mhurhangee/ep-ind-claims huggingface dataset:
Bracelet clasp, of the deployant buckle type, comprising first and second strips (2, 4) articulated to each other, by a first of their respective ends, between a closed position for wear, and at least one open position, said first strip carrying a member for attaching a first bracelet strand, said second, lower strip comprising at its second end means for adjusting the length of the bracelet, the clasp further comprising at least one locking member (38, 40) for holding said first and second strips (2, 4) in their closed position, characterised in that said length adjustment means comprise a bar movable relative to the second strip said bar is of rectangular shape and formed by a body 301, two pivots 302 arranged in the body 301 as well as two springs 303 disposed in the hollow body 301, the two pivots being able to slide in a respective end of the body 301, in that the bar carries a stud intended to be inserted into a suitable hole in the bracelet strand to define a point of anchoring of the latter to the clasp, the movable bar being able to be moved via pushers mounted on the second strip and thus to define at least two predefined positions associated with a predefined useful length of the bracelet. in that the second strip comprises two curved portions each having a recess for receiving a pusher arranged to act on the movable bar, each curved portion comprising a guide groove arranged to receive one end of the movable bar, and in that the guide groove comprises at each of its ends at least two circular spaces (271, 272) defining two distinct positions of the bar.
A hybrid tiltrotor drive system, comprising: two propulsion systems (12, 14), each propulsion system (12, 14) comprising: an engine coupled to a proprotor; an electrically controlled supplemental driver coupled to the proprotor; and a gearbox, the engine and electrically controlled supplemental driver coupled to the proprotor through the gearbox; means (78, 80, 82) for detecting the rotational speeds; an electronic control system configured to operate the supplemental driver of each propulsion system (12, 14) in response to measured or calculated rotational speeds, wherein the electronic control system is configured during a flight maneuver to actuate the supplemental driver of one of the propulsion systems (12, 14) to increase or decrease the speed of the associated proprotor, supplementing the associated engine to account for a lag time between the engines of the propulsion systems (12, 14) and maintain the proprotors of the propulsion systems (12, 14) at an equivalent rotational speed. two propulsion systems (12, 14), each propulsion system (12, 14) comprising: an engine coupled to a proprotor; an electrically controlled supplemental driver coupled to the proprotor; and a gearbox, the engine and electrically controlled supplemental driver coupled to the proprotor through the gearbox; means (78, 80, 82) for detecting the rotational speeds; an engine coupled to a proprotor; an electrically controlled supplemental driver coupled to the proprotor; and a gearbox, the engine and electrically controlled supplemental driver coupled to the proprotor through the gearbox; means (78, 80, 82) for detecting the rotational speeds; an electronic control system configured to operate the supplemental driver of each propulsion system (12, 14) in response to measured or calculated rotational speeds, wherein the electronic control system is configured during a flight maneuver to actuate the supplemental driver of one of the propulsion systems (12, 14) to increase or decrease the speed of the associated proprotor, supplementing the associated engine to account for a lag time between the engines of the propulsion systems (12, 14) and maintain the proprotors of the propulsion systems (12, 14) at an equivalent rotational speed.
A method for producing an artificial fiber, of the type of fibers produced from a polymer base, color masterbatch and UV stabilizers, characterized in that the method comprises: ✔ Mixing, in an extruder: ∘ polyolefin pellet in a percentage of between 55 and 92 % by weight with: ▪ zeolite in a percentage of between 5 and 30 % by weight, or ▪ cellulose in a percentage of between 3 and 20 % by weight ∘ color masterbatch and UV stabilizers in a percentage of 5 to 15 % by weight; ✔ heating the mixture at a temperature of 180 to 250 °C for 5 minutes; ✔ extruding the melted mixture; ✔ cooling the fiber as it exits the extruder die; ✔ drying the fiber; ✔ stretching the fiber by a ratio of between 3 and 6 at a temperature of between 90 and 120 °C; and ✔ winding and braiding the fiber by twisting it between 24 and 40 times. ✔ Mixing, in an extruder: ∘ polyolefin pellet in a percentage of between 55 and 92 % by weight with: ▪ zeolite in a percentage of between 5 and 30 % by weight, or ▪ cellulose in a percentage of between 3 and 20 % by weight ∘ color masterbatch and UV stabilizers in a percentage of 5 to 15 % by weight; ∘ polyolefin pellet in a percentage of between 55 and 92 % by weight with: ▪ zeolite in a percentage of between 5 and 30 % by weight, or ▪ cellulose in a percentage of between 3 and 20 % by weight ▪ zeolite in a percentage of between 5 and 30 % by weight, or ▪ cellulose in a percentage of between 3 and 20 % by weight ∘ color masterbatch and UV stabilizers in a percentage of 5 to 15 % by weight; ✔ heating the mixture at a temperature of 180 to 250 °C for 5 minutes; ✔ extruding the melted mixture; ✔ cooling the fiber as it exits the extruder die; ✔ drying the fiber; ✔ stretching the fiber by a ratio of between 3 and 6 at a temperature of between 90 and 120 °C; and ✔ winding and braiding the fiber by twisting it between 24 and 40 times.
A method comprising: comminuting a sheet, the sheet formed by compacting a first polyetherketoneketone (PEKK) powder or a first mixture of poly(arylene ether ketone) (PAEK) powders comprising a PEKK powder, to form a second PEKK powder or second mixture of PAEK powders comprising a PEKK powder; wherein the sheet has a thickness of 0.5 cm or less; wherein the second PEKK powder or second mixture of PAEK powders comprising a PEKK powder has a median particle diameter, as measured by laser diffraction, of between 10 microns and 2000 microns and a bulk density, as measured according to ASTM D1895, that is at least 9% greater, as compared to an uncompacted PEKK powder or mixture of PAEK powders comprising a PEKK powder having a median particle diameter of between 10 microns and 2000 microns. comminuting a sheet, the sheet formed by compacting a first polyetherketoneketone (PEKK) powder or a first mixture of poly(arylene ether ketone) (PAEK) powders comprising a PEKK powder, to form a second PEKK powder or second mixture of PAEK powders comprising a PEKK powder; wherein the sheet has a thickness of 0.5 cm or less; wherein the second PEKK powder or second mixture of PAEK powders comprising a PEKK powder has a median particle diameter, as measured by laser diffraction, of between 10 microns and 2000 microns and a bulk density, as measured according to ASTM D1895, that is at least 9% greater, as compared to an uncompacted PEKK powder or mixture of PAEK powders comprising a PEKK powder having a median particle diameter of between 10 microns and 2000 microns.
A portable air-conditioner in which a condenser and an evaporator are integrally installed, the portable air-conditioner comprising: a case in which an inlet and an outlet are formed; and an exhaust unit integrally coupled to the case and guiding air heat-exchanged with the condenser to an outdoor area, wherein the exhaust unit includes: - an exhaust pipe fixed to the case in one end thereof and disposed such that at least a portion thereof is inserted into the case, and - a shielding module fixed to the other end of the exhaust pipe and insertedly fixable to an indoor window, wherein the case includes an exhaust pipe fixing part to which the one end of the exhaust pipe is fixed and a shielding coupling recess in which the shielding module is receivable, and wherein the shielding module is fixedly caught by the shielding coupling recess according to a self-load of the exhaust pipe. a case in which an inlet and an outlet are formed; and an exhaust unit integrally coupled to the case and guiding air heat-exchanged with the condenser to an outdoor area, wherein the exhaust unit includes: - an exhaust pipe fixed to the case in one end thereof and disposed such that at least a portion thereof is inserted into the case, and - a shielding module fixed to the other end of the exhaust pipe and insertedly fixable to an indoor window, - an exhaust pipe fixed to the case in one end thereof and disposed such that at least a portion thereof is inserted into the case, and - a shielding module fixed to the other end of the exhaust pipe and insertedly fixable to an indoor window, wherein the case includes an exhaust pipe fixing part to which the one end of the exhaust pipe is fixed and a shielding coupling recess in which the shielding module is receivable, and wherein the shielding module is fixedly caught by the shielding coupling recess according to a self-load of the exhaust pipe.
Stator for an electric machine, with a stator main body which has radial stator teeth for receiving coils of an electrical winding, and the coils are continuously wound with an uninterrupted winding wire, wherein an insulating lamination with guide elements for the winding wire between the coils is arranged on an end side of the stator main body, wherein the stator has cutting-clamping elements and wherein each coil is assigned at least one receiving pocket for a cutting-clamping element on the insulating lamination, into which at least one receiving pocket the winding wire which is continuously wound in an uninterrupted manner is inserted for interconnection of the individual coils, characterized in that the cutting-clamping elements are moulded on annular conductor strips which are fitted in a plastics interconnect plate, and the cutting-clamping elements of the conductor strips are plugged axially over the winding wires into the receiving pockets (46, 47) in order to interconnect the coils to form individual phases, wherein the annular conductor strips in the interconnect plate are arranged radially next to one another and isolated from one another, and the conductor strips are fitted into annular channels which are open axially downwards, wherein the cross section of the conductor strips in the axial direction has a higher extent than in the radial direction, wherein axial centring pins are moulded on the insulating lamination and engage into corresponding centring receptacles in the interconnect plate, wherein the centring receptacles are designed as through holes, and the axial end of the centring pins is deformed by means of hot caulking in order to form a form-fitting connection with the interconnect plate. the cutting-clamping elements are moulded on annular conductor strips which are fitted in a plastics interconnect plate, and the cutting-clamping elements of the conductor strips are plugged axially over the winding wires into the receiving pockets (46, 47) in order to interconnect the coils to form individual phases, wherein the annular conductor strips in the interconnect plate are arranged radially next to one another and isolated from one another, and the conductor strips are fitted into annular channels which are open axially downwards, wherein the cross section of the conductor strips in the axial direction has a higher extent than in the radial direction, wherein axial centring pins are moulded on the insulating lamination and engage into corresponding centring receptacles in the interconnect plate, wherein the centring receptacles are designed as through holes, and the axial end of the centring pins is deformed by means of hot caulking in order to form a form-fitting connection with the interconnect plate.
A method of forming an engine component for a gas turbine engine, comprising: forming an engine component having an internal passageway, the internal passageway formed with an initial dimension; wherein the internal passageway includes at least one turbulator; and establishing a flow of machining fluid within the internal passageway, the machining fluid changing the initial dimension; characterized in that the machining fluid is provided with a Reynolds number matching an expected Reynolds number of a flow of cooling fluid within the internal passageway during operation of the gas turbine engine. forming an engine component having an internal passageway, the internal passageway formed with an initial dimension; wherein the internal passageway includes at least one turbulator; and establishing a flow of machining fluid within the internal passageway, the machining fluid changing the initial dimension; characterized in that the machining fluid is provided with a Reynolds number matching an expected Reynolds number of a flow of cooling fluid within the internal passageway during operation of the gas turbine engine.
Cosmetic spray consisting of a) an oil-in-water emulsion (O/W emulsion) comprising polyglyceryl-10 stearate and also b) a spray applicator system, wherein the spray applicator system used is a bag-on-valve applicator system, in which a bag containing the O/W emulsion is in a pressurized gas container under positive pressure. a) an oil-in-water emulsion (O/W emulsion) comprising polyglyceryl-10 stearate and also b) a spray applicator system, wherein the spray applicator system used is a bag-on-valve applicator system, in which a bag containing the O/W emulsion is in a pressurized gas container under positive pressure.
An aircraft radome comprising: - a composite structure defining at least one housing located inside or outside the composite structure and extending along the radome from a base of said radome, said at least one housing receiving an electrically conductive strip and said conductive strip being either in contact with an inner surface of an external wall of the composite structure when said at least one housing is inside the composite structure, or flush with the external wall of the composite structure when said at least one housing is outside the composite structure, - a conductive base located at the level of said radome base and connected to a ground of the aircraft, characterized in that said composite structure being devoid of any perforations or passages through the external wall at the electrically conductive strip and in that a first end of said electrically conductive strip being in contact with the conductive base. - a composite structure defining at least one housing located inside or outside the composite structure and extending along the radome from a base of said radome, said at least one housing receiving an electrically conductive strip and said conductive strip being either in contact with an inner surface of an external wall of the composite structure when said at least one housing is inside the composite structure, or flush with the external wall of the composite structure when said at least one housing is outside the composite structure, - a conductive base located at the level of said radome base and connected to a ground of the aircraft,
An implant system (100; 200; 400), comprising: a talar implant plate adapted to be positioned on a surface of a resected talus, the talar implant plate having a plurality of openings therethrough; a plurality of independently positionable pegs (120; 220; 420; 520) for attaching the talar implant plate to the resected talus, each peg having a longitudinal axis and comprising: a peg body (122; 222; 322; 422; 522) adapted to be inserted into a respective peg hole in the resected talus, the peg body having a transverse dimension (126; 226; 426; 526) in a direction normal to the longitudinal axis, the transverse dimension larger than the plurality of openings, and a retaining device (124; 224; 447; 553) separate from the peg body, the retaining device being configured to attach to the peg body through one of the plurality of openings and having at least a first portion positioned above an upper surface of the talar implant plate. a talar implant plate adapted to be positioned on a surface of a resected talus, the talar implant plate having a plurality of openings therethrough; a plurality of independently positionable pegs (120; 220; 420; 520) for attaching the talar implant plate to the resected talus, each peg having a longitudinal axis and comprising: a peg body (122; 222; 322; 422; 522) adapted to be inserted into a respective peg hole in the resected talus, the peg body having a transverse dimension (126; 226; 426; 526) in a direction normal to the longitudinal axis, the transverse dimension larger than the plurality of openings, and a retaining device (124; 224; 447; 553) separate from the peg body, the retaining device being configured to attach to the peg body through one of the plurality of openings and having at least a first portion positioned above an upper surface of the talar implant plate. a peg body (122; 222; 322; 422; 522) adapted to be inserted into a respective peg hole in the resected talus, the peg body having a transverse dimension (126; 226; 426; 526) in a direction normal to the longitudinal axis, the transverse dimension larger than the plurality of openings, and a retaining device (124; 224; 447; 553) separate from the peg body, the retaining device being configured to attach to the peg body through one of the plurality of openings and having at least a first portion positioned above an upper surface of the talar implant plate.
A method for processing a temporal envelope of an audio signal, comprising: obtaining a low-band signal of a current frame signal and a high-band signal of the current frame signal according to the received current frame signal; encoding the low-band signal of the current frame signal, to obtain a low-band encoded excitation signal; performing linear prediction on the high-band signal of the current frame signal, to obtain a linear prediction coefficient; quantizing the linear prediction coefficient, to obtain a quantized linear prediction coefficient; obtaining a predicted high-band signal according to the low-band encoded excitation signal and the quantized linear prediction coefficient; dividing the predicted high-band signal of the current frame into eight subframes; and calculating and quantizing a temporal envelope of each of the subframes, and encoding the quantized temporal envelopes; wherein the calculating a temporal envelope of each of the subframes comprises: performing windowing on the first subframe of the eight subframes and the last subframe of the eight subframes by using an asymmetric window function; and performing windowing on the subframes except the first subframe and the last subframe of the eight subframes by using a symmetric window function. obtaining a low-band signal of a current frame signal and a high-band signal of the current frame signal according to the received current frame signal; encoding the low-band signal of the current frame signal, to obtain a low-band encoded excitation signal; performing linear prediction on the high-band signal of the current frame signal, to obtain a linear prediction coefficient; quantizing the linear prediction coefficient, to obtain a quantized linear prediction coefficient; obtaining a predicted high-band signal according to the low-band encoded excitation signal and the quantized linear prediction coefficient; dividing the predicted high-band signal of the current frame into eight subframes; and calculating and quantizing a temporal envelope of each of the subframes, and encoding the quantized temporal envelopes; wherein the calculating a temporal envelope of each of the subframes comprises: performing windowing on the first subframe of the eight subframes and the last subframe of the eight subframes by using an asymmetric window function; and performing windowing on the subframes except the first subframe and the last subframe of the eight subframes by using a symmetric window function. performing windowing on the first subframe of the eight subframes and the last subframe of the eight subframes by using an asymmetric window function; and performing windowing on the subframes except the first subframe and the last subframe of the eight subframes by using a symmetric window function.
Method for chemical stabilisation of a compound of uranium carbide, corresponding to the formula: UCx + yC with x ≥ 1 and y > 0, x and y being real numbers, placed in a stabilisation chamber, characterised in that it comprises the following steps: - a step of raising the temperature of the inner temperature of the chamber to a temperature which is called the oxidation temperature of the compound based on uranium carbide of between 380°C and 550°C, the chamber being supplied with an inert gas; - a step of isothermic oxidation processing at the oxidation temperature, the chamber being placed under partial pressure of O 2; - a step of controlling the completion of the stabilisation of the compound comprising monitoring the quantity of dioxygen consumed and/or carbon dioxide released or carbon dioxide and carbon monoxide released until at least a value of an input set point for the dioxygen, a minimum threshold value for the quantity of carbon dioxide or threshold values for the carbon dioxide and the carbon monoxide has been reached. UCx + yC with x ≥ 1 and y > 0, x and y being real numbers, placed in a stabilisation chamber, characterised in that it comprises the following steps: - a step of raising the temperature of the inner temperature of the chamber to a temperature which is called the oxidation temperature of the compound based on uranium carbide of between 380°C and 550°C, the chamber being supplied with an inert gas; - a step of isothermic oxidation processing at the oxidation temperature, the chamber being placed under partial pressure of O 2; - a step of controlling the completion of the stabilisation of the compound comprising monitoring the quantity of dioxygen consumed and/or carbon dioxide released or carbon dioxide and carbon monoxide released until at least a value of an input set point for the dioxygen, a minimum threshold value for the quantity of carbon dioxide or threshold values for the carbon dioxide and the carbon monoxide has been reached. - a step of raising the temperature of the inner temperature of the chamber to a temperature which is called the oxidation temperature of the compound based on uranium carbide of between 380°C and 550°C, the chamber being supplied with an inert gas; - a step of isothermic oxidation processing at the oxidation temperature, the chamber being placed under partial pressure of O 2; - a step of controlling the completion of the stabilisation of the compound comprising monitoring the quantity of dioxygen consumed and/or carbon dioxide released or carbon dioxide and carbon monoxide released until at least a value of an input set point for the dioxygen, a minimum threshold value for the quantity of carbon dioxide or threshold values for the carbon dioxide and the carbon monoxide has been reached.