mhurhangee/ep-ind-claims huggingface dataset:
A method performed by a wireless device (112, 1300) for receiving and interpreting a Downlink Control Information, DCI, message, the method comprising receiving (206; 902), from a base station, a configuration of a DCI formatting indicator size, wherein a size of a DCI formatting indicator is equal to the configuration of the DCI formatting indicator size; receiving (214; 700; 910) a DCI message from the base station; obtaining (214; 702; 912) the DCI formatting indicator for the DCI message, wherein the DCI formatting indicator is a configurably sized indicator related to a flexible-interpretation DCI format, wherein the flexible-interpretation DCI format is a DCI format for which bits are interpreted differently based on the DCI formatting indicator; and interpreting (216; 704; 914) the DCI message in accordance with the DCI formatting indicator. receiving (206; 902), from a base station, a configuration of a DCI formatting indicator size, wherein a size of a DCI formatting indicator is equal to the configuration of the DCI formatting indicator size; receiving (214; 700; 910) a DCI message from the base station; obtaining (214; 702; 912) the DCI formatting indicator for the DCI message, wherein the DCI formatting indicator is a configurably sized indicator related to a flexible-interpretation DCI format, wherein the flexible-interpretation DCI format is a DCI format for which bits are interpreted differently based on the DCI formatting indicator; and interpreting (216; 704; 914) the DCI message in accordance with the DCI formatting indicator.
Luminaire, in particular floor luminaire or pendant luminaire, which has two light exit surfaces (2; 4) on two opposite sides of a luminaire housing in order to emit light for direct illumination and for indirect illumination, wherein illuminants in the form of LEDs (18; 24) for generating the direct illumination and the indirect illumination are arranged in thermal contact with the luminaire housing therein, and the luminaire housing being formed as an integral body from a solid thermally conductive material having a specific thermal conductivity of more than 30 W/Km, preferably more than 100 W/Km, and having cooling fins (8; 10) on portions of its surface, characterized in that the light-emitting surfaces (2; 4) on the two opposite sides are arranged offset from one another and non-overlapping.
A method for determining flow rate of a multiphase fluid comprising: measuring a first pressure differential of the multiphase fluid flowing through a rotodynamic pump operating at a rotational speed thereby driving the multiphase fluid, wherein the rotodynamic pump is a single-stage or multi-stage pump and the first pressure differential is a pressure difference between an inlet pressure and an outlet pressure of the single-stage or multi-stage rotodynamic pump or of a single-stage of the multi-stage rotodynamic pump; measuring a second pressure differential of the multiphase fluid flowing through a portion of a fluid conduit positioned in series with said rotodynamic pump; determining, based on the first and second pressure differentials (316, 326) and the rotational speed of said rotodynamic pump, a flow rate of the multiphase fluid; and. altering the rotodynamic pump speed based on said determined flow rate of the multiphase fluid so as to maintain the multiphase flow rate within a predetermined range. measuring a first pressure differential of the multiphase fluid flowing through a rotodynamic pump operating at a rotational speed thereby driving the multiphase fluid, wherein the rotodynamic pump is a single-stage or multi-stage pump and the first pressure differential is a pressure difference between an inlet pressure and an outlet pressure of the single-stage or multi-stage rotodynamic pump or of a single-stage of the multi-stage rotodynamic pump; measuring a second pressure differential of the multiphase fluid flowing through a portion of a fluid conduit positioned in series with said rotodynamic pump; determining, based on the first and second pressure differentials (316, 326) and the rotational speed of said rotodynamic pump, a flow rate of the multiphase fluid; and. altering the rotodynamic pump speed based on said determined flow rate of the multiphase fluid so as to maintain the multiphase flow rate within a predetermined range.
Method for producing a reference torque (C cons_corr) of an electric motor of an electric or hybrid motor vehicle, wherein a first reference torque (C cons) is calculated from a signal of the acceleration pedal of the motor vehicle, a frequency response (K(s)) is calculated in accordance with the rotation speed (Ω) of the engine, and this frequency response is added to the first reference torque (C cons), there is added to this first reference torque (C cons) a corrective increment when the rotation speed (Ω) of the electric engine is less in terms of an absolute value than a first rotation speed threshold by applying to the frequency response a multiplication coefficient (G NO) which amplifies the effect of the frequency response (K(s)), characterised in that the multiplier coefficient (G NO) is strictly greater than 1 and increases with the absolute value of the first reference torque (C cons), and the multiplier coefficient is multiplied by a signature value which is equal to +1 or -1 so that the reference torque increment added to or subtracted from the first reference torque (C cons) tends effectively to accelerate the passage of the rotation speed of the engine through zero.
A laminate having two adherends, at least one of which is a polyamide sheet or plate, and an adhesive layer formed of an adhesive composition between the adherends, wherein the adhesive composition comprises: (meth)acrylates, excluding the component, comprising the following ingredients,, and: a (meth)acrylate, excluding an ingredient, having the following formula: wherein Z represents a (meth)acryloyl group, and R 3 represents a hydrogen atom, a halogen atom, an alkyl group with 1 to 12 carbon atoms, or an alkoxy group with 1 to 12 carbon atoms; a (meth)acrylate having a hydroxy group and the following formula: Formula D Z-O-(R 7 O) q -H wherein Z represents a (meth)acryloyl group, R 7 represents an alkylene group, and q represents an integer from 1 to 10; and a (meth)acrylate represented by general formula; wherein Z and Z' each represent a (meth)acryloyl group, and Z and Z' are the same or different; R1 and R1' each represent an alkylene group, and R1 and R1' are the same or different; R2 and R2' each represent hydrogen or an alkyl group with 1 to 4 carbon atoms, and R2 and R2' are the same or different; and p and p' each represent an integer from 0 to 8, and p and p' are the same or different; an acidic phosphate compound; a polymerization initiator; and a reducing agent comprising a transition metal salt. a (meth)acrylate, excluding an ingredient, having the following formula: wherein Z represents a (meth)acryloyl group, and R 3 represents a hydrogen atom, a halogen atom, an alkyl group with 1 to 12 carbon atoms, or an alkoxy group with 1 to 12 carbon atoms; a (meth)acrylate having a hydroxy group and the following formula: Formula D Z-O-(R 7 O) q -H wherein Z represents a (meth)acryloyl group, R 7 represents an alkylene group, and q represents an integer from 1 to 10; and a (meth)acrylate represented by general formula; wherein Z and Z' each represent a (meth)acryloyl group, and Z and Z' are the same or different; R1 and R1' each represent an alkylene group, and R1 and R1' are the same or different; R2 and R2' each represent hydrogen or an alkyl group with 1 to 4 carbon atoms, and R2 and R2' are the same or different; and p and p' each represent an integer from 0 to 8, and p and p' are the same or different; an acidic phosphate compound; a polymerization initiator; and a reducing agent comprising a transition metal salt.
A method to navigate an unmanned aerial vehicle, comprising the steps of a) controlling a flight path of the unmanned aerial vehicle by a remote operator; b) obtaining a recognized air picture of an observation space surrounding the unmanned aerial vehicle, including tracking information with respect to aerial vehicles (10, 20, 30) within the observation space; c) assigning one of a plurality of threat levels to each of the aerial vehicles (10, 20, 30), the threat levels comprising a resolution advisory level and an automatic avoidance level; d) continuously automatically determining viable avoidance trajectories for the unmanned aerial vehicle; e) if at least one of the aerial vehicles (10, 20, 30) is assigned the resolution advisory level, providing a message to the remote operator including a first proposed viable avoidance trajectory; f) if at least one of the aerial vehicles (10, 20, 30) is assigned the automatic avoidance level, providing control signals to an on-board flight controller of the unmanned aerial vehicle instructing the vehicle to follow a flight path corresponding to a second proposed viable avoidance trajectory. a) controlling a flight path of the unmanned aerial vehicle by a remote operator; b) obtaining a recognized air picture of an observation space surrounding the unmanned aerial vehicle, including tracking information with respect to aerial vehicles (10, 20, 30) within the observation space; c) assigning one of a plurality of threat levels to each of the aerial vehicles (10, 20, 30), the threat levels comprising a resolution advisory level and an automatic avoidance level; d) continuously automatically determining viable avoidance trajectories for the unmanned aerial vehicle; e) if at least one of the aerial vehicles (10, 20, 30) is assigned the resolution advisory level, providing a message to the remote operator including a first proposed viable avoidance trajectory; f) if at least one of the aerial vehicles (10, 20, 30) is assigned the automatic avoidance level, providing control signals to an on-board flight controller of the unmanned aerial vehicle instructing the vehicle to follow a flight path corresponding to a second proposed viable avoidance trajectory.
A device for vibration decoupling, comprising a pulley for accommodating a belt, a drive shaft rotating the pulley, and a coupling device that connects the pulley with the drive shaft, wherein the coupling device has a freewheel member and an elastomeric spring body connected in series, wherein hardened counterfaces (5, 6) are associated with the freewheel member, a first counterface facing towards the pulley and a second counterface facing towards the elastomeric spring body, characterised in that at least one hardened counterface (5, 6) is formed on an insert (5a, 6a).
A tire (100, 200) comprising a tread having at least a left tread portion (110, 210), a right tread portion (120, 220), wherein the right tread portion (120, 220) and the left tread portion (110, 210) are axially separated by a longitudinally oriented groove (130, 230); a carcass layer, a left sidewall and a right sidewall, a left bead portion and a right bead portion; the left sidewall extending radially to join the left tread portion (110, 210) and the right sidewall extending radially to join the right tread portion (120, 220), and when the tire (100, 200) is mounted on a rim, the tread portions (110, 120, 210, 220), the left sidewall and the right sidewall, the left bead portion and the right bead portion enclose a cavity by which the tire (100, 200) is inflated for operation under various applied loads; a tread reinforcement extending in an axial direction of the tire (100, 200) comprising a plurality of tread reinforcing layers (115, 125, 135) wherein a plurality of reinforcement elements are formed of parallel reinforcements arranged in opposing layers, and each of the opposing layers has a bias angle β relative to a circumferential direction of the tire (100, 200), wherein the carcass layer comprises a plurality of reinforcing cords to form the left sidewall and the right sidewall, the reinforcing cords of the carcass layer are anchored, respectively, in the left bead portion and the right bead portion, and; the bias angle β of the reinforcement elements in each of the tread reinforcing layers (115, 125, 135) corresponds to a plurality of equilibrium membrane shapes determined from membrane equilibrium equations that are joined laterally together in a continuous, complex belt shape, characterized in that a central tread reinforcing layer corresponding to the longitudinally oriented groove (130, 230) has a concave shape and a bias angle β 1 that is less than a bias angle β 2 of both a left tread reinforcing layer and a right tread reinforcing layer, and a crown radius of the central tread reinforcing layer is less than a crown radius of the left tread reinforcing layer and less than a crown radius of the right tread reinforcing layer.
A rotational machine adapted as a bearing-free engine including a stator designed as a bearing and drive stator having a magnetic stator plane and a magnetic rotor having a magnetic rotor plane and supported magnetically in contact free manner within the stator, wherein an axial height of the rotor is smaller than or equal to a half diameter of the rotor and the rotor is stabilized passively by reluctance forces with respect to the magnetic stator plane both against an axial displacement (ΔY) and also against a tilting (Δα) from an equilibrium position and a sensor unit having a first sensor and a second sensor is provided at the stator such that for the determination of a deflection of the rotor from the equilibrium position a first sensor signal from a first measurement zone of the rotor can be evaluated by means of the first sensor and a second sensor signal from a second measurement zone can be evaluated by means of the second sensor, characterized in that for the determination of the tilting (Δα) of the rotor relative to the magnetic stator plane a first control measurement zone which is part of the first measurement zone is provided either below or above the magnetic rotor plane at the rotor such that at least 50 % of the first sensor signal which can be generated from the first measurement zone can be generated by the first control measurement zone at the first sensor.
A UV curable composition, the UV curable composition comprising, based on the total weight thereof as 100 wt%: 25 to 60 wt% of an ethylene-vinyl acetate copolymer; 20 to 60 wt% of an epoxy resin; 5 to 20 wt% of glass bubbles; 0.3 to 8 wt% of a hydroxy-containing compound; and 0.5 to 5 wt% of a photoinitiator, wherein the glass bubbles meet at least one of the following conditions A and B: A. the average true density of the glass bubbles ranges from 0.35 g/cc to 0.6 g/cc; and B. the hydrostatic pressure at which 10 vol% of the glass bubbles collapse is at least 20 MPa wherein the average true density and the hydrostatic pressure are measured by the methods according to the description. 25 to 60 wt% of an ethylene-vinyl acetate copolymer; 20 to 60 wt% of an epoxy resin; 5 to 20 wt% of glass bubbles; 0.3 to 8 wt% of a hydroxy-containing compound; and 0.5 to 5 wt% of a photoinitiator, wherein the glass bubbles meet at least one of the following conditions A and B: A. the average true density of the glass bubbles ranges from 0.35 g/cc to 0.6 g/cc; and B. the hydrostatic pressure at which 10 vol% of the glass bubbles collapse is at least 20 MPa wherein the average true density and the hydrostatic pressure are measured by the methods according to the description. A. the average true density of the glass bubbles ranges from 0.35 g/cc to 0.6 g/cc; and B. the hydrostatic pressure at which 10 vol% of the glass bubbles collapse is at least 20 MPa wherein the average true density and the hydrostatic pressure are measured by the methods according to the description.
A system for repeated determination of a first vector between: - a reference structure comprised in an anatomical volume, and - a medical imaging transducer configured to provide imaging data of the anatomical volume; the system comprising: - a user input configured to specify the reference structure; - an imager configured to receive the imaging data; the system being characterised by: - a model input configured to provide a model of the reference structure; - a segmenter configured to receive the model and to segment the imaging data, using the model, whereby the imaging data associated with the reference structure is at least partially annotated, and - a determiner configured to receive the annotated imaging data of the reference structure and to determine the first vector between the transducer and the reference structure based on the annotated imaging data. - a reference structure comprised in an anatomical volume, and - a medical imaging transducer configured to provide imaging data of the anatomical volume; - a user input configured to specify the reference structure; - an imager configured to receive the imaging data; the system being characterised by: - a model input configured to provide a model of the reference structure; - a segmenter configured to receive the model and to segment the imaging data, using the model, whereby the imaging data associated with the reference structure is at least partially annotated, and - a determiner configured to receive the annotated imaging data of the reference structure and to determine the first vector between the transducer and the reference structure based on the annotated imaging data. - a model input configured to provide a model of the reference structure; - a segmenter configured to receive the model and to segment the imaging data, using the model, whereby the imaging data associated with the reference structure is at least partially annotated, and - a determiner configured to receive the annotated imaging data of the reference structure and to determine the first vector between the transducer and the reference structure based on the annotated imaging data.
Arrangement with a glass body and a packaging for the glass body, wherein the packaging comprises: • a first packaging section and a second packaging section, wherein the first packaging section and the second packaging section are connected to one another by means of a first connection region to be swivelled in relation to one another around a first swivel axis, wherein the first packaging section has at least one fastening region, which is fastened to a complementary fastening region of the second packaging section, • at least one protective element, which is fastened to the second packaging section in such a manner that in an open position of the packaging it faces the first packaging section and is arranged at a predeterminable distance (d) from the first packaging section, wherein the packaging can be moved from the open position into a closed position by swivelling the first packaging section relative to the second packaging section around the first swivel axis, wherein the distance (d) between the protective element and the first packaging section is smaller in the closed position than in the open position, wherein the distance (d) between the protective element and the first packaging section is measured between the first packaging section and the point of the protective element, which lies on the surface of the protective element facing the first packaging section and which has the maximum Euclidean distance from the swivel axis S1, wherein the distance (d) between the protective element and the first packaging section in the open position is designed such that in the open position of the packaging the glass body is arranged between the first packaging section and the second packaging section without coming into contact with the protective element, and wherein the protective element is configured as a cuboid or cylinder, characterised in that the distance (d) between the protective element and the first packaging section in the closed position is designed such that in the closed position of the packaging the glass body comes into contact with the protective element at least in some regions, and that the cuboid or the cylinder has at least one recess. • a first packaging section and a second packaging section, • at least one protective element, which is fastened to the second packaging section in such a manner that in an open position of the packaging it faces the first packaging section and is arranged at a predeterminable distance (d) from the first packaging section,
Method for starting an electronic control circuit for the windings (2.1, 2.2, 2.3) of an electric motor, ∘ having a control unit connected to a voltage source, ∘ having a capacitor connected to the connecting terminals (93, 95) of the voltage source via a system switch element, ∘ wherein the capacitor lies on the input terminals (3, 5) parallel to the control circuit, ∘ and having an operating circuit for the system switch element, ∘ wherein, before the motor is started, the system switch element is closed and the capacitor is charged, ∘ and wherein, after the capacitor has been charged, the system switch element is opened, ∘ and the control unit starts a test step for the control circuit ∘ and wherein, during the test step, the system switch element is open and the control circuit is fed only by the capacitor voltage of the charged capacitor. ∘ having a control unit connected to a voltage source, ∘ having a capacitor connected to the connecting terminals (93, 95) of the voltage source via a system switch element, ∘ wherein the capacitor lies on the input terminals (3, 5) parallel to the control circuit, ∘ and having an operating circuit for the system switch element, ∘ wherein, before the motor is started, the system switch element is closed and the capacitor is charged, ∘ and wherein, after the capacitor has been charged, the system switch element is opened, ∘ and the control unit starts a test step for the control circuit ∘ and wherein, during the test step, the system switch element is open and the control circuit is fed only by the capacitor voltage of the charged capacitor.
A method for diagnosing (i) severe sepsis, or (ii) risk of developing severe sepsis, or (iii) risk of severe sepsis-induced organ failure, in a subject, the method comprising determining in a biological sample obtained from the subject a level of expression for each of a plurality of at least six Endotoxin Tolerance Signature genes to provide a sample gene signature, and comparing the sample gene signature with a reference gene signature, wherein the reference gene signature represents a standard level of expression of each of the plurality of genes; wherein a difference between the sample gene signature and the reference gene signature indicates that the subject has severe sepsis or is at risk of developing severe sepsis or severe sepsis-induced organ failure, wherein the plurality of genes is selected from ADAM15, ADAMDEC1, ALCAM, ALDH1A1, ANKRD1, C19orf59, CA12, CAMP, CCL1, CCL19, CCL22, CCL24, CCL7, CD14, CD300LF, CD93, CDK5RAP2, CPVL, CST3, CST6, CTSK, CXCL10, CYP1B1, CYP27B1, DDIT4, DHRS9, DPYSL3, EGR2, EMR1, EMR3, FBP1, FCER1G, FCER2, FPR1, FPR2, GK, GPNMB, GPR137B, HBEGF, HIST1H1C, HIST2H2AA3, HIST2H2AC, HK2, HK3, HPSE, HSD11B1, HTRA1, IL18BP, IL3RA, ITGB8, KIAA1199, LILRA3, LILRA5, LIPA, LY86, MARCO, MGST1, MMP7, MT1F, MT1G, MT1H, MT1M, MT1X, MXD1, MYADM, NEFH, NQO1, NRIP3, OLIG2, PANX2, PAPLN, PDLIM7, PLAUR, PLD3, PPBP, PROCR, PSTPIP2, PTGES, PTGR1, RAB13, RARRES1, RETN, RHBDD2, RNASE1, S100A12, S100A4, S100A8, S100A9, SERPINA1, SERPINB7, SLC16A10, SLC7A11, TGM2, TLR7, TMEM158, TREM1, TSPAN4, UPP1 and VCAN.