mhurhangee/patent-ind-claim-en huggingface dataset:
A method to predict the predisposition to muscular and/or ligament injuries in a human individual comprising: a) assaying a genetic sample obtained from the human individual for the presence of at least one genetic variation in each of the following genes: ACTN3, COL5A1, MCT1, VEGF, HFE, to obtain a polymorphism profile; b) determining a regression function associated to the polymorphism profile; c) classifying the individual's predisposition to muscular and/or ligament injuries on the basis of the value of said regression function, wherein: - the genetic variation of ACTN3 is a C to T polymorphism in position 18705 of the gene corresponding to SNP rs1815739; - the genetic variation of COL5A1 is a C to T polymorphism in position 205765 of the gene corresponding to SNP rs12722; - the genetic variation of MCT1 is an A to T polymorphism in position 47005 of the gene corresponding to SNP rs1049434; - the genetic variation of VEGF is a C to G polymorphism in position 5398 of the gene corresponding to SNP rs2010963; - the genetic variation of HFE is a C to G polymorphism in position 8671 of the gene corresponding to SNP rs1799945. a) assaying a genetic sample obtained from the human individual for the presence of at least one genetic variation in each of the following genes: ACTN3, COL5A1, MCT1, VEGF, HFE, to obtain a polymorphism profile; b) determining a regression function associated to the polymorphism profile; c) classifying the individual's predisposition to muscular and/or ligament injuries on the basis of the value of said regression function, wherein: - the genetic variation of ACTN3 is a C to T polymorphism in position 18705 of the gene corresponding to SNP rs1815739; - the genetic variation of COL5A1 is a C to T polymorphism in position 205765 of the gene corresponding to SNP rs12722; - the genetic variation of MCT1 is an A to T polymorphism in position 47005 of the gene corresponding to SNP rs1049434; - the genetic variation of VEGF is a C to G polymorphism in position 5398 of the gene corresponding to SNP rs2010963; - the genetic variation of HFE is a C to G polymorphism in position 8671 of the gene corresponding to SNP rs1799945. - the genetic variation of ACTN3 is a C to T polymorphism in position 18705 of the gene corresponding to SNP rs1815739; - the genetic variation of COL5A1 is a C to T polymorphism in position 205765 of the gene corresponding to SNP rs12722; - the genetic variation of MCT1 is an A to T polymorphism in position 47005 of the gene corresponding to SNP rs1049434; - the genetic variation of VEGF is a C to G polymorphism in position 5398 of the gene corresponding to SNP rs2010963; - the genetic variation of HFE is a C to G polymorphism in position 8671 of the gene corresponding to SNP rs1799945.
A measuring apparatus for measuring a DC component of at least one electric current, each electric current being output from a corresponding source , the measuring apparatus comprising a computer and at least one current detector , each current detector being associated to a corresponding source and including: - a first conductor extending between a first terminal and a second terminal for connection to the source ; - a tube-shaped screen made in an electrically conductive material and defining an inner volume , the screen being configured to provide a closed electrical path for eddy current flow to generate a compensation magnetic field for compensating a time-dependent component of a response magnetic field generated by a flow, in the first conductor , of the corresponding electric current; and - a magnetic sensor arranged in the inner volume of the screen , the magnetic sensor being configured to detect a resulting magnetic field in the inner volume , and to output a detection signal representative of the detected resulting magnetic field, the first conductor being arranged outside the inner volume of the screen , the computer being connected to the magnetic sensor of each current detector to receive the corresponding detection signal, the computer further being configured to determine, for each source , the DC component of the corresponding electric current based on the detection signal output from the magnetic sensor of the associated current detector . - a first conductor extending between a first terminal and a second terminal for connection to the source ; - a tube-shaped screen made in an electrically conductive material and defining an inner volume , the screen being configured to provide a closed electrical path for eddy current flow to generate a compensation magnetic field for compensating a time-dependent component of a response magnetic field generated by a flow, in the first conductor , of the corresponding electric current; and - a magnetic sensor arranged in the inner volume of the screen , the magnetic sensor being configured to detect a resulting magnetic field in the inner volume , and to output a detection signal representative of the detected resulting magnetic field, the first conductor being arranged outside the inner volume of the screen , the computer being connected to the magnetic sensor of each current detector to receive the corresponding detection signal, the computer further being configured to determine, for each source , the DC component of the corresponding electric current based on the detection signal output from the magnetic sensor of the associated current detector .
A method for generating an ion flow asymmetry in a capacitively coupled radiofrequency plasma reactor , the plasma reactor containing one or several mixed gases under a total pressure P, and including a first electrode , supplied with radiofrequency energy, and a second electrode , the method comprising a step for energizing the first electrode with a periodic radiofrequency voltage waveform V(t) having a lower frequency corresponding to a fundamental harmonic of a fundamental period T of the waveform; characterized in that the voltage waveform standardized in time and in amplitude over the interval [-1; 1], f(u) is an approximate waveform with a degree of approximation of a standardized sawtooth radiofrequency function f SAW (u), u being the standardized time defined as the ratio of the time t over the fundamental period T, and the standardized sawtooth radiofrequency function has a periodic pattern of fundamental period T consisting in a first linear portion of the time development of the standardized voltage with a first slope p1, immediately followed by a second linear portion of time development of the standardized voltage with a second slope p2, the first and second slopes being of different amplitudes and of opposite signs, the minimum and the maximum of the pattern having the same unit amplitude; and the degree of approximation of the approximate waveform and the total pressure P of the gas or the mixed gases are sufficiently high so as to cause appearance of an asymmetry of the ion flows between the ion flow at the first electrode and the ion flow at the second electrode.
A method for improving ground comprising: - a step of drilling a drilling hole (H) in a ground (G) to be improved; - a step of moving a jet device in a vertical direction by rotating the same while the jet device is inserted into the drilling hole (H) and a fluid for cutting the ground (G) is injected from the jet device ; and - a step of injecting a solidification material from the jet device from a discharge port at a lower end of the jet device, characterised in that said step of moving the jet device in a vertical direction by rotating the same while the fluid for cutting the ground (G) is injected from the jet device comprises the steps of: o cutting the ground (G) by injecting a partition forming material from a plurality of jetting ports at a portion which is vertically higher than the lower end portion of the jet device ; and o after having cut the ground by injecting the partition forming material, injecting the solidification material from the discharge port while the ground (G) is cut by injecting a stable liquid from the plurality of jetting ports , and in that the solidification material is a rich-mixed solidification material comprising a cement and having a ratio of water to cement in the range of 26% to 40%. - a step of drilling a drilling hole (H) in a ground (G) to be improved; - a step of moving a jet device in a vertical direction by rotating the same while the jet device is inserted into the drilling hole (H) and a fluid for cutting the ground (G) is injected from the jet device ; and - a step of injecting a solidification material from the jet device from a discharge port at a lower end of the jet device, characterised in that said step of moving the jet device in a vertical direction by rotating the same while the fluid for cutting the ground (G) is injected from the jet device comprises the steps of: o cutting the ground (G) by injecting a partition forming material from a plurality of jetting ports at a portion which is vertically higher than the lower end portion of the jet device ; and o after having cut the ground by injecting the partition forming material, injecting the solidification material from the discharge port while the ground (G) is cut by injecting a stable liquid from the plurality of jetting ports , and in that the solidification material is a rich-mixed solidification material comprising a cement and having a ratio of water to cement in the range of 26% to 40%. o cutting the ground (G) by injecting a partition forming material from a plurality of jetting ports at a portion which is vertically higher than the lower end portion of the jet device ; and o after having cut the ground by injecting the partition forming material, injecting the solidification material from the discharge port
A combustion head comprising the following elements: - a fire tube (10; 10*) with a substantially cylindrical shape and having a central symmetry axis (X) and at least one first hole (11; 11*) for the recirculation of the combustion products; - a flame disc , which is arranged perpendicularly to said central symmetry axis (X) and has a central second hole ; - a conical diffuser with a double conical inclination consisting of an axial symmetry element with an outer conical surface converging relative to a flow (F1) of the primary fuel/air mixture, and a central inner conical third hole having a surface diverging relative to said flow (F1); - a nozzle , which is designed to atomize liquid fuel; and - fire lighting means ; the combustion head is characterized in that said conical diffuser is such that recirculating combustion products having entered the fire tube (10; 10*) through the first hole (11; 11*) lap the outer conical converging surface and the diverging surface before being distanced by the flow (F1) of the primary fuel/air mixture coming from the second hole and from the third hole . - a fire tube (10; 10*) with a substantially cylindrical shape and having a central symmetry axis (X) and at least one first hole (11; 11*) for the recirculation of the combustion products; - a flame disc , which is arranged perpendicularly to said central symmetry axis (X) and has a central second hole ; - a conical diffuser with a double conical inclination consisting of an axial symmetry element with an outer conical surface converging relative to a flow (F1) of the primary fuel/air mixture, and a central inner conical third hole having a surface diverging relative to said flow (F1); - a nozzle , which is designed to atomize liquid fuel; and - fire lighting means ;
A wing assembly comprising a main wing (220; 320; 350; 370; 440; 540; 640; 740; 850; 920) having spars and at least one moveable control surface ; and a raked wing tip which is defined by a leading edge sweep angle that is greater than the main wing leading edge sweep angle and a chord length decreasing significantly in a spanwise direction, wherein a root of the wing tip is fixed to the main wing and wherein the wing tip has an outboard portion (312; 344; 364; 420; 520; 620; 1040) and an inboard raked portion; wherein the outboard portion is hinged about a hinge line (H L ) to the inboard raked portion of the raked wing tip, the inboard raked portion being that portion between the hinge line and the root; the outboard portion of the raked wing tip does not carry any moveable flight control surfaces; and the outboard portion (312; 344; 364; 420; 520; 620; 1040) is movable between a vertically folded position and an extended position in which the outboard portion of the raked wing tip is approximately in the same plane as the rest of the main wing to increase wingspan for flight. a main wing (220; 320; 350; 370; 440; 540; 640; 740; 850; 920) having spars and at least one moveable control surface ; and a raked wing tip which is defined by a leading edge sweep angle that is greater than the main wing leading edge sweep angle and a chord length decreasing significantly in a spanwise direction, wherein a root of the wing tip is fixed to the main wing and wherein the wing tip has an outboard portion (312; 344; 364; 420; 520; 620; 1040) and an inboard raked portion; wherein the outboard portion is hinged about a hinge line (H L ) to the inboard raked portion of the raked wing tip, the inboard raked portion being that portion between the hinge line and the root; the outboard portion of the raked wing tip does not carry any moveable flight control surfaces; and the outboard portion (312; 344; 364; 420; 520; 620; 1040) is movable between a vertically folded position and an extended position in which the outboard portion of the raked wing tip is approximately in the same plane as the rest of the main wing to increase wingspan for flight.
A paper cup comprising: a cup body formed from a paper-based material, the cup body comprising a sidewall and a floor that collectively define a cavity having a cavity axis (A-A); and an insert formed from a paper-based material, the insert positioned within the cavity of the cup body adjacent to the floor , the insert having a ledge that is spaced axially from the floor and that protrudes inwardly from an inner surface of the sidewall of the cup body towards the cavity axis (A-A); wherein the insert extends from a bottom end to a top end , wherein the insert comprises a sidewall portion , characterised in that the sidewall portion of the insert is formed corrugated, and when the insert is positioned within the cavity the sidewall portion of the insert is pivoted so that pleats formed by the corrugated sidewall portion side against the sidewall of the cup body 210. a cup body formed from a paper-based material, the cup body comprising a sidewall and a floor that collectively define a cavity having a cavity axis (A-A); and an insert formed from a paper-based material, the insert positioned within the cavity of the cup body adjacent to the floor , the insert having a ledge that is spaced axially from the floor and that protrudes inwardly from an inner surface of the sidewall of the cup body towards the cavity axis (A-A); wherein the insert extends from a bottom end to a top end , wherein the insert comprises a sidewall portion , characterised in that the sidewall portion of the insert is formed corrugated, and when the insert is positioned within the cavity the sidewall portion of the insert is pivoted so that pleats formed by the corrugated sidewall portion side against the sidewall of the cup body 210.
Component device, in particular for a primary structural component of an aircraft, comprising - a first component element ; - a second component element ; - an adhesive bond which provides a connection between the first component element and the second component element ; - a detector installation having at least one interior sensor installation which is configured for measuring a variation in a pressure and/or a concentration of a gas surrounding the interior sensor installation ; - wherein the first component element , the second component element , and the adhesive bond delimit an interior ; and - wherein the interior sensor installation is disposed in the interior , characterized in that the interior sensor installation comprises dissimilar second interior sensors which are configured for measuring the partial pressure of dissimilar gases, and/or comprises dissimilar third interior sensors which are configured for measuring the concentration of dissimilar gases, wherein the second interior sensors are configured as coated optical fibres. - a first component element ; - a second component element ; - an adhesive bond which provides a connection between the first component element and the second component element ; - a detector installation having at least one interior sensor installation which is configured for measuring a variation in a pressure and/or a concentration of a gas surrounding the interior sensor installation ; - wherein the first component element , the second component element , and the adhesive bond delimit an interior ; and - wherein the interior sensor installation is disposed in the interior ,
Oxygen module for the supply of oxygen to aircraft passengers, comprising - an oxygen source - a mask and - a hose between the oxygen source and the mask, wherein the oxygen module comprises a mounting member for mounting in a supply channel of an aircraft, a cover coverable by a fairing flap of the supply channel, and a locking member , wherein the locking element is configured such that the cover of the oxygen module is lockable and does not open during an opening test of the fairing flap and that the cover of the oxygen module is unlocked and released and opens during an automatic opening of the fairing flap. - an oxygen source - a mask and - a hose between the oxygen source and the mask,
An upgraded preexisting flight management system (FMS) having increased functionality over a preexisting FMS , the preexisting FMS having a legacy advanced flight management computer (AFMC) having aircraft performance capabilities exploitable throughout a flight of an aircraft having the preexisting FMS on board the aircraft; an inertial reference unit (IRU) , a central air data computer (CADC) , a distance measuring equipment (DME) receiver , and a digital flight guidance computer (DFGC) , the IRU , CADC , DME receiver and DFGC being in communication with the legacy AFMC ; the upgraded preexisting FMS comprising a data concentrator unit , the CADC , IRU and DME receiver being connected to the data concentrator unit for providing input information thereto, the data concentrator unit and the legacy AFMC being operatively connected to each other for exchanging input and output information therebetween, the DFGC being connected to the data concentrator unit for receiving output information therefrom; and a global positioning system (GPS) receiver operatively connected to the data concentrator unit for providing input information thereto; wherein the upgraded preexisting FMS is configured to: blend GPS data from the GPS receiver with IRU position data from the IRU ; or in instances where GPS data from the GPS receiver is not available for a certain amount of time, use data from the DME receiver to augment the IRU position data from the IRU ; and transmit the blended data or augmented data to the AFMC ; such that the upgraded preexisting FMS is capable of at least required navigation performance (RNP), vertical navigation (VNAV) and area navigation (RNAV) capability utilizing a GPS based navigation solution, while still enabling the legacy AFMC to exploit its aircraft performance capabilities throughout the flight of an aircraft having the upgraded preexisting FMS on board. blend GPS data from the GPS receiver with IRU position data from the IRU ; or in instances where GPS data from the GPS receiver is not available for a certain amount of time, use data from the DME receiver to augment the IRU position data from the IRU ; and transmit the blended data or augmented data to the AFMC ;
A dispersive supply device comprising: a dispersion portion configured to disperse articles supplied from above toward a periphery; a plurality of conveying portions radially arrayed around the dispersion portion and configured to further convey the articles supplied from the dispersion portion in radial directions; and characterized by a plurality of block bodies arranged between the adjacent conveying portions, wherein the block bodies include a first block body configured to restrict the articles supplied from the dispersion portion from entering a portion between the conveying portions, and a second block body configured to allow the articles supplied from the dispersion portion to enter the portion between the conveying portions, the second block body including an inclined surface that inclines toward the conveying portions on both sides from a ridge along the radial direction. a dispersion portion configured to disperse articles supplied from above toward a periphery; a plurality of conveying portions radially arrayed around the dispersion portion and configured to further convey the articles supplied from the dispersion portion in radial directions; and characterized by a plurality of block bodies arranged between the adjacent conveying portions, wherein the block bodies include a first block body configured to restrict the articles supplied from the dispersion portion from entering a portion between the conveying portions, and a second block body configured to allow the articles supplied from the dispersion portion to enter the portion between the conveying portions, the second block body including an inclined surface that inclines toward the conveying portions on both sides from a ridge along the radial direction. a first block body configured to restrict the articles supplied from the dispersion portion from entering a portion between the conveying portions, and a second block body configured to allow the articles supplied from the dispersion portion to enter the portion between the conveying portions, the second block body including an inclined surface that inclines toward the conveying portions on both sides from a ridge along the radial direction.
A method of improving the fidelity of m/z dependent measurements for a species of interest in an analyte in a mass spectrometer, which method comprises the steps of: acquiring raw data produced in a mass spectrometer; within the raw data, identifying the spectra and the range of arrival times containing ions of a particular species; peak detecting the spectra thus identified; forming a mathematical model relating the effective number of experiments to the underlying ion arrival rates in each spectrum and the observed ion arrival times and the observed number of events in each spectrum, to calculate the joint probability distribution of the parameters and the data, wherein the parameters comprise the ion arrival rates and the effective number of experiments; obtaining samples from the joint probability distribution; using the samples to produce the required inferences including corrected m/z dependent measurements with associated uncertainties. acquiring raw data produced in a mass spectrometer; within the raw data, identifying the spectra and the range of arrival times containing ions of a particular species; peak detecting the spectra thus identified; forming a mathematical model relating the effective number of experiments to the underlying ion arrival rates in each spectrum and the observed ion arrival times and the observed number of events in each spectrum, to calculate the joint probability distribution of the parameters and the data, wherein the parameters comprise the ion arrival rates and the effective number of experiments; obtaining samples from the joint probability distribution; using the samples to produce the required inferences including corrected m/z dependent measurements with associated uncertainties.