mhurhangee/patent-ind-claim-en huggingface dataset:
Inductor core for magnetic inductor, comprising a body comprising : - a body comprising a ferromagnetic material, and - several magnets (6, A1, A2, A3, A4, A5), each magnet comprising an exterior lateral face between the south pole and the north pole, said magnets being arranged relative to the others with the north pole of a magnet that is near to a south pole of a successive magnet to form a first path for circulating magnetic flux lines produced by the magnets (6, A1, A2, A3, A4, A5), said first path comprising at one end a south pole (S), and at another end a north pole (N), and in which the ferromagnetic material forms a second path for circulating said magnetic flux lines, intermediate non-magnetic zone non-magnetic zone, arranged between the poles of two successive magnets to guide the magnetic field from a magnet to another and isolate the magnetic field flowing in the magnets from the one flowing in the ferromagnetic material, said ferromagnetic material extending continuously from the south pole (S) to the north pole (N) along the magnets (6, A1, A2, A3, A4, A5), and comprising, facing the end north pole (N), a first non-magnetic zone forcing the magnetic flux lines coming out of the end north pole to take the second path and, facing the end south pole (S), a second non-magnetic zone forcing the magnetic flux lines coming out of the second path to loop back on the end south pole, said body comprising several cavities, each cavity receiving a magnet, said cavities being such that the lateral face of each magnet is at least partly surrounded by the ferromagnetic material of the body. - a body comprising a ferromagnetic material, and - several magnets (6, A1, A2, A3, A4, A5), each magnet comprising an exterior lateral face between the south pole and the north pole, said magnets being arranged relative to the others with the north pole of a magnet that is near to a south pole of a successive magnet to form a first path for circulating magnetic flux lines produced by the magnets (6, A1, A2, A3, A4, A5), said first path comprising at one end a south pole (S), and at another end a north pole (N), and in which the ferromagnetic material forms a second path for circulating said magnetic flux lines, intermediate non-magnetic zone non-magnetic zone, arranged between the poles of two successive magnets to guide the magnetic field from a magnet to another and isolate the magnetic field flowing in the magnets from the one flowing in the ferromagnetic material, said ferromagnetic material extending continuously from the south pole (S) to the north pole (N) along the magnets (6, A1, A2, A3, A4, A5), and comprising, facing the end north pole (N), a first non-magnetic zone forcing the magnetic flux lines coming out of the end north pole to take the second path and, facing the end south pole (S), a second non-magnetic zone forcing the magnetic flux lines coming out of the second path to loop back on the end south pole, said body comprising several cavities, each cavity receiving a magnet, said cavities being such that the lateral face of each magnet is at least partly surrounded by the ferromagnetic material of the body.
Method for visual quality control of high-visibility clothing by means of an electronic image evaluation system comprising the following steps: - recording at least one image of a garment , - selecting at least one partial region of the recorded garment in the image , - assessing at least some pixels in the selected partial region and determining an assessment variable of the pixels on the basis of the brightness of the pixels, - wherein selecting the at least one partial region of the recorded garment is effected on the basis of a first image of the garment and wherein selecting the at least one partial region comprises an edge recognition of reflectors of the garment , - and wherein assessing at least some pixels in the selected partial region is effected on the basis of a second image of the same garment , - wherein the first image and the second image are substantially congruent and differ from one another with regard to exposure duration, brightness, intensity and/or contrast, - wherein the first image is highly exposed or overexposed and wherein the second image is normally exposed or underexposed, - comparing the assessment variable with a predefined threshold value. - recording at least one image of a garment , - selecting at least one partial region of the recorded garment in the image , - assessing at least some pixels in the selected partial region and determining an assessment variable of the pixels on the basis of the brightness of the pixels, - wherein selecting the at least one partial region of the recorded garment is effected on the basis of a first image of the garment and wherein selecting the at least one partial region comprises an edge recognition of reflectors of the garment , - and wherein assessing at least some pixels in the selected partial region is effected on the basis of a second image of the same garment , - wherein the first image and the second image are substantially congruent and differ from one another with regard to exposure duration, brightness, intensity and/or contrast, - wherein the first image is highly exposed or overexposed and wherein the second image is normally exposed or underexposed, - comparing the assessment variable with a predefined threshold value.
A method to recover a time source for an autonomous driving vehicle, ADV, the method comprising: generating timestamps using time obtained from a local time source, while a global positioning system, GPS, time source is unavailable; determining a difference in time between first time derived from the local time source and second time derived from the GPS time source, in response to determining that the GPS time source becomes available; determining that the difference between the first time and the second time is less than a predetermined max limit; and in this case, performing a smooth recovery of the time source by gradually converging the local time source to the GPS time source within a predetermined max recovery time interval based on a predetermined time increment; and generating subsequent timestamps based on the recovered time source, wherein the subsequent timestamps are utilized to timestamp sensor data obtained from a plurality of sensors mounted on a plurality of locations of the ADV, and wherein the sensor data is utilized by a host system to perceive a driving environment surrounding the ADV and to autonomously drive the ADV based on perception data. generating timestamps using time obtained from a local time source, while a global positioning system, GPS, time source is unavailable; determining a difference in time between first time derived from the local time source and second time derived from the GPS time source, in response to determining that the GPS time source becomes available; determining that the difference between the first time and the second time is less than a predetermined max limit; and in this case, performing a smooth recovery of the time source by gradually converging the local time source to the GPS time source within a predetermined max recovery time interval based on a predetermined time increment; and generating subsequent timestamps based on the recovered time source, wherein the subsequent timestamps are utilized to timestamp sensor data obtained from a plurality of sensors mounted on a plurality of locations of the ADV, and wherein the sensor data is utilized by a host system to perceive a driving environment surrounding the ADV and to autonomously drive the ADV based on perception data.
An immunosuppressive medicament for use in the treatment of a condition in a subject in need of immunosuppressive medicament therapy, wherein the subject has a decreased risk of progressive multifocal leukoencephalopathy (PML) due to an infection of the brain by John Cunningham virus (JCV), wherein the subject's decreased risk is due to the absence of a genomic variation selected from the group consisting of: chr9:137779251, G>A and chr1:160769595, AG>A, wherein chromosome position of the genomic variation is defined with respect to UCSC hg19. wherein the subject has a decreased risk of progressive multifocal leukoencephalopathy (PML) due to an infection of the brain by John Cunningham virus (JCV), wherein the subject's decreased risk is due to the absence of a genomic variation selected from the group consisting of: chr9:137779251, G>A and chr1:160769595, AG>A, wherein chromosome position of the genomic variation is defined with respect to UCSC hg19.
A polyisocyanate composition that is obtained from an aliphatic diisocyanate including 1,6-diisocyanatohexane, the composition comprising: an isocyanurate group; a uretdione group; and a group represented by Formula (I), wherein a viscosity measured at 25°C is 200 mPa·s to 2,000 mPa·s, and in the polyisocyanate composition, a ratio of a molar amount of the group represented by Formula (I) with respect to a total molar amount of the isocyanurate group, the uretdione group, and the group represented by Formula (I) is 0.005 to 0.10; wherein in Formula (I), R 11 , R 12 , and R 13 each independently represents a hydrogen atom or a hydrocarbon group having 1 to 20 carbon atoms that may include at least any one of an ester group and an ether group. an isocyanurate group; a uretdione group; and a group represented by Formula (I), wherein a viscosity measured at 25°C is 200 mPa·s to 2,000 mPa·s, and in the polyisocyanate composition, a ratio of a molar amount of the group represented by Formula (I) with respect to a total molar amount of the isocyanurate group, the uretdione group, and the group represented by Formula (I) is 0.005 to 0.10; wherein in Formula (I), R 11 , R 12 , and R 13 each independently represents a hydrogen atom or a hydrocarbon group having 1 to 20 carbon atoms that may include at least any one of an ester group and an ether group.
A diversion apparatus comprising a diversion element , wherein said diversion element comprises: a frame ; a follower link pivotally mounted to said frame , for diverting a product, the follower link having a camming surface ; a cam ; a coupler engaged with said follower link by the cam , wherein the camming surface provides mobile location for the transfer of force from the cam to the follower link ; and an extensible and retractable input link which, in use, provides movement to the coupler and is pivotally engaged with the coupler at a first connection; wherein said input link is pivotably mounted to the frame ; and wherein said coupler is pivotally mounted to said frame between said cam and said first connection. a frame ; a follower link pivotally mounted to said frame , for diverting a product, the follower link having a camming surface ; a cam ; a coupler engaged with said follower link by the cam , wherein the camming surface provides mobile location for the transfer of force from the cam to the follower link ; and an extensible and retractable input link which, in use, provides movement to the coupler and is pivotally engaged with the coupler at a first connection; wherein said input link is pivotably mounted to the frame ; and wherein said coupler is pivotally mounted to said frame between said cam and said first connection.
Double axle drive having two drive axles and having a single drive motor arranged between the two drive axles , the axis of rotation of said drive motor extending transversely, in particular perpendicular to the drive axles , wherein a wheel set shaft can be driven by means of a drive shaft of the drive motor via in each case a transmission , wherein the entire double axle drive is arranged in a single housing unit which has two housing sections , wherein the housing sections in each case protrude beyond the drive axles in the direction of the axis of rotation of the drive motor and surround these up to 180 degrees, and wherein the housing sections are in each case closed off by a transmission cover , which is attached to the respective housing section by means of a flange connection , characterised in that the two housing sections have flange surfaces facing one another, on which the housing sections can be fixed, wherein the flange surface extends in particular perpendicular or parallel to the drive shaft .
Lid stay comprising: a base body , a setting arm with a setting contour , a hinge pin by means of which the setting arm is attached to the base body so as to be pivotable about an axis of rotation (D), a actuating drive arranged on the base body with a pressure element and with an energy accumulator , wherein the pressure element is force loaded by means of the energy accumulator , characterized in that the hinge pin is releasably fastened to the base body , wherein, in a state of the hinge pin inserted on the base body , the setting arm is mounted on the base body such that it can be pivoted via the hinge pin , and wherein, in a state of the hinge pin released from the base body , the setting arm can be removed from the base body , and that the lid stay further has a securing element , the actuating drive being supported against the securing element in a secured position of the securing element , without the pressure element of the actuating drive coming into contact with the setting contour of the setting arm , and wherein the pressure element of the actuating drive is supported against the setting contour of the setting arm in an unlocked position of the securing element and is force loaded.
An actuation unit configured for actuating a foldable wing tip portion of a wing for an aircraft , the actuation unit comprising a first housing part including a first attachment device configured for attaching the actuation unit to a fixed wing of the wing , and a second housing part including a second attachment device configured for attaching the actuation unit to a wing tip portion foldably mounted to the fixed wing , wherein the second housing part is connected to the first housing part such that it is rotatable relative to the first housing part about a main axis of rotation , wherein the second housing part includes a toothed rack having a concave shape and facing the main axis of rotation , wherein the actuation unit further comprises a drive pinion supported at the first housing part and engaging the toothed rack for driving the second housing part rotatingly relative to the first housing part , wherein the drive pinion is driven by a coupling arrangement that is configured to be coupled to an output of a motor unit , and wherein the main axis of rotation proceeds within a cross sectional extension of the actuation unit , such that the main axis of rotation intersects the actuation unit or proceeds inside of the outer boundary or contour of the actuation unit , when viewed in a cross section across the main axis of rotation . a first housing part including a first attachment device configured for attaching the actuation unit to a fixed wing of the wing , and a second housing part including a second attachment device configured for attaching the actuation unit to a wing tip portion foldably mounted to the fixed wing , wherein the second housing part is connected to the first housing part such that it is rotatable relative to the first housing part about a main axis of rotation , wherein the second housing part includes a toothed rack having a concave shape and facing the main axis of rotation , wherein the actuation unit further comprises a drive pinion supported at the first housing part and engaging the toothed rack for driving the second housing part rotatingly relative to the first housing part , wherein the drive pinion is driven by a coupling arrangement that is configured to be coupled to an output of a motor unit , and wherein the main axis of rotation proceeds within a cross sectional extension of the actuation unit , such that the main axis of rotation intersects the actuation unit or proceeds inside of the outer boundary or contour of the actuation unit , when viewed in a cross section across the main axis of rotation .
A vane or blade for a gas turbine engine comprising: an airfoil having a leading edge portion and a trailing edge portion , the airfoil further including an aerodynamic surface extending between the leading and trailing edge portions ; wherein the airfoil transitions into a hub positioned radially inward from the airfoil , the hub includes a first portion , a second portion , and an axially extending portion extending between the first and second portions ; and wherein in an intersection of the airfoil at the hub includes a fillet extending axially from the leading edge portion of the airfoil to the trailing edge portion of the airfoil , the fillet including a constant radius fillet having a first radius (R1) and a compound radius fillet having the first radius (R1) and a second radius (R2), characterised in that the constant radius fillet begins at the leading edge portion of the airfoil and extends until a transition zone , and the compound radius fillet begins axially downstream of the constant radius fillet at the transition zone and continues towards the trailing edge portion of the airfoil . an airfoil having a leading edge portion and a trailing edge portion , the airfoil further including an aerodynamic surface extending between the leading and trailing edge portions ; wherein the airfoil transitions into a hub positioned radially inward from the airfoil , the hub includes a first portion , a second portion , and an axially extending portion extending between the first and second portions ; and wherein in an intersection of the airfoil at the hub includes a fillet extending axially from the leading edge portion of the airfoil to the trailing edge portion of the airfoil , the fillet including a constant radius fillet having a first radius (R1) and a compound radius fillet having the first radius (R1) and a second radius (R2), characterised in that the constant radius fillet begins at the leading edge portion of the airfoil and extends until a transition zone , and the compound radius fillet begins axially downstream of the constant radius fillet at the transition zone and continues towards the trailing edge portion of the airfoil .
A rotor head assembly for providing vertical lift to an aircraft, comprising: a base plate ; an operating wheel rotatable around a central point, and rotatable relative the base plate ; a plurality of blades , each blade comprising a blade spar , a proximal end of each blade spar attached to the operating wheel ; whereby movement of the operating wheel causes the radial distance between the distal tip of the attached blade spar and the center of the rotor head to alter; whereby for each blade there is provided: a pitch horn (24") having an opening, said blade spar passing through the opening in a sliding fit; a pitch arm link for connecting the pitch horn (24") to a swash plate; a pitch horn base ; a first spherical bearing interacting between the pitch horn (24") and the pitch arm link , the pitch arm link interacting between the pitch horn (24") and the swash plate whereby the pitch horn (24") controls the pitch of the blade spar. characterized in that for each blade the pitch horn base comprises an opening sized to provide clearance for the pitch arm link , and aligned with a corresponding opening in the base plate , the pitch horn base being secured to the base plate by snap rings and a pitch horn base bushing through which the pitch arm link extends, thereby securing the pitch horn (24") to the base plate and permitting the pitch horn base to swivel relative to the base plate ; wherein the pitch horn (24") is rotatably retained in the pitch horn base by means of bushings . a base plate ; an operating wheel rotatable around a central point, and rotatable relative the base plate ; a plurality of blades , each blade comprising a blade spar , a proximal end of each blade spar attached to the operating wheel ; whereby movement of the operating wheel causes the radial distance between the distal tip of the attached blade spar and the center of the rotor head to alter; whereby for each blade there is provided: a pitch horn (24") having an opening, said blade spar passing through the opening in a sliding fit; a pitch arm link for connecting the pitch horn (24") to a swash plate; a pitch horn (24") having an opening, said blade spar passing through the opening in a sliding fit; a pitch arm link for connecting the pitch horn (24") to a swash plate;
A vehicle-body lower face structure, comprising: a torsion beam type of rear suspension comprising a pair of right-and-left trailing arms and a torsion beam connecting the trailing arms ; a floor under cover for airflow straightening attached to a portion of a vehicle body in front of the rear suspension so as to cover a vehicle-body lower face; and an arm cover for airflow straightening attached to a lower portion of each of the trailing arms of the rear suspension so as to cover a lower face of the trailing arm , wherein said arm cover comprises a main part and a front part which is provided in front of the main part , and the main part and the front part of the arm cover are configured such that both of the main part and the front part are respectively inclined rearwardly and downwardly, and an angle of inclination of said rearwardly-and-downwardly inclined front part is smaller than an angle of inclination of said rearwardly-and-downwardly inclined main part of the arm cover . a torsion beam type of rear suspension comprising a pair of right-and-left trailing arms and a torsion beam connecting the trailing arms ; a floor under cover for airflow straightening attached to a portion of a vehicle body in front of the rear suspension so as to cover a vehicle-body lower face; and an arm cover for airflow straightening attached to a lower portion of each of the trailing arms of the rear suspension so as to cover a lower face of the trailing arm , wherein said arm cover comprises a main part and a front part which is provided in front of the main part , and the main part and the front part of the arm cover are configured such that both of the main part and the front part are respectively inclined rearwardly and downwardly, and an angle of inclination of said rearwardly-and-downwardly inclined front part is smaller than an angle of inclination of said rearwardly-and-downwardly inclined main part of the arm cover .
A method for shunting data, comprising: determining , by a first network device in a first network, a second quality of service parameter in a second network according to a first quality of service parameter in the first network for data to be transmitted, before shunting part of the data for a user equipment to the second network for transmission to reduce a load of the first network; sending , by the first network device, the second quality of service parameter to a second network device in the second network via a control plane interface between the first network device and the second network device, so that the second network device transmits in the second network the part of the data to be transmitted according to the second quality of service parameter; and transmitting , by the first network device, part of the data to be transmitted to the second network device in the second network according to the second quality of service parameter.