mhurhangee/ep-ind-claims huggingface dataset:
Punch press with a crank or eccentric drive, comprising a crankshaft or eccentric shaft (1a, 1b) and active connecting rods (9a, 9b) for generating the stroke movement of the press ram, and with balancing weights (2a, 2b) for balancing the vertical and horizontal mass forces, wherein the punch press is adapted in such a way that the horizontal drive movements required for the horizontal mass balancing are tapped directly at the crankshaft or eccentric shaft (1a, 1b), wherein the punch press is adapted in such a way that each of the balancing weights (2a, 2b) serves for balancing horizontal mass forces as well as for balancing vertical mass forces, characterized in that the punch press is adapted in such a way that the drive movements required for the vertical mass balancing are tapped directly at the crankshaft or eccentric shaft (1a, 1b), in particular above the crankshaft or eccentric shaft (1a, 1b). wherein the punch press is adapted in such a way that the horizontal drive movements required for the horizontal mass balancing are tapped directly at the crankshaft or eccentric shaft (1a, 1b), wherein the punch press is adapted in such a way that each of the balancing weights (2a, 2b) serves for balancing horizontal mass forces as well as for balancing vertical mass forces, characterized in that the punch press is adapted in such a way that the drive movements required for the vertical mass balancing are tapped directly at the crankshaft or eccentric shaft (1a, 1b), in particular above the crankshaft or eccentric shaft (1a, 1b).
A lock for releasably connecting a panel to a structure, said lock comprising: - a bracket suitable for attachment to the panel; - a striker (32, 132), hinged to the bracket in rotation about a first axis; - a plunger articulated to the bracket in rotation about a second axis parallel to the first axis; - a spring, comprising a first and a second arm connected by at least one intermediate portion, one end of each of said first and second arms bearing on the striker and on the plunger respectively; the lock being movable between a closed configuration, in which the striker is in contact with the plunger, and an open configuration, in which the striker is spaced away from the plunger; a first stress of the spring in the closed position being greater than a second stress of said spring in the open position; the at least one intermediate portion of the spring being disposed about the second axis; the lock being characterised in that: - the lock further comprises a travel surface connected to or near the end of at least the first arm; and - the striker has a movement profile (58, 158) in contact with the travel surface in the closed and open configurations of the lock, said travel surface being adapted to move over said movement profile upon movement of said lock between said closed and open configurations. - a bracket suitable for attachment to the panel; - a striker (32, 132), hinged to the bracket in rotation about a first axis; - a plunger articulated to the bracket in rotation about a second axis parallel to the first axis; - a spring, comprising a first and a second arm connected by at least one intermediate portion, one end of each of said first and second arms bearing on the striker and on the plunger respectively; the lock being movable between a closed configuration, in which the striker is in contact with the plunger, and an open configuration, in which the striker is spaced away from the plunger; a first stress of the spring in the closed position being greater than a second stress of said spring in the open position; the at least one intermediate portion of the spring being disposed about the second axis; the lock being characterised in that: - the lock further comprises a travel surface connected to or near the end of at least the first arm; and - the striker has a movement profile (58, 158) in contact with the travel surface in the closed and open configurations of the lock, said travel surface being adapted to move over said movement profile upon movement of said lock between said closed and open configurations. - the lock further comprises a travel surface connected to or near the end of at least the first arm; and - the striker has a movement profile (58, 158) in contact with the travel surface in the closed and open configurations of the lock, said travel surface being adapted to move over said movement profile upon movement of said lock between said closed and open configurations.
A wind turbine configuration system (WTCS), said configuration system being configured for processing of a plurality of configuration parameter settings, each setting being collected from the control system of one of a plurality of comparable wind turbines, wherein the configuration system comprises processing means arranged to analyse the plurality of configuration parameter settings so as to identify a preferred range of setting for the configuration parameter (S302, S405), the configuration system further being configured for initiating an optimization action of configuration parameter settings based on said identified preferred range(s) of setting(s) (S303, S304), characterised in that said processing of configuration parameter settings is configured for identifying outlying configuration parameter settings of the analysed configuration parameter settings by means of the identified preferred range(s) of setting(s), and wherein said optimization action comprises correction of said identified outlying configuration parameter settings.
A received power control device configured to perform control of received energy, which is an amount of power received from a power system per predetermined time at a power receiving point to which a load and an electric storage device are electrically connected, the received power control device configured to perform the control by controlling charge and discharge of at least the electric storage device, the received power control device comprising: a received energy obtainer configured to periodically obtain information indicating the received energy; a controller configured to cause at least the electric storage device to discharge to prevent the received energy from exceeding a first threshold; and a remaining capacity obtainer configured to periodically obtain information indicating a remaining capacity of the electric storage device, characterized in that the received power control device future comprises a threshold setter configured to increase the first threshold when an amount of decrease in the remaining capacity per unit time exceeds a second threshold. a received energy obtainer configured to periodically obtain information indicating the received energy; a controller configured to cause at least the electric storage device to discharge to prevent the received energy from exceeding a first threshold; and a remaining capacity obtainer configured to periodically obtain information indicating a remaining capacity of the electric storage device, characterized in that the received power control device future comprises a threshold setter configured to increase the first threshold when an amount of decrease in the remaining capacity per unit time exceeds a second threshold.
A method, performed at a network element, comprising: receiving an attach request from a user equipment, said attach request comprising information regarding one or more integrity algorithms, in a user equipment network capability information element of the attach request, and an additional user plane integrity supported, UIS, bit indicating whether the user equipment supports user plane integrity with all the one or more integrity algorithms listed in the user equipment network capability information element, or does not support user plane integrity at all; and sending a response to the attach request to the user equipment, said response including an additional user plane integrity applied, UIA, bit, wherein, if the UIA bit is set, the response comprises information configured to identify only one integrity algorithm selected from the one or more integrity algorithms and including the UIA bit indicating that said selected integrity algorithm is to be used by the user equipment for both the control plane integrity and the user plane integrity, and if the UIA bit is not set, the response comprises information configured to identify only one integrity algorithm selected from the one or more integrity algorithms to be used by the user equipment only for the control plane integrity. receiving an attach request from a user equipment, said attach request comprising information regarding one or more integrity algorithms, in a user equipment network capability information element of the attach request, and an additional user plane integrity supported, UIS, bit indicating whether the user equipment supports user plane integrity with all the one or more integrity algorithms listed in the user equipment network capability information element, or does not support user plane integrity at all; and sending a response to the attach request to the user equipment, said response including an additional user plane integrity applied, UIA, bit, wherein, if the UIA bit is set, the response comprises information configured to identify only one integrity algorithm selected from the one or more integrity algorithms and including the UIA bit indicating that said selected integrity algorithm is to be used by the user equipment for both the control plane integrity and the user plane integrity, and if the UIA bit is not set, the response comprises information configured to identify only one integrity algorithm selected from the one or more integrity algorithms to be used by the user equipment only for the control plane integrity.
An ink jet recording method that is performed on a low-absorbable or non-absorbable recording medium using a colored ink composition containing a coloring material, a clear ink composition containing resin, and a processing solution that contains an aggregating agent for aggregating constituents in the colored ink composition, the method comprising: causing the processing solution that contains the aggregating agent to adhere to the recording medium; and causing ink to adhere through main scanning in which the colored ink composition and the clear ink composition are ejected while relative positions of a carriage with an ink jet head mounted thereon and the recording medium are changed in a main scanning direction and sub scanning in which the relative positions of the carriage and the recording medium are changed in a sub scanning direction that intersects the main scanning direction, wherein the ink jet head is configured to have an overlapping region where a recording region in which the colored ink composition is ejected from the ink jet head in the main scanning and a recording region in which the clear ink composition is ejected in the main scanning overlap with one another in the sub scanning direction. causing the processing solution that contains the aggregating agent to adhere to the recording medium; and causing ink to adhere through main scanning in which the colored ink composition and the clear ink composition are ejected while relative positions of a carriage with an ink jet head mounted thereon and the recording medium are changed in a main scanning direction and sub scanning in which the relative positions of the carriage and the recording medium are changed in a sub scanning direction that intersects the main scanning direction, wherein the ink jet head is configured to have an overlapping region where a recording region in which the colored ink composition is ejected from the ink jet head in the main scanning and a recording region in which the clear ink composition is ejected in the main scanning overlap with one another in the sub scanning direction.
A method of making an aero-derivative gas turbine engine, the method comprising: removing a combustor outer casing of an existing aero gas turbine engine; removing an annular combustor of the existing aero gas turbine engine; removing a first row of turbine vanes of the existing aero gas turbine engine; installing a can annular combustor assembly within the existing aero gas turbine engine the can annular combustor assembly configured to accelerate and orient combustion gasses directly onto a first row of turbine blades of the existing aero gas turbine engine, the can annular combustor assembly comprising a plurality of combustors and associated transition ducts; and installing a can annular combustor assembly outer casing to produce the aero-derivative gas turbine engine, characterised in that the can annular combustor assembly is installed within an axial span of the existing aero gas turbine engine vacated by the annular combustor and the first row of turbine vanes. removing a combustor outer casing of an existing aero gas turbine engine; removing an annular combustor of the existing aero gas turbine engine; removing a first row of turbine vanes of the existing aero gas turbine engine; installing a can annular combustor assembly within the existing aero gas turbine engine the can annular combustor assembly configured to accelerate and orient combustion gasses directly onto a first row of turbine blades of the existing aero gas turbine engine, the can annular combustor assembly comprising a plurality of combustors and associated transition ducts; and installing a can annular combustor assembly outer casing to produce the aero-derivative gas turbine engine, characterised in that the can annular combustor assembly is installed within an axial span of the existing aero gas turbine engine vacated by the annular combustor and the first row of turbine vanes.
Shelving system for installation in a vehicle having at least two vertical shelf posts (1, 2) and at least one insert part (3, 4) arranged horizontally between the shelf posts (1, 2), wherein at least one attachment element is present between the shelf posts (1, 2) and the end-face sides (5, 6) of the insert parts (3, 4) facing them, wherein the length of the end-face sides (5, 6) of the insert part (3, 4) is greater than a greatest width of the shelf posts (1, 2), wherein each insert part (3, 4) is attachable to the shelf posts (1, 2) in at least two positions horizontally, characterised in that the or each insert part (3, 4) has on its underside a recess in the form of a T-shaped groove, the ends of which are stoppable by the attachment element and hence define the two positions of the insert part (3, 4) with respect to the shelf posts (1, 2).
A medical device for causing the hemostasis of a blood vessel for use through an endoscope, said medical device comprising: a clip, the clip having at least two clip legs; a control wire; a sheath enclosing the control wire; an outer sleeve that is deployable from the sheath, wherein the control wire is able to be pulled in a proximal direction to pull the clip through the outer sleeve, thereby closing the at least two clip legs; a retainer, the retainer being releasably coupled to the outer sleeve; a handle coupled to the sheath; and an actuator coupled to the control wire, the control wire engageable by the actuator to open the at least two clip legs and to close the at least two clip legs; characterized in that the device further comprises a retainer release arrangement, the retainer release arrangement able to engage the retainer to uncouple the retainer from the outer sleeve. a clip, the clip having at least two clip legs; a control wire; a sheath enclosing the control wire; an outer sleeve that is deployable from the sheath, wherein the control wire is able to be pulled in a proximal direction to pull the clip through the outer sleeve, thereby closing the at least two clip legs; a retainer, the retainer being releasably coupled to the outer sleeve; a handle coupled to the sheath; and an actuator coupled to the control wire, the control wire engageable by the actuator to open the at least two clip legs and to close the at least two clip legs; characterized in that the device further comprises a retainer release arrangement, the retainer release arrangement able to engage the retainer to uncouple the retainer from the outer sleeve.
A spoke for a non-pneumatic wheel defining radial, axial, and circumferential directions, the spoke comprising: a web-like body extending along the radial direction between a radially-outer end and a radially inner end and extending along an axial direction between opposing edges (108, 110) of the web-like body, characterized in that the web like body comprising a reinforcement structure extending along the radial direction and forming an outer fold at the radially-outer end and an inner fold at the radially-inner end; an outer anchor positioned at the radially outer end and comprising an outer pair of arms (116, 118) extending in an opposing manner along the circumferential direction away from the web-like body; and an inner anchor positioned at the radially inner end and comprising an inner pair of arms extending in an opposing manner along the circumferential direction away from the web-like body. a web-like body extending along the radial direction between a radially-outer end and a radially inner end and extending along an axial direction between opposing edges (108, 110) of the web-like body, characterized in that the web like body comprising a reinforcement structure extending along the radial direction and forming an outer fold at the radially-outer end and an inner fold at the radially-inner end; an outer anchor positioned at the radially outer end and comprising an outer pair of arms (116, 118) extending in an opposing manner along the circumferential direction away from the web-like body; and an inner anchor positioned at the radially inner end and comprising an inner pair of arms extending in an opposing manner along the circumferential direction away from the web-like body.
SCR or Selective Catalytic Reduction method for purifying the exhaust gases of an internal combustion engine of a vehicle, according to which ammonia gas is exclusively metered in the exhaust gases, the method comprising a step of releasing ammonia gas from at least one solid absorbing matrix where it is stored by sorption and a step of metering the released ammonia gas in the exhaust gases, wherein the method comprises a step of regenerating the solid absorbing matrix that consists in: - generating a refilling ammonia gas by chemically decomposing a ammonia precursor in a biochemical decomposition unit mounted on board the vehicle and storing at least one protein component adapted to decompose said ammonia precursor; - separating water from the refilling ammonia gas by means of a liquid-vapour separator unit; - directing the refilling ammonia gas to the solid absorbing matrix where it is stored thereon. - generating a refilling ammonia gas by chemically decomposing a ammonia precursor in a biochemical decomposition unit mounted on board the vehicle and storing at least one protein component adapted to decompose said ammonia precursor; - separating water from the refilling ammonia gas by means of a liquid-vapour separator unit; - directing the refilling ammonia gas to the solid absorbing matrix where it is stored thereon.
A self-cooled orifice structure comprising: a hot side panel; a cold side panel spaced from the hot side panel; a continuous first wall extending axially between the hot and cold side panels and spaced radially outward from a centerline; a first plurality of helical vanes (136; 152) projecting laterally, radially, inward from the first wall; an outward face extending axially between the hot and cold side panels and spaced radially inward from the first wall, wherein a plurality of helical channels (138; 154; 150") are defined radially between the outward face and the first wall and defined laterally between respective adjacent vanes of the first plurality of helical vanes, and communicate through the hot and cold side panels; and a continuous second wall having the outward face and an opposite inward face, wherein the inward face defines an orifice; wherein: the hot side panel is engaged to the first wall and spaced radially outward from the second wall; wherein the self-cooled structure further comprises: a second plurality of helical vanes projecting radially outward from the first wall and disposed at least in-part between the hot and cold side panels. a hot side panel; a cold side panel spaced from the hot side panel; a continuous first wall extending axially between the hot and cold side panels and spaced radially outward from a centerline; a first plurality of helical vanes (136; 152) projecting laterally, radially, inward from the first wall; an outward face extending axially between the hot and cold side panels and spaced radially inward from the first wall, wherein a plurality of helical channels (138; 154; 150") are defined radially between the outward face and the first wall and defined laterally between respective adjacent vanes of the first plurality of helical vanes, and communicate through the hot and cold side panels; and a continuous second wall having the outward face and an opposite inward face, wherein the inward face defines an orifice; wherein: the hot side panel is engaged to the first wall and spaced radially outward from the second wall; wherein the self-cooled structure further comprises: a second plurality of helical vanes projecting radially outward from the first wall and disposed at least in-part between the hot and cold side panels.
A lock bracket arrangement of a vehicle lock, in particular, for a front hood, having a lock bracket with at least one side arm (4, 5) and a transverse arm, and having a carrier plate with at least one receiving opening (7, 8), into which the at least one side arm (4, 5) is inserted, wherein the at least one side arm is supported in a bearing element by means of a form-locking connection and/or a force-locking connection, characterized in that the bearing element is tied into the at least one receiving opening so that the bearing element in the case of a predetermined stress in the pressure direction, particularly in the case of a pedestrian impact, unties with a dive through the carrier plate and thus a displacement path is cleared for the lock bracket, wherein the at least one side arm is supported adjustable for height in the bearing element.
A tool comprising a lock module for locking the tool to a tool holder, the lock module comprising: a body; at least one wing projecting laterally from a side of the body and lying on a first plane; at least one lock member slidably supported in the body, the lock member being actuatable to extend from the body in a direction substantially orthogonal to the first plane to a lock position; and an abutment member supported in the body to move between a first position and a second position, the abutment member being in abutting engagement with the lock member wherein movement of the abutment member to the second position extends the at least one lock member to the lock position. a body; at least one wing projecting laterally from a side of the body and lying on a first plane; at least one lock member slidably supported in the body, the lock member being actuatable to extend from the body in a direction substantially orthogonal to the first plane to a lock position; and an abutment member supported in the body to move between a first position and a second position, the abutment member being in abutting engagement with the lock member wherein movement of the abutment member to the second position extends the at least one lock member to the lock position. at least one lock member slidably supported in the body, the lock member being actuatable to extend from the body in a direction substantially orthogonal to the first plane to a lock position; and an abutment member supported in the body to move between a first position and a second position, the abutment member being in abutting engagement with the lock member wherein movement of the abutment member to the second position extends the at least one lock member to the lock position.