mhurhangee/patent-ind-claim-en huggingface dataset:
A sheet loading device comprising: a device body to load a sheet (S); a guide disposed extending in a sheet conveying direction in the device body ; a restricting body to move along the guide of the device body and to restrict a position of an end portion of the sheet (S); and a securing body to attach to the restricting body and the guide and detach from the restricting body and the guide , the restricting body being secured to the device body at an arbitrary position on the guide by engagement of the securing body with the device body , wherein the securing body has an engaging body to engage with the guide at an arbitrary position on the guide in the sheet conveying direction, wherein the securing body includes a switching body to operate the engaging body , and wherein the restricting body is secured to the device body by rotating the switching body which rotates the engaging body to engage with the guide of the device body . a device body to load a sheet (S); a guide disposed extending in a sheet conveying direction in the device body ; a restricting body to move along the guide of the device body and to restrict a position of an end portion of the sheet (S); and a securing body to attach to the restricting body and the guide and detach from the restricting body and the guide , the restricting body being secured to the device body at an arbitrary position on the guide by engagement of the securing body with the device body , wherein the securing body has an engaging body to engage with the guide at an arbitrary position on the guide in the sheet conveying direction, wherein the securing body includes a switching body to operate the engaging body , and wherein the restricting body is secured to the device body by rotating the switching body which rotates the engaging body to engage with the guide of the device body .
Assembly kit for an aircraft seat , with at least one mounting unit (12a; 12b), with at least one backrest (14a; 14b) which is fixedly coupled with the mounting unit (12a; 12b) in a state when assembled and ready for flight, and with at least one connection module (28a; 28b), via which the backrest (14a; 14b) is oriented rigidly in a position relative to the mounting unit (12a; 12b) in the assembled and ready-for-flight state, characterized in that the connection module (28a; 28b) comprises at least two connection elements (34a, 36a, 38a; 34b; 34c, 36c; 34d, 36d, 38d; 34e, 36e, 38e), by means of which the backrest can be fixedly mounted in at least two different backrest adjustment angles relative to the mounting unit , the at least two connection elements (34a, 36a, 38a; 34b; 34c, 36c; 34d, 36d, 38d; 34e, 36e, 38e) being mountable without requiring new approval, wherein "without requiring new approval" is to mean that no new approval is necessary for an approved aircraft seat if the backrest adjustment angle is changed by +3 degrees or -3 degrees with respect to the standard position of the backrest (14a; 14b), taking the manufacturing tolerance of +1 degree and -1 degree into account, wherein by means of each connection element (34a, 36a, 38a; 34b; 34c, 36c; 34d, 36d, 38d; 34e, 36e, 38e) a different backrest adjustment angle can be provided and the backrest (14a; 14b) cannot be adjusted in the assembled and ready-to-flight state. with at least one mounting unit (12a; 12b), with at least one backrest (14a; 14b) which is fixedly coupled with the mounting unit (12a; 12b) in a state when assembled and ready for flight, and with at least one connection module (28a; 28b), via which the backrest (14a; 14b) is oriented rigidly in a position relative to the mounting unit (12a; 12b) in the assembled and ready-for-flight state, characterized in that the connection module (28a; 28b) comprises at least two connection elements (34a, 36a, 38a; 34b; 34c, 36c; 34d, 36d, 38d; 34e, 36e, 38e), by means of which the backrest can be fixedly mounted in at least two different backrest adjustment angles relative to the mounting unit , the at least two connection elements (34a, 36a, 38a; 34b; 34c, 36c; 34d, 36d, 38d; 34e, 36e, 38e) being mountable without requiring new approval, wherein "without requiring new approval" is to mean that no new approval is necessary for an approved aircraft seat if the backrest adjustment angle is changed by +3 degrees or -3 degrees with respect to the standard position of the backrest (14a; 14b), taking the manufacturing tolerance of +1 degree and -1 degree into account, wherein by means of each connection element (34a, 36a, 38a; 34b; 34c, 36c; 34d, 36d, 38d; 34e, 36e, 38e) a different backrest adjustment angle can be provided and the backrest (14a; 14b) cannot be adjusted in the assembled and ready-to-flight state.
A communication terminal comprising a transceiver configured to communicate using carrier aggregation according to a first carrier aggregation setting; a detector configured to detect a need for the communication terminal to reduce its power consumption; an estimator configured to estimate a power savings amount by which the power consumption of the communication terminal is reduced based on switching from the first carrier aggregation setting to a second carrier aggregation setting, wherein the first carrier aggregation setting comprises a secondary cell being configured for the communication terminal for a time interval and the second carrier aggregation setting comprises the secondary cell not being configured for the communication terminal for the time interval; and a controller configured to initiate a switch from the first carrier aggregation setting to the second carrier aggregation setting based on the detector detecting the need for the communication terminal to reduce its power consumption and the estimator estimating the power savings amount is above a predetermined threshold. a transceiver configured to communicate using carrier aggregation according to a first carrier aggregation setting; a detector configured to detect a need for the communication terminal to reduce its power consumption; an estimator configured to estimate a power savings amount by which the power consumption of the communication terminal is reduced based on switching from the first carrier aggregation setting to a second carrier aggregation setting, wherein the first carrier aggregation setting comprises a secondary cell being configured for the communication terminal for a time interval and the second carrier aggregation setting comprises the secondary cell not being configured for the communication terminal for the time interval; and a controller configured to initiate a switch from the first carrier aggregation setting to the second carrier aggregation setting based on the detector detecting the need for the communication terminal to reduce its power consumption and the estimator estimating the power savings amount is above a predetermined threshold.
A humeral implant assembly comprising: a stem portion comprising a stem engagement feature; a metaphyseal portion comprising a metaphyseal engagement feature and a lumen extending longitudinally therethrough; a locking element positioned in the metaphyseal lumen of the metaphyseal portion; characterised in that it further comprises an intermediate portion comprising at least one spacer , each spacer comprising: a proximal engagement feature ; a distal engagement feature ; lumen extending longitudinally through said spacer, the lumen configured to be longitudinally aligned with the metaphyseal lumen when the assembly is in a locked configuration; and a pin slidable within the lumen of said spacer; wherein distal movement of the locking element translates the pin of each spacer to secure the metaphyseal portion, the intermediate portion, and the stem portion in the locked configuration. a stem portion comprising a stem engagement feature; a metaphyseal portion comprising a metaphyseal engagement feature and a lumen extending longitudinally therethrough; a locking element positioned in the metaphyseal lumen of the metaphyseal portion; characterised in that it further comprises an intermediate portion comprising at least one spacer , each spacer comprising: a proximal engagement feature ; a distal engagement feature ; lumen extending longitudinally through said spacer, the lumen configured to be longitudinally aligned with the metaphyseal lumen when the assembly is in a locked configuration; and a pin slidable within the lumen of said spacer; a proximal engagement feature ; a distal engagement feature ; lumen extending longitudinally through said spacer, the lumen configured to be longitudinally aligned with the metaphyseal lumen when the assembly is in a locked configuration; and a pin slidable within the lumen of said spacer; wherein distal movement of the locking element translates the pin of each spacer to secure the metaphyseal portion, the intermediate portion, and the stem portion in the locked configuration.
A mantle block for chimneys with a multi-shell structure with inner pipe and thermal insulation, wherein the mantle block is designed as a thin-walled hollow block, in the cavity of which the inner pipe for flue gas guidance and the thermal insulation surrounding the inner pipe can be arranged, produced from a concrete mixture, wherein the concrete mixture has a bulk density of less than 1300 kg/m 3 , characterized in that the mantle block , in the dry state, along a flow direction (z) oriented perpendicularly to the outer surface of the mantle block, has a leakage volume flow of less than 1.4 (m 3 /h)/m 2 for a wall thickness (x) of up to 5 cm, at a differential pressure of 50 Pa and relative to the outer surface (A) of the mantle block , wherein the concrete mixture is prepared from a formulation comprising a plasticiser, and wherein the formulation has a w/c ratio of > 0.6.
A system, comprising: a single-pole switching device , comprising: an armature configured to move between a first position that electrically couples a first contact to a second contact and a second position that electrically uncouples the first contact from the second contact ; a coil is configured to receive a voltage configured to magnetize the coil , thereby causing the armature to move from the first position to the second position, characterized in that the system comprises: a control system comprising a processor, wherein the control system is configured to: receive an indication that the armature is in the second position; and send a signal to an actuator in response to receiving the indication, wherein the signal is configured to cause an arm associated with the actuator to move the armature to achieve a gap distance between the first contact and the second contact , wherein the gap distance is determined by the processor. an armature configured to move between a first position that electrically couples a first contact to a second contact and a second position that electrically uncouples the first contact from the second contact ; a coil is configured to receive a voltage configured to magnetize the coil , thereby causing the armature to move from the first position to the second position, characterized in that the system comprises: a control system comprising a processor, wherein the control system is configured to: receive an indication that the armature is in the second position; and send a signal to an actuator in response to receiving the indication, wherein the signal is configured to cause an arm associated with the actuator to move the armature to achieve a gap distance between the first contact and the second contact , wherein the gap distance is determined by the processor. receive an indication that the armature is in the second position; and send a signal to an actuator in response to receiving the indication, wherein the signal is configured to cause an arm associated with the actuator to move the armature to achieve a gap distance between the first contact and the second contact , wherein the gap distance is determined by the processor.
A method for sending a long training sequence in a wireless local area network which supports Orthogonal Frequency Division Multiple Access, OFDMA, technology, by an access point or a station, wherein the method comprises: selecting a long training sequence according to a bandwidth, wherein the long training sequence is a 2x mode long training sequence; and sending a sub-sequence segment of the long training sequence according to a location and a size of an allocated resource unit, RU, wherein the sub-sequence segment at a corresponding location of the long training sequence is carried on subcarriers at the corresponding location, wherein the allocated RU is in the bandwidth and comprises consecutive subcarriers, wherein, when the bandwidth is 80-MHz, the 2x mode long training sequence includes values on subcarriers with indexes -500:2:500, and the values on subcarriers with indexes -500:2:500 are selecting a long training sequence according to a bandwidth, wherein the long training sequence is a 2x mode long training sequence; and sending a sub-sequence segment of the long training sequence according to a location and a size of an allocated resource unit, RU, wherein the sub-sequence segment at a corresponding location of the long training sequence is carried on subcarriers at the corresponding location, wherein the allocated RU is in the bandwidth and comprises consecutive subcarriers, wherein, when the bandwidth is 80-MHz, the 2x mode long training sequence includes values on subcarriers with indexes -500:2:500, and the values on subcarriers with indexes -500:2:500 are
Instrument panel holder for a motor vehicle, which has a cross-beam which can be incorporated between the A-columns of a motor vehicle body, wherein the cross-beam is equipped at least at one end with a mounting component for fastening to an A-column, wherein the mounting component is configured to be U-shaped and has a rib with two legs and in each leg are provided at least two mounting openings (17 - 20) arranged at a vertical distance from one another, characterised in that the driver-side longitudinal portion of the cross-beam is divided in a vertical plane.
A stand mixer arrangement including a pedestal for a mixing bowl , an electric motor and a drive system including a downwardly facing rotary drive outlet for being disposed overhead of the bowl, capable of imparting a mixing action to a tool suspended into the bowl from a socket supported by said drive outlet; characterised by illumination means encircling, or substantially encircling, said drive outlet and arranged to direct light downwardly into the mixing bowl to illuminate ingredients therein.
A reverse door ring assembly for a vehicle comprising: a door ring member defining an interior face and an exterior face opposite of the interior face, the door ring member having a thickness between an inner bodyside and an outer bodyside spaced apart from the inner bodyside, the door ring member including a sill and a bulkhead extending perpendicularly from a front end of the sill and defining an upper portion spaced apart from the sill, the door ring member including an A-pillar base sloping upwardly from the bulkhead to a roof edge , the door ring member including a B-pillar base extending from the sill to the roof edge; and an elongate member having a tubular shape disposed adjacent the exterior face of the door ring member and extending along the A-pillar base; characterised by a front reinforcement member secured on the exterior face of the door ring member on the upper portion of the bulkhead, wherein the upper portion of the bulkhead defines a shoulder sloping inwardly from the outer bodyside toward the inner bodyside; and wherein the front reinforcement member overlies the shoulder of the bulkhead. a door ring member defining an interior face and an exterior face opposite of the interior face, the door ring member having a thickness between an inner bodyside and an outer bodyside spaced apart from the inner bodyside, the door ring member including a sill and a bulkhead extending perpendicularly from a front end of the sill and defining an upper portion spaced apart from the sill, the door ring member including an A-pillar base sloping upwardly from the bulkhead to a roof edge , the door ring member including a B-pillar base extending from the sill to the roof edge; and an elongate member having a tubular shape disposed adjacent the exterior face of the door ring member and extending along the A-pillar base; characterised by a front reinforcement member secured on the exterior face of the door ring member on the upper portion of the bulkhead, wherein the upper portion of the bulkhead defines a shoulder sloping inwardly from the outer bodyside toward the inner bodyside; and wherein the front reinforcement member overlies the shoulder of the bulkhead.
Crosslinked polymer composition comprising a) at least a plastomer fulfilling the characteristics (i) and (ii) (i) being a copolymer of ethylene and a C 4 to C 8 alpha olefin comonomer and (ii) having a density (according to ISO 1183) in the range of 855 kg/m 3 to 890 kg/m 3 , b) optionally conductive fillers, whereby the composition has • a Shore A value measured according to ISO 868 of equal to or below 80 and • an elongation at break measured according to ISO 527-2 of at least 300% and • wherein other polymers than the plastomer are substantially absent. a) at least a plastomer fulfilling the characteristics (i) and (ii) (i) being a copolymer of ethylene and a C 4 to C 8 alpha olefin comonomer and (ii) having a density (according to ISO 1183) in the range of 855 kg/m 3 to 890 kg/m 3 , (i) being a copolymer of ethylene and a C 4 to C 8 alpha olefin comonomer and (ii) having a density (according to ISO 1183) in the range of 855 kg/m 3 to 890 kg/m 3 , b) optionally conductive fillers, • a Shore A value measured according to ISO 868 of equal to or below 80 and • an elongation at break measured according to ISO 527-2 of at least 300% and • wherein other polymers than the plastomer are substantially absent.
A pneumatic tire comprising, in a tread surface , two or more circumferential main grooves extending in a tread circumferential direction, and a land portion partitioned between the circumferential main grooves or by one of the circumferential main grooves and a tread edge (TE), wherein the land portion comprises a width direction sipe extending in a tread width direction, the width direction sipe comprises, in a cross section along a depth direction, a linear portion extending from an opening of the width direction sipe toward a bottom of the width direction sipe , and a bent portion connected to the linear portion , bending and extending from a connecting portion with the linear portion to the bottom of the width direction sipe , and the linear portion of the width direction sipe has a length in the depth direction increasing as the linear portion extends from a center portion of the width direction sipe in the tread width direction toward an end portion in the tread width direction, and wherein in the cross section along the depth direction, the bent portion of the width direction sipe includes two or more apexes in the center portion of the width direction sipe in the tread width direction, characterized in that in the end portion of the width direction sipe in the tread width direction, a number of apexes is smaller than a number of the apexes in the center portion in the tread width direction. the land portion comprises a width direction sipe extending in a tread width direction, the width direction sipe comprises, in a cross section along a depth direction, a linear portion extending from an opening of the width direction sipe toward a bottom of the width direction sipe , and a bent portion connected to the linear portion , bending and extending from a connecting portion with the linear portion to the bottom of the width direction sipe , and the linear portion of the width direction sipe has a length in the depth direction increasing as the linear portion extends from a center portion of the width direction sipe in the tread width direction toward an end portion in the tread width direction, and wherein in the cross section along the depth direction, the bent portion of the width direction sipe includes two or more apexes in the center portion of the width direction sipe in the tread width direction, characterized in that in the end portion of the width direction sipe in the tread width direction, a number of apexes is smaller than a number of the apexes in the center portion in the tread width direction.
Amphibious vehicle comprising at least one semi-rigid hull having a length dimension, a width dimension and a depth dimension, and comprising at least one running gear provided with at least one wheel , said running gear being configured so as to be positioned alternately in at least one retracted position and in a deployed position wherein the at least one wheel is in connection with the ground, the running gear comprising a fairing element secured to said running gear , the fairing element being situated below the at least one wheel according to the depth dimension of the hull , in the retracted position of the running gear , the hull comprising at least two pneumatic fenders on a periphery of said hull , the running gear being, in the retracted position , positioned longitudinally between the at least two pneumatic fenders in line with them and in a section with no fenders, so that the fairing element provides hydrodynamic continuity with said at least two pneumatic fenders in the retracted position .
A method of three-dimensional wire frame printing wherein material is printed by a printhead configured to move relative to the material at a printhead speed and extrude material at an extruding speed, the method comprising: printing an initial portion of material from a starting point ; pausing printing of the initial portion of material so as to form a first anchor point , such that a first direction is defined from the starting point to the first anchor point , and wherein the anchor point lies in a plane substantially perpendicular to the first direction such that the initial portion of material is on the printed side of the plane ; resuming printing from the first anchor point by printing, from the first anchor point , two or more intermediate portions of material on the non-printed side of the plane ; and printing a final portion of material to a second anchor point on the printed side of the plane ; wherein: the printhead speed and the extruding speed are independently variable; the average printhead speed is greater than the average extruding speed for the period of time during which the intermediate and final portions of material are printed between the first and second anchor points ; and a first intermediate portion is printed on the opposite side of the initial portion to the second anchor point . printing an initial portion of material from a starting point ; pausing printing of the initial portion of material so as to form a first anchor point , such that a first direction is defined from the starting point to the first anchor point , and wherein the anchor point lies in a plane substantially perpendicular to the first direction such that the initial portion of material is on the printed side of the plane ; resuming printing from the first anchor point by printing, from the first anchor point , two or more intermediate portions of material on the non-printed side of the plane ; and printing a final portion of material to a second anchor point on the printed side of the plane ; the printhead speed and the extruding speed are independently variable; the average printhead speed is greater than the average extruding speed for the period of time during which the intermediate and final portions of material are printed between the first and second anchor points ; and a first intermediate portion is printed on the opposite side of the initial portion to the second anchor point .