receiving bores being located at a respective axially opposite end portion of the cylindrical body; a flange extending radially outward from the cylindrical body at a location between the pair of bearing-receiving bores (124,126) in the cylindrical body; a barrel portion of the cylindrical body extending between the flange and one of the pair of bearing-receiving bores, the barrel portion having an outer diameter; a plurality of circumferentially-spaced wheel mounting pilots extending axially from the flange and spaced from the barrel portion of the cylindrical body; and a reservoir channel formed in the cylindrical body extending from the lubrication chamber and at least partially located radially inward of the flange, the reservoir channel having an inner diameter greater than an outer diameter of the barrel portion of the cylindrical body. a substantially cylindrical body having axially opposite end portions and a longitudinal central axis, the cylindrical body defining a lubrication chamber; a pair of bearing-receiving bores (124,126) formed in the cylindrical body, each one of the pair of bearing-receiving bores being located at a respective axially opposite end portion of the cylindrical body; a flange extending radially outward from the cylindrical body at a location between the pair of bearing-receiving bores (124,126) in the cylindrical body; a barrel portion of the cylindrical body extending between the flange and one of the pair of bearing-receiving bores, the barrel portion having an outer diameter; a plurality of circumferentially-spaced wheel mounting pilots extending axially from the flange and spaced from the barrel portion of the cylindrical body; and a reservoir channel formed in the cylindrical body extending from the lubrication chamber and at least partially located radially inward of the flange, the reservoir channel having an inner diameter greater than an outer diameter of the barrel portion of the cylindrical body.
A communication method for a wireless local area network, applicable to a work station device, comprising: generating a request frame, the request frame comprising identification information, and the identification information being used for instructing the work station device to support receiving a wake up frame (S 102); sending the request frame in order to instruct an access point device to obtain cached downlink data according to the wake up frame, wherein the access point is supporting sending a wake up frame to indicate whether there is cached downlink data; and receiving a management frame in which Traffic Indication Map, TIM, identification information is set, wherein the TIM identification information corresponding to the work station device supporting receiving a wake up frame is set to "0" or no setting is made thereto, and the management frame is a beacon frame. generating a request frame, the request frame comprising identification information, and the identification information being used for instructing the work station device to support receiving a wake up frame (S 102); sending the request frame in order to instruct an access point device to obtain cached downlink data according to the wake up frame, wherein the access point is supporting sending a wake up frame to indicate whether there is cached downlink data; and receiving a management frame in which Traffic Indication Map, TIM, identification information is set, wherein the TIM identification information corresponding to the work station device supporting receiving a wake up frame is set to "0" or no setting is made thereto, and the management frame is a beacon frame.
A radiance source comprising: a housing comprising an interior wall forming a single chamber, wherein substantially all of the interior wall is spherical such as to enclose an interior volume, and an exit port; a light source disposed within the interior volume of the housing and supported from the interior wall of the housing, wherein the exit port and the light source lie on a symmetry diameter of the spherical interior wall; a baffle structure disposed to block and reflect a light ray that would otherwise travel directly from the light source to the exit port without reflecting from the interior wall, wherein the baffle structure comprises: a body having a curved back surface facing the light source and acting as a baffle and a curved front surface facing the exit port and acting as a calibration target, wherein a radius of curvature of the curved back surface is larger than a radius of curvature of the curved front surface so as to define a minimum thickness of the baffle structure of 0.5 cm (0.2 inches) or greater; and a support positioning the body relative to the exit port and to the light source; and an optically diffuse reflecting surface comprising pressed, cast, and machined polytetrafluoroethylene on at least: the spherical portion of the interior wall of the housing, the back surface of the body, and the front surface of the body. a housing comprising an interior wall forming a single chamber, wherein substantially all of the interior wall is spherical such as to enclose an interior volume, and an exit port; a light source disposed within the interior volume of the housing and supported from the interior wall of the housing, wherein the exit port and the light source lie on a symmetry diameter of the spherical interior wall; a baffle structure disposed to block and reflect a light ray that would otherwise travel directly from the light source to the exit port without reflecting from the interior wall, wherein the baffle structure comprises: a body having a curved back surface facing the light source and acting as a baffle and a curved front surface facing the exit port and acting as a calibration target, wherein a radius of curvature of the curved back surface is larger than a radius of curvature of the curved front surface so as to define a minimum thickness of the baffle structure of 0.5 cm (0.2 inches) or greater; and a support positioning the body relative to the exit port and to the light source; and an optically diffuse reflecting surface comprising pressed, cast, and machined polytetrafluoroethylene on at least: the spherical portion of the interior wall of the housing, the back surface of the body, and the front surface of the body. the spherical portion of the interior wall of the housing, the back surface of the body, and the front surface of the body.
A power tool, in which a predetermined elongate detachably coupled tool bit is linearly driven to perform a predetermined operation, comprising a tool body, a motor that is housed within the tool body and disposed such that an extension of a motor output shaft extends transversely to an axis of the tool bit, a striking part that is housed within a front region of the tool body and strikes the tool bit, a motion converting part that is disposed above the motor and converts an output of rotating the motor output shaft when the motor is driven, into an output of striking the tool bit by the striking part, a first cooling air passage that is provided within the tool body and through which cooling air can be led to the motor, a second cooling air passage that is provided within the tool body and through which cooling air can be led to the striking part, wherein the first and second cooling air passages are hermetically formed by a partition wall which is disposed within the tool body, wherein the first cooling air passage is formed between a second inlet and a second outlet, and wherein the second cooling air passage is formed between a first inlet and a first outlet, characterised by a motor cooling fan that is disposed below the motor and connected to a lower part of the motor output shaft and activated to supply cooling air to the first cooling air passage when the motor is driven and disposed downstream of the first cooling air passage, and a striking part cooling fan that is disposed between the motor and the motion converting part and connected to an upper part of the motor output shaft and activated to supply cooling air to the second cooling air passage when the motor is driven and disposed downstream of the second cooling air passage, wherein the striking part and the motor are cooled by cooling air which is produced by induced cooling fans.