mhurhangee/patent-ind-claim-en huggingface dataset:
Method for operating a partially or fully automatic cross-wound bobbin-producing spinning machine , in particular an open-end rotor spinning machine, having a plurality of identical workstations which are arranged next to one another and are at least partially self-sufficient, wherein each of the workstations has a spinning device for producing a thread and a winding device , which has a bobbin holder , for winding the thread onto a cross-wound bobbin , and wherein, when a batch end of one of the workstations is reached, the relevant workstation is stopped, characterized in that , at the workstation which has reached the batch end, a requirement for carrying out at least one manual maintenance activity in the form of text or a graphic symbol is displayed by an optical display element , which is assigned to the workstation and is in the form of a graphic display .
A method of configuring information, performed by a base station, comprising: generating (S101) first configuration information, wherein the first configuration information indicates a time-frequency position of a synchronization signal block, SSB, corresponding to a common control resource set, CORESET, of current remaining minimum system information, RMSI; and sending (S102) the first configuration information to user equipment, UE; wherein the sending the first configuration information to the UE comprises: adding (S201) the first configuration information to an information element, IE; adding (S202) the IE to second configuration information, wherein the second configuration information is used to configure a bandwidth part corresponding to the CORESET of the current RMSI as an active bandwidth part; and sending (S203) the second configuration information to the UE through radio resource control, RRC, signaling. generating (S101) first configuration information, wherein the first configuration information indicates a time-frequency position of a synchronization signal block, SSB, corresponding to a common control resource set, CORESET, of current remaining minimum system information, RMSI; and sending (S102) the first configuration information to user equipment, UE; wherein the sending the first configuration information to the UE comprises: adding (S201) the first configuration information to an information element, IE; adding (S202) the IE to second configuration information, wherein the second configuration information is used to configure a bandwidth part corresponding to the CORESET of the current RMSI as an active bandwidth part; and sending (S203) the second configuration information to the UE through radio resource control, RRC, signaling. adding (S201) the first configuration information to an information element, IE; adding (S202) the IE to second configuration information, wherein the second configuration information is used to configure a bandwidth part corresponding to the CORESET of the current RMSI as an active bandwidth part; and sending (S203) the second configuration information to the UE through radio resource control, RRC, signaling.
Pneumatic vehicle tyre having a tread with at least one circumferential groove which is delimited by a groove base and two mutually opposite groove flanks and in which at least one sound absorber that is embodied in two parts and is made up of two protrusions is positioned, the protrusions thereof having different volumes, wherein the protrusions of the sound absorber are formed separately from one another in an axial direction and in a manner bearing against the mutually opposite groove flanks , wherein the smaller protrusion is located opposite a cutout that passes through the larger protrusion in a radial direction and is cross-sectionally U-shaped parallel to the tread surface, wherein, as seen in a longitudinal direction through the circumferential groove , the distance (a 2 ), measured at the groove base , between the protrusions of the sound absorber is 2.0 mm to 3.0 mm, characterized in that the larger protrusion is formed approximately in the shape of half a truncated cone and reaches at its groove flank to a height (h 2 ) determined in a radial direction from the groove base , said height (h 2 ) being preferably greater than the height (h 1 ) of the smaller protrusion and corresponding at most to half the depth (T) of the circumferential groove .
A subsea termination gland for providing a termination and connection to an electrical conductor in an underwater environment, wherein the subsea termination gland comprises: - a dry mateable first connector interface , configured to be mated with a complementary second connector interface of a connector front end , - a termination assembly comprising a connection member providing a first connection section of said first connector interface , the connection member comprising one or more pressure resistant components and a moulding ; wherein the moulding forms a passage which is tapered, wherein an inner diameter of the passage is larger at a front portion in proximity to the pressure resistant components , the front portion configured to allow a pin of the connector front end to enter the passage and wherein the inner diameter is reduced towards the middle of the insulator; the connection member being connectable to said electrical conductor , wherein the first connection section is exposed to the ambient environment when the termination gland is not mated with the connector front end , and, - a sealing section for sealing the termination gland to the connector front end , - characterized in that the moulding is a flexible or resilient moulding and wherein the passage of the moulding has an inner diameter that is at least over part of its length smaller than an outer diameter of the pin of the connector front end so that when the connector front end is mated with the termination gland, an interference fit is obtained between at least part of the passage and the pin of the connector front end . - a dry mateable first connector interface , configured to be mated with a complementary second connector interface of a connector front end , - a termination assembly comprising a connection member providing a first connection section of said first connector interface , the connection member comprising one or more pressure resistant components and a moulding ; wherein the moulding forms a passage which is tapered, wherein an inner diameter of the passage is larger at a front portion in proximity to the pressure resistant components , the front portion configured to allow a pin of the connector front end to enter the passage and wherein the inner diameter is reduced towards the middle of the insulator; the connection member being connectable to said electrical conductor , wherein the first connection section is exposed to the ambient environment when the termination gland is not mated with the connector front end , and, - a sealing section for sealing the termination gland to the connector front end , - characterized in that the moulding is a flexible or resilient moulding and wherein the passage of the moulding has an inner diameter that is at least over part of its length smaller than an outer diameter of the pin of the connector front end so that when the connector front end is mated with the termination gland, an interference fit is obtained between at least part of the passage and the pin of the connector front end .
A substrate processing apparatus comprising: a gas introduction structure made of a non-metallic material, penetrating a side wall of a process vessel and integrated with the side wall as a single structure, wherein a front end thereof protrudes into the process vessel; a nozzle made of a non-metallic material and comprising a first straight portion inserted into the gas introduction structure and fluidically communicating with the gas introduction structure; and a second straight portion fluidically communicating with the first straight portion and extending along an inner wall of the process vessel; and a fixing block provided at an inner side of the side wall of the process vessel and above the gas introduction structure, wherein the fixing block is provided with a groove in which the nozzle is capable of being moved in a radial direction of the process vessel. a gas introduction structure made of a non-metallic material, penetrating a side wall of a process vessel and integrated with the side wall as a single structure, wherein a front end thereof protrudes into the process vessel; a nozzle made of a non-metallic material and comprising a first straight portion inserted into the gas introduction structure and fluidically communicating with the gas introduction structure; and a second straight portion fluidically communicating with the first straight portion and extending along an inner wall of the process vessel; and a first straight portion inserted into the gas introduction structure and fluidically communicating with the gas introduction structure; and a second straight portion fluidically communicating with the first straight portion and extending along an inner wall of the process vessel; and a fixing block provided at an inner side of the side wall of the process vessel and above the gas introduction structure, wherein the fixing block is provided with a groove in which the nozzle is capable of being moved in a radial direction of the process vessel.
A film material insert molding method for forming a transparent resin layer on a front surface of a film material having a design portion and a substrate resin layer on a back surface of the film material , the method comprising: an intermediate part forming step (S1) of forming a first intermediate part having an edge extending radially from the film material , the edge being disposed at the inside of an outer peripheral end of a final shape of the film material ; a transparent resin layer forming step (S2) of forming a second intermediate part including a transparent resin layer , by injection molding, on a front surface of the first intermediate part , with the edge of the first intermediate part being fixed to a transparent resin layer forming unit by itself; and a substrate resin layer forming step (S3) of forming an insert-molded article including a substrate resin layer , by injection molding, on a back surface of the second intermediate part , the substrate resin layer covering a surface of a radial end of the edge . an intermediate part forming step (S1) of forming a first intermediate part having an edge extending radially from the film material , the edge being disposed at the inside of an outer peripheral end of a final shape of the film material ; a transparent resin layer forming step (S2) of forming a second intermediate part including a transparent resin layer , by injection molding, on a front surface of the first intermediate part , with the edge of the first intermediate part being fixed to a transparent resin layer forming unit by itself; and a substrate resin layer forming step (S3) of forming an insert-molded article including a substrate resin layer , by injection molding, on a back surface of the second intermediate part , the substrate resin layer covering a surface of a radial end of the edge .
A bearing housing for a turbocharger , the bearing housing comprising: a body configured to receive one or more bearings , the one or more bearings being configured to support rotation of a shaft about an axis ; and a mounting flange , the mounting flange extending around the body and comprising: a plurality of bores configured to receive a fastener therethrough; a first face configured to engage a corresponding mounting flange of a turbine housing ; and a plurality of cavities in communication with the plurality of bores , the plurality of cavities being formed in, and axially recessed relative to, the first face . a body configured to receive one or more bearings , the one or more bearings being configured to support rotation of a shaft about an axis ; and a mounting flange , the mounting flange extending around the body and comprising: a plurality of bores configured to receive a fastener therethrough; a first face configured to engage a corresponding mounting flange of a turbine housing ; and a plurality of cavities in communication with the plurality of bores , the plurality of cavities being formed in, and axially recessed relative to, the first face . a plurality of bores configured to receive a fastener therethrough; a first face configured to engage a corresponding mounting flange of a turbine housing ; and a plurality of cavities in communication with the plurality of bores , the plurality of cavities being formed in, and axially recessed relative to, the first face .
A assembly for a blade of a gas turbine engine, the assembly comprising: • a fastener defining a recess for receiving a blade root , the fastener having two flanks defining between them a passage leading into the recess and forming stops preventing the root from emerging from the recess through the passage, • two wedges , each wedge comprising: o a first support surface to come into contact with the foot , o a second support surface opposite the first support surface for abutting the fastener when the wedge is received in the recess, o a thread, wherein the respective first and second support surfaces of the two wedges are as follows: o fixed together, ∘ oriented so that a displacement of one of the two wedges in the recess with respect to the other wedge varies the amount of load exerted on the foot by the two wedges , • a clamping screw cooperating with the respective threads of the two wedges in such a way that a rotation of the clamping screw causes a displacement of one of the two wedges with respect to the other wedge . • a fastener defining a recess for receiving a blade root , the fastener having two flanks defining between them a passage leading into the recess and forming stops preventing the root from emerging from the recess through the passage, • two wedges , each wedge comprising: o a first support surface to come into contact with the foot , o a second support surface opposite the first support surface for abutting the fastener when the wedge is received in the recess, o a thread, wherein the respective first and second support surfaces of the two wedges are as follows: o fixed together, ∘ oriented so that a displacement of one of the two wedges in the recess with respect to the other wedge varies the amount of load exerted on the foot by the two wedges , o a first support surface to come into contact with the foot , o a second support surface opposite the first support surface for abutting the fastener when the wedge is received in the recess, o a thread, o fixed together, ∘ oriented so that a displacement of one of the two wedges in the recess with respect to the other wedge varies the amount of load exerted on the foot by the two wedges , • a clamping screw cooperating with the respective threads of the two wedges in such a way that a rotation of the clamping screw causes a displacement of one of the two wedges with respect to the other wedge .
A method of treating a tobacco material to enhance storage stability, comprising: receiving a tobacco material having at least about 40% water based on the total weight; subjecting the tobacco material to a process pressure of at least about 5.17 · 10 8 Pa [75,000 psi] for a holding time in the range of about 180 seconds to about 300 seconds to form a high pressure processed tobacco material; wherein the high pressure processed tobacco material has a storage stability of at least about 25 days at a temperature of about 37°C, and wherein the storage stability is defined as an aerobic plate count below about 3,000,000 CFU/g. receiving a tobacco material having at least about 40% water based on the total weight; subjecting the tobacco material to a process pressure of at least about 5.17 · 10 8 Pa [75,000 psi] for a holding time in the range of about 180 seconds to about 300 seconds to form a high pressure processed tobacco material; wherein the high pressure processed tobacco material has a storage stability of at least about 25 days at a temperature of about 37°C, and wherein the storage stability is defined as an aerobic plate count below about 3,000,000 CFU/g.
An alternative twin cylinder air compressor comprising: - a first and a second pumping unit, said two pumping units being arranged in line and having respective cylinders , - an electric motor (EM) interposed between said first and second pumping unit, comprising a respective axis of rotation (A), said cylinders extending transversely to said axis (A) of rotation, - pneumatic connection means designed to allow the flow of air towards and away from said cylinders , characterised in that it comprises, interposed between the cylinders , a containment body for containing the pneumatic connection means , the containment body comprising a chamber for housing a filter for the air and defining at least one intake conduit for air intake, in common for the cylinders , the intake conduit extending transversely relative to the axis (A) of rotation of the electric motor (EM) and leading to the inside of said chamber . - a first and a second pumping unit, said two pumping units being arranged in line and having respective cylinders , - an electric motor (EM) interposed between said first and second pumping unit, comprising a respective axis of rotation (A), said cylinders extending transversely to said axis (A) of rotation, - pneumatic connection means designed to allow the flow of air towards and away from said cylinders , characterised in that it comprises, interposed between the cylinders , a containment body for containing the pneumatic connection means , the containment body comprising a chamber for housing a filter for the air and defining at least one intake conduit for air intake, in common for the cylinders , the intake conduit extending transversely relative to the axis (A) of rotation of the electric motor (EM) and leading to the inside of said chamber .
A multilayer active oxygen barrier film comprising a multilayer oxygen barrier component comprising at least one of i) an active oxygen barrier layer that is disposed between two opposing passive oxygen barrier layers, or ii) a passive oxygen barrier layer that is disposed between two opposing active oxygen barrier layers, wherein the active oxygen barrier layer(s) and the passive oxygen barrier layer(s) are in direct contact with each other; wherein the active oxygen barrier layer comprises an oxygen scavenging composition that is a blend of: (A) a thermoplastic resin having carbon-carbon double bonds substantially in its main chain, which is at least one resin selected from the group consisting of polybutadiene, polyisoprene, polychloroprene, and polyoctenylene; (B) a transition metal salt; and (C) an oxygen barrier polymer, wherein the passive oxygen barrier layer(s) have an oxygen permeability measured according to ASTM D-3985 of 20cc-20μm/(m 2 -day-atm) or less at 65% RH and 20°C, wherein the multilayer oxygen barrier component is disposed between an outer sealant layer and an outer abuse layer, and wherein the film has an oxygen scavenging rate that is at least 0.01 cc oxygen per day per gram of the oxygen scavenging composition blend. i) an active oxygen barrier layer that is disposed between two opposing passive oxygen barrier layers, or ii) a passive oxygen barrier layer that is disposed between two opposing active oxygen barrier layers, (A) a thermoplastic resin having carbon-carbon double bonds substantially in its main chain, which is at least one resin selected from the group consisting of polybutadiene, polyisoprene, polychloroprene, and polyoctenylene; (B) a transition metal salt; and (C) an oxygen barrier polymer,
A device for assisting a driver of a vehicle, in particular a utility vehicle, wherein a start-stop device is provided, by means of which an internal combustion engine, which forms a drive device of the vehicle, can be automatically turned off when the travelling vehicle stops, wherein the start-stop device has a starting device which can be operated by the driver and by way of the operation of which the turned-off internal combustion engine can be restarted, wherein a deactivation device which can be operated by the driver is provided, it being possible for the start-stop device to be deactivated for a defined deactivation time interval (Δt) by way of the operation of the deactivation device, wherein the start-stop device can be automatically reactivated once the deactivation time interval (Δt) has elapsed, characterized in that a setting device which can be operated by the driver is provided, it being possible for the deactivation time interval (Δt) to be set by the driver by means of the setting device.
Wiper blade device with at least one spring strip (10a; 10b), a wiper blade adapter and at least one liquid-conducting element (12a; 12b), characterized in that the liquid-conducting element (12a; 12b) is formed integrally with the spring strip (10a; 10b) and is provided to guide liquid past the wiper blade adapter .
A method for turning electronic book, e-book, pages in a portable terminal having an e-book function, the method comprising: displaying a page of an e-book on a screen of the portable terminal; detecting a touch in a right user interface, UI, activation region of the e-book or a left UI activation region of the e-book; displaying the right UI activation region or the left UI activation region on the at least one side of the e-book; displaying a number of page to be turned at a position adjacent to a drag on the right UI activation region or the left UI activation region, wherein the number of the page to be turned increases or decreases respectively, corresponding to the amount of the drag of the detected touch; moving to a page of the e-book corresponding to the number of the page according to releasing the drag and touch up in left direction or in right direction ; and displaying the next page corresponding to the number of increased pages or decreased pages , respectively. displaying a page of an e-book on a screen of the portable terminal; detecting a touch in a right user interface, UI, activation region of the e-book or a left UI activation region of the e-book; displaying the right UI activation region or the left UI activation region on the at least one side of the e-book; displaying a number of page to be turned at a position adjacent to a drag on the right UI activation region or the left UI activation region, wherein the number of the page to be turned increases or decreases respectively, corresponding to the amount of the drag of the detected touch; moving to a page of the e-book corresponding to the number of the page according to releasing the drag and touch up in left direction or in right direction ; and displaying the next page corresponding to the number of increased pages or decreased pages , respectively.
An agent which binds an antibody directed to Caspr2, and which comprises a peptide comprising the sequence of an extracellular portion of a Caspr2, for use in inhibiting or reducing development of an autism spectrum disorder in a fetus or an infant comprising administering an amount of said agent to a mother pregnant with the fetus or prior to the fetus being born as an infant while the mother is pregnant or extracorporeally contacting blood of a mother (i) pregnant with the fetus or (ii) prior to the fetus being born as an infant with an amount of said agent so as to reduce the blood levels of the antibody directed to Caspr2 and recirculating the blood so treated back into the mother.