mhurhangee/patent-ind-claim-en huggingface dataset:
Collective structure comprising an arrangement for connecting at least two housing parts (2, 3, 4; 21, 22) of a housing (1; 20) or component by means of at least one screw (5; 24), also comprising the at least two housing parts, further comprising the at least one screw and additionally comprising at least one damping member, wherein at least one housing part (3; 21) has a through-bore (7; 23) and the at least one screw (5; 24) has a screw shank (5a; 24c), which passes through the through-bore (7; 23) with an annular gap being left in the process, wherein the annular damping member (13; 28) is arranged in the region of the annular gap and is in contact, on the one hand, with the screw shank (5a; 24c) and, on the other hand, with the wall of the through-bore (7; 23), wherein the through-bore (7; 23) is delimited by a first and a second clamping location , wherein the damping member (13; 28) is arranged approximately in the centre between the first and second clamping locations , and wherein the damping member is designed in the form of a rubber ring (13; 28), characterized in that at least one sleeve (10; 26, 27) is arranged in the annular gap , between the first and second clamping locations , for the purpose of positioning the damping member (13; 28), in that the through-bore is designed in the form of a stepped bore with a shoulder and in that the damping member is arranged in abutment against the shoulder , or in that a second sleeve is provided and in that the damping member (13; 28) is squeezed in the axial direction between the first and second sleeves or between the shoulder and the at least one sleeve . in that the through-bore is designed in the form of a stepped bore with a shoulder and in that the damping member is arranged in abutment against the shoulder , or in that a second sleeve is provided and in that the damping member (13; 28) is squeezed in the axial direction between the first and second sleeves or between the shoulder and the at least one sleeve .
A method for transmitting uplink control information in a LTE system, comprising: receiving downlink information; and based on the downlink information, transmitting a hybrid automatic repeat request-acknowledgment, HARQ-ACK, signal using a predefined physical uplink shared channel, PUSCH, format, wherein the predefined PUSCH format is used to only transmit the HARQ-ACK signal, characterized in that the predefined PUSCH format occupies a single subcarrier along a frequency domain and extends across 2 milliseconds, ms, along a time domain. receiving downlink information; and based on the downlink information, transmitting a hybrid automatic repeat request-acknowledgment, HARQ-ACK, signal using a predefined physical uplink shared channel, PUSCH, format, wherein the predefined PUSCH format is used to only transmit the HARQ-ACK signal, characterized in that the predefined PUSCH format occupies a single subcarrier along a frequency domain and extends across 2 milliseconds, ms, along a time domain.
Apparatus, comprising an insulating body made from plastic, a cable receptacle for a cable being configured in the insulating body , a conductor receptacle for a conductor bolt being arranged in a head section of the insulating body , the insulating body being of elastic configuration or comprising an elastomeric material or being manufactured from a material of this type, a plurality of supporting elements being received within the insulating body , the supporting elements being manufactured from an electrically insulating material and being configured as rods or bars, characterized in that the supporting elements are arranged in a self-supporting manner at least in the head section and lie within the insulating body here and are embedded into the latter, the supporting elements ending with a free end in the insulating body , without emerging from the latter.
Computer-implemented method for communicating direction information to a user, wherein a position and viewing direction of the user are available to the computer, comprising the steps of: - detecting a situation in which direction information is to be communicated to the user, on the basis of the viewing direction of the user, wherein direction information is to be communicated to the user at least when the viewing direction of the user deviates from a target direction in which the user is to move; - determining direction information to be communicated, wherein the direction information indicates the target direction; and - controlling at least one actuator from a group of actuators to generate a haptic signal having a directional characteristic according to the direction information to be communicated; wherein direction information is not communicated to the user if the user moves in the target direction despite a deviating viewing direction. - detecting a situation in which direction information is to be communicated to the user, on the basis of the viewing direction of the user, wherein direction information is to be communicated to the user at least when the viewing direction of the user deviates from a target direction in which the user is to move; - determining direction information to be communicated, wherein the direction information indicates the target direction; and - controlling at least one actuator from a group of actuators to generate a haptic signal having a directional characteristic according to the direction information to be communicated;
A turboprop propulsion system adapted for use in an airplane with an airframe, the system comprising: a propeller mounted for rotation about a propeller axis ; a gas turbine engine mounted to establish an engine axis of rotation different from the propeller axis to form an offset angle therebetween; a gearbox coupled between the propeller and the gas turbine engine and configured to accommodate the offset angle between the propeller axis and the engine axis of rotation; and a nacelle that houses the gas turbine engine and at least part of the gearbox and the nacelle is configured to be integrated into the airframe and supports the propeller , the gas turbine engine , and the gearbox relative to the rest of an airframe, the nacelle including an exhaust duct shaped to provide a direct line of sight from an exhaust discharge outlet of the gas turbine engine to an exhaust-outlet aperture of the nacelle; characterised in that the turboprop propulsion system further comprising an infrared suppressor coupled to the gas turbine engine and configured to conduct exhaust gases at least part way from the exhaust discharge outlet of the gas turbine engine to the exhaust-outlet aperture of the nacelle, wherein the infrared suppressor has a direct line of sight from the exhaust discharge outlet of the gas turbine engine to the exhaust-outlet aperture of the nacelle . a propeller mounted for rotation about a propeller axis ; a gas turbine engine mounted to establish an engine axis of rotation different from the propeller axis to form an offset angle therebetween; a gearbox coupled between the propeller and the gas turbine engine and configured to accommodate the offset angle between the propeller axis and the engine axis of rotation; and a nacelle that houses the gas turbine engine and at least part of the gearbox and the nacelle is configured to be integrated into the airframe and supports the propeller , the gas turbine engine , and the gearbox relative to the rest of an airframe, the nacelle including an exhaust duct shaped to provide a direct line of sight from an exhaust discharge outlet of the gas turbine engine to an exhaust-outlet aperture of the nacelle; characterised in that the turboprop propulsion system further comprising an infrared suppressor coupled to the gas turbine engine and configured to conduct exhaust gases at least part way from the exhaust discharge outlet of the gas turbine engine to the exhaust-outlet aperture of the nacelle, wherein the infrared suppressor has a direct line of sight from the exhaust discharge outlet of the gas turbine engine to the exhaust-outlet aperture of the nacelle .
Surgical treatment instrument , in particular for tenolysis, tenotomy or neurolysis, comprising: - a main body comprising a longitudinal lumen for passage of fluid from a proximal end to a distal end to a distal end of the main body , and - a distal part (12; 14) including a curved portion forming a hook (124; 144) and being provided with a cutting blade (125; 145) on the inner side of the hook (124; 144), the main body further comprising an elbow presenting a concavity facing the same side as the hook (124; 144), characterised in that the main body has, in the vicinity of its distal end : - an over-pressure chamber , - an injection channel , the injection channel being in fluidic connection with the lumen via the over-pressure chamber , the injection channel being configured to direct a fluid stream above the hook , the over-pressure chamber being configured to deliver pressurised fluid to the injection channel . - a main body comprising a longitudinal lumen for passage of fluid from a proximal end to a distal end to a distal end of the main body , and - a distal part (12; 14) including a curved portion forming a hook (124; 144) and being provided with a cutting blade (125; 145) on the inner side of the hook (124; 144), the main body further comprising an elbow presenting a concavity facing the same side as the hook (124; 144), characterised in that the main body has, in the vicinity of its distal end : - an over-pressure chamber , - an injection channel , - an over-pressure chamber , - an injection channel , the injection channel being in fluidic connection with the lumen via the over-pressure chamber , the injection channel being configured to direct a fluid stream above the hook , the over-pressure chamber being configured to deliver pressurised fluid to the injection channel .
A mechanochemically carbonated clay which has a specific surface area of less than 50 m 2 /g and having a strength activity index, SAI, at day 7 determined according to ASTM C311/C311M-22 which is at least 105% and having a strength activity index, SAI, at day 28 determined according to ASTM C311/C311M-22 which is at least 110%.
A telecommunications frame (110/120) comprising: a first set of mounting features for allowing a first type of telecommunications device to be mounted to the frame (110/120); and a second set of mounting features for allowing a second type of telecommunications device to be mounted to the frame (110/120), the second type of telecommunications device defining a different width from a right side to a left side than the first type of telecommunications device, wherein the first set of mounting features and the second set of mounting features are provided on a single integral structure defining a backwall of the telecommunications frame (110/120), wherein the first set of mounting features are provided on both the right side and the left side of the structure and wherein the second set of mounting features are provided on both the right side and the left side of the structure , wherein the single integral structure defines a flange positioned forwardly from the backwall and formed around the perimeter of the backwall , the flange defining an abutment edge for limiting the amount of lateral movement of parts of the telecommunications devices mounted to the frame (110/120) caused by lateral forces applied to the telecommunications devices , wherein the first set of mounting features is provided in a vertically stacked arrangement along the flange on both the right side and the left side of the structure and wherein the second set of mounting features is provided in a vertically stacked arrangement on both the right and left sides of the structure set back from the flange . a first set of mounting features for allowing a first type of telecommunications device to be mounted to the frame (110/120); and a second set of mounting features for allowing a second type of telecommunications device to be mounted to the frame (110/120), the second type of telecommunications device defining a different width from a right side to a left side than the first type of telecommunications device, wherein the first set of mounting features and the second set of mounting features are provided on a single integral structure defining a backwall of the telecommunications frame (110/120), wherein the first set of mounting features are provided on both the right side and the left side of the structure and wherein the second set of mounting features are provided on both the right side and the left side of the structure , wherein the single integral structure defines a flange positioned forwardly from the backwall and formed around the perimeter of the backwall , the flange defining an abutment edge for limiting the amount of lateral movement of parts of the telecommunications devices mounted to the frame (110/120) caused by lateral forces applied to the telecommunications devices , wherein the first set of mounting features is provided in a vertically stacked arrangement along the flange on both the right side and the left side of the structure and wherein the second set of mounting features is provided in a vertically stacked arrangement on both the right and left sides of the structure set back from the flange .
A method for receiving digital media data in a client device, the method comprising: transmitting, to a server, a service subscription message for requesting a streaming service of a content; receiving, from the server, a grant message including service description information required for the streaming service of the content; transmitting, to an initial client device of neighbouring client devices, a join request message for receiving digital media data corresponding to the content based on the service description information; receiving, from the initial client device, a partnership request message that grants transmission of the digital media data; transmitting, to the initial client device, a data request message for requesting the transmission of the digital media data; and receiving, from the initial client device, the digital media data, wherein the digital media data and the grant message are received using an adaptive streaming scheme based on a Moving Picture Experts Group, MPEG, file format that comprises additional information necessary to support the adaptive streaming service between clients. transmitting, to a server, a service subscription message for requesting a streaming service of a content; receiving, from the server, a grant message including service description information required for the streaming service of the content; transmitting, to an initial client device of neighbouring client devices, a join request message for receiving digital media data corresponding to the content based on the service description information; receiving, from the initial client device, a partnership request message that grants transmission of the digital media data; transmitting, to the initial client device, a data request message for requesting the transmission of the digital media data; and receiving, from the initial client device, the digital media data, wherein the digital media data and the grant message are received using an adaptive streaming scheme based on a Moving Picture Experts Group, MPEG, file format that comprises additional information necessary to support the adaptive streaming service between clients.
Method for calculating a surface of a filling material of a blast furnace , in which, by means of an antenna device having a plurality of antennas arranged in a common housing , both at least two electromagnetic signals , namely radar signals, are transmitted onto the filling material , which signals are reflected at subregions (A1 to AN) of the filling material surface , and reflected signals (1") are received, and in which the surface of the filling material is calculated from at least the data dependent on the transmitted and received electromagnetic signals (1', 1"), characterized in that , by means of the antenna device , which is non-pivotable and forms a synthetic aperture by way of the antennas , electromagnetic signals are transmitted which are each reflected substantially at all subregions (A1 to AN) of the surface of the filling material that is to be calculated.
A silk fibroin composite comprising: a plurality of coupled layers wherein at least one of the coupled layers includes a composite matrix of at least one non-silk polymer and silk fibroin material derived at least in part from expression of one or more spider silk genes within at least one living organism, the plurality of coupled layers comprising: at least one backing or surface layer, the at least one backing or surface layer including a polymer having a fiber reinforcement including spider silk fibers and carbon fibers; a honeycomb-like core including a plurality of cells, the honeycomb-like core coupled to the at least one backing or surface layer with a fiber-reinforced polymer so as to close openings of the cells, wherein the fiber-reinforced polymer is a phenolic resin matrix reinforced with spider silk fibers and carbon fibers. at least one backing or surface layer, the at least one backing or surface layer including a polymer having a fiber reinforcement including spider silk fibers and carbon fibers; a honeycomb-like core including a plurality of cells, the honeycomb-like core coupled to the at least one backing or surface layer with a fiber-reinforced polymer so as to close openings of the cells, wherein the fiber-reinforced polymer is a phenolic resin matrix reinforced with spider silk fibers and carbon fibers.
An intramedullary implant system , comprising: an implant including a plate portion and an integral intramedullary portion ; a locking screw received through an opening of the plate portion ; a crossing screw received through an additional opening of the plate portion or the integral intramedullary portion , wherein the crossing screw extends at a non-perpendicular angle relative to a centerline axis (A) of the implant ; characterized in that the system comprises talons provided on the integral intramedullary portion and configured to deploy from a first position (X) to a second position (X') to increase stability of the implant relative to a bone, wherein the talons include barbs, claws, or a combination of barbs and claws. an implant including a plate portion and an integral intramedullary portion ; a locking screw received through an opening of the plate portion ; a crossing screw received through an additional opening of the plate portion or the integral intramedullary portion , wherein the crossing screw extends at a non-perpendicular angle relative to a centerline axis (A) of the implant ; characterized in that the system comprises talons provided on the integral intramedullary portion and configured to deploy from a first position (X) to a second position (X') to increase stability of the implant relative to a bone, wherein the talons include barbs, claws, or a combination of barbs and claws.
A catheter apparatus for insertion into vasculature of a patient and to a target area in the vasculature, comprising: a hollow inner shaft with a distal end and a proximal end; a removable non-occluding self-expandable scaffold coupled to the distal end of the inner shaft and disposed at the distal end of the hollow inner shaft , a portion of the distal end of the hollow inner shaft being disposed at least in part inside the self-expandable scaffold ; and a hollow outer shaft with a distal end and a proximal end, the hollow outer shaft being slidable over the hollow inner shaft and the scaffold ; wherein the outer shaft can be moved relative to the inner shaft and expandable scaffold so as to withdraw the outer shaft and enable the scaffold to assume its expanded state; wherein the scaffold when expanded is approximately cylindrical in shape and wherein the scaffold has a distal end that tapers towards the inner shaft; the scaffold is configured to center the distal end of the inner shaft along the central longitudinal axis of the scaffold when the scaffold is expanded; and the outer shaft is configured to enable the removal of the inner shaft and the scaffold through the proximal end of the outer shaft while the distal end of the outer shaft remains near the target area without the inner shaft and the scaffold being disposed within the outer shaft ; characterised in that the hollow outer shaft is configured to cover the scaffold and hold it in a non-expanded state when the outer shaft is disposed around the scaffold such that the scaffold is positioned inside the outer shaft between the outer shaft and the inner shaft. a hollow inner shaft with a distal end and a proximal end; a removable non-occluding self-expandable scaffold coupled to the distal end of the inner shaft and disposed at the distal end of the hollow inner shaft , a portion of the distal end of the hollow inner shaft being disposed at least in part inside the self-expandable scaffold ; and a hollow outer shaft with a distal end and a proximal end, the hollow outer shaft being slidable over the hollow inner shaft and the scaffold ; wherein the outer shaft can be moved relative to the inner shaft and expandable scaffold so as to withdraw the outer shaft and enable the scaffold to assume its expanded state; wherein the scaffold when expanded is approximately cylindrical in shape and wherein the scaffold has a distal end that tapers towards the inner shaft; the scaffold is configured to center the distal end of the inner shaft along the central longitudinal axis of the scaffold when the scaffold is expanded; and the outer shaft is configured to enable the removal of the inner shaft and the scaffold through the proximal end of the outer shaft while the distal end of the outer shaft remains near the target area without the inner shaft and the scaffold being disposed within the outer shaft ; characterised in that the hollow outer shaft is configured to cover the scaffold and hold it in a non-expanded state when the outer shaft is disposed around the scaffold such that the scaffold is positioned inside the outer shaft between the outer shaft and the inner shaft.
A circularly polarised antenna device for multiband global navigational satellite systems, comprising: a spiral antenna ; and a high impedance surface comprising a ground plane; the high impedance surface further comprises only a single conductive layer of resonant elements, the single conductive layer comprising a first region for operating at a first frequency range and a separate second region for operating at a second frequency range different from the first frequency range, the first region of the single conductive layer is provided with at least one resonant element of a first resonant frequency and the second region of the single conductive layer is provided with at least one resonant element of a second resonant frequency, the first and second regions are split along a substantially straight line, and the first region comprises one half of the single conductive layer and the second region comprises another half of the single conductive layer. a spiral antenna ; and a high impedance surface comprising a ground plane; the high impedance surface further comprises only a single conductive layer of resonant elements, the single conductive layer comprising a first region for operating at a first frequency range and a separate second region for operating at a second frequency range different from the first frequency range, the first region of the single conductive layer is provided with at least one resonant element of a first resonant frequency and the second region of the single conductive layer is provided with at least one resonant element of a second resonant frequency, the first and second regions are split along a substantially straight line, and the first region comprises one half of the single conductive layer and the second region comprises another half of the single conductive layer.