mhurhangee/patent-ind-claim-en huggingface dataset:
A data cable, comprising a type-A interface and a type-C interface , wherein the type-A interface and the type-C interface are connected by using a cable , the type-A interface and the type-C interface each comprise a VBUS pin, a CC pin, a D+ pin, a D- pin, and a GND pin, and a VBUS pin, a D+ pin, a D- pin, and a GND pin of the type-A interface are connected to a VBUS pin, a D+ pin, a D- pin, and a GND pin of the type-C interface , respectively; a circuit identification module is disposed in the data cable, and the circuit identification module comprises a switch circuit , a filtering circuit , a voltage regulator circuit , and a comparator circuit ; and the switch circuit is connected to the CC pin of the type-C interface , an output terminal of the voltage regulator circuit , and the CC pin of the type-A interface , a control terminal of the switch circuit is connected to an output terminal of the comparator circuit , an input terminal of the voltage regulator circuit is connected to a VBUS cable in the cable , an output terminal of the voltage regulator circuit is further connected to a first input terminal of the comparator circuit , a second input terminal of the comparator circuit is connected to an output terminal of the filtering circuit , and an input terminal of the filtering circuit is connected to the CC pin of the type-A interface ; wherein under the control of the comparator circuit , the switch circuit is configured to connect the CC pin of the type-A interface to the CC pin of the type-C interface , or connect the output terminal of the voltage regulator circuit to the CC pin of the type-C interface . a circuit identification module is disposed in the data cable, and the circuit identification module comprises a switch circuit , a filtering circuit , a voltage regulator circuit , and a comparator circuit ; and the switch circuit is connected to the CC pin of the type-C interface , an output terminal of the voltage regulator circuit , and the CC pin of the type-A interface , a control terminal of the switch circuit is connected to an output terminal of the comparator circuit , an input terminal of the voltage regulator circuit is connected to a VBUS cable in the cable , an output terminal of the voltage regulator circuit is further connected to a first input terminal of the comparator circuit , a second input terminal of the comparator circuit is connected to an output terminal of the filtering circuit , and an input terminal of the filtering circuit is connected to the CC pin of the type-A interface ; wherein under the control of the comparator circuit , the switch circuit is configured to connect the CC pin of the type-A interface to the CC pin of the type-C interface , or connect the output terminal of the voltage regulator circuit to the CC pin of the type-C interface .
A sensor system for recording the position of an elevator car of an elevator installation displaceable along an elevator shaft , the sensor system comprising a tape measure which is disposable vertically to the elevator car , extends along a length (L) in the assembled state and has a position coding formed by a material change and a sensor unit which is disposable on the elevator car and is configured for registering magnetic fields, in particular a stray magnetic field, on the inlet side which are caused or influenced by the position coding and for generating at least one analog signal therefrom on the outlet side, the sensor system comprising a conversion unit for converting the at least one analog signal into a digital signal , characterized in that the sensor system comprises a calibration unit which is configured for changing the digital signal by means of a static and/or dynamic calibration.
A method implemented by computer means, for managing an electronic television programme guide application presented over a time range including a present moment, the method including commanding an on-screen display of a succession ordered in time of thumbnails associated with respective television programmes, the display of the thumbnails being separated into three sections, a section for the thumbnails associated with past programmes, already broadcast (AB) in their entirety during said time range, a section for the thumbnails associated with present programmes, currently being broadcast (CBB), and a section for the thumbnails associated with future programmes whose broadcast has not yet started (L), the method including the following steps for each recurring past and/or future television programme: - identifying (E3) contents associated with this recurring television programme, and - developing (E4) a command for displaying a common thumbnail for all the contents associated with this recurring programme in a presentation of past or future programmes, the display being such that, for the section of thumbnails associated with past programmes and/or for the section of thumbnails associated with future programmes, said common thumbnail is the only thumbnail displayed for this programme in the corresponding section, the method being such that each common thumbnail displays the number of contents (NO) associated with the recurring programme corresponding to this thumbnail. the method including the following steps for each recurring past and/or future television programme: - identifying (E3) contents associated with this recurring television programme, and - developing (E4) a command for displaying a common thumbnail for all the contents associated with this recurring programme in a presentation of past or future programmes, - identifying (E3) contents associated with this recurring television programme, and - developing (E4) a command for displaying a common thumbnail for all the contents associated with this recurring programme in a presentation of past or future programmes, the display being such that, for the section of thumbnails associated with past programmes and/or for the section of thumbnails associated with future programmes, said common thumbnail is the only thumbnail displayed for this programme in the corresponding section, the method being such that each common thumbnail displays the number of contents (NO) associated with the recurring programme corresponding to this thumbnail.
A packer mechanism for an agricultural baler, the mechanism comprising: - a crank shaft , that is rotatable about a central rotation axis , the crank shaft comprising two or more eccentrically placed crank pins , fixed between respective pairs of crank arms (A1-A5), the crank pins comprising two outer ends and a central portion , - a plurality of packer teeth mounted rotatably with respect to the crank pins , - at least one rotary bearing mounted on the central portion of each of the crank pins , for enabling the rotation of the teeth relative to the pins, - a plurality of support rods for controlling the orientation of the packer teeth during rotation of the crank shaft , characterized in that at least one of the crank pins is assembled to one or both of a pair of crank arms by a tapered spline connection, the tapered spline connection comprising: - on at least one of the outer ends of the crank pin : a first angular array of tapered spline features , the spline features comprising at least a portion that tapers downward from a first diameter (D1) to a second diameter (D2) lower than the first diameter, - in at least one of the openings provided on the outer ends of the crank arms : a second angular array of tapered spline features of which at least a portion is tapered and configured to interlock with the first angular array when a pin is inserted into an opening , whereby the tapered portions of the respective spline features are in contact with each other, - mechanical locking features for locking the tapered spline connection. - a crank shaft , that is rotatable about a central rotation axis , the crank shaft comprising two or more eccentrically placed crank pins , fixed between respective pairs of crank arms (A1-A5), the crank pins comprising two outer ends and a central portion , - a plurality of packer teeth mounted rotatably with respect to the crank pins , - at least one rotary bearing mounted on the central portion of each of the crank pins , for enabling the rotation of the teeth relative to the pins, - a plurality of support rods for controlling the orientation of the packer teeth during rotation of the crank shaft , - on at least one of the outer ends of the crank pin : a first angular array of tapered spline features , the spline features comprising at least a portion that tapers downward from a first diameter (D1) to a second diameter (D2) lower than the first diameter, - in at least one of the openings provided on the outer ends of the crank arms : a second angular array of tapered spline features of which at least a portion is tapered and configured to interlock with the first angular array when a pin is inserted into an opening , whereby the tapered portions of the respective spline features are in contact with each other, - mechanical locking features for locking the tapered spline connection.
Rotary coupling arrangement for a coordinate measuring machine, with a slip-ring assembly with a rotor arrangement , which has a shaft element and at least one contact ring , wherein the shaft element is at least partially in the form of a hollow shaft with a hollow interior and a casing wall , wherein the shaft element has a middle section , wherein each contact ring is arranged on the shaft element in the middle section , wherein the middle section has at least one cutout through the casing wall into the interior , wherein each contact ring is connected to a cable element , which is guided through one of the at least one cutout into the interior , wherein the shaft element has a first end section with an outer circumferential cross section for rotationally fixed coupling, wherein the middle section is offset in relation to the first end section by a flange , wherein the flange has an outside diameter which is larger than a smallest outside diameter of the first end section and larger than an outside diameter of the middle section , wherein a smallest outside diameter of the first end section is larger than an outside diameter of the middle section , wherein the outer circumferential cross section of the first end section is formed as a non-circular profile cross section, wherein the shaft element is formed in one piece, and wherein the rotor arrangement has more than one contact ring , and wherein an insulating ring which electrically insulates the adjacent contact rings from one another is arranged in each case between two adjacent contact rings , and wherein the rotary coupling arrangement has furthermore a rotatable coupling assembly , which has a first end and a second end , opposite from the first end, wherein the first end has a coupling interface , and wherein the second end has a slip-ring assembly interface for rotationally fixed coupling to the first end section of the rotor arrangement , and with a rotary position measuring system for determining a rotary position of the rotor arrangement of the slip-ring assembly .
Passenger motor vehicle with a system for heating the vehicle cabin via a heater/air conditioner with a heating system heat exchanger through which the liquid coolant of the engine flows with the waste heat of the liquid-cooled engine and/or the components thereof, wherein the heating system heat exchanger has a soldered heat transfer matrix consisting of coolant-side flat pipes and air-side fins with a plurality of turbulence-generating recesses, so-called "louvres", that follow one another in the air flow direction, characterized in that the heating system heat exchanger has a volume V_Matrix of the heat exchanger matrix around which the heating air flows, a centre-to-centre distance of the air-side fins t_Rippe as well as a centre-to-centre distance of the flat coolant pipes t_Rohr such that the specific heat exchanger volume V_Spec formed therefrom, calculated using the equation V_Spec = V_Matrix / (t_Rohr + (4 * t_Rippe)), exceeds a lower limit value of 0.180 m 2 .
A heat exchanger comprising: • a first section comprising a first set of heat exchange tubes that are arranged substantially horizontally, wherein edges of the first set of heat exchange tubes define a first air-inlet surface (X) ; • a second section comprising a second set of heat exchange tubes , wherein edges of the second set of heat exchange tubes define a second air-inlet surface (Y); • a receiver drier disposed parallel with respect to the first set of heat exchange tubes and adapted to configure fluid communication between the first section and the second section , wherein the first air-inlet surface (X) and the second air-inlet surface (Y) do not overlap when viewed in a direction perpendicular to the first air-inlet surface (X) and when viewed in a direction perpendicular to the second air-inlet surface (Y), characterised in that the first section and the second section are separate cores that are arranged in non-overlapping configuration with respect to each other, each of the first section and the second section is configured with a separate first pair of collectors and and a second pair of collectors and respectively for heat exchange fluid. • a first section comprising a first set of heat exchange tubes that are arranged substantially horizontally, wherein edges of the first set of heat exchange tubes define a first air-inlet surface (X) ; • a second section comprising a second set of heat exchange tubes , wherein edges of the second set of heat exchange tubes define a second air-inlet surface (Y); • a receiver drier disposed parallel with respect to the first set of heat exchange tubes and adapted to configure fluid communication between the first section and the second section , wherein the first air-inlet surface (X) and the second air-inlet surface (Y) do not overlap when viewed in a direction perpendicular to the first air-inlet surface (X) and when viewed in a direction perpendicular to the second air-inlet surface (Y), characterised in that the first section and the second section are separate cores that are arranged in non-overlapping configuration with respect to each other, each of the first section and the second section is configured with a separate first pair of collectors and and a second pair of collectors and respectively for heat exchange fluid.
A method of manufacturing a decorative building board, comprising: ejecting active ray-curable ink from an ink jet recording head onto a building board that includes a base material selected from a metallic base material and a ceramic base material and an ink receiving layer arranged on the base material, the ink receiving layer being non-permeable with respect to the active ray-curable ink, being obtained by curing a resin composition and having an arithmetic average roughness (Ra) specified under JIS B 0601:2001 of from 0.4 μm to 3 μm, to thereby perform printing on the ink receiving layer; and irradiating the active ray-curable ink with an active ray from 2.2 seconds to 30 seconds after the active ray-curable ink lands on the ink receiving layer. ejecting active ray-curable ink from an ink jet recording head onto a building board that includes a base material selected from a metallic base material and a ceramic base material and an ink receiving layer arranged on the base material, the ink receiving layer being non-permeable with respect to the active ray-curable ink, being obtained by curing a resin composition and having an arithmetic average roughness (Ra) specified under JIS B 0601:2001 of from 0.4 μm to 3 μm, to thereby perform printing on the ink receiving layer; and irradiating the active ray-curable ink with an active ray from 2.2 seconds to 30 seconds after the active ray-curable ink lands on the ink receiving layer.
A solid bioerodible implant suitable for treating an inflammation-mediated condition of the eye, said implant comprising: a steroidal anti-inflammatory agent which is dexamethasone homogeneously dispersed in a bioerodible polyester polymer without an added release modulator, wherein the implant is obtainable by extrusion; the steroidal anti-inflammatory agent makes up from 50% to 80% by the weight of the implant; the total mass of the implant is from 250μg to 5000μg and the implant is structured to be placed in the vitreous of the eye, and wherein following implantation, a concentration of 0.05 μg/ml dexamethasone is achieved within the vitreous within 48 hours and thereafter a concentration of at least 0.03 μg/ml is maintained for at least 3 weeks.
A surgical anvil assembly for use with a circular stapling instrument, comprising: an anvil center rod having a distal portion and a proximal portion , the proximal portion defining a pair of slots therein; and an anvil head pivotally coupled to distal portion of the anvil center rod and movable between a first, operative condition and a second, tilted condition; wherein the surgical anvil assembly further comprises a pair of legs received within the pair of slots, each of the pair of legs including a distal end portion fixedly coupled to the proximal body portion , and a proximal end portion free to pivot within the respective slot, the pair of legs cooperatively defining a cavity therebetween dimensioned for receipt of an anvil retainer , characterised in that the distal end portion of each of the pair of legs is welded to an inner periphery of the proximal portion of the anvil center rod . an anvil center rod having a distal portion and a proximal portion , the proximal portion defining a pair of slots therein; and an anvil head pivotally coupled to distal portion of the anvil center rod and movable between a first, operative condition and a second, tilted condition; wherein the surgical anvil assembly further comprises a pair of legs received within the pair of slots, each of the pair of legs including a distal end portion fixedly coupled to the proximal body portion , and a proximal end portion free to pivot within the respective slot, the pair of legs cooperatively defining a cavity therebetween dimensioned for receipt of an anvil retainer , characterised in that the distal end portion of each of the pair of legs is welded to an inner periphery of the proximal portion of the anvil center rod .
An ejector comprising: a primary inlet for admitting a motive flow; a secondary inlet ; an outlet ; a primary flowpath from the primary inlet; a secondary flowpath from the secondary inlet; a mixer convergent section downstream of the secondary inlet; and a motive nozzle surrounding the primary flowpath upstream of a junction with the secondary flowpath and having an exit , means for introducing swirl to the motive flow; characterised in that the ejector further comprises a control needle inside the motive nozzle 100; the means is inside the motive nozzle ; the means comprises a plurality of vanes ; and the vanes are carried on the control needle . a primary inlet for admitting a motive flow; a secondary inlet ; an outlet ; a primary flowpath from the primary inlet; a secondary flowpath from the secondary inlet; a mixer convergent section downstream of the secondary inlet; and a motive nozzle surrounding the primary flowpath upstream of a junction with the secondary flowpath and having an exit , means for introducing swirl to the motive flow; characterised in that the ejector further comprises a control needle inside the motive nozzle 100; the means is inside the motive nozzle ; the means comprises a plurality of vanes ; and the vanes are carried on the control needle .
A dic-wclding system for an aircraft dc-iccr assembly comprising: a die ; a die base ; a high energy source ; and a composite aircraft de-icer assembly comprised from bottom to top of: a bottom layer or ply of neoprene; a first intermediate non-stretchable woven nylon fabric welded-material layer ; a second intermediate stretchable woven nylon fabric welded-material layer ; a top layer or ply of neoprene or urethane; wherein at least one of the die and the die base includes a welded-portion pattern thereon configured to weld the first welded-material layer to the second welded-material layer in the pattern of the welded-portion pattern such that inflatable portions are formed within the welded-portion pattern formed in the de-icer assembly between non-welded sections of the first welded-material layer and the second welded-material layer, wherein at least one first inflatable portion is fluidly isolated from at least one second inflatable portion by a weld formed between the first welded-material layer and the second welded-material layer; wherein the high energy source is a radio frequency source. a die ; a die base ; a high energy source ; and a composite aircraft de-icer assembly comprised from bottom to top of: a bottom layer or ply of neoprene; a first intermediate non-stretchable woven nylon fabric welded-material layer ; a second intermediate stretchable woven nylon fabric welded-material layer ; a top layer or ply of neoprene or urethane; wherein at least one of the die and the die base includes a welded-portion pattern thereon configured to weld the first welded-material layer to the second welded-material layer in the pattern of the welded-portion pattern such that inflatable portions are formed within the welded-portion pattern formed in the de-icer assembly between non-welded sections of the first welded-material layer and the second welded-material layer, wherein at least one first inflatable portion is fluidly isolated from at least one second inflatable portion by a weld formed between the first welded-material layer and the second welded-material layer; wherein the high energy source is a radio frequency source. a bottom layer or ply of neoprene; a first intermediate non-stretchable woven nylon fabric welded-material layer ; a second intermediate stretchable woven nylon fabric welded-material layer ; a top layer or ply of neoprene or urethane; wherein at least one of the die and the die base includes a welded-portion pattern thereon configured to weld the first welded-material layer to the second welded-material layer in the pattern of the welded-portion pattern such that inflatable portions are formed within the welded-portion pattern formed in the de-icer assembly between non-welded sections of the first welded-material layer and the second welded-material layer, wherein at least one first inflatable portion is fluidly isolated from at least one second inflatable portion by a weld formed between the first welded-material layer and the second welded-material layer; wherein the high energy source is a radio frequency source.