mhurhangee/patent-ind-claim-en huggingface dataset:
Cosmetic or dermatological preparations in emulsion form, comprising combinations of a) honokiol and magnolol or magnolia bark extract having an effective content of honokiol and magnolol and b) sodium stearyl sulfate. a) honokiol and magnolol or magnolia bark extract having an effective content of honokiol and magnolol and b) sodium stearyl sulfate.
A turning insert comprising a top surface , an opposite bottom surface , wherein a reference plane (RP) located parallel to and between the top surface and the bottom surface , wherein a center axis (A1) extends perpendicular to the reference plane (RP), a side surface connecting the top surface and the bottom surface , a nose portion comprising a convex nose cutting edge , a first cutting edge and a second cutting edge , wherein the nose cutting edge connects the first and second cutting edges , in that in a top view the first and second cutting edges forms a nose angle (α) of 71-85° relative to each other, wherein a bisector extends equidistantly from the first and second cutting edges, in that the nose portion comprises a third convex cutting edge adjacent to the first cutting edge and a fourth cutting edge adjacent to the third convex cutting edge , in that in a top view the fourth cutting edge forms an angle (β) of 10-30° relative to the bisector , in that the bisector intersect the nose cutting edge at a nose cutting edge center point , in that the third convex cutting edge and the fourth cutting edge is connected by a first transition point , in that the first cutting edge and third convex cutting edge is connected by a second transition point , in that the top surface comprises a first protrusion , in that the first protrusion comprises a first chip breaker wall facing the fourth cutting edge , in that the first chip breaker wall is arranged between an upper border line and a lower border line , characterized in that a distance from at least a portion of the fourth cutting edge to the reference plane (RP) is increasing at increasing distance from the nose cutting edge , in that a second protrusion is arranged between the nose cutting edge and the first protrusion , in that the second protrusion intersects the bisector , in that the second protrusion comprises a second chip breaker wall , in that in a distance from the second chip breaker wall to the reference plane (RP) is shorter than a distance from the upper border line of the first chip breaker wall to the reference plane (RP).
A pressure sensitive adhesive composition comprising: an ultra-high solid polyurethane dispersion comprising: a first component, wherein said first component comprises a first polyurethane prepolymer comprising the reaction product of a polyol and polyisocyanate; a second component, wherein said second component comprises a media phase selected from the group consisting of a seed latex, wherein said seed latex is selected from the group consisting of emulsions of polyvinyl acetate, polyethylene-vinyl acetate, polyacrylic or polyacrylic-styrenic; latexes of polystyrene-butadiene, polyacrylonitrile-butadiene, or polyacrylic-butadiene; aqueous dispersions of polyethylene and polyolefin ionomers; or various aqueous dispersions of polyurethane, polyester, polyamide, epoxy resin, copolymers thereof, or alloys thereof; and a chain extender, wherein the chain extender is a diamine or a mixture of water and diamine wherein said ultra-high solid polyurethane dispersion has a solid content of at least 60 percent by weight of solid content, excluding the weight of any filler, based on the total weight of said ultra-high solid polyurethane dispersion, and a viscosity of less than 5 Pa.s (5000 cps) at 20 rpm at 21° C using spindle #4 with Brookfield viscometer. a first component, wherein said first component comprises a first polyurethane prepolymer comprising the reaction product of a polyol and polyisocyanate; a second component, wherein said second component comprises a media phase selected from the group consisting of a seed latex, wherein said seed latex is selected from the group consisting of emulsions of polyvinyl acetate, polyethylene-vinyl acetate, polyacrylic or polyacrylic-styrenic; latexes of polystyrene-butadiene, polyacrylonitrile-butadiene, or polyacrylic-butadiene; aqueous dispersions of polyethylene and polyolefin ionomers; or various aqueous dispersions of polyurethane, polyester, polyamide, epoxy resin, copolymers thereof, or alloys thereof; and a chain extender, wherein the chain extender is a diamine or a mixture of water and diamine wherein said ultra-high solid polyurethane dispersion has a solid content of at least 60 percent by weight of solid content, excluding the weight of any filler, based on the total weight of said ultra-high solid polyurethane dispersion, and a viscosity of less than 5 Pa.s (5000 cps) at 20 rpm at 21° C using spindle #4 with Brookfield viscometer.
A turbine comprising: (i) a turbine wheel having an axis , (ii) a turbine housing for defining a chamber for receiving the turbine wheel for rotation of the turbine wheel about an axis, the turbine housing further defining a gas inlet , and an annular inlet passage from the gas inlet to the chamber, (iii) a ring-shaped shroud (6; 406; 406a; 506; 606) defining a plurality of slots (30; 130; 230; 330; 530; 630; 730) and encircling the axis; and (iv) a nozzle ring (5; 405) supporting a plurality of vanes (7; 107; 207; 307; 407) which extend from the nozzle ring parallel to the axis, and project through respective ones of the slots; the shroud and nozzle ring being positioned on opposite sides of the inlet passage and rotatable relative to each other about the axis by an angular amount of at least 0.1 degrees, the turbine being characterized in that : the nozzle ring is rotatable relative to the turbine housing about the axis by at least 0.1 degree; and a rotation mechanism is provided for, in use, urging the nozzle ring to rotate around the axis in a predefined sense. (i) a turbine wheel having an axis , (ii) a turbine housing for defining a chamber for receiving the turbine wheel for rotation of the turbine wheel about an axis, the turbine housing further defining a gas inlet , and an annular inlet passage from the gas inlet to the chamber, (iii) a ring-shaped shroud (6; 406; 406a; 506; 606) defining a plurality of slots (30; 130; 230; 330; 530; 630; 730) and encircling the axis; and (iv) a nozzle ring (5; 405) supporting a plurality of vanes (7; 107; 207; 307; 407) which extend from the nozzle ring parallel to the axis, and project through respective ones of the slots; the shroud and nozzle ring being positioned on opposite sides of the inlet passage and rotatable relative to each other about the axis by an angular amount of at least 0.1 degrees, the turbine being characterized in that : the nozzle ring is rotatable relative to the turbine housing about the axis by at least 0.1 degree; and a rotation mechanism is provided for, in use, urging the nozzle ring to rotate around the axis in a predefined sense. the shroud and nozzle ring being positioned on opposite sides of the inlet passage and rotatable relative to each other about the axis by an angular amount of at least 0.1 degrees, the turbine being characterized in that : the nozzle ring is rotatable relative to the turbine housing about the axis by at least 0.1 degree; and a rotation mechanism is provided for, in use, urging the nozzle ring to rotate around the axis in a predefined sense. the nozzle ring is rotatable relative to the turbine housing about the axis by at least 0.1 degree; and a rotation mechanism is provided for, in use, urging the nozzle ring to rotate around the axis in a predefined sense.
A control method for a machine tool for machining a workpiece while causing relative movement between a tool rotated by a spindle motor and the workpiece fixed to a table, comprising the steps of: calculating an actual cutting force received from the workpiece at a predetermined position of the tool during machining of the workpiece based on a torque command value, a current command value, or an actual current value of the spindle motor , the actual cutting force acting in a radial direction of the tool ; displaying the calculated actual cutting force on a display part ; determining a determination value based on an allowable cutting force that is allowed to be applied at the predetermined position of the tool ; and reducing a relative speed of the tool with respect to the workpiece when the actual cutting force exceeds the determination value; wherein the step of determining the determination value includes a step of calculating the allowable cutting force for the tool , which relates to damage to the tool , calculating the allowable cutting force for a bearing , which relates to damage to the bearing in a spindle device and calculating the allowable cutting force for the spindle motor , which relates to damage to the spindle motor and a step of setting the determination value based on the smallest allowable cutting force among the allowable cutting force for the tool , the allowable cutting force for the bearing and the allowable cutting force for the spindle motor each time the tool is changed. calculating an actual cutting force received from the workpiece at a predetermined position of the tool during machining of the workpiece based on a torque command value, a current command value, or an actual current value of the spindle motor , the actual cutting force acting in a radial direction of the tool ; displaying the calculated actual cutting force on a display part ; determining a determination value based on an allowable cutting force that is allowed to be applied at the predetermined position of the tool ; and reducing a relative speed of the tool with respect to the workpiece when the actual cutting force exceeds the determination value; wherein the step of determining the determination value includes a step of calculating the allowable cutting force for the tool , which relates to damage to the tool , calculating the allowable cutting force for a bearing , which relates to damage to the bearing in a spindle device and calculating the allowable cutting force for the spindle motor , which relates to damage to the spindle motor and a step of setting the determination value based on the smallest allowable cutting force among the allowable cutting force for the tool , the allowable cutting force for the bearing and the allowable cutting force for the spindle motor each time the tool is changed.
A multi-spool gas turbine engine comprising: a low pressure (LP) spool ; a high pressure (HP) spool , the LP spool and the HP spool being independently rotatable from one another about a central axis , the LP spool comprising an LP compressor and an LP turbine , the HP spool comprising an HP turbine and an HP compressor ; and an accessory gear box (AGB) mounted in axial series at one end of the engine , the LP compressor being positioned between the HP compressor and the AGB ; characterized in that : the AGB is drivingly connected to the HP spool through the center of the LP compressor , wherein the AGB has an input shaft , the input shaft extending along the central axis through a central bore of the LP compressor , the input shaft of the AGB is drivingly connected to the HP compressor via a first gear train , the LP turbine is drivingly connected to an LP shaft , which is, in turn, drivingly connected to the LP compressor via a second gear train (66;66'); and the first gear train is positioned axially between the HP compressor and the LP compressor . a low pressure (LP) spool ; a high pressure (HP) spool , the LP spool and the HP spool being independently rotatable from one another about a central axis , the LP spool comprising an LP compressor and an LP turbine , the HP spool comprising an HP turbine and an HP compressor ; and an accessory gear box (AGB) mounted in axial series at one end of the engine , the LP compressor being positioned between the HP compressor and the AGB ; characterized in that : the AGB is drivingly connected to the HP spool through the center of the LP compressor , wherein the AGB has an input shaft , the input shaft extending along the central axis through a central bore of the LP compressor , the input shaft of the AGB is drivingly connected to the HP compressor via a first gear train , the LP turbine is drivingly connected to an LP shaft , which is, in turn, drivingly connected to the LP compressor via a second gear train (66;66'); and the first gear train is positioned axially between the HP compressor and the LP compressor . the AGB is drivingly connected to the HP spool through the center of the LP compressor , wherein the AGB has an input shaft , the input shaft extending along the central axis through a central bore of the LP compressor , the input shaft of the AGB is drivingly connected to the HP compressor via a first gear train , the LP turbine is drivingly connected to an LP shaft , which is, in turn, drivingly connected to the LP compressor via a second gear train (66;66'); and the first gear train is positioned axially between the HP compressor and the LP compressor .
A robotic servicing system , comprising: an evacuation system comprising a first quick connect fitting configured to mate with a quick connect valve of a vehicle; a refill system comprising a second quick connect fitting configured to mate with the quick connect valve of the vehicle; and a robotic assembly couplable to the evacuation system and the refill system , wherein the robotic servicing system further comprises a processing circuit and is configured to initiate an evacuation operation by autonomously attaching the first quick connect fitting to the quick connect valve of the vehicle; and following completion of the evacuation operation, initiate a refill operation by autonomously attaching the second quick connect fitting to the quick connect valve of the vehicle. an evacuation system comprising a first quick connect fitting configured to mate with a quick connect valve of a vehicle; a refill system comprising a second quick connect fitting configured to mate with the quick connect valve of the vehicle; and a robotic assembly couplable to the evacuation system and the refill system , wherein the robotic servicing system further comprises a processing circuit and is configured to initiate an evacuation operation by autonomously attaching the first quick connect fitting to the quick connect valve of the vehicle; and following completion of the evacuation operation, initiate a refill operation by autonomously attaching the second quick connect fitting to the quick connect valve of the vehicle.
A catalyst consisting of an alumina support, one metal selected from group VIB and one metal selected from group VIII of the periodic table, and phosphorus, in which said alumina is obtained from a kneaded and extruded boehmite gel, and in which the specific surface area of said catalyst determined in accordance with the ASTM standard D3663-03 (BET method) is in the range 60 to 150 m 2 /g, in which the metal from group VIB is molybdenum and the metal from group VIII is cobalt, in which the density of molybdenum, expressed as the number of atoms of molybdenum per nm of catalyst, is in the range 3 to 5, the Co/Mo atomic ratio is in the range 0.3 to 0.5 and the P/Mo atomic ratio is in the range 0.1 to 0.3.
Cooling element of an electrical storage device for a motor vehicle, comprising at least one first wall extending primarily in a first plane and in which is created at least one first channel and at least one second wall extending primarily in a second plane and in which is created at least one second channel , the first channel and the second channel being adapted to be taken by a heat transport fluid, characterized in that the first plane in which the first wall extends and the second plane in which the second wall extends intersect, and in that at least the first wall is configured to support the electrical storage device , and in that the cooling element comprises fluidic connection means configured to connect the first channel created in the first wall to the second channel created in the second wall, each fluidic connection means being created within said first and second walls.
A joystick device operable to provide speed, direction and steering commands for controlling a marine vessel , the joystick device comprising a movable steering lever extending on an axis (V) and adapted to be tilted from a neutral position in at least four directions including a forward, a rearward, a leftward, and a rightward direction, characterized in that : - an active length of the movable steering lever is adjustable between a first (L1) and a second (L2) lever length, - the first lever length (L1) is shorter than the second lever length (L2), - the movable steering lever comprises a first and a second movable steering lever portion, wherein a first end of the first movable steering lever portion is arranged in relation to a base at a first controllable pivot point , and a second end of the first movable steering lever portion is connected to a first end of the second first movable steering lever portion at a second controllable pivot point , allowing the active length of the movable steering lever to be adjusted without adjusting an overall length of the movable steering lever , - the movable steering lever is adjusted to the first lever length (L1) by arranging the first controllable pivot point to be fixed and the second controllable pivot point to be movable, for operating the marine vessel in a first low speed mode, and - the movable steering lever is adjusted to the second lever length (L2) by arranging the first controllable pivot point to be movable and the second controllable pivot point to be fixed, for operating the marine vessel in a second high-speed drive mode. - an active length of the movable steering lever is adjustable between a first (L1) and a second (L2) lever length, - the first lever length (L1) is shorter than the second lever length (L2), - the movable steering lever comprises a first and a second movable steering lever portion, wherein a first end of the first movable steering lever portion is arranged in relation to a base at a first controllable pivot point , and a second end of the first movable steering lever portion is connected to a first end of the second first movable steering lever portion at a second controllable pivot point , allowing the active length of the movable steering lever to be adjusted without adjusting an overall length of the movable steering lever , - the movable steering lever is adjusted to the first lever length (L1) by arranging the first controllable pivot point to be fixed and the second controllable pivot point to be movable, for operating the marine vessel in a first low speed mode, and - the movable steering lever is adjusted to the second lever length (L2) by arranging the first controllable pivot point to be movable and the second controllable pivot point to be fixed, for operating the marine vessel in a second high-speed drive mode.
A medical device for supporting and stabilizing a head of a patient during a medical procedure, wherein the medical device is configured to connect with an operating table directly or indirectly via one or more intermediate structures, wherein the medical device comprises: (a) a central head support configured to provide subjacent support to the head of the patient; (b) a cushion connectable with the central head support, wherein the cushion is configured to contact the head of the patient, wherein the cushion comprises: (i) a first chamber configured to receive a select one of a first fluid and a first shape-conforming material; (c) two or more lateral head supports, wherein each of the two or more lateral head supports is configured to provide lateral support to the head of the patient; and (d) two or more pads configured to contact the head of the patient, wherein each of the two or more pads is connectable with a respective one of the two or more lateral head supports, wherein each of the two or more pads comprises: (i) a second chamber configured to receive a second fluid, and (ii) a third chamber configured to receive a second shape-conforming material. (a) a central head support configured to provide subjacent support to the head of the patient; (b) a cushion connectable with the central head support, wherein the cushion is configured to contact the head of the patient, wherein the cushion comprises: (i) a first chamber configured to receive a select one of a first fluid and a first shape-conforming material; (i) a first chamber configured to receive a select one of a first fluid and a first shape-conforming material; (c) two or more lateral head supports, wherein each of the two or more lateral head supports is configured to provide lateral support to the head of the patient; and (d) two or more pads configured to contact the head of the patient, wherein each of the two or more pads is connectable with a respective one of the two or more lateral head supports, wherein each of the two or more pads comprises: (i) a second chamber configured to receive a second fluid, and (ii) a third chamber configured to receive a second shape-conforming material. (i) a second chamber configured to receive a second fluid, and (ii) a third chamber configured to receive a second shape-conforming material.
An electroluminescent device , comprising a first electrode ; a hole transport layer disposed on the first electrode and comprising a first organic material having a conjugated structure; an emission layer disposed directly on the hole transport layer and comprising a plurality of light emitting particles; an electron transport layer disposed on the emission layer; and a second electrode disposed on the electron transport layer wherein at least one of the light emitting particles comprises a core and a hydrophilic ligand attached to a surface of the core, wherein the hole transport layer has a first thickness and a second thickness at any two point locations, and the first thickness and the second thickness satisfy Equation 1 t 1 − t 2 t 1 × 100 ≤ A wherein, in Equation 1, t 1 is the first thickness, t 2 is the second thickness, t 1 -t 2 ≥0, t 1 >0, t 2 >0, and 0≤A≤25, and characterized in that the first organic material comprises a compound represented by Chemical Formula 1, Chemical Formula 2, or a bicarbazole compound: a first electrode ; a hole transport layer disposed on the first electrode and comprising a first organic material having a conjugated structure; an emission layer disposed directly on the hole transport layer and comprising a plurality of light emitting particles; an electron transport layer disposed on the emission layer; and a second electrode disposed on the electron transport layer wherein at least one of the light emitting particles comprises a core and a hydrophilic ligand attached to a surface of the core, wherein the hole transport layer has a first thickness and a second thickness at any two point locations, and the first thickness and the second thickness satisfy Equation 1 t 1 − t 2 t 1 × 100 ≤ A wherein, in Equation 1, t 1 is the first thickness, t 2 is the second thickness, t 1 -t 2 ≥0, t 1 >0, t 2 >0, and 0≤A≤25, and characterized in that the first organic material comprises a compound represented by Chemical Formula 1, Chemical Formula 2, or a bicarbazole compound: