mhurhangee/patent-ind-claim-en huggingface dataset:
Method for coupling/uncoupling a guided vehicle unit A2 to/from a guided vehicle unit A1 while said guided vehicle units A1 and A2 are operating and moving on a track according to a predefined itinerary, the guided vehicle unit A1 being located ahead the guided vehicle unit A2, each guided vehicle unit comprising an on-board signaling system and a rolling stock system, the method comprising: - a reception by at least one of the guided vehicle units of a command for coupling/uncoupling the guided vehicles units A1 and A2; - checking coupling/uncoupling conditions by means of at least one of the on-board signaling systems; - locating, by means of at least one of the on-board signaling systems, a coupling/uncoupling track section on the itinerary of the guided vehicle units A1 and A2, wherein the coupling/uncoupling track section is a track section fulfilling criteria defined for ensuring safe coupling/uncoupling operation, wherein the on-board signaling system is configured for determining whether the track section fulfills said criteria; - if a coupling/uncoupling track section has been located and the coupling/uncoupling conditions are fulfilled, then automatically performing the coupling/uncoupling of the guided vehicle units A1 and A2 when the guided vehicle units A1 and A2 enter said coupling/uncoupling track section , otherwise moving the coupled/uncoupled guided vehicles units A1 and A2 according to said itinerary until a coupling/uncoupling track section is located or a station (S1, S2, S3) reached, characterized in that said criteria comprise a non-braking criterion defined for the whole length of the coupling/uncoupling track section for the guided vehicle units, said non-braking criterion ensuring that there is no braking need for the guided vehicle units when moving over the length of the track section when considering the track section topology and infrastructure. - a reception by at least one of the guided vehicle units of a command for coupling/uncoupling the guided vehicles units A1 and A2; - checking coupling/uncoupling conditions by means of at least one of the on-board signaling systems; - locating, by means of at least one of the on-board signaling systems, a coupling/uncoupling track section on the itinerary of the guided vehicle units A1 and A2, wherein the coupling/uncoupling track section is a track section fulfilling criteria defined for ensuring safe coupling/uncoupling operation, wherein the on-board signaling system is configured for determining whether the track section fulfills said criteria; - if a coupling/uncoupling track section has been located and the coupling/uncoupling conditions are fulfilled, then automatically performing the coupling/uncoupling of the guided vehicle units A1 and A2 when the guided vehicle units A1 and A2 enter said coupling/uncoupling track section , otherwise moving the coupled/uncoupled guided vehicles units A1 and A2 according to said itinerary until a coupling/uncoupling track section
Method for analyzing the operation of a machine and/or for calibrating a control system of the machine , in particular of an internal combustion engine, wherein test points which are defined by values of a plurality of predetermined operating parameters and are selected from a multi-dimensional test space by means of a statistical test plan, are approached , wherein, when approaching the test points, in each case a plurality of operating parameters (P 1 ) are changed in a plurality of steps from one test point (T n ) to the next test point (T n+1 ) by means of a slow dynamic slopes method, wherein operating measurements (meas) are carried out at measuring points (M n ), which are determined by a respective step size, and at the actual test points (T n , T n+1 ), so that the test points are connected to one another by measurement ramps, with measurement data from the operating measurements being output for analysis and calibration of the controller and being continuously stored , wherein the measurement data are fed to a model building algorithm , wherein a model is adapted by means of the model building algorithm during an execution of the method , wherein test points not yet measured and/or additional test points are placed by means of the adapted model.
Apparatus for liquefying at least one gas, comprising: - at least one inlet via which the pressurized gas can be introduced into the apparatus ; - at least one countercurrent heat exchanger having at least one first channel that can be supplied with the pressurized gas via the inlet and through which gas flow is possible in a first direction, - at least one expansion nozzle into which the first channel opens, such that the gas that flows from the first channel into the expansion nozzle , flows through the expansion nozzle and flows out of the expansion nozzle is expandable by means of the expansion nozzle to form an aerosol comprising a gaseous phase and liquid droplets; - an aerosol breaker by means of which at least some of the droplets can be separated out of the gaseous phase; - a collecting region for gathering and collecting the droplets dripping off the aerosol breaker ; and - a second channel of the countercurrent heat exchanger that surrounds the first channel , wherein flow of the gaseous phase flowing out of the expansion nozzle that has been decompressed and is colder compared to the gas through the second channel is possible in a second direction that is the opposite of the first direction and the second channel surrounds the first channel , characterized in that the apparatus is in one-piece form. - at least one inlet via which the pressurized gas can be introduced into the apparatus ; - at least one countercurrent heat exchanger having at least one first channel that can be supplied with the pressurized gas via the inlet and through which gas flow is possible in a first direction, - at least one expansion nozzle into which the first channel opens, such that the gas that flows from the first channel into the expansion nozzle , flows through the expansion nozzle and flows out of the expansion nozzle is expandable by means of the expansion nozzle to form an aerosol comprising a gaseous phase and liquid droplets; - an aerosol breaker by means of which at least some of the droplets can be separated out of the gaseous phase; - a collecting region for gathering and collecting the droplets dripping off the aerosol breaker ; and - a second channel of the countercurrent heat exchanger that surrounds the first channel , wherein flow of the gaseous phase flowing out of the expansion nozzle that has been decompressed and is colder compared to the gas through the second channel is possible in a second direction that is the opposite of the first direction and the second channel surrounds the first channel , characterized in that the apparatus is in one-piece form.
A LED lamp filament, comprising: an elongated substrate having opposite first and second surfaces and lateral opposite sides; wherein said opposite sides of the substrate are provided with a plurality of protrusions respectively, and the plurality of protrusions are distributed along an extending direction of the substrate , the protrusions on the same side of the substrate being arranged by equal interval; a plurality of light emitting units located on the first surface of the substrate and distributed along the extending direction of the substrate ; wherein the plurality of light emitting units are arranged in a line, and at equal distance from the opposite sides of the substrate ; and a fluorescent adhesive layer covering the first surface and the plurality of light emitting units characterized in that the fluorescent adhesive layer further covers the plurality of protrusions and regions that are located between two adjacent protrusions arranged on the same side of the substrate ; wherein partial light emitted from the light emitting units and excited by the fluorescent adhesive layer is emitted along a direction from a portion between two adjacent protrusions arranged on the same side of the substrate towards the second surface of the substrate . an elongated substrate having opposite first and second surfaces and lateral opposite sides; wherein said opposite sides of the substrate are provided with a plurality of protrusions respectively, and the plurality of protrusions are distributed along an extending direction of the substrate , the protrusions on the same side of the substrate being arranged by equal interval; a plurality of light emitting units located on the first surface of the substrate and distributed along the extending direction of the substrate ; wherein the plurality of light emitting units are arranged in a line, and at equal distance from the opposite sides of the substrate ; and a fluorescent adhesive layer covering the first surface and the plurality of light emitting units characterized in that the fluorescent adhesive layer further covers the plurality of protrusions and regions that are located between two adjacent protrusions arranged on the same side of the substrate ; wherein partial light emitted from the light emitting units and excited by the fluorescent adhesive layer is emitted along a direction from a portion between two adjacent protrusions arranged on the same side of the substrate towards the second surface of the substrate . characterized in that the fluorescent adhesive layer further covers the plurality of protrusions and regions that are located between two adjacent protrusions arranged on the same side of the substrate ; wherein partial light emitted from the light emitting units and excited by the fluorescent adhesive layer is emitted along a direction from a portion between two adjacent protrusions arranged on the same side of the substrate towards the second surface of the substrate .
A gate driver circuit (300, 500, 600-1, 600-2), comprising: a gate driver configured to generate an on-current during a plurality of turn-on switching events to drive a transistor , wherein a voltage across the transistor changes from a first value to a second value with a slope during the plurality of turn-on switching events, wherein the slope is of either an active type or a passive type, and wherein the slope of the active type is dependent on an amplitude of the on-current; and a sensing circuit configured to determine whether the slope during a first turn-on switching event is the active type or the passive type, and to regulate the amplitude of the on-current to target a particular slope during a second turn-on switching event that is subsequent to the first turn-on switching event if the slope is the active type and to maintain the amplitude of the on-current as unchanged during the second turn-on switching event if the slope is the passive type; wherein the slope is the passive type if the slope occurs at least partially within a dead time of a switching cycle that includes the first turn-on switching event, and a slope is the active type if the slope occurs entirely after the dead time of the switching cycle. a gate driver configured to generate an on-current during a plurality of turn-on switching events to drive a transistor , wherein a voltage across the transistor changes from a first value to a second value with a slope during the plurality of turn-on switching events, wherein the slope is of either an active type or a passive type, and wherein the slope of the active type is dependent on an amplitude of the on-current; and a sensing circuit configured to determine whether the slope during a first turn-on switching event is the active type or the passive type, and to regulate the amplitude of the on-current to target a particular slope during a second turn-on switching event that is subsequent to the first turn-on switching event if the slope is the active type and to maintain the amplitude of the on-current as unchanged during the second turn-on switching event if the slope is the passive type; wherein the slope is the passive type if the slope occurs at least partially within a dead time of a switching cycle that includes the first turn-on switching event, and a slope is the active type if the slope occurs entirely after the dead time of the switching cycle.
A composition that is radiation curable to a polythioether polymer, comprising: k) at least one thiol terminated polythioether polymer which comprises pendent hydroxide groups; l) at least one multifunctional monomer having at least three ethenyl groups; and m) at least one photoinitiator selected from 2,2-dimethoxy-1,2-diphenylethan-1-one and phenylbis(2,4,6-trimethylbenzoyl)phosphine oxide. k) at least one thiol terminated polythioether polymer which comprises pendent hydroxide groups; l) at least one multifunctional monomer having at least three ethenyl groups; and m) at least one photoinitiator selected from 2,2-dimethoxy-1,2-diphenylethan-1-one and phenylbis(2,4,6-trimethylbenzoyl)phosphine oxide.
Method for operating a wind power installation (WPI, 100), comprising a generator, for feeding electrical power into an electrical supply network, wherein after a first operating state with a first power output and a first rotational speed, a controlled change is made into a second operating state with a second power output and a second rotational speed, characterized in that , for the controlled change into the second operating state, - an aerodynamic power available ( P̂ ava DC ) for the feed is determined, wherein the available power ( P̂ ava DC ) is determined from a rotational speed (ω) of the generator and the power fed into (P DC ) an intermediate electrical storage unit, in particular a DC voltage intermediate circuit, - a setpoint rotational speed (ω soll ) is determined from this available power, and - a setpoint power (P soll ) to be adjusted at the generator is specified from the setpoint rotational speed. - an aerodynamic power available ( P̂ ava DC ) for the feed is determined, wherein the available power ( P̂ ava DC ) is determined from a rotational speed (ω) of the generator and the power fed into (P DC ) an intermediate electrical storage unit, in particular a DC voltage intermediate circuit, - a setpoint rotational speed (ω soll ) is determined from this available power, and - a setpoint power (P soll ) to be adjusted at the generator is specified from the setpoint rotational speed.
A method of determining a total HF concentration metric in an environment comprising: (a) measuring an uncorrected HF concentration metric in the environment based on a first infrared absorption measurement at a wavelength corresponding to a vibrational frequency of a non-hydrogen bonded gas phase HF molecule; (b) determining an ambient H 2 O concentration metric in the environment available for reaction with the non-hydrogen bonded gas phase HF molecules at or about the time of obtaining the first infrared absorption measurement; CHARACTERIZED IN THAT the method further comprises: (c) calculating a HF hydrate concentration metric in the environment based on the uncorrected HF concentration metric, the ambient H 2 O concentration metric and a reaction equilibrium relationship between the non-hydrogen bonded gas phase HF molecule and the HF hydrate; and (d) determining the total HF concentration metric in the environment based on the uncorrected HF concentration metric and an amount of HF determined by the HF hydrate concentration metric. (a) measuring an uncorrected HF concentration metric in the environment based on a first infrared absorption measurement at a wavelength corresponding to a vibrational frequency of a non-hydrogen bonded gas phase HF molecule; (b) determining an ambient H 2 O concentration metric in the environment available for reaction with the non-hydrogen bonded gas phase HF molecules at or about the time of obtaining the first infrared absorption measurement; (c) calculating a HF hydrate concentration metric in the environment based on the uncorrected HF concentration metric, the ambient H 2 O concentration metric and a reaction equilibrium relationship between the non-hydrogen bonded gas phase HF molecule and the HF hydrate; and (d) determining the total HF concentration metric in the environment based on the uncorrected HF concentration metric and an amount of HF determined by the HF hydrate concentration metric.
A vehicle body floor structure comprising: a plurality of first vehicle body framework members (13; 21; 22; 71; 72; 73; 74; 75; 76) extending along a vehicle body front-rear direction; a plurality of second vehicle body framework members (31; 32; 41; 42; 51; 52; 61) extending along a vehicle width direction; and a floor panel to which each of the first vehicle body framework members (13; 21; 22; 71; 72; 73; 74; 75; 76) and the second vehicle body framework members (31; 32; 41; 42; 51; 52; 61) is joined, the floor panel including a plurality of steps having ridge lines (R) extending along a short-side direction of a first region (A1, A2, A3, A4, A5, A6, A7, A8, A9, A10, A11, A12), the steps being arrayed along a long-side direction of the first region (A1, A2, A3, A4, A5, A6, A7, A8, A9, A10, A11, A12), the first region (A1, A2, A3, A4, A5, A6, A7, A8, A9, A10, A11, A12) being surrounded by the first vehicle body framework members (13; 21; 22; 71; 72; 73; 74; 75; 76) that are adjacent to each other in the vehicle width direction and the second vehicle body framework members (31; 32; 41; 42; 51; 52; 61) that are adjacent to each other in the vehicle body front-rear direction; characterized by : a vibration damping material applied to a surface of the floor panel , the vibration damping material being applied along at least one outer edge portion of the first region (A1, A2, A3, A4, A5, A6, A7, A8, A9, A10, A11, A12) extending along the long-side direction. a plurality of first vehicle body framework members (13; 21; 22; 71; 72; 73; 74; 75; 76) extending along a vehicle body front-rear direction; a plurality of second vehicle body framework members (31; 32; 41; 42; 51; 52; 61) extending along a vehicle width direction; and a floor panel to which each of the first vehicle body framework members (13; 21; 22; 71; 72; 73; 74; 75; 76) and the second vehicle body framework members (31; 32; 41; 42; 51; 52; 61) is joined, the floor panel including a plurality of steps having ridge lines (R) extending along a short-side direction of a first region (A1, A2, A3, A4, A5, A6, A7, A8, A9, A10, A11, A12), the steps being arrayed along a long-side direction of the first region (A1, A2, A3, A4, A5, A6, A7, A8, A9, A10, A11, A12), the first region (A1, A2, A3, A4, A5, A6, A7, A8, A9, A10, A11, A12) being surrounded by the first vehicle body framework members (13; 21; 22; 71; 72; 73; 74; 75; 76) that are adjacent to each other in the vehicle width direction and the second vehicle body framework members (31; 32; 41; 42; 51; 52; 61) that are adjacent to each other in the vehicle body front-rear direction; characterized by : a vibration damping material applied to a surface of the floor panel , the vibration damping material being applied along at least one outer edge portion of the first region (A1, A2, A3, A4, A5, A6, A7, A8, A9, A10, A11, A12) extending along the long-side direction.
A system (210; 310; 420) for visualizing a tissue treatment, comprising: a tissue treatment instrument (212; 430) having a first electromagnetic energy sensor; an ultrasound imaging instrument (228, 230; 434, 436) configured to generate an ultrasound imaging plane, wherein the ultrasound imaging instrument (228, 230; 434, 436) has a second electromagnetic energy sensor; an electromagnetic field generator configured for placement in proximity to a patient body and configured to generate an electromagnetic field that interacts with the first and second electromagnetic energy sensors; and a console in communication with the first and second electromagnetic energy sensors and with the electromagnetic field generator , wherein the console is configured to generate a representative image of the tissue treatment instrument (212; 430) oriented relative to the ultrasound imaging plane based upon calculating a position and orientation of the first and second electromagnetic energy sensors relative to one another within the electromagnetic field; characterized in that the tissue treatment instrument (212; 430) has one or more deployable stylets , and the console is also configured to generate an image of an expected ablation border or expected treatment zone having a size that is based upon a deployment length of the one or more stylets . a tissue treatment instrument (212; 430) having a first electromagnetic energy sensor; an ultrasound imaging instrument (228, 230; 434, 436) configured to generate an ultrasound imaging plane, wherein the ultrasound imaging instrument (228, 230; 434, 436) has a second electromagnetic energy sensor; an electromagnetic field generator configured for placement in proximity to a patient body and configured to generate an electromagnetic field that interacts with the first and second electromagnetic energy sensors; and a console in communication with the first and second electromagnetic energy sensors and with the electromagnetic field generator , wherein the console is configured to generate a representative image of the tissue treatment instrument (212; 430) oriented relative to the ultrasound imaging plane based upon calculating a position and orientation of the first and second electromagnetic energy sensors relative to one another within the electromagnetic field; characterized in that the tissue treatment instrument (212; 430) has one or more deployable stylets , and the console is also configured to generate an image of an expected ablation border or expected treatment zone having a size that is based upon a deployment length of the one or more stylets .
Method of protecting a margin for controlling the yaw attitude of a hybrid helicopter , said hybrid helicopter including a lift rotor arranged above a fuselage , as well as at least one first propeller and at least one second propeller arranged on either side of the fuselage , said hybrid helicopter having a thrust control configured to generate at least a first order or a second order for modifying a first pitch of first blades of the first propeller and a second pitch of second blades of the second propeller , said hybrid helicopter having a yaw control configured to modify the yaw attitude of said hybrid helicopter by increasing the first pitch of said first blades and by reducing the second pitch of said second blades , characterized in that the method includes a protection phase (PPROT) comprising the following step: - after a said first order (OA) for increasing the first pitch and the second pitch has been issued, inhibition (STP3) by a control computer of this first order (OA) when said hybrid helicopter reaches an operating point for which a yaw attitude control margin is less than, or equal to, a threshold (S) and/or for which a prediction of said yaw attitude control margin that will be reached within a predetermined interval of time is less than, or equal to, the threshold (S). - after a said first order (OA) for increasing the first pitch and the second pitch has been issued, inhibition (STP3) by a control computer of this first order (OA) when said hybrid helicopter reaches an operating point for which a yaw attitude control margin is less than, or equal to, a threshold (S) and/or for which a prediction of said yaw attitude control margin that will be reached within a predetermined interval of time is less than, or equal to, the threshold (S).
The compound of the following chemical formula: ABZ 1 -Dap(O2(Cbz)) 2 -Dap(O1) 3 -Dap(O2) 4 -Arg 5 -ANB 6 -NH 2 where: ABZ stands for 2-aminobenzoic acid DAP stands for diaminopropanoic acid (Dap) derivatives, modified by functionalised residues of mono-ethylene or diethylene glycol (PEG) ANB stands for 5-amino-2-nitrobenzoic acid O1 stands 5-amino-3-oxapentanoic acid O2 stands an abbreviation 8-amino-3,6-dioxaoctanoic acid ABZ stands for 2-aminobenzoic acid DAP stands for diaminopropanoic acid (Dap) derivatives, modified by functionalised residues of mono-ethylene or diethylene glycol (PEG) ANB stands for 5-amino-2-nitrobenzoic acid O1 stands 5-amino-3-oxapentanoic acid O2 stands an abbreviation 8-amino-3,6-dioxaoctanoic acid