mhurhangee/patent-ind-claim-en huggingface dataset:
Abituzumab for use in the treatment of colorectal cancer (CRC) and/or metastases thereof in a subject, wherein said subject is characterised by a) high levels of one or more proteins in at least one body fluid of said subject, wherein said one or more proteins comprise: TPO (UniProt ID: P07202), and optionally b) low levels of one protein in at least one body fluid of said subject, wherein said protein is: TGM3 (UniProt ID: Q08188); and wherein said Abituzumab is to be administered to said subject, wherein the level of said protein in at least one body fluid of said subject is a) classified as high, if the respective protein level in said body fluid is at least 2 % higher than the median threshold determined for the respective protein, and b) classified as low, if the respective protein level in said body fluid is at least 2 % lower, more preferably at least 5% lower, even more preferably at least 10% lower and especially at least 25% lower than said median threshold for the respective protein. a) high levels of one or more proteins in at least one body fluid of said subject, wherein said one or more proteins comprise: TPO (UniProt ID: P07202), and optionally b) low levels of one protein in at least one body fluid of said subject, wherein said protein is: TGM3 (UniProt ID: Q08188); a) classified as high, if the respective protein level in said body fluid is at least 2 % higher than the median threshold determined for the respective protein, and b) classified as low, if the respective protein level in said body fluid is at least 2 % lower, more preferably at least 5% lower, even more preferably at least 10% lower and especially at least 25% lower than said median threshold for the respective protein.
A method of controlling association of a mobile terminal with at least a first access point in a wireless communication system comprising at least two access points and a network equipment, the mobile terminal being associated to a second access point, and the first access point having a service area adjacent or overlapping with the service area of the second access point, the method comprising: - the at least first access point receiving , from a network equipment of the wireless communication system, a command to send probe request messages to the mobile terminal; - the first access point determining, from a response received from the mobile terminal in response to the corresponding probe request message, a value representing a quality of a connection between the first access point and the mobile terminal; - the first access point transmitting the value representing the quality of the connection between the first access point and the mobile terminal to said network equipment, - the first access point receiving a command to selectively accept or reject a future association request issued by the mobile terminal, wherein the command is received from the network equipment and is based on the transmitted value representing the quality of the connection between the first access point and the mobile terminal. - the at least first access point receiving , from a network equipment of the wireless communication system, a command to send probe request messages to the mobile terminal; - the first access point determining, from a response received from the mobile terminal in response to the corresponding probe request message, a value representing a quality of a connection between the first access point and the mobile terminal; - the first access point transmitting the value representing the quality of the connection between the first access point and the mobile terminal to said network equipment, - the first access point receiving a command to selectively accept or reject a future association request issued by the mobile terminal, wherein the command is received from the network equipment and is based on the transmitted value representing the quality of the connection between the first access point and the mobile terminal.
Plant for processing incoherent plastics, comprising: - at least one container with at least one inlet of material to be processed, at least one outlet of the processed material, at least one inlet of process gas suitable for processing the material, at least one outlet of gas used for processing the material; - at least one separator (4; 5; 13) with an inlet side and with an outlet side connected to said at least one inlet of process gas; - generating means for generating a gas flow through said separator (4; 5; 13) from said inlet side to said outlet side; - analyzing means for measuring concentration of at least one contaminant in the gas in said container or in the gas coming from said at least one outlet of used gas, said analyzing means comprising at least one analysis instrument ; - control means configured to control said plant based on said concentration; characterized in that said at least one analysis instrument is configured to measure concentration of said at least one contaminant by gas chromatographic analysis and in that said at least one contaminant is limonene. - at least one container with at least one inlet of material to be processed, at least one outlet of the processed material, at least one inlet of process gas suitable for processing the material, at least one outlet of gas used for processing the material; - at least one separator (4; 5; 13) with an inlet side and with an outlet side connected to said at least one inlet of process gas; - generating means for generating a gas flow through said separator (4; 5; 13) from said inlet side to said outlet side; - analyzing means for measuring concentration of at least one contaminant in the gas in said container or in the gas coming from said at least one outlet of used gas, said analyzing means comprising at least one analysis instrument ; - control means configured to control said plant based on said concentration;
A container packaging comprising a container for receiving a filling material and a closure cap , wherein the container comprises a container body , a container shoulder , and an applicator fixedly connected to the container shoulder , wherein the applicator comprises an applicator base section (5.1) and an applicator dispensing section (5.2) with a dispensing opening , and the applicator has an external thread in the area of the applicator base section (5.1), wherein the closure cap has a sheath section (2.1) and a cover section (2.2), and the closure cap in its sheath section (2.1) has an internal thread corresponding to the external thread in the applicator base section (5.1), wherein the dispensing opening is arranged offset to the axis of rotation (D) of the external thread of the applicator base section (5.1), wherein the closure cap has a circumferential groove concentric to the axis of rotation (D) in the area of its cover section (2.2) facing the sheath section (2.1), wherein the groove interacts with the applicator dispensing section (5.2) in such a way that during a screwing of the closure cap to the container , carried out by aid of the external thread of the applicator base section (5.1) and the internal thread of the sheath section (2.1) of the closure cap , the applicator dispensing section (5.2) with its dispensing opening engages into the groove and the dispensing opening is closed in the groove , wherein the groove has a width (B) and the dispensing opening has an outer diameter (A), characterized in that the width (B) of the groove is at most of 1.2 times the outer diameter (A) of the dispensing opening .
A method of mounting a trailer skirt to a trailer , comprising: attaching a skirt-supporting member to a trailer in a cantilevered configuration, and, operably coupling a trailer skirt to the skirt-supporting member , the coupling being a sliding coupling between the trailer skirt and the skirt-supporting member permitting sliding of the trailer skirt relative to the skirt-supporting member when the trailer skirt bends, where the skirt-supporting member is an elongate bending member configured to elastically bend with application of a lateral force component. attaching a skirt-supporting member to a trailer in a cantilevered configuration, and, operably coupling a trailer skirt to the skirt-supporting member , the coupling being a sliding coupling between the trailer skirt and the skirt-supporting member permitting sliding of the trailer skirt relative to the skirt-supporting member when the trailer skirt bends, where the skirt-supporting member is an elongate bending member configured to elastically bend with application of a lateral force component.
An intercooled cooling system for a gas turbine engine , the intercooled cooling system comprising: a plurality of cooling stages , wherein a first cooling stage of the plurality of cooling stages is fluidly coupled to a bleed port of a compressor of the gas turbine engine to receive and cool bleed air to produce a cool bleed air; and a cooling pump fluidly coupled to the first cooling stage to receive and increase a pressure of the cool bleed air to produce a pressurized cool bleed air, wherein a second cooling stage of the plurality of cooling stages is fluidly coupled to the cooling pump to receive and cool the pressurized cool bleed air to produce an intercooled cooling air, characterised by further comprising: a valve downstream of said first cooling stage , said valve selectively delivering air into a mixing chamber where it is mixed with air from a tap that is compressed to a higher pressure than the air from said bleed port , and said valve also selectively supplying air from said first cooling stage to a use on an aircraft associated with the gas turbine engine , wherein the use is an environmental control system for an associated aircraft, said cooling pump is driven within a range of a desired speed, a clutch selectively opens to stop drive of said cooling pump , and a selection valve is positioned in said first cooling stage and downstream of a heat exchanger in said first cooling stage , and upstream of said cooling pump , said selection valve selectively diverting air around said cooling pump and to said use. a plurality of cooling stages , wherein a first cooling stage of the plurality of cooling stages is fluidly coupled to a bleed port of a compressor of the gas turbine engine to receive and cool bleed air to produce a cool bleed air; and a cooling pump fluidly coupled to the first cooling stage to receive and increase a pressure of the cool bleed air to produce a pressurized cool bleed air, wherein a second cooling stage of the plurality of cooling stages is fluidly coupled to the cooling pump to receive and cool the pressurized cool bleed air to produce an intercooled cooling air, characterised by further comprising: a valve downstream of said first cooling stage , said valve selectively delivering air into a mixing chamber where it is mixed with air from a tap that is compressed to a higher pressure than the air from said bleed port , and said valve also selectively supplying air from said first cooling stage to a use on an aircraft associated with the gas turbine engine , wherein the use is an environmental control system for an associated aircraft, said cooling pump is driven within a range of a desired speed, a clutch selectively opens to stop drive of said cooling pump , and a selection valve is positioned in said first cooling stage and downstream of a heat exchanger in said first cooling stage , and upstream of said cooling pump , said selection valve selectively diverting air around said cooling pump and to said use.
A method of hot forming a component comprising performing the following steps in order: reversibly attaching a location feature to a base element from which the component is to be formed, the location feature protruding from the base element, the location feature and the base element forming an assembly ; opening a pre-heated high-temperature forming rig containing a pre-heated forming tool ; loading the assembly into the opened forming rig by locating the location feature into a corresponding datum feature in the forming tool; closing the forming rig ; allowing the component to form at high temperature in the forming rig ; re-opening the forming rig and removing the formed component from the forming rig ; and removing the location feature from the formed component. reversibly attaching a location feature to a base element from which the component is to be formed, the location feature protruding from the base element, the location feature and the base element forming an assembly ; opening a pre-heated high-temperature forming rig containing a pre-heated forming tool ; loading the assembly into the opened forming rig by locating the location feature into a corresponding datum feature in the forming tool; closing the forming rig ; allowing the component to form at high temperature in the forming rig ; re-opening the forming rig and removing the formed component from the forming rig ; and removing the location feature from the formed component.
A self-supporting module for assembly around a heat exchanger of a boiler comprising a horizontal passage, which module has at least one hollow tubular upright (1311a-1311d, 1312a-1312p, 1411a-1411d, 1412a-1412o) intended to extend along the layers of said exchanger and that is in fluid connection with the top part of the tank of said boiler to allow the circulation of dry saturated steam in said upright (1311a-1311d, 1312a-1312p; 1411a-1411d, 1412a-1412o), the self-supporting module comprising a main part which comprises at least four vertical hollow tubular uprights (1311a-1311d; 1411a-1411d) defining a housing parallelepiped of said exchanger and a plurality of horizontal hollow tubular uprights (1312a-1312p; 1412a-1412o) extending between two adjacent vertical uprights (1311a-1311d; 1411a-1411d) and in fluid connection with these uprights (1311a-1311d; 1411a-1411d ), at least one saturated dry steam inlet (A) connected to the top part of the tank of the boiler , at least one saturated dry steam outlet (B), and the vertical tubular uprights (1311a-1311d; 1411a-1411d) and horizontal tubular uprights (1312a-1312p; 1412a-1412o) being configured to ensure the circulation of the saturated dry steam in all the uprights (1311a-1311d, 1312a-1312p; 1411a-1411d, 1412a-1412o) of the main part , the self-supporting module comprising a first plurality of screen tubes intended to be located on the outer side of the horizontal passage of the boiler , which are arranged vertically between two vertical tubular uprights (1311c, 1311d; 1411c, 1411d) of the main part of the module , and which are in fluid connection with the main part of the module , the self-supporting module comprising a secondary part adjacent to the main part and extending laterally outside said main part and comprising at least one hollow tubular upper upright and a hollow tubular lower upright which are in fluid connection with the main part of the module and between which extend a second plurality of screen tubes of which a first part (13b1, 14b1) is arranged vertically adjacent and in the same plane as the first plurality of vertical screen tubes , and a second part (13b2, 14b2) is arranged horizontally at the top part of the module , which second plurality of screen tubes is in fluid connection with the upper and lower legs of the secondary part of the module .
An elongated solar panel mounting bar , comprising a longitudinal surface between a first end and a second end of the elongated solar panel mounting bar , wherein a first groove in the longitudinal surface extends diagonally from a position close to an upper extremity of the first end towards a position close to a lower extremity of the second end , and the first groove ends before the second end , characterized in that the first groove opens into the first end , and the second end comprises a second groove in the longitudinal surface between said first groove and the upper extremity of the second end , wherein the second groove overlaps the first groove and opens into the second end . wherein a first groove in the longitudinal surface extends diagonally from a position close to an upper extremity of the first end towards a position close to a lower extremity of the second end , and the first groove ends before the second end , characterized in that the first groove opens into the first end , and the second end comprises a second groove in the longitudinal surface between said first groove and the upper extremity of the second end , wherein the second groove overlaps the first groove and opens into the second end .
A tin-plated copper-alloy material for terminal comprising: a substrate made of Cu or Cu alloy; an Sn-based surface layer formed on a surface of the substrate; and a Cu-Ni-Sn alloy layer including Ni formed between the Sn-based surface layer and the substrate, wherein the Cu-Ni-Sn alloy layer is made of: fine Cu-Ni-Sn alloy particles containing Ni not less than 10 at% and not more than 40 at% in a state of column crystal having a cross-sectional diameter of not less than 0.1 μm and not more than 0.8 μm and an aspect ratio of not less than 1.5; and coarse Cu-Ni-Sn alloy particles having a cross-sectional diameter more than 0.8 μm, wherein the coarse Cu-Ni-Sn alloy particles may include column-crystal particles, and the cross-sectional diameter of the column particles is a short length thereof; an average thickness of the Sn-based surface layer is not less than 0.2 μm and not more than 0.6 μm, an area ratio of the Cu-Ni-Sn alloy layer exposed at a surface of the Sn-based surface layer is not less than 10% and not more than 40%, and a coefficient of kinetic friction of the tin-plated copper-alloy material for terminal is not more than 0.3, wherein the coefficient of kinetic friction is measured under a load P of 0,98N; optionally comprising a barrier layer consisting of Ni or Ni alloy having a thickness of not less than 0.05 μm and not more than 0.5 μm between the substrate and the Cu-Ni-Sn alloy layer. a substrate made of Cu or Cu alloy; an Sn-based surface layer formed on a surface of the substrate; and a Cu-Ni-Sn alloy layer including Ni formed between the Sn-based surface layer and the substrate, wherein the Cu-Ni-Sn alloy layer is made of: fine Cu-Ni-Sn alloy particles containing Ni not less than 10 at% and not more than 40 at% in a state of column crystal having a cross-sectional diameter of not less than 0.1 μm and not more than 0.8 μm and an aspect ratio of not less than 1.5; and coarse Cu-Ni-Sn alloy particles having a cross-sectional diameter more than 0.8 μm, wherein the coarse Cu-Ni-Sn alloy particles may include column-crystal particles, and the cross-sectional diameter of the column particles is a short length thereof; an average thickness of the Sn-based surface layer is not less than 0.2 μm and not more than 0.6 μm, an area ratio of the Cu-Ni-Sn alloy layer exposed at a surface of the Sn-based surface layer is not less than 10% and not more than 40%, and a coefficient of kinetic friction of the tin-plated copper-alloy material for terminal is not more than 0.3, wherein the coefficient of kinetic friction is measured under a load P of 0,98N; optionally comprising a barrier layer consisting of Ni or Ni alloy having a thickness of not less than 0.05 μm and not more than 0.5 μm between the substrate and the Cu-Ni-Sn alloy layer.
A computer-implemented seismic data processing method for obtaining an image of an explored subsurface formation, the method comprising: obtaining detected data related to waves traveling through the formation; generating modeled data corresponding to the detected data, using a velocity model of the formation; back-propagating residuals representing differences between the modeled data and the detected data; updating the velocity model using a local optimization based on a deconvolution formula employing a backward propagating wavefield and a forward propagating wavefield; and imaging geophysical features of the formation based on the updated velocity model, wherein the deconvolution formula in a common shot domain used to calculate a perturbation of the velocity model is: δν x = ν 0 3 2 πρ ∫ dω i ω 3 ∇ p B ⋅ ∇ p ̅ F + p B ∇ 2 p ̅ F p F p F ̅ , where ν 0 is the initial velocity, ρ is density, p F is the forward propagating wavefield from wave source to point x, p B is the backward propagating wavefield from a receiver to point x, p F and p B being based on the velocity model and the bar denoting the complex conjugate, and ω is an angular frequency, and wherein the generating of the model data, the calculating of the differences, the back-propagating of the residuals and the updating of the velocity model are performed iteratively until a predetermined criterion is met. obtaining detected data related to waves traveling through the formation; generating modeled data corresponding to the detected data, using a velocity model of the formation; back-propagating residuals representing differences between the modeled data and the detected data; updating the velocity model using a local optimization based on a deconvolution formula employing a backward propagating wavefield and a forward propagating wavefield; and imaging geophysical features of the formation based on the updated velocity model, wherein the deconvolution formula in a common shot domain used to calculate a perturbation of the velocity model is: δν x = ν 0 3 2 πρ ∫ dω i ω 3 ∇ p B ⋅ ∇ p ̅ F + p B ∇ 2 p ̅ F p F p F ̅ , where ν 0 is the initial velocity, ρ is density, p F is the forward propagating wavefield from wave source to point x, p B is the backward propagating wavefield from a receiver to point x, p F and p B being based on the velocity model and the bar denoting the complex conjugate, and ω is an angular frequency, and wherein the generating of the model data, the calculating of the differences, the back-propagating of the residuals and the updating of the velocity model are performed iteratively until a predetermined criterion is met.