mhurhangee/patent-ind-claim-en huggingface dataset:
A short-circuit detection device in a switching arm , the switching arm being positioned between a first terminal and a second voltage supply terminal , the potential of the first terminal being suitable for being greater than the potential of the second terminal , the switching arm comprising two higher and lower switching half-arms in series, the higher switching half-arm being electrically connected to the first terminal and the lower switching half-arm being electrically connected to the second terminal , the switching half-arms each including at least one semiconductor switch , each switch comprising a control electrode and two conduction electrodes, the short-circuit detection device comprising: - for each switching half-arm, a pair of measuring terminals , comprising a third terminal and a fourth terminal , configured to be connected to the terminals of a stray inductance in series with one of the conduction electrodes of the at least one switch of said switching half-arm , the fourth terminal being suitable for being positioned between the third terminal and the first terminal , and - an information processing unit connected as input to the pairs of measuring terminals and having a logic output able to supply a signal indicating the detection of a short-circuit in the switching arm , characterized in that the processing unit includes: - for each pair of measuring terminals , a detection module configured to send, as output, an output signal representative of the sign of the difference between the potential of the fourth terminal and the potential of the third terminal , and - a comparison module capable of supplying, via the logic output, the signal indicating the detection of a short-circuit, only when the output signals sent by the two detection modules are each representative of a positive sign. - for each switching half-arm, a pair of measuring terminals , comprising a third terminal and a fourth terminal , configured to be connected to the terminals of a stray inductance in series with one of the conduction electrodes of the at least one switch of said switching half-arm , the fourth terminal being suitable for being positioned between the third terminal and the first terminal , and - an information processing unit connected as input to the pairs of measuring terminals and having a logic output able to supply a signal indicating the detection of a short-circuit in the switching arm , - for each pair of measuring terminals , a detection module configured to send, as output, an output signal representative of the sign of the difference between the potential of the fourth terminal and the potential of the third terminal , and - a comparison module capable of supplying, via the logic output, the signal indicating the detection of a short-circuit, only when the output signals sent by the two detection modules are each representative of a positive sign.
A plate fin fluid processing device comprising: a. a plurality of active layers, where each active layer includes a fin plate sandwiched between parting sheets so that an active fluid space is defined between the parting sheets, and where the plurality of active layers includes an outermost active layer having an inlet and an outlet; b. a contingent layer body positioned adjacent to the outermost active layer, said contingent layer body including a fin plate positioned between a parting sheet and a cap sheet, said contingent layer body having a fluid space that is sealed with respect to the atmosphere and contains an inert gas at a predetermined pressure that is above or below atmospheric pressure; c. a pressure monitoring system in communication with the fluid space of the contingent layer body; and d. an emergency pressure relief device configured to release a pressure within the fluid space if a preset pressure is exceeded. a. a plurality of active layers, where each active layer includes a fin plate sandwiched between parting sheets so that an active fluid space is defined between the parting sheets, and where the plurality of active layers includes an outermost active layer having an inlet and an outlet; b. a contingent layer body positioned adjacent to the outermost active layer, said contingent layer body including a fin plate positioned between a parting sheet and a cap sheet, said contingent layer body having a fluid space that is sealed with respect to the atmosphere and contains an inert gas at a predetermined pressure that is above or below atmospheric pressure; c. a pressure monitoring system in communication with the fluid space of the contingent layer body; and d. an emergency pressure relief device configured to release a pressure within the fluid space if a preset pressure is exceeded.
A method for stabilizing an extracellular nucleic acid population comprised in a cell-containing biological sample by contacting the cell-containing biological sample with butanamide.
Sorter (A) for separating out discrete products (P), which are conveyed in a conveying direction (F) along a conveying path leading over the sorter (A), the sorter comprising a) a swivel axis (S), about which a base body (L) of the sorter (A) can be swivelled, b) wherein the base body (L) has a plurality of (n) flat support surfaces (T 1 , T 2 , ... T n ), which extend parallel to the swivel axis (S) and are arranged evenly around it, c) wherein the base body (L) can be swivelled about the swivel axis (S) such that selectively precisely one of the support surfaces (T 1 , T 2 , ... T n ) is swivelled into the conveying path and then runs parallel to the conveying direction (F) and acts as conveying plane (E F ) for receiving a product delivered to the sorter (A) and for conveying it further in the conveying direction (F), characterized in that d) the support surfaces (T 1 , T 2 , ... T n ) of the base body (L) form a regular prism. a) a swivel axis (S), about which a base body (L) of the sorter (A) can be swivelled, b) wherein the base body (L) has a plurality of (n) flat support surfaces (T 1 , T 2 , ... T n ), which extend parallel to the swivel axis (S) and are arranged evenly around it, c) wherein the base body (L) can be swivelled about the swivel axis (S) such that selectively precisely one of the support surfaces (T 1 , T 2 , ... T n ) is swivelled into the conveying path and then runs parallel to the conveying direction (F) and acts as conveying plane (E F ) for receiving a product delivered to the sorter (A) and for conveying it further in the conveying direction (F), characterized in that d) the support surfaces (T 1 , T 2 , ... T n ) of the base body (L) form a regular prism.
An aircraft comprising a passenger cabin and a system, the system comprising: a vestibule disposed in the passenger cabin of the aircraft, the vestibule including at least one staircase for accessing at least one passenger rest cabin , each of the at least one passenger rest cabin implemented above or below the passenger cabin of the aircraft; at least one external view camera configured to capture images outside of the aircraft; and a plurality of passenger rest compartments implemented in the at least one passenger rest cabin, each of the plurality of the passenger rest compartments including a bed and a passenger service unit, PSU, ; wherein each of the plurality of the passenger rest compartments further includes a display , wherein for each of the plurality of the passenger rest compartments the display is configured to be a virtual window configured to present at least a portion of the images outside of the aircraft; and wherein each of the plurality of passenger rest compartments further includes at least one sensor configured to detect a position of an occupant's head, wherein for each of the plurality of passenger rest compartments, the display is configured to be the virtual window configured to present at least the portion of the images outside of the aircraft based on the detected position of the occupant's head. a vestibule disposed in the passenger cabin of the aircraft, the vestibule including at least one staircase for accessing at least one passenger rest cabin , each of the at least one passenger rest cabin implemented above or below the passenger cabin of the aircraft; at least one external view camera configured to capture images outside of the aircraft; and a plurality of passenger rest compartments implemented in the at least one passenger rest cabin, each of the plurality of the passenger rest compartments including a bed and a passenger service unit, PSU, ; wherein each of the plurality of the passenger rest compartments further includes a display , wherein for each of the plurality of the passenger rest compartments the display is configured to be a virtual window configured to present at least a portion of the images outside of the aircraft; and wherein each of the plurality of passenger rest compartments further includes at least one sensor configured to detect a position of an occupant's head, wherein for each of the plurality of passenger rest compartments, the display is configured to be the virtual window configured to present at least the portion of the images outside of the aircraft based on the detected position of the occupant's head.
A resin material for an acoustic wave probe, comprising: a polymer that is formed of at least - a structural unit (a) having a polysiloxane bond of Formula , and - a structural unit (b) which has a partial structure of Formula and is an acryloyloxy structural unit (b1), an acrylamide structural unit (b2) or a styrene structural unit (b3), wherein n is an integer of 10-10,000, and R is H or a monovalent organic group; and a bond line extending downward from a carbon atom to which R bonds is a bond. a polymer that is formed of at least - a structural unit (a) having a polysiloxane bond of Formula , and - a structural unit (b) which has a partial structure of Formula and is an acryloyloxy structural unit (b1), an acrylamide structural unit (b2) or a styrene structural unit (b3), - a structural unit (a) having a polysiloxane bond of Formula , and - a structural unit (b) which has a partial structure of Formula and is an acryloyloxy structural unit (b1), an acrylamide structural unit (b2) or a styrene structural unit (b3), wherein n is an integer of 10-10,000, and R is H or a monovalent organic group; and a bond line extending downward from a carbon atom to which R bonds is a bond.
An avionic communication system comprising: - a plurality of switches (22A,..., 22N) connected to each other in order to form a computer network; - a plurality of equipment units (24A,..., 24N), each equipment unit (24A,..., 24N) being a transmitter and/or receiver of digital data and being connected to at least one switch (22A,..., 22N); the system being such that: - each transmitting equipment unit (24A,..., 24N) is capable of generating digital data that are present in the form of a plurality of frames, each frame having an identifier (VL, Flow_ID ) and being of a first type or of a second type, the frames of the first type being in compliance with a first protocol and the frames of the second type being in compliance with a second protocol which is different from the first protocol, the frames of a same type having the same identifier (VL; Flow_ID) forming a data flow of this type; - each switch (22A,..., 22N) and each receiving equipment unit (24A,..., 24N) are configured so as to determine the type of each frame received and, based on the determined type, to process this frame in accordance with the first protocol or in accordance with the second protocol, each frame of the first type being processed on a prioritised basis in relation to each frame of the second type; and - the first protocol is of the type ARINC 664 P7 and the second protocol is of the type Ethernet with predetermined routing, wherein each transmitting equipment unit (24A,..., 24N) is configured so as to transmit the frames of the second type included in the same data flow according to a bandwidth defined for this data flow. - a plurality of switches (22A,..., 22N) connected to each other in order to form a computer network; - a plurality of equipment units (24A,..., 24N), each equipment unit (24A,..., 24N) being a transmitter and/or receiver of digital data and being connected to at least one switch (22A,..., 22N); - each transmitting equipment unit (24A,..., 24N) is capable of generating digital data that are present in the form of a plurality of frames, each frame having an identifier (VL, Flow_ID ) and being of a first type or of a second type, the frames of the first type being in compliance with a first protocol and the frames of the second type being in compliance with a second protocol which is different from the first protocol, the frames of a same type having the same identifier (VL; Flow_ID) forming a data flow of this type; - each switch (22A,..., 22N) and each receiving equipment unit (24A,..., 24N) are configured so as to determine the type of each frame received and, based on the determined type, to process this frame in accordance with the first protocol or in accordance with the second protocol, each frame of the first type being processed on a prioritised basis in relation to each frame of the second type; and - the first protocol is of the type ARINC 664 P7 and the second protocol is of the type Ethernet with predetermined routing,
A system for analyzing turbomachinery comprising: an intelligent turbomachinery tracking filter ITTF, system configured to determine one or more performance shifts and to derive one or more profile trends for one or more components of a turbomachinery based on a plurality of measured turbomachinery parameters; and a root cause analyzer configured to determine a root cause of the turbomachinery performance based on the one or more performance shifts, characterized in that the root cause analyzer comprises: a trend quantifier configured to process and quantify trend values in the one or more profile trends to produce a quantified profile trend including one or more of a trend slope or gradient, an amount of noise in the trend values, an amount of shifting in the trend, maximum values in the trend, and/or minimum values in the trend; and a fuzzy logic engine configured to derive one or more fuzzy values based on the quantified profile trend to derive a root cause analysis; wherein the root cause analyzer is configured to apply one or more models and rules to the one or more fuzzy values to derive one or more possible root causes and to derive a probability of accuracy of each of the one or more possible root causes. an intelligent turbomachinery tracking filter ITTF, system configured to determine one or more performance shifts and to derive one or more profile trends for one or more components of a turbomachinery based on a plurality of measured turbomachinery parameters; and a root cause analyzer configured to determine a root cause of the turbomachinery performance based on the one or more performance shifts, characterized in that the root cause analyzer comprises: a trend quantifier configured to process and quantify trend values in the one or more profile trends to produce a quantified profile trend including one or more of a trend slope or gradient, an amount of noise in the trend values, an amount of shifting in the trend, maximum values in the trend, and/or minimum values in the trend; and a fuzzy logic engine configured to derive one or more fuzzy values based on the quantified profile trend to derive a root cause analysis; wherein the root cause analyzer is configured to apply one or more models and rules to the one or more fuzzy values to derive one or more possible root causes and to derive a probability of accuracy of each of the one or more possible root causes. a trend quantifier configured to process and quantify trend values in the one or more profile trends to produce a quantified profile trend including one or more of a trend slope or gradient, an amount of noise in the trend values, an amount of shifting in the trend, maximum values in the trend, and/or minimum values in the trend; and a fuzzy logic engine configured to derive one or more fuzzy values based on the quantified profile trend to derive a root cause analysis; wherein the root cause analyzer is configured to apply one or more models and rules to the one or more fuzzy values to derive one or more possible root causes and to derive a probability of accuracy of each of the one or more possible root causes.
A compound of the formula 1a, 1b, 1c, 1d, or 1e or a pharmaceutically acceptable salt or solvate thereof, for use as a medicament.
A VCSEL device comprising: a VCSEL, the VCSEL comprising: a light-generating quantum well active region ; a first mirror layer arranged on a first side of the active region and configured to emit at least 50% of light generated by the active region ; a second mirror layer arranged on a second side of the active region and configured to emit no more than 50% of light generated by the active region ; a metal contact layer disposed below the second mirror layer and patterned with an opening aligned with a light emission direction of the VCSEL, the opening sized and configured to receive light emitted from the second mirror layer ; and a dielectric layer deposited in the opening of the metal contact layer; and a photodiode arranged between the metal contact layer and a submount , the photodiode being configured to receive light emitted from the second mirror layer ; wherein the VCSEL is mounted directly on the photodiode . a light-generating quantum well active region ; a first mirror layer arranged on a first side of the active region and configured to emit at least 50% of light generated by the active region ; a second mirror layer arranged on a second side of the active region and configured to emit no more than 50% of light generated by the active region ; a metal contact layer disposed below the second mirror layer and patterned with an opening aligned with a light emission direction of the VCSEL, the opening sized and configured to receive light emitted from the second mirror layer ; and a dielectric layer deposited in the opening of the metal contact layer; and a photodiode arranged between the metal contact layer and a submount , the photodiode being configured to receive light emitted from the second mirror layer ; wherein the VCSEL is mounted directly on the photodiode .
A method for manufacturing clinker fillets , - with at least one extrusion press for extruding at least one extrudate of a plasticized mass, particularly a plasticized ceramic mass, - with at least one forming device for producing structure elements in at least one surface of the plasticized extrudate to be structured, - and with at least one cutting device for separating fillet sections from the extrudate , wherein the at least one forming device comprises a plurality of forming units , which can be moved over the surface of the extrudate to be structured in a direction that respectively extends obliquely to the extruding direction of the extrudate or obliquely to the longitudinal direction of the extrudate such that structure elements can thereby be produced in the surface to be structured, and wherein the motion of the forming units takes place in such a way that the structure elements produced in the surface of the extrudate are respectively arranged transverse - particularly perpendicular or essentially perpendicular - to the extruding direction of the extrudate or to the longitudinal direction of the extrudate , characterized in that the forming units and/or the at least one forming device can be respectively moved obliquely to the extruding direction or the longitudinal direction of the extrudate in an oscillating manner - preferably in a periodically oscillating manner. - with at least one extrusion press for extruding at least one extrudate of a plasticized mass, particularly a plasticized ceramic mass, - with at least one forming device for producing structure elements in at least one surface of the plasticized extrudate to be structured, - and with at least one cutting device for separating fillet sections from the extrudate ,
Method for determining the direction and the amplitude of a stress applied to a pod comprising a fixed part and a mobile part deformable under the effect of said stress, wherein: - mechanical deformations applied onto the mobile part under the effect of said stress are measured by measuring a distance between the fixed part and the mobile part in the direction of application of the stress, and - the distance measurements are processed to determine the amplitude and the direction of the stress, characterised in that the direction of the stress is determined from the position of at least one measurement sensor delivering a measurement value extreme with respect to measurement values respectively provided by a set of angularly distributed measurement sensors measuring the movement of the mobile part with respect to the fixed part . - mechanical deformations applied onto the mobile part under the effect of said stress are measured by measuring a distance between the fixed part and the mobile part in the direction of application of the stress, and - the distance measurements are processed to determine the amplitude and the direction of the stress, characterised in that the direction of the stress is determined from the position of at least one measurement sensor delivering a measurement value extreme with respect to measurement values respectively provided by a set of angularly distributed measurement sensors measuring the movement of the mobile part with respect to the fixed part .