mhurhangee/patent-ind-claim-en huggingface dataset:
A method for detecting a phase separation of a composition, comprising: - providing the coating composition in a receptacle; - providing a measurement instrument for receiving the receptacle, the measurement instrument comprising a measurement probe; - controlling the measurement instrument to displace the measurement probe through the coating composition along a predefined measurement path, the predefined measurement path extending along a length axis of the receptacle; and - outputting a detection result; characterized in that the composition is a waterborne or solvent-borne or solvent-free coating composition, wherein the measurement probe is displaced through the coating composition along the predefined measurement path with a predefined speed profile, and wherein the method further comprises: - acquiring a force-displacement profile by measuring a force exercised on the measurement probe while the probe is being displaced along the predefined measurement path with the predefined speed profile; and - processing the force-displacement profile for detecting at least one phase separation of the coating composition by detecting changes in the recorded force-displacement profile. - providing the coating composition in a receptacle; - providing a measurement instrument for receiving the receptacle, the measurement instrument comprising a measurement probe; - controlling the measurement instrument to displace the measurement probe through the coating composition along a predefined measurement path, the predefined measurement path extending along a length axis of the receptacle; and - outputting a detection result; - acquiring a force-displacement profile by measuring a force exercised on the measurement probe while the probe is being displaced along the predefined measurement path with the predefined speed profile; and - processing the force-displacement profile for detecting at least one phase separation of the coating composition by detecting changes in the recorded force-displacement profile.
A food composition comprising a food component and an additive component, the additive component comprising isolated S-equol; wherein the food composition comprises from 10 mg to 200 mg of S-equol per serving of food.
Sensor arrangement for colour measurement with interference ripple suppression containing at least one silicon-based optical sensor having at least three separate light-sensitive sensor faces and a sensor passivation, which is composed of a combination of SiO 2 layer and anti-reflection-adapted Si 3 N 4 layer , characterised in that - the SiO 2 layer has a thickness in the range from 5 to 10 nm, - above the sensor passivation, there is arranged a substrate which carries at least three spectrally different interference filters (21; 23, 24, 25) and which is connected to the sensor by means of an adhesive and which forms between each of the light-sensitive sensor faces and an interference filter which is associated with the respective sensor face an intermediate space in the manner of an optical layer (32; 33) with a lower refractive index (n 2 ) with respect to the sensor passivation of the sensor , and - the optical layer (32; 33) over each associated light-sensitive sensor face has a height variation (Δh), wherein the height variation (Δh) is produced by means of a tilting of the substrate with the optical filters (21; 23, 24, 25) with respect to the light-sensitive sensor faces , wherein spacers for defined adjustment of the substrate tilting are provided on the substrate at predetermined positions which are produced in the process of the production of the optical filters (21; 23, 24, 25) by sequential coating of filters (21; 23, 24, 25) of known layer thicknesses at a defined height. - the SiO 2 layer has a thickness in the range from 5 to 10 nm, - above the sensor passivation, there is arranged a substrate which carries at least three spectrally different interference filters (21; 23, 24, 25) and which is connected to the sensor by means of an adhesive and which forms between each of the light-sensitive sensor faces and an interference filter which is associated with the respective sensor face an intermediate space in the manner of an optical layer (32; 33) with a lower refractive index (n 2 ) with respect to the sensor passivation of the sensor , and - the optical layer (32; 33) over each associated light-sensitive sensor face has a height variation (Δh), wherein the height variation (Δh) is produced by means of a tilting of the substrate with the optical filters (21; 23, 24, 25) with respect to the light-sensitive sensor faces , wherein spacers for defined adjustment of the substrate tilting are provided on the substrate at predetermined positions which are produced in the process of the production of the optical filters (21; 23, 24, 25) by sequential coating of filters (21; 23, 24, 25) of known layer thicknesses at a defined height.
A shaving razor comprising a cartridge comprising a housing having a front portion and a rear portion , a guard at the front portion of said housing and a cap at the rear portion of the housing and a blade array located in-between the guard and cap , wherein the blade array comprises at least two blades, a primary blade and a final blade , each blade having a blade edge that extends parallel to the housing ; having a blade plane: (x) tangential to the primary blade edge and the final blade edge , characterized in that each angle between each blade and the blade plane (x) is 50° or greater.
A method for performing an assembly operation , the method comprising: macro-positioning a tool within an interior of a fuselage assembly ; micro-positioning the tool relative to a particular location on a panel of the fuselage assembly ; and performing the assembly operation at the particular location on the panel using the tool , wherein: macro-positioning the tool comprises moving a platform base of an internal mobile platform carrying the tool with at least one degree of freedom relative to a floor inside the fuselage assembly ; and wherein: a track system including a first track and a second track is associated with the platform base , the first and second tracks being for driving the internal mobile platform in a first direction ; and the first and second tracks include a roller chain , a plurality of rollers , and a plurality of support plates . macro-positioning a tool within an interior of a fuselage assembly ; micro-positioning the tool relative to a particular location on a panel of the fuselage assembly ; and macro-positioning the tool comprises moving a platform base of an internal mobile platform carrying the tool with at least one degree of freedom relative to a floor inside the fuselage assembly ; and wherein: a track system including a first track and a second track is associated with the platform base , the first and second tracks being for driving the internal mobile platform in a first direction ; and the first and second tracks include a roller chain , a plurality of rollers , and a plurality of support plates . a track system including a first track and a second track is associated with the platform base , the first and second tracks being for driving the internal mobile platform in a first direction ; and the first and second tracks include a roller chain , a plurality of rollers , and a plurality of support plates .
A method for manufacturing a device for locating an impact comprising: - an interactive surface having a front face (A) for receiving an impact (P), and - at least three transducers (PT A , PT B , PT C , PT D ; PT), that need to be distributed and attached against the front face (A) or a rear face (B) of the interactive surface , designed to capture the progressive mechanical waves propagating in the interactive surface from the impact (P) and transform them into electrical signals, with the method for manufacturing comprising the following steps: - determining a central positioning point (C A , C B , C C C D ; C) for each transducer (PT A , PT B , PT C , PT D ; PT) on the front face (A) or rear face (B) of the interactive surface , - attaching each transducer (PT A , PT B , PTc, PT D ; PT) around the central positioning point (C A , C B , C C C D ; C) of same, with each transducer (PT A , PT B , PT C , PT D ; PT) having a lower conductive layer forming a first electrode through which it is attached against the front face (A) or the rear face (B) of the interactive surface , a piezoelectric intermediate layer and a free upper conductive layer intended to form a second electrode, characterized in that it further comprises, following the attaching of each transducer (PT A , PT B , PT C PT D ; PT), a step of machining the free upper conductive layer of at least one of the transducers (PT A , PT B , PT C PT D ; PT) using a machine tool at least as far as the piezoelectric intermediate layer of this transducer (PT A , PT B , PT C , PT D ; PT) in order to form the second electrode of this transducer (PT A , PT B , PT C PT D ; PT) by centering it around the central positioning point (C A , C B , C C , C D ; C) of same as a portion of the upper conductive layer arranged in the free upper conductive layer . - an interactive surface having a front face (A) for receiving an impact (P), and - at least three transducers (PT A , PT B , PT C , PT D ; PT), that need to be distributed and attached against the front face (A) or a rear face (B) of the interactive surface , designed to capture the progressive mechanical waves propagating in the interactive surface from the impact (P) and transform them into electrical signals, - determining a central positioning point (C A , C B , C C C D ; C) for each transducer (PT A , PT B , PT C , PT D ; PT) on the front face (A) or rear face (B) of the interactive surface , - attaching each transducer (PT A , PT B , PTc, PT D ; PT) around the central positioning point (C A , C B , C C C D ; C) of same, with each transducer (PT A , PT B , PT C , PT D ; PT) having a lower conductive layer forming a first electrode through which it is attached against the front face (A) or the rear face (B) of the interactive surface , a piezoelectric intermediate layer and a free upper conductive layer intended to form a second electrode,
System for testing a communication device, wherein the system comprises a signal generator for generating test signals and an apparatus for testing a communication device , wherein the apparatus for testing a communication device comprises a positioning device , wherein the positioning device is configured to position the device under test in a test chamber , an analysing device , wherein the analysing device is configured to analyse signals generated by the device under test in in response to a test signal, and a transmitting unit , wherein the transmitting unit is configured to transmit the signals generated by the device under test from the positioning device to the analysing device , wherein the transmitting unit comprises a first signal converter for converting the signals generated by the device under test from the electromagnetic domain into the optical domain to generate first converted signals, at least one fibre optic cable to transmit the first converted signals from the first converter to a second converter for converting the first converted signals from the optical domain to the electromagnetic domain to generate second converted signals, and wherein the analysing device is configured to analyse the second converted signals, characterized in that the system comprises a further transmitting unit for transmitting the test signals generated by the signal generator into the test chamber , wherein the further transmitting unit comprises a third signal converter for converting the test signals generated by the signal generator from the electromagnetic domain into the optical domain to generate third converted signals, a further fibre optic cable to transmit the third converted signals from the third converter to a fourth converter , wherein the fourth converter is placed in the test chamber, and wherein the fourth converter is configured to convert the third converted signals from the optical domain to the electromagnetic domain to generate fourth converted signals that are emitted in the test chamber .
A method of controlling an operating temperature of a first combustion zone of a combustor of a rotary machine , the combustor including the first combustion zone and a second combustion zone , said method comprising: i) determining a current operating temperature of the first combustion zone using a digital simulation of the rotary machine ; ii) determining a target operating temperature of the first combustion zone ; iii) determining a derivative of the current operating temperature of the first combustion zone with respect to a current fuel split using the digital simulation, wherein the fuel split apportions a total flow of fuel to the combustor between the first combustion zone and the second combustion zone ; iv) calculating , using the determined derivative , a calculated fuel split that results in a calculated operating temperature of the first combustion zone approaching the target operating temperature; v) channeling a first flow of fuel to the first combustion zone and a second flow of fuel to the second combustion zone , wherein the first flow of fuel and the second flow of fuel are determined in response to the calculated fuel split ; and vi) iterating steps i through v until the calculated fuel split equals a target fuel split , wherein the target fuel split is the fuel split that results in the target operating temperature. i) determining a current operating temperature of the first combustion zone using a digital simulation of the rotary machine ; ii) determining a target operating temperature of the first combustion zone ; iii) determining a derivative of the current operating temperature of the first combustion zone with respect to a current fuel split using the digital simulation, wherein the fuel split apportions a total flow of fuel to the combustor between the first combustion zone and the second combustion zone ; iv) calculating , using the determined derivative , a calculated fuel split that results in a calculated operating temperature of the first combustion zone approaching the target operating temperature; v) channeling a first flow of fuel to the first combustion zone and a second flow of fuel to the second combustion zone , wherein the first flow of fuel and the second flow of fuel are determined in response to the calculated fuel split ; and vi) iterating steps i through v until the calculated fuel split equals a target fuel split , wherein the target fuel split is the fuel split that results in the target operating temperature.
A composite structure , comprising: a laminate having a plurality of composite plies ; a compression discontinuity associated with the laminate ; and a stabilizing element included with the composite plies and being located proximate the compression discontinuity , wherein the laminate comprises a panel formed of the plurality of the composite plies ; the compression discontinuity comprises a region of low compaction pressure located proximate a structural member edge of a structural member mounted to the panel ; and the stabilizing element being included with the composite plies and being located proximate the structural member edge . a laminate having a plurality of composite plies ; a compression discontinuity associated with the laminate ; and a stabilizing element included with the composite plies and being located proximate the compression discontinuity , wherein the laminate comprises a panel formed of the plurality of the composite plies ; the compression discontinuity comprises a region of low compaction pressure located proximate a structural member edge of a structural member mounted to the panel ; and the stabilizing element being included with the composite plies and being located proximate the structural member edge .
A wing of an aircraft comprising: a wing leading edge , a wing trailing edge , and a wing surface defined by a wing upper surface and a wing lower surface , the wing extending from a wing root to a wingtip having a wingtip chord; a winglet extending from the wingtip and having a winglet leading edge , a winglet trailing edge , a winglet inboard surface , a winglet outboard surface , a winglet root having a winglet root chord (Cwi), and a winglet tip , wherein an intersection of the winglet leading edge with the wingtip is located aft of the wing leading edge at the wingtip ; and a flow fence disposed on the wing surface inboard from the winglet in a top planform view of the wing, where in an outboard side view of the winglet the flow fence extends from a first position located on the wing upper surface which overlaps with the winglet to a second position located on the wing lower surface , where in the top planform view of the wing an inboard spacing of the flow fence from the wingtip does not exceed 100% of a length of the winglet root chord (Cwi), wherein the flow fence is adapted to delay and/or prevent airflow separation on the winglet inboard surface at high angle of sideslip, increasing lateral stability and linearizing aircraft behavior at high angle of sideslip, wherein the flow fence is adapted to generate vortices between the flow fence and the winglet by airflow flowing from the wing lower surface to the wing upper surface around the wingtip and the wing leading edge , wherein the vortices redirect airflow to limit low-pressure peaks on the winglet leading edge . a wing leading edge , a wing trailing edge , and a wing surface defined by a wing upper surface and a wing lower surface , the wing extending from a wing root to a wingtip having a wingtip chord; a winglet extending from the wingtip and having a winglet leading edge , a winglet trailing edge , a winglet inboard surface , a winglet outboard surface , a winglet root having a winglet root chord (Cwi), and a winglet tip , wherein an intersection of the winglet leading edge with the wingtip is located aft of the wing leading edge at the wingtip ; and a flow fence disposed on the wing surface inboard from the winglet in a top planform view of the wing, where in an outboard side view of the winglet the flow fence extends from a first position located on the wing upper surface which overlaps with the winglet to a second position located on the wing lower surface , where in the top planform view of the wing an inboard spacing of the flow fence from the wingtip does not exceed 100% of a length of the winglet root chord (Cwi), wherein the flow fence is adapted to delay and/or prevent airflow separation on the winglet inboard surface at high angle of sideslip, increasing lateral stability and linearizing aircraft behavior at high angle of sideslip, wherein the flow fence is adapted to generate vortices between the flow fence and the winglet by airflow flowing from the wing lower surface to the wing upper surface around the wingtip and the wing leading edge , wherein the vortices redirect airflow to limit low-pressure peaks on the winglet leading edge .
A system , comprising: one or more network nodes which communicate with each other via a first network protocol, wherein at least one network node is configured to establish a wireless connection with a mobile end device via a second network protocol, wherein the network node comprises a transmission component which is configured to establish a connection between the mobile end device and a target node of the network nodes , wherein the second network protocol is translated by the transmission component into the first network protocol, and wherein the mobile end device is configured to select the network node among those accessible wirelessly which has the best connection quality to the mobile end device , characterized in that the target node is determined on the basis of a user input into the mobile end device . one or more network nodes which communicate with each other via a first network protocol, wherein at least one network node is configured to establish a wireless connection with a mobile end device via a second network protocol, wherein the network node comprises a transmission component which is configured to establish a connection between the mobile end device and a target node of the network nodes , wherein the second network protocol is translated by the transmission component into the first network protocol, and wherein the mobile end device is configured to select the network node among those accessible wirelessly which has the best connection quality to the mobile end device , characterized in that the target node is determined on the basis of a user input into the mobile end device .
A microwave ablation cable assembly comprising: a first coaxial cable having a first diameter, an inner conductor , an outer conductor , and a dielectric formed between the inner and outer conductors; a second coaxial cable having a second diameter smaller than the first diameter, an inner conductor , an outer conductor , and a dielectric formed between the inner and outer conductors; a transition between the first and second coaxial cables positionable within the anatomy of a patient to reduce the diameter of the cable assembly to a diameter necessary to reach desired locations within a body with the second coaxial cable, the transition reducing in diameter from the first diameter at the first coaxial cable to the second diameter at the second coaxial cable, and having an inner conductor , an outer conductor , and a dielectric formed between the inner and outer conductors; and a radiating section at a distal end of the assembly in electrical communication with the first coaxial cable via the second coaxial cable and the transition, wherein the radiating section is coupled to the distal end of the second coaxial cable; wherein the inner conductors of the first and second coaxial cables and the transition are in electrical communication and the outer conductors of the first and second coaxial cables and the transition are in electrical communication. a first coaxial cable having a first diameter, an inner conductor , an outer conductor , and a dielectric formed between the inner and outer conductors; a second coaxial cable having a second diameter smaller than the first diameter, an inner conductor , an outer conductor , and a dielectric formed between the inner and outer conductors; a transition between the first and second coaxial cables positionable within the anatomy of a patient to reduce the diameter of the cable assembly to a diameter necessary to reach desired locations within a body with the second coaxial cable, the transition reducing in diameter from the first diameter at the first coaxial cable to the second diameter at the second coaxial cable, and having an inner conductor , an outer conductor , and a dielectric formed between the inner and outer conductors; and a radiating section at a distal end of the assembly in electrical communication with the first coaxial cable via the second coaxial cable and the transition, wherein the radiating section is coupled to the distal end of the second coaxial cable; wherein the inner conductors of the first and second coaxial cables and the transition are in electrical communication and the outer conductors of the first and second coaxial cables and the transition are in electrical communication.