mhurhangee/patent-ind-claim-en huggingface dataset:
A process for treating a raw vent gas containing bitumen vapours released by at least one piece of equipment configured to carry out a step of treating a filler powder , wherein said piece of equipment is supplied with said filler powder and/or performs a mixing operation of said filler powder with said bitumen , during said step of treating said filler powder , said raw vent gas turning from a substantially powder-free normal raw vent gas , into a powder-containing raw vent gas that also contains an amount of said filler powder , said process comprising the steps of: - prearranging a gas-washing device configured to supply a washing solution containing a surfactant; - prearranging a boiler ; - first conveying said raw vent gas containing an amount of said filler powder into said gas-washing device ; - bringing said raw vent gas containing an amount of said filler powder into contact with said washing solution containing a surfactant; - removing said amount of filler powder from said powder-containing raw vent gas; - releasing, by said gas-washing device a purified vent gas substantially free from said filler powder; - second conveying said purified vent gas into said boiler and burning said purified vent gas , thus obtaining a combustion gas . - prearranging a gas-washing device configured to supply a washing solution containing a surfactant; - prearranging a boiler ; - first conveying said raw vent gas containing an amount of said filler powder into said gas-washing device ; - bringing said raw vent gas containing an amount of said filler powder into contact with said washing solution containing a surfactant; - removing said amount of filler powder from said powder-containing raw vent gas; - releasing, by said gas-washing device a purified vent gas substantially free from said filler powder; - second conveying said purified vent gas into said boiler and burning said purified vent gas , thus obtaining a combustion gas .
An electric sub-surface safety valve (eSSSV) system comprising: a master control system ; a subsea control module ; an electric sub-surface safety valve comprising dual, redundant electronic modules consisting of a first downhole electronics unit and a second downhole electronics unit that are configured to control power to a first electromagnetic actuator and a second electromagnetic actuator that move a single valve ; and wherein the subsea control module includes two independent control modules and wherein the independent control modules each include an electric sub-surface safety valve IWIS controller card, eSIC, (121a, b) and an electric sub-surface safety valve IWIS power supply card, eSIPS, (122a, b); wherein the eSIPS each respectively includes a feed-through switch (130a,b), wherein the switch enables the modules to either communicate independently or in tandem with the downhole electronic units. a master control system ; a subsea control module ; an electric sub-surface safety valve comprising dual, redundant electronic modules consisting of a first downhole electronics unit and a second downhole electronics unit that are configured to control power to a first electromagnetic actuator and a second electromagnetic actuator that move a single valve ; and wherein the subsea control module includes two independent control modules and wherein the independent control modules each include an electric sub-surface safety valve IWIS controller card, eSIC, (121a, b) and an electric sub-surface safety valve IWIS power supply card, eSIPS, (122a, b); wherein the eSIPS each respectively includes a feed-through switch (130a,b), wherein the switch enables the modules to either communicate independently or in tandem with the downhole electronic units.
A contactor assembly , comprising: a first conductor rotatable about a longitudinal axis and having a first set of axially extending protrusions and a plurality of first spaces, wherein each first space is defined as a space between two adjacent protrusions of the first set of axially extending protrusions ; and characterised by a second conductor aligned with the longitudinal axis and rotationally fixed and having a second set of axially extending protrusions and a plurality of second spaces, wherein each second space is defined as a space between two adjacent protrusions of the second set of axially extending protrusions ; wherein each protrusion of the first set of axially extending protrusions is positioned within a respective second space of the plurality of second spaces and each protrusion of the second set of axially extending protrusions is positioned within a respective first space of the plurality of first spaces; at least a subset of the first set of extending protrusions and at least a subset of the second set of protrusions are conductively connected when the first conductor is rotated about the longitudinal axis to a first rotational position; and the first set of extending protrusions and the second set of protrusions are not conductively connected when the first conductor is rotated about the longitudinal axis to a second rotational position. a first conductor rotatable about a longitudinal axis and having a first set of axially extending protrusions and a plurality of first spaces, wherein each first space is defined as a space between two adjacent protrusions of the first set of axially extending protrusions ; and characterised by a second conductor aligned with the longitudinal axis and rotationally fixed and having a second set of axially extending protrusions and a plurality of second spaces, wherein each second space is defined as a space between two adjacent protrusions of the second set of axially extending protrusions ; wherein each protrusion of the first set of axially extending protrusions is positioned within a respective second space of the plurality of second spaces and each protrusion of the second set of axially extending protrusions is positioned within a respective first space of the plurality of first spaces; at least a subset of the first set of extending protrusions and at least a subset of the second set of protrusions are conductively connected when the first conductor is rotated about the longitudinal axis to a first rotational position; and the first set of extending protrusions and the second set of protrusions are not conductively connected when the first conductor is rotated about the longitudinal axis to a second rotational position.
Sealing coupling for distribution ducts, designed to join, by their ends, distribution duct pipes of a fluid installation, comprising a tightening collar formed by an open rim having ends defining a closure assembly that, in a position of use, immobilizes the pipes to be sealed, where said closure assembly comprises respective protruding flanges joined respectively to either end of the tightening collar of the coupling , each of said protruding flanges being provided with one or more main through holes which, in the position of use, face corresponding main through holes of the other protruding flange , where at least one sealing screw and a transversal joining shaft are, in the position of use, inserted between said protruding flanges , characterized in that the closure assembly further comprises circumferential compensation means comprising one or more additional screws which, in the position of use, are inserted through one or more additional holes provided in an additional portion of each of the protruding flanges , so that said additional screws are provided in a circumferentially external position with respect to the sealing screws , where said closure assembly comprises respective protruding flanges joined respectively to either end of the tightening collar of the coupling , each of said protruding flanges being provided with one or more main through holes which, in the position of use, face corresponding main through holes of the other protruding flange , where at least one sealing screw and a transversal joining shaft are, in the position of use, inserted between said protruding flanges , characterized in that the closure assembly further comprises circumferential compensation means comprising one or more additional screws which, in the position of use, are inserted through one or more additional holes provided in an additional portion of each of the protruding flanges , so that said additional screws are provided in a circumferentially external position with respect to the sealing screws ,
A shoe comprising a sole composed of a thermoplastic material adhered to an upper shoe with a hot melt adhesive that is applied between the sole and the upper shoe, characterised in that the upper shoe is mechanically connected to the sole by adhering the upper shoe to a surface of the sole, the sole being composed of a thermoplastic material that has a melting temperature T M , the method comprising: - Heating the hot melt adhesive to a temperature T HM such that it softens; - Heating the sole such that the thermoplastic material obtains a surface temperature T SUB below T M ; - Applying the heated hot melt adhesive to the surface of the heated sole; - Applying the upper shoe to the sole to form a workpiece; - Cooling the workpiece such that the hot melt adhesive hardens; - Wherein the temperatures are chosen such that (T HM + T SUB )/2 is equal to or higher than (T M -10°C); - Wherein the workpiece is used to manufacture the shoe, whereby the method results in the absence of a borderline and/or distinct boundary between materials in Scanning Electronic Microscopy (SEM) pictures at an enlargement of 500 to 1000 times. - Heating the hot melt adhesive to a temperature T HM such that it softens; - Heating the sole such that the thermoplastic material obtains a surface temperature T SUB below T M ; - Applying the heated hot melt adhesive to the surface of the heated sole; - Applying the upper shoe to the sole to form a workpiece; - Cooling the workpiece such that the hot melt adhesive hardens; - Wherein the temperatures are chosen such that (T HM + T SUB )/2 is equal to or higher than (T M -10°C); - Wherein the workpiece is used to manufacture the shoe,
A method for stopping a loom, the loom including a control device that controls rotation of a main shaft on the basis of a predetermined command rotation rate, and an electromagnetic brake that brakes the main shaft , the control device being configured to control the rotation of the main shaft on the basis of a preset steady rotation rate in steady operation, the control device being also configured to execute a first braking step that is started at a time point at which a stop command has been generated or later, the first braking step dropping a rotation rate of the main shaft toward a predetermined stop rotation rate that is lower than the steady rotation rate; and a second braking step of actuating the electromagnetic brake at a time point at which the rotation rate has reached the stop rotation rate or later and braking the main shaft , the second braking step stopping the rotation of the main shaft , the method being characterized in that the rotation rate of the main shaft in the first braking step is dropped by changing the command rotation rate two times or more; and in that the command rotation rate is changed in the first braking step every period of one rotation or more of the main shaft .
A method for manufacturing an SOI wafer, comprising: implanting at least one gas ion selected from a hydrogen ion and a rare gas ion into a bond wafer composed of silicon single crystal from a surface of the bond wafer to form a layer of the implanted ion; bonding the surface from which the ion is implanted into the bond wafer and a surface of a base wafer through an insulator film ; and then separating the bond wafer along the layer of the implanted ion to form the SOI wafer, wherein the insulator film is formed at least on all surfaces of the base wafer , and while protecting a first part of the insulator film, the first part being on a back surface on the opposite side from a bonded surface of the base wafer , a bonded wafer before separating the bond wafer along the layer of the implanted ion is brought into contact with a liquid capable of dissolving the insulator film or exposed to a gas capable of dissolving the insulator film , such that a second part of the insulator film is etched up to a location from 0.3 mm to 10 mm away from an outer circumferential edge of the bonded wafer and toward the center of the bonded wafer , the second part being interposed between the bond wafer and the base wafer . implanting at least one gas ion selected from a hydrogen ion and a rare gas ion into a bond wafer composed of silicon single crystal from a surface of the bond wafer to form a layer of the implanted ion; bonding the surface from which the ion is implanted into the bond wafer and a surface of a base wafer through an insulator film ; and then separating the bond wafer along the layer of the implanted ion to form the SOI wafer, wherein the insulator film is formed at least on all surfaces of the base wafer , and while protecting a first part of the insulator film, the first part being on a back surface on the opposite side from a bonded surface of the base wafer , a bonded wafer before separating the bond wafer along the layer of the implanted ion is brought into contact with a liquid capable of dissolving the insulator film or exposed to a gas capable of dissolving the insulator film , such that a second part of the insulator film is etched up to a location from 0.3 mm to 10 mm away from an outer circumferential edge of the bonded wafer and toward the center of the bonded wafer , the second part being interposed between the bond wafer and the base wafer .
A multimode interference coupler comprising: a multimode interference (MMI) region (411; 511) including: first and second region ends (413, 415; 515, 517) separated by a region length along a longitudinal axis (417; 509), and first and second curved edges (412, 414; 512, 513) between the first and second region ends (413, 415; 515, 517), defining the MMI region (411; 511), which varies in width along the region length ; wherein each of the first and second curved edges (412, 414; 512, 513) includes a plurality of transitions, and varies in slope relative to the longitudinal axis (417; 509) on each side of each transition; at least one port optically (401; 501, 502) coupled to the first region end (413; 515); and at least one port optically (402; 503, 505) coupled to the second region end (415; 517), wherein the plurality of transitions comprises a plurality of changes in curvature and more than three critical points in each of the first and second curved edges (412, 414; 512, 513), excluding any intersection with the first and second region ends (413, 415; 515, 517); and wherein the critical points correspond to at least two peaks and at least two valleys in each of the first and second curved edges (412, 414; 512, 513). a multimode interference (MMI) region (411; 511) including: first and second region ends (413, 415; 515, 517) separated by a region length along a longitudinal axis (417; 509), and first and second curved edges (412, 414; 512, 513) between the first and second region ends (413, 415; 515, 517), defining the MMI region (411; 511), which varies in width along the region length ; wherein each of the first and second curved edges (412, 414; 512, 513) includes a plurality of transitions, and varies in slope relative to the longitudinal axis (417; 509) on each side of each transition; first and second region ends (413, 415; 515, 517) separated by a region length along a longitudinal axis (417; 509), and first and second curved edges (412, 414; 512, 513) between the first and second region ends (413, 415; 515, 517), defining the MMI region (411; 511), which varies in width along the region length ; wherein each of the first and second curved edges (412, 414; 512, 513) includes a plurality of transitions, and varies in slope relative to the longitudinal axis (417; 509) on each side of each transition; at least one port optically (401; 501, 502) coupled to the first region end (413; 515); and at least one port optically (402; 503, 505) coupled to the second region end (415; 517), wherein the plurality of transitions comprises a plurality of changes in curvature and more than three critical points in each of the first and second curved edges (412, 414; 512, 513), excluding any intersection with the first and second region ends (413, 415; 515, 517); and wherein the critical points correspond to at least two peaks and at least two valleys in each of the first and second curved edges (412, 414; 512, 513).
A method of updating flight calculations, the method comprising: flying an aircraft along a current flight path ; automatically collecting, by a receiving module , aircraft traffic information including aircraft position, type, mass or mass category from at least one of a network of aircraft operating in a nearby region or a ground station ; automatically collecting, by the receiving module , real-time weather data; predicting, by a routing module , at least one vortex with a vortex magnitude to be encountered by the current flight path based on the automatically collected aircraft traffic information and the automatically collected real-time weather data; comparing, by the routing module , the vortex magnitude to a predetermined threshold specific for the aircraft , wherein the predetermined threshold is based upon a vortex magnitude deemed too great for the aircraft to traverse; determining, by the routing module , that the vortex magnitude satisfies the predetermined threshold if the vortex magnitude exceeds the predetermined threshold; and displaying, by the advisory module , on an aircraft flight display , a suggested alternative flight path if the vortex magnitude satisfies the predetermined threshold, wherein the displaying the suggested alternative flight path further comprises determining a Strategic Lateral Offset Procedure, which defines a portion of the suggested alternative flight path. flying an aircraft along a current flight path ; automatically collecting, by a receiving module , aircraft traffic information including aircraft position, type, mass or mass category from at least one of a network of aircraft operating in a nearby region or a ground station ; automatically collecting, by the receiving module , real-time weather data; predicting, by a routing module , at least one vortex with a vortex magnitude to be encountered by the current flight path based on the automatically collected aircraft traffic information and the automatically collected real-time weather data; comparing, by the routing module , the vortex magnitude to a predetermined threshold specific for the aircraft , wherein the predetermined threshold is based upon a vortex magnitude deemed too great for the aircraft to traverse; determining, by the routing module , that the vortex magnitude satisfies the predetermined threshold if the vortex magnitude exceeds the predetermined threshold; and displaying, by the advisory module , on an aircraft flight display , a suggested alternative flight path if the vortex magnitude satisfies the predetermined threshold, wherein the displaying the suggested alternative flight path further comprises determining a Strategic Lateral Offset Procedure, which defines a portion of the suggested alternative flight path.
Socket module for an electrosurgical device, wherein the socket module has a housing , at least two connectors each with two contacts , and at least one first connection means which electrically connects a first contact of the first connector to a first contact of the second connector , characterized in that - the first connection means has two contact regions , a first contact region of which is connected to the first contact of the first connector and a second contact region of which is connected to the first contact of the second connector , in each case in a form-fitting and/or force-fitting manner, and - a circuit board is arranged in the housing and is electrically connected to the first connector , wherein the circuit board has a third contact region which connects the first connector to the circuit board in a form-fitting or force-fitting manner, and - a second connection means electrically connects a second contact of the first connector to a second contact of the second connector , wherein the second connection means has two contact regions , a first contact region of which is connected to the second contact of the first connector in a form-fitting and/or force-fitting manner and a second contact region of which is connected to the second contact of the second connector in a form-fitting and/or force-fitting manner or with a material bond, and wherein the first connection means is connected to a removable cover of the housing and the second connection means is connected to a base of the housing . - the first connection means has two contact regions , a first contact region of which is connected to the first contact of the first connector and a second contact region of which is connected to the first contact of the second connector , in each case in a form-fitting and/or force-fitting manner, and - a circuit board is arranged in the housing and is electrically connected to the first connector , wherein the circuit board has a third contact region which connects the first connector to the circuit board in a form-fitting or force-fitting manner, and - a second connection means electrically connects a second contact of the first connector to a second contact of the second connector , wherein the second connection means has two contact regions , a first contact region of which is connected to the second contact of the first connector in a form-fitting and/or force-fitting manner and a second contact region of which is connected to the second contact of the second connector in a form-fitting and/or force-fitting manner or with a material bond, and wherein the first connection means is connected to a removable cover of the housing and the second connection means is connected to a base of the housing .