mhurhangee/patent-ind-claim-en huggingface dataset:
A computer-implemented method for generating an electronic record for operating a robotics apparatus, the method comprising the steps of: providing sequences of pre-programmed instructions for mini-manipulations in a mini-manipulation library , wherein each mini-manipulation produces at least one functional result in a stage of preparing at least one food dish; sensing a sequence of observations corresponding to a chefs movements by a plurality of sensors as the chef prepares a food dish using ingredients and kitchen equipment or acquiring user input ; detecting mini-manipulations in the sequence of observations or associated with the acquired user input, wherein a detected mini-manipulation corresponds to one or more observations in the sequence of observations or to the acquired user input, and the detected mini-manipulations correspond to the preparation of the food dish; transforming the sensed sequence of observations or the acquired user input into robotic instructions based on software-implemented methods for recognizing the sequences of pre-programmed instructions for the mini-manipulations detected in the sensed sequence of observations corresponding to the chefs movements or the acquired user input, the mini-manipulations each comprising a sequence of robotic instructions, and the robotic instructions including dynamic sensing operations and robotic action operations; and storing the detected mini-manipulations and their corresponding robotic instructions in electronic media as a respective electronic record for preparing the food dish. providing sequences of pre-programmed instructions for mini-manipulations in a mini-manipulation library , wherein each mini-manipulation produces at least one functional result in a stage of preparing at least one food dish; sensing a sequence of observations corresponding to a chefs movements by a plurality of sensors as the chef prepares a food dish using ingredients and kitchen equipment or acquiring user input ; detecting mini-manipulations in the sequence of observations or associated with the acquired user input, wherein a detected mini-manipulation corresponds to one or more observations in the sequence of observations or to the acquired user input, and the detected mini-manipulations correspond to the preparation of the food dish; transforming the sensed sequence of observations or the acquired user input into robotic instructions based on software-implemented methods for recognizing the sequences of pre-programmed instructions for the mini-manipulations detected in the sensed sequence of observations corresponding to the chefs movements or the acquired user input, the mini-manipulations each comprising a sequence of robotic instructions, and the robotic instructions including dynamic sensing operations and robotic action operations; and storing the detected mini-manipulations and their corresponding robotic instructions in electronic media as a respective electronic record for preparing the food dish.
A solid freeform fabrication material set comprising: a first solid freeform fabrication liquid material including a solvent, a first resin soluble in the solvent such that 10% by mass or greater dissolves in the solvent at 25 °C, and an inorganic particulate material; and a second solid freeform fabrication liquid material including a second resin soluble in water such that 10% by mass or greater dissolves in water at 25 °C, and a colorant, wherein the second resin is reactive with the first resin. a first solid freeform fabrication liquid material including a solvent, a first resin soluble in the solvent such that 10% by mass or greater dissolves in the solvent at 25 °C, and an inorganic particulate material; and a second solid freeform fabrication liquid material including a second resin soluble in water such that 10% by mass or greater dissolves in water at 25 °C, and a colorant, wherein the second resin is reactive with the first resin.
Reduction gear with epicyclic gear train for a turbine engine , in particular for an aircraft, comprising - a planetary shaft having a rotation axis A, - a ring having an axis A extending around said planetary shaft , - planet gears distributed around said axis A, which are meshed with said ring and the planetary shaft , and - a planet support comprising members for supporting bearings of the planet gears , the supporting members having an axial extension along the rotation axis B and being evenly distributed around the axis A, and a part (20-38) holding each supporting member , characterised in that the part (20-38) holds each supporting member substantially by the middle of the axial extension thereof along the axis B thereof, and said supporting members are formed in a single piece with means for supplying said bearings with lubricating oil. - a planetary shaft having a rotation axis A, - a ring having an axis A extending around said planetary shaft , - planet gears distributed around said axis A, which are meshed with said ring and the planetary shaft , and - a planet support comprising members for supporting bearings of the planet gears , the supporting members having an axial extension along the rotation axis B and being evenly distributed around the axis A, and a part (20-38) holding each supporting member ,
A tire inflation system , comprising: an axle housing ; a sealing ring disposed on the axle housing , the sealing ring having a conduit formed therethrough; a hub rotatably disposed on the axle housing , the hub disposed adjacent the sealing ring and having a conduit formed therethrough which is in fluid communication with a conduit formed through a fastener engaged with the hub ; an inner rotary seal disposed between the sealing ring and the hub ; an outer rotary seal disposed between the sealing ring and the hub , wherein the conduit formed through the hub is in fluid communication with the conduit formed through the sealing ring through an area between the inner rotary seal and the outer rotary seal , and wherein the inner rotary seal and the outer rotary seal are spaced apart; and a bearing seal disposed between the hub and the axle housing on one of the axle housing and the hub and disposed outboard of the outer rotary seal ; characterized in that a vent is formed in the hub , wherein the vent is in fluid communication with a space confined by the bearing seal , the sealing ring and the outer rotary seal , wherein the inner rotary seal is disposed in a first recess formed in an inner surface of the hub , the outer rotary seal is disposed in a second recess formed in the inner surface of the hub , and the bearing seal is disposed in a third recess formed in the inner surface of the hub wherein the bearing seal is in sealing contact with the axle housing . an axle housing ; a sealing ring disposed on the axle housing , the sealing ring having a conduit formed therethrough; a hub rotatably disposed on the axle housing , the hub disposed adjacent the sealing ring and having a conduit formed therethrough which is in fluid communication with a conduit formed through a fastener engaged with the hub ; an inner rotary seal disposed between the sealing ring and the hub ; an outer rotary seal disposed between the sealing ring and the hub , wherein the conduit formed through the hub is in fluid communication with the conduit formed through the sealing ring through an area between the inner rotary seal and the outer rotary seal , and wherein the inner rotary seal and the outer rotary seal are spaced apart; and a bearing seal disposed between the hub and the axle housing on one of the axle housing and the hub and disposed outboard of the outer rotary seal ; characterized in that a vent is formed in the hub , wherein the vent is in fluid communication with a space confined by the bearing seal , the sealing ring and the outer rotary seal , wherein the inner rotary seal is disposed in a first recess formed in an inner surface of the hub , the outer rotary seal is disposed in a second recess formed in the inner surface of the hub , and the bearing seal is disposed in a third recess formed in the inner surface of the hub wherein the bearing seal is in sealing contact with the axle housing .
A magnetic field therapy apparatus, comprising a magnetic field generating apparatus for generating a magnetic field which can be applied to a patient , and a control apparatus for controlling a field strength of the magnetic field such that a stepwise increase of the magnetic field strength takes place during a first time period (T 1 ) and a constant field strength is generated during a second period (T 2 ), wherein the ratio of the first period (T 1 ) to the second period (T 2 ) corresponds to the golden section +/- 0.1, preferably +/- 0.01.
A seal assembly for a rotatable component having an axis of rotation , the seal assembly comprising: a first seal mounted to a housing and configured to be in sealing engagement with the rotatable component ; a second seal mounted to the housing an axial distance apart from the first seal and configured to be in sealing engagement with the rotatable component , wherein the axial distance is parallel with the axis of rotation , wherein the first seal and the second seal are mechanically retained to the housing , wherein the seal assembly further comprises a buffer fluid chamber defined between the first seal and the second seal ; wherein the seal assembly further comprises a spacer disposed between the first seal and the second seal , wherein the spacer includes holes, slots, apertures or other passageways to allow buffer fluid to pressurize the buffer fluid chamber, characterised by a buffer fluid inlet extending through one or more walls of the rotatable component and configured for buffer fluid comprising air or a combustion gas to flow radially outward through the buffer fluid inlet and into the buffer fluid chamber . a first seal mounted to a housing and configured to be in sealing engagement with the rotatable component ; a second seal mounted to the housing an axial distance apart from the first seal and configured to be in sealing engagement with the rotatable component , wherein the axial distance is parallel with the axis of rotation , wherein the first seal and the second seal are mechanically retained to the housing , wherein the seal assembly further comprises a buffer fluid chamber defined between the first seal and the second seal ; wherein the seal assembly further comprises a spacer disposed between the first seal and the second seal , wherein the spacer includes holes, slots, apertures or other passageways to allow buffer fluid to pressurize the buffer fluid chamber, characterised by a buffer fluid inlet extending through one or more walls of the rotatable component and configured for buffer fluid comprising air or a combustion gas to flow radially outward through the buffer fluid inlet and into the buffer fluid chamber .
A method performed by a radio access network node for selecting a transmit or receive beam for communication with a wireless device in a communication network, the radio access network node comprising a plurality of antenna elements configurable to provide a plurality of transmit or receive beams , the communication network further comprising one or more wireless light communication, LC, network nodes , the method comprising: obtaining information identifying a wireless LC network node to which the wireless device is connected; based on the identified wireless LC network node, selecting a subset of the plurality of transmit or receive beams; and initiating a beam-sweeping procedure using the subset of transmit or receive beams to select a transmit or receive beam for communication with the wireless device. obtaining information identifying a wireless LC network node to which the wireless device is connected; based on the identified wireless LC network node, selecting a subset of the plurality of transmit or receive beams; and initiating a beam-sweeping procedure using the subset of transmit or receive beams to select a transmit or receive beam for communication with the wireless device.
A composition for oral administration comprising: 5-azacytidine , tetrahydrouridine (THU) or 2'-fluorinated tetrahydrouridine (2'-F-THU), and a pharmaceutically acceptable excipient, wherein the composition comprises 5-azacytidine in an amount suitable to provide about 10 to about 100 mg/m 2 of 5-azacytidine and tetrahydrouridine or 2'-fluorinated tetrahydrouridine in an amount suitable to provide about 400 to 500 mg/m 2 of tetrahydrouridine or 2'-fluorinated tetrahydrouridine, for use in a method of treating a cancer or a blood disorder, wherein said method comprises administering the composition for oral administration to a patient sequentially or alternately or simultaneously with a composition comprising decitabine, tetrahydrouridine or 2'-fluorinated tetrahydrouridine, and a pharmaceutically acceptable carrier. 5-azacytidine , tetrahydrouridine (THU) or 2'-fluorinated tetrahydrouridine (2'-F-THU), and a pharmaceutically acceptable excipient, wherein the composition comprises 5-azacytidine in an amount suitable to provide about 10 to about 100 mg/m 2 of 5-azacytidine and tetrahydrouridine or 2'-fluorinated tetrahydrouridine in an amount suitable to provide about 400 to 500 mg/m 2 of tetrahydrouridine or 2'-fluorinated tetrahydrouridine,
A method for determining purity in a sample of OXY133 monohydrate, the method comprising: providing an HPLC eluent comprising OXY133 monohydrate , OXY133 monohydrate impurities and a mobile volatile phase; generating an aerosol of liquid droplets from the HPLC eluent; drying the droplets to obtain residue particles comprising OXY133 monohydrate and OXY133 monohydrate impurities; contacting the residue particles with an ion stream which applies a size-dependent electrical charge to each of the residue particles to generate an electrical signal having a level proportional to the amount of charged residue particles; and measuring the electrical signal to determine the purity of the OXY133 monohydrate in the sample. providing an HPLC eluent comprising OXY133 monohydrate , OXY133 monohydrate impurities and a mobile volatile phase; generating an aerosol of liquid droplets from the HPLC eluent; drying the droplets to obtain residue particles comprising OXY133 monohydrate and OXY133 monohydrate impurities; contacting the residue particles with an ion stream which applies a size-dependent electrical charge to each of the residue particles to generate an electrical signal having a level proportional to the amount of charged residue particles; and measuring the electrical signal to determine the purity of the OXY133 monohydrate in the sample.
A process for testing a combustor of a gas turbine engine under low atmospheric conditions, the process comprising the steps of: filling an underground storage reservoir with compressed air; securing a combustor to be tested on a test stand; passing compressed air from the underground storage reservoir through a heater through a first air line to increase a temperature of the compressed air; passing the heated compressed air into the combustor for testing; burning a fuel with the heated compressed air within the combustor to produce a hot gas stream, the hot gas stream being exhausted from the combustor ; and passing additional compressed air from the underground storage reservoir into an ejector located downstream of the combustor through a second air line and into the hot gas stream exhausted from the combustor to decrease a pressure at an exhaust of the combustor to simulate a low atmospheric condition. filling an underground storage reservoir with compressed air; securing a combustor to be tested on a test stand; passing compressed air from the underground storage reservoir through a heater through a first air line to increase a temperature of the compressed air; passing the heated compressed air into the combustor for testing; burning a fuel with the heated compressed air within the combustor to produce a hot gas stream, the hot gas stream being exhausted from the combustor ; and passing additional compressed air from the underground storage reservoir into an ejector located downstream of the combustor through a second air line and into the hot gas stream exhausted from the combustor to decrease a pressure at an exhaust of the combustor to simulate a low atmospheric condition.
A method of calibrating a measuring system comprising a fluid detector having a preconcentrator and a fluid sensor , wherein a concentration of a substance to be detected is measured at a sorption phase during which the fluid to be detected is enriched in the preconcentrator in a first state for a sorption time period ( t ), and at a measuring phase in which a concentration of the substance to be detected resulting from release of the substance to be detected enriched in the preconcentrator is measured, wherein the measuring system is calibrated by adjusting the sorption time period ( t ).
A brushless motor comprising: a stator disposed along an axis ; and a rotor disposed radially inward from the stator , and including a core , a plurality of first magnets and a plurality of second magnets configured to have opposite poles relative to the plurality of first magnets , and wherein the plurality of first and second magnets each have a substantially rectangular cross-section and are in contact with a substantially flat surface carried by the core that faces radially outward, wherein each one of the plurality of first and second magnets include first and second segments (30A", 30B", 32A", 32B") disposed adjacent to and spaced circumferentially apart from one-another, characterized in that the rotor includes a plurality of T-shaped retainers disposed circumferentially between the first and second segments (30A", 30B", 32A", 32B"), wherein each one of the T-shaped retainers includes a flange portion spanning circumferentially over a portion of the first and second segments (30A", 30B", 32A", 32B") of each one of the plurality of first and second magnets , and a base portion engaged to and projecting radially between the core and the flange portion , wherein the rotor includes a plurality of ribs (34") projecting radially outward from the core and distributed circumferentially between each one of the plurality of first and second magnets . a stator disposed along an axis ; and a rotor disposed radially inward from the stator , and including a core , a plurality of first magnets and a plurality of second magnets configured to have opposite poles relative to the plurality of first magnets , and wherein the plurality of first and second magnets each have a substantially rectangular cross-section and are in contact with a substantially flat surface carried by the core that faces radially outward, wherein each one of the plurality of first and second magnets include first and second segments (30A", 30B", 32A", 32B") disposed adjacent to and spaced circumferentially apart from one-another, characterized in that the rotor includes a plurality of T-shaped retainers disposed circumferentially between the first and second segments (30A", 30B", 32A", 32B"), wherein each one of the T-shaped retainers includes a flange portion spanning circumferentially over a portion of the first and second segments (30A", 30B", 32A", 32B") of each one of the plurality of first and second magnets , and a base portion engaged to and projecting radially between the core and the flange portion , wherein the rotor includes a plurality of ribs (34") projecting radially outward from the core and distributed circumferentially between each one of the plurality of first and second magnets .
A blood flow regulating device for a vessel, comprising: a delivery catheter extending along a longitudinal axis; and a vessel shaping device having a retracted configuration in the delivery catheter and an expanded configuration out of the delivery catheter , the vessel shaping device being arranged to expand to the expanded configuration along a transverse axis, perpendicular to the longitudinal axis of the delivery catheter , to reshape the vessel to a flattened configuration, wherein the vessel shaping device comprises a frame including a first arm extending transversely outward from the central longitudinal axis to define a first apex , and a second arm extending transversely outward from the central longitudinal axis in an opposite direction from the first arm to define a second apex , a proximal end of the first arm and a proximal end of the second arm are coupled to a proximal collar , and a distal end of the first arm and a distal end of the second arm are coupled to a distal collar , characterized in that : the vessel shaping device further comprises a first stability member extending across the first apex from a proximal portion of the first arm to a distal portion of the first arm , and a second stability member extending across the second apex from a proximal portion of the second arm to a distal portion of the second arm . a delivery catheter extending along a longitudinal axis; and a vessel shaping device having a retracted configuration in the delivery catheter and an expanded configuration out of the delivery catheter , the vessel shaping device being arranged to expand to the expanded configuration along a transverse axis, perpendicular to the longitudinal axis of the delivery catheter , to reshape the vessel to a flattened configuration, wherein the vessel shaping device comprises a frame including a first arm extending transversely outward from the central longitudinal axis to define a first apex , and a second arm extending transversely outward from the central longitudinal axis in an opposite direction from the first arm to define a second apex , a proximal end of the first arm and a proximal end of the second arm are coupled to a proximal collar , and a distal end of the first arm and a distal end of the second arm are coupled to a distal collar , characterized in that : the vessel shaping device further comprises a first stability member extending across the first apex from a proximal portion of the first arm to a distal portion of the first arm , and a second stability member extending across the second apex from a proximal portion of the second arm to a distal portion of the second arm .
A wind turbine comprising a tower ; a nacelle supported by said tower; a rotor supported by said nacelle; at least one unit to be cooled and arranged in the tower or the nacelle; a tower-mounted heat exchange structure arranged outside the nacelle and tower; and a circuit facilitating flow of a fluid medium between the at least one unit and the heat exchange structure, wherein the heat exchange structure comprises at least one set of panels, said set of panels comprising at least a first panel and a second panel each having a generally planar shape and having a mutual angle therebetween of between 5° and 175°, said first panel and said second panel being arranged in a V-shape extending out from said tower, characterized in that said first panel and said second panel are mounted proximate each other on the same fixation structure with a distance between these of less than half the width of one of said first and second panels.