mhurhangee/patent-ind-claim-en huggingface dataset:
A railway vehicle comprising at least one car and at least one bogie carrying the car , the bogie comprising a chassis and a secondary suspension system between the chassis and the car , the secondary suspension system , comprising: - a set of springs mounted between the chassis and the car ; - a jack comprising two ends extending along a same axis (X); and - a supply system of the jack ; the jack being configured to go from a first so-called retracted configuration in which the jack is only connected to the car by the first end of the jack , to a second so-called deployed configuration in which the jack is also connected to the chassis by the second end of the jack , the power supply device being configured, in the deployed configuration, to supply the jack so as to move the car away from the chassis or to keep the distance between the car and the chassis constant, characterized in that the first end of the jack is connected to the car by a knuckle joint-type connection . - a set of springs mounted between the chassis and the car ; - a jack comprising two ends extending along a same axis (X); and - a supply system of the jack ;
A polymerization reactor comprising: (i) a first portion having a cylindrical housing, an inlet at one end of said first portion housing, the opposed end of said first portion housing being the outlet of said first portion, where said first portion includes a rotatable shaft positioned axially within said housing and including at least two shearing paddles extending radially from said rotatable shaft; (ii) a second portion having a frustoconical housing having a first end larger than a second end, said first end constituting an inlet to said second portion and coextensive with said opposed end of said first portion housing, and an outlet at said second end, where said second portion includes a rotatable shaft positioned axially within said housing and including at least one helical flight extending radially from said rotatable shaft, wherein said helical flight extending radially from said rotatable shaft within said second portion includes a tip, and where a gap exists between said tip and said inner wall of said second portion, and; (iii) a third portion having a cylindrical housing, an inlet at one end of said third portion and coextensive with said outlet at said second end of said second portion, and an outlet proximate to an opposed end of said third portion, where said third portion includes a rotatable shaft positioned axially within said housing and including at least one helical flight extending radially from said rotatable shaft. (i) a first portion having a cylindrical housing, an inlet at one end of said first portion housing, the opposed end of said first portion housing being the outlet of said first portion, where said first portion includes a rotatable shaft positioned axially within said housing and including at least two shearing paddles extending radially from said rotatable shaft; (ii) a second portion having a frustoconical housing having a first end larger than a second end, said first end constituting an inlet to said second portion and coextensive with said opposed end of said first portion housing, and an outlet at said second end, where said second portion includes a rotatable shaft positioned axially within said housing and including at least one helical flight extending radially from said rotatable shaft, wherein said helical flight extending radially from said rotatable shaft within said second portion includes a tip, and where a gap exists between said tip and said inner wall of said second portion, and; (iii) a third portion having a cylindrical housing, an inlet at one end of said third portion and coextensive with said outlet at said second end of said second portion, and an outlet proximate to an opposed end of said third portion, where said third portion includes a rotatable shaft positioned axially within said housing and including at least one helical flight extending radially from said rotatable shaft.
Method of manufacturing semiconductor devices, the method comprising the following steps (a') providing a first semiconductor wafer having first predominantly functional devices and a few first non-functional devices in a first pitch (x,y), wherein the first devices are laterally held on the first semiconductor wafer by tethering elements; (b') providing a second semiconductor wafer having second devices in a second pitch (x',y'); (a) removing the non-functional first devices from the first semiconductor wafer in first individual transfer printing steps; (b) transferring a plurality of the first functional devices from the first wafer to the associated second devices of the second wafer in a second transfer printing step; (c) transferring individual functional first components of the first semiconductor wafer to second components without printed first components in third respective individual transfer printing steps; (a") depositing at least one insulator layer and/or at least one conductive layer on the second semiconductor wafer; (b") patterning (structuring) the at least one insulator layer and/or the at least one conductive layer on the second semiconductor wafer. (a') providing a first semiconductor wafer having first predominantly functional devices and a few first non-functional devices in a first pitch (x,y), wherein the first devices are laterally held on the first semiconductor wafer by tethering elements; (b') providing a second semiconductor wafer having second devices in a second pitch (x',y'); (a) removing the non-functional first devices from the first semiconductor wafer in first individual transfer printing steps; (b) transferring a plurality of the first functional devices from the first wafer to the associated second devices of the second wafer in a second transfer printing step; (c) transferring individual functional first components of the first semiconductor wafer to second components without printed first components in third respective individual transfer printing steps; (a") depositing at least one insulator layer and/or at least one conductive layer on the second semiconductor wafer; (b") patterning (structuring) the at least one insulator layer and/or the at least one conductive layer on the second semiconductor wafer.
A method of determining a drop delay of a flow stream in a flow cytometer, the method comprising: flowing a liquid sample containing particles through a detection region of the flow cytometer, wherein the detection region comprises a flow cell having: an input, into which the liquid sample is introduced, an interrogation point, and a nozzle from which a flow stream of the liquid sample exits the flow cell; wherein the flow stream exits the nozzle as a continuous flow stream that transitions to a stream of liquid droplets at a break off point, wherein the break off point is a point at which, upstream from the break off point, the flow stream is a continuous and connected fluidic stream and, downstream from the break off point, the flow stream is composed of a plurality of droplets having no physical contact with each other; capturing images of the flow stream to obtain an imaged flow stream; identifying a disturbance comprising a change at the break off point in the imaged flow stream; calculating the drop delay of the flow stream based on the identified disturbance, wherein the drop delay is the amount of time between the time a particle is detected by the flow cytometer at the interrogation point and the time a corresponding charge is applied to a droplet at the break off point of the flow stream. flowing a liquid sample containing particles through a detection region of the flow cytometer, wherein the detection region comprises a flow cell having: an input, into which the liquid sample is introduced, an interrogation point, and a nozzle from which a flow stream of the liquid sample exits the flow cell; wherein the flow stream exits the nozzle as a continuous flow stream that transitions to a stream of liquid droplets at a break off point, wherein the break off point is a point at which, upstream from the break off point, the flow stream is a continuous and connected fluidic stream and, downstream from the break off point, the flow stream is composed of a plurality of droplets having no physical contact with each other; capturing images of the flow stream to obtain an imaged flow stream; identifying a disturbance comprising a change at the break off point in the imaged flow stream; calculating the drop delay of the flow stream based on the identified disturbance, wherein the drop delay is the amount of time between the time a particle is detected by the flow cytometer at the interrogation point and the time a corresponding charge is applied to a droplet at the break off point of the flow stream.
A method for controlling at least one pressure control mechanism in at least one turbofan engine of a multiple engine aircraft , each turbofan engine having a permitting heat exchange between ambient air and bleed air and supplying cooled bleed air, the method comprising: detecting at least one of an engine failure or a bleed system failure; detecting at least one of an ice condition or an activation of an anti-ice system; and actuating the pressure control mechanism, thereby altering the heat exchange between the ambient air and the bleed air in response to a reduction of cooled bleed air supply due to the engine failure or the bleed system failure of the multiple engine aircraft; characterized in that actuating the pressure control mechanism comprises opening a pressure relief door in the turbofan engine to increase flow of ambient air through the precooler. detecting at least one of an engine failure or a bleed system failure; detecting at least one of an ice condition or an activation of an anti-ice system; and actuating the pressure control mechanism, thereby altering the heat exchange between the ambient air and the bleed air in response to a reduction of cooled bleed air supply due to the engine failure or the bleed system failure of the multiple engine aircraft; characterized in that actuating the pressure control mechanism comprises opening a pressure relief door in the turbofan engine to increase flow of ambient air through the precooler.
Container treatment machine comprising a drive device, which has a first motor and a second motor , wherein the first motor has a first drive pinion and the second motor has a second drive pinion , or are connected in a force-transmitting manner, wherein the two motors are arranged in a fixed position relative to a bearing device , wherein a ring gear with a circular toothing and which is part of a gyroscope on which containers can be held is mounted in the bearing device such as to rotate about a rotation axis (R), wherein each of the two drive pinions of the motors mesh with the toothing of the ring gear of the gyroscope , or another connection is formed between the drive pinions of the motors and the ring gear of the gyroscope , and the two drive pinions of the motors are arranged spaced apart from one another in the circumferential direction of the toothing, characterised in that the first motor is arranged in a first column of the bearing device and the second motor is arranged in a second column of the bearing device . wherein the two motors are arranged in a fixed position relative to a bearing device , wherein a ring gear with a circular toothing and which is part of a gyroscope on which containers can be held is mounted in the bearing device such as to rotate about a rotation axis (R), wherein each of the two drive pinions of the motors mesh with the toothing of the ring gear of the gyroscope , or another connection is formed between the drive pinions of the motors and the ring gear of the gyroscope , and the two drive pinions of the motors are arranged spaced apart from one another in the circumferential direction of the toothing, characterised in that the first motor is arranged in a first column of the bearing device and the second motor is arranged in a second column of the bearing device .
A method of determining the density profile of material within a vessel comprising positioning a source of penetrating radiation having its characteristic energy level or levels at above 700 keV adjacent said vessel at a first location, positioning a radiation detector adjacent said vessel in alignment with said source to detect radiation at at least one energy level in the range 80 keV to 700 keV that has passed through a portion of said material at said first location, determining the intensity and/or energy level of said radiation at said energy level within said range, moving said source and detector to a second location displaced from said first location and determining the intensity and/or energy level of said radiation at said at least one energy level in said range at said second location, and comparing the determined intensities and/or energy levels and thereby determining the density of said material at said second location relative to its density at the first location.
A method , comprising: identifying a first connection with a network orchestrator during establishment of a second connection with the network orchestrator from a network controller; establishing a sibling session that links the second connection and the first connection at a control plane; inserting a sibling data message that identifies the sibling session into control messages sent; receiving a message from the network orchestrator over the second connection, the message including an address of the network controller associated with the second connection; and transmitting the second address of the network controller over the first connection to the network orchestrator, wherein the network orchestrator receives the second address of the network controller and associates the first connection and the second connection as a single logical connection, wherein the network orchestrator is configured to transmit the first address and the second address during setup of network edge devices. identifying a first connection with a network orchestrator during establishment of a second connection with the network orchestrator from a network controller; establishing a sibling session that links the second connection and the first connection at a control plane; inserting a sibling data message that identifies the sibling session into control messages sent; receiving a message from the network orchestrator over the second connection, the message including an address of the network controller associated with the second connection; and transmitting the second address of the network controller over the first connection to the network orchestrator, wherein the network orchestrator receives the second address of the network controller and associates the first connection and the second connection as a single logical connection, wherein the network orchestrator is configured to transmit the first address and the second address during setup of network edge devices.
A polarization independent optical isolator comprising: two polarizing separation members each configured to separate polarization components of a transmitted light; an absorptive polarizer arranged on optical paths of separated transmitted lights and corresponding to a plane of polarization of each separated transmitted light; and a Faraday rotator , wherein the Faraday rotator is arranged downstream of the absorptive polarizer in a forward direction, a half-wave plate is arranged downstream of the absorptive polarizer in the forward direction, and the polarizing separation members are a polarizing prism. two polarizing separation members each configured to separate polarization components of a transmitted light; an absorptive polarizer arranged on optical paths of separated transmitted lights and corresponding to a plane of polarization of each separated transmitted light; and a Faraday rotator , wherein the Faraday rotator is arranged downstream of the absorptive polarizer in a forward direction, a half-wave plate is arranged downstream of the absorptive polarizer in the forward direction, and the polarizing separation members are a polarizing prism.
A method of building a tire carcass on a tire building drum , the method comprising the steps of: applying one or more tire building components onto a tire building drum forming a cylindrically shaped tire carcass; placing a first and second bead onto the tire carcass so that the lateral ends of the tire carcass extend axially outwardly of the respective bead ; radially expanding a first and second bead lock mechanism into engagement with a respective first and second bead ; characterized in that the method further comprises the steps of: inflating the carcass under a pressure of less than 400 mbar into engagement with a belt and tread package while moving the beads axially inward; and continuing to move the beads axially inwardly and then turning up the outer lateral ends of the tire carcass about the respective first and second bead . applying one or more tire building components onto a tire building drum forming a cylindrically shaped tire carcass; placing a first and second bead onto the tire carcass so that the lateral ends of the tire carcass extend axially outwardly of the respective bead ; radially expanding a first and second bead lock mechanism into engagement with a respective first and second bead ; characterized in that the method further comprises the steps of: inflating the carcass under a pressure of less than 400 mbar into engagement with a belt and tread package while moving the beads axially inward; and continuing to move the beads axially inwardly and then turning up the outer lateral ends of the tire carcass about the respective first and second bead . inflating the carcass under a pressure of less than 400 mbar into engagement with a belt and tread package while moving the beads axially inward; and continuing to move the beads axially inwardly and then turning up the outer lateral ends of the tire carcass about the respective first and second bead .
A motorcycle tire pair comprising a front tire and a rear tire , wherein each of the front tire and the rear tire includes a pair of beads , a carcass extending on and between a first bead and a second bead , a tread located outward of the carcass in a radial direction, and a band located between the tread and the carcass in the radial direction, the carcass includes a large number of carcass cords aligned with each other and each tilted relative to an equator plane, and the band includes a band cord extending substantially in a circumferential direction, characterized in that a ratio (Jf/Jr) of a bending stiffness (Jf) of the band cord of the front tire to a bending stiffness (Jr) of the band cord of the rear tire is not less than 0.0 and less than 0.7. each of the front tire and the rear tire includes a pair of beads , a carcass extending on and between a first bead and a second bead , a tread located outward of the carcass in a radial direction, and a band located between the tread and the carcass in the radial direction, the carcass includes a large number of carcass cords aligned with each other and each tilted relative to an equator plane, and the band includes a band cord extending substantially in a circumferential direction, characterized in that a ratio (Jf/Jr) of a bending stiffness (Jf) of the band cord of the front tire to a bending stiffness (Jr) of the band cord of the rear tire is not less than 0.0 and less than 0.7.
Shock absorber for a motor vehicle, wherein the shock absorber is made of plastics material and intended to be secured at one end to a cross member and at the other end to a body of the vehicle, characterized in that at least one metal insert which connects the two ends of the absorber is integrated with the shock absorber , wherein the shock absorber is a hollow structure and said at least one metal insert is positioned on an interior surface of the shock absorber .
A digital radiographic image sensor panel comprising: a flexible first substrate (802; 902); an image sensor array (803; 903) formed on a first side of the first substrate (802; 902); at least one bonding pad (805; 905) formed in a peripheral region outside the image sensor array (803; 903) on the first side of the first substrate (802; 902); and a second substrate (804; 904) having a top surface attached to a second side of the first substrate (802; 902) opposite the first side, the second substrate (804; 904) comprising a scribed or perforated break line (812; 912) to enable removal of a peripheral region of the second substrate (804; 904) along the break line (812; 912); and the top surface having a first adhesive (810; 910) in a first portion thereof, wherein the first adhesive (810; 910) contacts the second side of the first substrate (802; 902) directly opposite the image sensor array (803; 903); and a second adhesive (811; 911) in a second portion thereof, wherein the second adhesive (811; 911) comprises a lower tack than the first adhesive (810; 910) and contacts the second side of the first substrate (802; 902) outside of the region directly opposite the image sensor array (803; 903). a flexible first substrate (802; 902); an image sensor array (803; 903) formed on a first side of the first substrate (802; 902); at least one bonding pad (805; 905) formed in a peripheral region outside the image sensor array (803; 903) on the first side of the first substrate (802; 902); and a second substrate (804; 904) having a top surface attached to a second side of the first substrate (802; 902) opposite the first side, the second substrate (804; 904) comprising a scribed or perforated break line (812; 912) to enable removal of a peripheral region of the second substrate (804; 904) along the break line (812; 912); and the top surface having a first adhesive (810; 910) in a first portion thereof, wherein the first adhesive (810; 910) contacts the second side of the first substrate (802; 902) directly opposite the image sensor array (803; 903); and a second adhesive (811; 911) in a second portion thereof, wherein the second adhesive (811; 911) comprises a lower tack than the first adhesive (810; 910) and contacts the second side of the first substrate (802; 902) outside of the region directly opposite the image sensor array (803; 903). a first adhesive (810; 910) in a first portion thereof, wherein the first adhesive (810; 910) contacts the second side of the first substrate (802; 902) directly opposite the image sensor array (803; 903); and a second adhesive (811; 911) in a second portion thereof, wherein the second adhesive (811; 911) comprises a lower tack than the first adhesive (810; 910) and contacts the second side of the first substrate (802; 902) outside of the region directly opposite the image sensor array (803; 903).
A pneumatic tire mounted on a rim, the pneumatic tire comprising a carcass , the carcass having one or more cord reinforced plies and a pair of bead portions, each bead portion having at least one annular bead core , a tread and a belt reinforcing structure disposed radially outward of the carcass , the bead core having a flat or substantially flat bead face or at least a flat or substantially flat portion of the bead face , the bead face being the radially innermost face of the bead core , wherein the bead face is joined together with rounded ends on each side of the bead face , characterized in that (i) the bead core has a bead face oriented at an angle (α) with respect to the axial direction of the tire in a range of from 6 to 8 degrees, and in that the angle (α) is greater than the taper angle (β) of a rim flange of a rim on which the tire is designed to be mounted; or in that (ii) the bead core has a bead face formed of a dual taper surface comprising a first flat surface and a second flat surface , the first flat surface being angled at an angle (α 1 ) in the range of from 10 to 14 degrees and the second flat surface being angled at an angle (α 2 ) in the range of from 4 to 6 degrees.