mhurhangee/patent-ind-claim-en huggingface dataset:
Method for inspecting, on a metallic coated coil being wound, the coating thickness homogeneity, said method comprising the following steps: A) measuring a first distance (D1) between a first reference point (R1) and a first point on the coil surface (C1) by means of a first distance measurement system (M1), B) measuring a second distance (D2) between a second reference point (R2), and a second point on the coil surface (C2) by means of a second distance measurement system (M2), - said first and second points on the coil being situated at different spots along the coil width, C) computing a difference (Δ12true) between said first distance (D1) and said second distance (D2), said difference is noted Δ12true D) saving said difference (Δ12true), E) repeating said steps A, B, C and D while moving at least one of the first or the second point on the coil surface along at least a tenth of the whole coil width, by displacing said first and second distance measurement systems along the coil width, - defining a threshold value (M), - comparing each saved difference Δ12true to said threshold value (M) or comparing a sum of differences Δ12true to said threshold value (M), - emitting an alert when said difference Δ12true or said sum of differences Δ12true is higher than said threshold value (M), wherein a build-up profile along coil width is done by using said computed differences (Δ12true). A) measuring a first distance (D1) between a first reference point (R1) and a first point on the coil surface (C1) by means of a first distance measurement system (M1), B) measuring a second distance (D2) between a second reference point (R2), and a second point on the coil surface (C2) by means of a second distance measurement system (M2), - said first and second points on the coil being situated at different spots along the coil width, - said first and second points on the coil being situated at different spots along the coil width, C) computing a difference (Δ12true) between said first distance (D1) and said second distance (D2), said difference is noted Δ12true D) saving said difference (Δ12true), E) repeating said steps A, B, C and D while moving at least one of the first or the second point on the coil surface along at least a tenth of the whole coil width, by displacing said first and second distance measurement systems along the coil width, - defining a threshold value (M), - comparing each saved difference Δ12true to said threshold value (M) or comparing a sum of differences Δ12true to said threshold value (M), - emitting an alert when said difference Δ12true or said sum of differences Δ12true is higher than said threshold value (M), - defining a threshold value (M), - comparing each saved difference Δ12true to said threshold value (M) or comparing a sum of differences Δ12true to said threshold value (M), - emitting an alert when said difference Δ12true or said sum of differences Δ12true is higher than said threshold value (M),
A method of receiving slot format related information, SFI, by a user equipment , UE, in a wireless communication system, the method characterized by comprising: receiving a first group common-physical downlink control channel, GC-PDCCH, including a first SFI at a first period based on a monitoring periodicity for GC-PDCCH monitoring; determining respective slot formats for first slots based on the first SFI; receiving a second GC-PDCCH including a second SFI at a second period based on the monitoring periodicity; and determining respective slot formats for second slots based on the second SFI, wherein a duration of slot formats indicated by the first SFI is longer than the monitoring periodicity of GC-PDCCH, wherein the second slots comprise a slot overlapping with the first slots, and wherein the second SFI is restricted to indicate a same slot format for the overlapping slot as a slot format indicated by the first SFI for the overlapping slot. receiving a first group common-physical downlink control channel, GC-PDCCH, including a first SFI at a first period based on a monitoring periodicity for GC-PDCCH monitoring; determining respective slot formats for first slots based on the first SFI; receiving a second GC-PDCCH including a second SFI at a second period based on the monitoring periodicity; and determining respective slot formats for second slots based on the second SFI, wherein a duration of slot formats indicated by the first SFI is longer than the monitoring periodicity of GC-PDCCH, wherein the second slots comprise a slot overlapping with the first slots, and wherein the second SFI is restricted to indicate a same slot format for the overlapping slot as a slot format indicated by the first SFI for the overlapping slot.
Air inlet outlet for a motor vehicle air conditioning unit , the air intake outlet being located between a front transverse edge of a windscreen of the motor vehicle and a rear transverse edge of a hood of the said motor vehicle , the outlet of the vehicle air inlet comprising: - a flashing grid extending across the intake of air ; and - a deflector configured to prevent a liquid from crashing from the windscreen on the flashing grid , the deflector consisting of a cap that extends from a rear edge of the flashing grid on the side of the front transverse edge the windscreen of the motor vehicle and the flashing grid , characterized in that the deflector includes a peripheral frame at the screen grid , the cap of the said deflector being connected to that peripheral frame through peripheral bulkheads to the said timestamp . - a flashing grid extending across the intake of air ; and - a deflector configured to prevent a liquid from crashing from the windscreen on the flashing grid , the deflector consisting of a cap that extends from a rear edge of the flashing grid on the side of the front transverse edge the windscreen of the motor vehicle and the flashing grid ,
A phosphinate copolycarbonate comprising units of the formula wherein each R a is independently a halogen atom, C 1-10 alkyl, C 1-10 haloalkyl, C 1-12 alkoxy, C 6-10 aryl, or C 6-12 haloaryl; each X a is independently a single bond, -O-, -S-, -S(O)-, -S(O) 2 -, -C(O)-, C 3-18 cycloalkylidene; a C 1-25 alkylidene of the formula -C(R c )(R d )- wherein R c and R d are each independently hydrogen, C 1-12 alkyl, C 1-12 cycloalkyl, C 1-12 arylalkyl, C 1-12 heteroalkyl, or cyclic C 7-12 heteroarylalkyl; or a group of the formula -C(=R h )-wherein R h is a divalent C 1-12 hydrocarbon group; R e and R f are independently a halogen atom, C 1-10 alkyl, C 1-10 haloalkyl, C 1-10 alkoxy, C 1-10 haloalkoxy, C 2-10 alkenyl, or C 3-10 cycloalkyl; each R g is a substituted or unsubstituted C 6-18 aryl, C 1-10 alkyl, C 1-10 haloalkyl, C 1-10 alkoxy, C 1-10 haloalkoxy, C 2-10 alkenyl, C 3-10 cycloalkyl, C 6-10 aryl, or C 6-12 haloaryl; Ar a and Ar b are each independently the same or different C 6-18 aryl; a, e, and f are each independently 0 to 4, or 0 to 2, or 0; c is 0 or 1; and x and y represent the molar ratio of each unit in the phosphinate copolycarbonate, and are 0.5:99.5 to 99.5:0.5, or 1:99 to 99:1, or 10:90 to 90:10, or 20:80 to 80:20. each R a is independently a halogen atom, C 1-10 alkyl, C 1-10 haloalkyl, C 1-12 alkoxy, C 6-10 aryl, or C 6-12 haloaryl; each X a is independently a single bond, -O-, -S-, -S(O)-, -S(O) 2 -, -C(O)-, C 3-18 cycloalkylidene; a C 1-25 alkylidene of the formula -C(R c )(R d )- wherein R c and R d are each independently hydrogen, C 1-12 alkyl, C 1-12 cycloalkyl, C 1-12 arylalkyl, C 1-12 heteroalkyl, or cyclic C 7-12 heteroarylalkyl; or a group of the formula -C(=R h )-wherein R h is a divalent C 1-12 hydrocarbon group; R e and R f are independently a halogen atom, C 1-10 alkyl, C 1-10 haloalkyl, C 1-10 alkoxy, C 1-10 haloalkoxy, C 2-10 alkenyl, or C 3-10 cycloalkyl; each R g is a substituted or unsubstituted C 6-18 aryl, C 1-10 alkyl, C 1-10 haloalkyl, C 1-10 alkoxy, C 1-10 haloalkoxy, C 2-10 alkenyl, C 3-10 cycloalkyl, C 6-10 aryl, or C 6-12 haloaryl; Ar a and Ar b are each independently the same or different C 6-18 aryl; a, e, and f are each independently 0 to 4, or 0 to 2, or 0; c is 0 or 1; and x and y represent the molar ratio of each unit in the phosphinate copolycarbonate, and are 0.5:99.5 to 99.5:0.5, or 1:99 to 99:1, or 10:90 to 90:10, or 20:80 to 80:20.
An optical anti-counterfeiting element, comprising: a substrate , having a first surface and a second surface which are opposite to each other; and an interference color layer located on the first surface of the substrate , the interference color layer is located in a non-hollow area of the optical anti-counterfeiting element and is not located in a hollow area , the interference color layer is a Fabry-Perot filter structure , an absorbing layer of the Fabry-Perot filter structure is in contact with the substrate , and a material of the absorbing layer is an alloy, characterized in that the alloy is formed by at least two metals, one metal forming the alloy is a gray metal, and another metal is a metal susceptible to corrosion by solution, so that when manufacturing the optical anti-counterfeiting element, the interference color layer in a hollow area is corroded completely to realize all hollowing of the interference color layer while keeping high color saturation of the optical anti-counterfeiting element. a substrate , having a first surface and a second surface which are opposite to each other; and an interference color layer located on the first surface of the substrate , the interference color layer is located in a non-hollow area of the optical anti-counterfeiting element and is not located in a hollow area , the interference color layer is a Fabry-Perot filter structure , an absorbing layer of the Fabry-Perot filter structure is in contact with the substrate , and a material of the absorbing layer is an alloy, characterized in that the alloy is formed by at least two metals, one metal forming the alloy is a gray metal, and another metal is a metal susceptible to corrosion by solution, so that when manufacturing the optical anti-counterfeiting element, the interference color layer in a hollow area is corroded completely to realize all hollowing of the interference color layer while keeping high color saturation of the optical anti-counterfeiting element.
A mattress , the mattress comprising: one or more climate units , the one or more climate units comprising: one or more fan units , each fan unit comprising one or more fan blades, characterized in that the one or more fan blades of the one or more fan units have an inner cavity , wherein the inner cavity of the one or more fan blades of the one or more fan units is configured such that the inner cavity is partially or fully fillable with liquid. one or more fan units , each fan unit comprising one or more fan blades, characterized in that the one or more fan blades of the one or more fan units have an inner cavity , wherein the inner cavity of the one or more fan blades of the one or more fan units is configured such that the inner cavity is partially or fully fillable with liquid.
A multiple beam antenna system establishing a plurality of directive radiating beams for wireless communications, the system comprising: a spherical dielectric lens , wherein the dielectric lens has an exterior surface ; a plurality of antenna elements , wherein the antenna elements exhibit dual polarization; an element support structure connected to the plurality of antenna elements , wherein the element support structure is connected to an RF ground and positioned at a first predetermined distance from the exterior surface of the dielectric lens ; and wherein the plurality of antenna elements are connected to the element support structure and are positioned with respect to the exterior surface of the lens at a second predetermined distance from the exterior surface of the dielectric lens ; and a positioning system configured to selectively move the support structure in a rotational manner with respect to a center of the lens to modify the position of the plurality of antenna elements and their corresponding secondary radiation beams, wherein the positioning system includes a two-axis positioner attached to the element support structure by a mounting plate and configured to move the element support structure relative to the spherical dielectric lens in an azimuth direction and in an elevation direction, and wherein the secondary radiation beams are the beams generated by each of the plurality of antenna elements after a radiation of the plurality of antenna elements leaves the spherical dielectric lens . a spherical dielectric lens , wherein the dielectric lens has an exterior surface ; a plurality of antenna elements , wherein the antenna elements exhibit dual polarization; an element support structure connected to the plurality of antenna elements , wherein the element support structure is connected to an RF ground and positioned at a first predetermined distance from the exterior surface of the dielectric lens ; and wherein the plurality of antenna elements are connected to the element support structure and are positioned with respect to the exterior surface of the lens at a second predetermined distance from the exterior surface of the dielectric lens ; and a positioning system configured to selectively move the support structure in a rotational manner with respect to a center of the lens to modify the position of the plurality of antenna elements and their corresponding secondary radiation beams, wherein the positioning system includes a two-axis positioner attached to the element support structure by a mounting plate and configured to move the element support structure relative to the spherical dielectric lens in an azimuth direction and in an elevation direction, and wherein the secondary radiation beams are the beams generated by each of the plurality of antenna elements after a radiation of the plurality of antenna elements leaves the spherical dielectric lens .
A Y-tool for use with a pumping system that includes an electric submersible pump and bypass tubing , the Y-tool comprising: a slave valve assembly, wherein the slave valve assembly controls access to the bypass tubing ; a master valve assembly driven by pressure from the electric submersible pump ; and a linkage assembly connected between the master valve assembly and the slave valve assembly; characterized in that the slave valve assembly comprises a rotary ball valve ; the master valve assembly comprises: a sliding flow sleeve ; and a floating check valve assembly ; and wherein the linkage assembly is connected between the sliding flow sleeve and the rotary ball valve and configured to rotate the rotary ball valve in response to linear movement of the sliding flow sleeve . a slave valve assembly, wherein the slave valve assembly controls access to the bypass tubing ; a master valve assembly driven by pressure from the electric submersible pump ; and a linkage assembly connected between the master valve assembly and the slave valve assembly; characterized in that the slave valve assembly comprises a rotary ball valve ; the master valve assembly comprises: a sliding flow sleeve ; and a floating check valve assembly ; and a sliding flow sleeve ; and a floating check valve assembly ; and wherein the linkage assembly is connected between the sliding flow sleeve and the rotary ball valve and configured to rotate the rotary ball valve in response to linear movement of the sliding flow sleeve .
A high-strength and high-toughness non-heat-treatable die-casting aluminum-silicon alloy, characterized by comprising the following components in percentage by weight: 8.0-10.0% of Si, 0.1-0.5% of Mg, 0.5-0.8% of Mn, 0.05-0.5% of Cu, 0.05-0.2% of Ti, 0.01-0.05% of Sr, 0.01-0.1% of V, 0.01-0.15% of RE, less than 0.2% of Fe, less than or equal to 0.4% of other impurities, and a balance of Al, wherein the RE is one or more of elements La, Ce, and Er.
A distributed parachute system, for recovering an aircraft, the system comprising: a portion of the aircraft comprising a channel; a parachute (404; 450; 506) at least partially deployed along one or more dimensions and folded accordion-style in a first dimension and not folded in a direction perpendicular to the accordion-style folds to create a plurality of substantially parallel width-wise folds in said first dimension a deployment mechanism configured to deploy the parachute, the deployment mechanism comprising an explosive (504; 512) locatable in a portion of the aircraft, the explosive operative to remove the portion of the aircraft in order to expose the parachute for deployment, wherein the distributed parachute system is configured to be stored in the channel oriented along the first dimension. a portion of the aircraft comprising a channel; a parachute (404; 450; 506) at least partially deployed along one or more dimensions and folded accordion-style in a first dimension and not folded in a direction perpendicular to the accordion-style folds to create a plurality of substantially parallel width-wise folds in said first dimension a deployment mechanism configured to deploy the parachute, the deployment mechanism comprising an explosive (504; 512) locatable in a portion of the aircraft, the explosive operative to remove the portion of the aircraft in order to expose the parachute for deployment, wherein the distributed parachute system is configured to be stored in the channel oriented along the first dimension.
Method for operating an exhaust-gas aftertreatment device for a vehicle , in particular a motor vehicle, having at least one tank for storing and providing a liquid exhaust-gas aftertreatment medium, having at least one controllable delivery device for delivering the exhaust-gas aftertreatment medium, having at least two injection apparatuses which are arranged at different heights and which serve for injecting the exhaust-gas aftertreatment medium into an exhaust gas, and having at least one delivery line for connecting the tank to the at least two injection apparatuses , wherein the delivery line has at least one branch point at which the delivery line is divided into a first sub-line , which is connected to at least a first one of the injection apparatuses , and a second sub-line , which is connected to at least a second one of the injection apparatuses , wherein, for putting the exhaust-gas aftertreatment device out of operation, the delivery device is controlled so as to suck back the exhaust-gas aftertreatment medium at least from the sub-lines , characterized in that , in a first step, the exhaust-gas aftertreatment medium is sucked back from the first sub-line , which is connected to the lower injection apparatus , and only afterwards, in a second step, is the exhaust-gas aftertreatment medium sucked back from the second sub-line , which is connected to the higher injection apparatus .
A method comprising: transmitting , from a first network entity to a peer network entity , an offer to perform at least one networking function, wherein the offer includes a set of parameters indicating at least one networking capability that may be employed by the first network entity to perform the networking function; receiving , by the first network entity , from the peer network entity , a set of parameters indicating at least one networking capability that may be employed by the peer network entity to perform the networking function; determining , by the first network entity , if at least one networking capability may be employed by both the first network entity and peer network entity to perform the networking function; and if at least one networking capability may be employed by both the first network entity and peer network entity to perform the networking function, selecting at the first network entity at least one networking capability to employ to perform the networking function, transmitting the selected networking capability from the first network entity to the peer network entity , and performing the networking function at the first network entity in partnership with the peer network entity by employing the selected networking capability; wherein the networking function is a handover of a mobile station from a serving base station to a target base station , and wherein the first network entity is the serving base station , the peer network entity is the target base station , and the offer is a handover request message . transmitting , from a first network entity to a peer network entity , an offer to perform at least one networking function, wherein the offer includes a set of parameters indicating at least one networking capability that may be employed by the first network entity to perform the networking function; receiving , by the first network entity , from the peer network entity , a set of parameters indicating at least one networking capability that may be employed by the peer network entity to perform the networking function; determining , by the first network entity , if at least one networking capability may be employed by both the first network entity and peer network entity to perform the networking function; and if at least one networking capability may be employed by both the first network entity and peer network entity to perform the networking function, selecting at the first network entity at least one networking capability to employ to perform the networking function, transmitting the selected networking capability from the first network entity to the peer network entity , and performing the networking function at the first network entity in partnership with the peer network entity by employing the selected networking capability;