mhurhangee/patent-ind-claim-en huggingface dataset:
A diffuser case support structure for a gas turbine engine comprising: a fairing (48; 648) disposed circumferentially about a longitudinal axis , the fairing (48; 648) defining a plurality of passages circumferentially spaced apart and forming at least a portion of a fluid path between a compressor and a combustor of the gas turbine engine ; a diffuser frame (58; 658) comprising a plurality of struts , each of the plurality of struts disposed between a pair of adj acent passages of the plurality of passages ; and a sliding joint forming an interface between the fairing (48; 648) and the diffuser frame (58; 658), the sliding joint comprising a fastener extending generally axially through an aperture disposed in the fairing (48; 648); wherein the diffuser frame (58; 658) is configured to couple an inner diffuser case to an outer diffuser case , characterised in that the sliding joint further comprises a bushing extending through the aperture , the bushing compressed between the diffuser frame (58; 658) and the fastener , wherein the fairing (48; 648) is configured to move radially with respect to the diffuser frame (58; 658) via the sliding joint , in response to at least one of thermal expansion and contraction of the fairing (48; 648) in a radial direction. a fairing (48; 648) disposed circumferentially about a longitudinal axis , the fairing (48; 648) defining a plurality of passages circumferentially spaced apart and forming at least a portion of a fluid path between a compressor and a combustor of the gas turbine engine ; a diffuser frame (58; 658) comprising a plurality of struts , each of the plurality of struts disposed between a pair of adj acent passages of the plurality of passages ; and a sliding joint forming an interface between the fairing (48; 648) and the diffuser frame (58; 658), the sliding joint comprising a fastener extending generally axially through an aperture disposed in the fairing (48; 648); wherein the diffuser frame (58; 658) is configured to couple an inner diffuser case to an outer diffuser case , characterised in that the sliding joint further comprises a bushing extending through the aperture , the bushing compressed between the diffuser frame (58; 658) and the fastener , wherein the fairing (48; 648) is configured to move radially with respect to the diffuser frame (58; 658) via the sliding joint , in response to at least one of thermal expansion and contraction of the fairing (48; 648) in a radial direction.
A method for producing a polymer, comprising: a step of polymerizing a starting material composition (I) that includes a monomer mixture (I-1) containing a macromonomer (a) represented by the following Formula and a vinyl monomer (b) and 0.07 to 5 parts by mass of a non-metallic chain transfer agent with respect to 100 parts by mass of the monomer mixture (I-1), wherein the non-metallic chain transfer agent is a sulfur-containing chain transfer agent: in Formula , R and R 1 to R n each independently represent a hydrogen atom, an alkyl group, a cycloalkyl group, an aryl group, or a heterocyclic group, X 1 to X n each independently represent a hydrogen atom or a methyl group, Z represents a terminal group, and n represents an integer of 2 to 10,000.
An operating mechanism of a circuit breaker comprising: a housing ; a cam element positioned within the housing , wherein the cam element is installed on a mechanically driven first shaft ; a transmission lever provided with a first roller element , wherein the transmission lever is installed on a second shaft such that the second shaft is parallel to the first shaft ; and a support assembly coupled to an inner surface of a vertical wall of the housing , wherein the support assembly comprises: a fork joint having a moveable end and a pivoted end , wherein the moveable end is adapted to support a second roller element; and a damper element having a first end and a second end , characterised in that the first end of the damper element is rigidly pivoted on an upper horizontal surface of the housing of the circuit breaker , and the second end of the damper element is coupled to the moveable end of the fork joint , a housing ; a cam element positioned within the housing , wherein the cam element is installed on a mechanically driven first shaft ; a transmission lever provided with a first roller element , wherein the transmission lever is installed on a second shaft such that the second shaft is parallel to the first shaft ; and a support assembly coupled to an inner surface of a vertical wall of the housing , wherein the support assembly comprises: a fork joint having a moveable end and a pivoted end , wherein the moveable end is adapted to support a second roller element; and a damper element having a first end and a second end , characterised in that the first end of the damper element is rigidly pivoted on an upper horizontal surface of the housing of the circuit breaker , and the second end of the damper element is coupled to the moveable end of the fork joint , a fork joint having a moveable end and a pivoted end , wherein the moveable end is adapted to support a second roller element; and a damper element having a first end and a second end , characterised in that the first end of the damper element is rigidly pivoted on an upper horizontal surface of the housing of the circuit breaker , and the second end of the damper element is coupled to the moveable end of the fork joint ,
A sample holder for use in a centrifuge, the sample holder being generally planar and comprising: an aperture or recess for releasably retaining a sample storage member including a sample chamber adapted to contain a volume of liquid; a centre point around which the holder will rotate during use; and one or more calibration features , wherein the calibration feature(s) comprise one or more outer edges (20, 44a-d, 48a-f, 53), which lie on the side of the or each calibration feature which is furthest from the centre point , and the one or more outer edges (20, 44a-d, 48a-f, 53) comprise a series of radially spaced-apart outer edge portions or positions which are spaced at different distances from the centre point as a function of angular position around the centre point , and wherein the or each calibration feature is an aperture formed through the entire thickness of the holder , or is an insert of a transparent or substantially transparent material which is placed into a hole in the holder . an aperture or recess for releasably retaining a sample storage member including a sample chamber adapted to contain a volume of liquid; a centre point around which the holder will rotate during use; and one or more calibration features , wherein the calibration feature(s) comprise one or more outer edges (20, 44a-d, 48a-f, 53), which lie on the side of the or each calibration feature which is furthest from the centre point , and the one or more outer edges (20, 44a-d, 48a-f, 53) comprise a series of radially spaced-apart outer edge portions or positions which are spaced at different distances from the centre point as a function of angular position around the centre point , and wherein the or each calibration feature is an aperture formed through the entire thickness of the holder , or is an insert of a transparent or substantially transparent material which is placed into a hole in the holder .
A wear detection device for a conveyor belt, comprising: a magnet member buried in a conveyor belt having an endless belt shape; a magnetic sensor (13a to 13j) arranged opposite to an outer circumferential surface of the conveyor belt and configured to detect a magnetic field from the magnet member to generate an output signal; a calculation unit configured to calculate a thickness of the conveyor belt according to the output signal generated by the magnetic sensor (13a to 13j); and a storage unit configured to store the thickness calculated by the calculation unit , characterized in that the wear detection device comprises: a processing unit configured to calculate a decrease amount of the thickness per a predetermined moving load amount of the conveyor belt according to the thickness stored in the storage unit and determine whether or not the value exceeds a threshold value set in advance. a magnet member buried in a conveyor belt having an endless belt shape; a magnetic sensor (13a to 13j) arranged opposite to an outer circumferential surface of the conveyor belt and configured to detect a magnetic field from the magnet member to generate an output signal; a calculation unit configured to calculate a thickness of the conveyor belt according to the output signal generated by the magnetic sensor (13a to 13j); and a storage unit configured to store the thickness calculated by the calculation unit , characterized in that the wear detection device comprises: a processing unit configured to calculate a decrease amount of the thickness per a predetermined moving load amount of the conveyor belt according to the thickness stored in the storage unit and determine whether or not the value exceeds a threshold value set in advance.
A panel for attenuating noise, comprising: a porous first skin ; a second skin ; and a core connected between the porous first skin and the second skin , the core including a corrugated body and a stringer body ; the corrugated body including a plurality of corrugations configured from at least a plurality of baffles and a plurality of septums , each of the corrugations including a respective one of the baffles and a respective one of the porous septums , wherein a first of the corrugations forms a first channel that extends laterally between and longitudinally along a first of the baffles and a first of the porous septums ; and the stringer body including a plurality of sidewalls arranged longitudinally along the first channel , each of the sidewalls disposed within the first channel and configured to fluidly isolate longitudinally adjacent portions of the first channel from one another; characterised in that the septums are porous septums ; the stringer body further includes a plurality of bridges arranged at an interface between the first of the baffles and the first of the porous septums ; and each of the bridges extends longitudinally between and connects a respective longitudinally adjacent pair of the sidewalls . a porous first skin ; a second skin ; and a core connected between the porous first skin and the second skin , the core including a corrugated body and a stringer body ; the corrugated body including a plurality of corrugations configured from at least a plurality of baffles and a plurality of septums , each of the corrugations including a respective one of the baffles and a respective one of the porous septums , wherein a first of the corrugations forms a first channel that extends laterally between and longitudinally along a first of the baffles and a first of the porous septums ; and the stringer body including a plurality of sidewalls arranged longitudinally along the first channel , each of the sidewalls disposed within the first channel and configured to fluidly isolate longitudinally adjacent portions of the first channel from one another; characterised in that the septums are porous septums ; the stringer body further includes a plurality of bridges arranged at an interface between the first of the baffles and the first of the porous septums ; and each of the bridges extends longitudinally between and connects a respective longitudinally adjacent pair of the sidewalls .
A method for analysing the condition of a machine having a rotating shaft , the method comprising: receiving an analogue electric measurement signal (S EA ) dependent on mechanical vibrations emanating from rotation of said shaft ; sampling said analogue measurement signal at a sampling frequency (f S ) so as to generate a digital measurement data signal (S MD ) in response to said received analogue measurement data; performing a decimation (470; 470A; 470B; S2100, S2110) of the digital measurement data signal (S MD ) so as to achieve a digital signal (S RED ) having a reduced sampling frequency (f SR2 ); wherein said decimation includes the step of controlling (470; 470A; 470B; S2100, S2110) the reduced sampling frequency (f SR2 ) such that the number of sample values per revolution of the shaft is kept at a substantially constant value; characterized by receiving said digital signal (S RED , S RED2 ) at an input of an enhancer ; performing a correlation in said enhancer so as to produce an output signal sequence (O) wherein repetitive signal amplitude components are amplified in relation to stochastic signal components; performing a condition analysis function (F1, F2, Fn) for analysing the condition of the machine dependent on said output signal sequence (O). receiving an analogue electric measurement signal (S EA ) dependent on mechanical vibrations emanating from rotation of said shaft ; sampling said analogue measurement signal at a sampling frequency (f S ) so as to generate a digital measurement data signal (S MD ) in response to said received analogue measurement data; performing a decimation (470; 470A; 470B; S2100, S2110) of the digital measurement data signal (S MD ) so as to achieve a digital signal (S RED ) having a reduced sampling frequency (f SR2 ); wherein said decimation includes the step of controlling (470; 470A; 470B; S2100, S2110) the reduced sampling frequency (f SR2 ) such that the number of sample values per revolution of the shaft is kept at a substantially constant value; characterized by receiving said digital signal (S RED , S RED2 ) at an input of an enhancer ; performing a correlation in said enhancer so as to produce an output signal sequence (O) wherein repetitive signal amplitude components are amplified in relation to stochastic signal components; performing a condition analysis function (F1, F2, Fn) for analysing the condition of the machine dependent on said output signal sequence (O).
An antibody having a binding specificity to PD-L1, comprising (i) the variable light chain sequence of SEQ ID NO: 1; and (ii) the variable heavy chain sequence of SEQ ID NO: 2. (i) the variable light chain sequence of SEQ ID NO: 1; and (ii) the variable heavy chain sequence of SEQ ID NO: 2.
Method for configuring a plurality of networked cameras, said method comprising: connecting a separate client computer to the plurality of networked cameras to set an initial configuration of the plurality of cameras upon installation, sending, by the client computer, a request to the plurality of networked cameras, wherein said request is requesting information relating to enabled storage type of each networked camera, receiving, at the client computer, a response from networked cameras, the response includes information relating to storage type enabled in each responsive networked camera, wherein the information relating to the storage type indicates whether the networked camera is able to store information on a camera located memory card or at a Networked Storage Device, NSD, determining, at the client computer, storage type to use for each networked camera that is enabled to autonomously store images at a storage means, wherein the determining of storage type to use for a networked camera is performed based on the information relating to enabled storage types in that networked camera, and sending, from the client computer, a storage instruction to each camera for which a storage type has been determined, wherein the storage instruction instructs a camera to store captured images on the storage type determined for that networked camera, and disconnecting the client computer from the plurality of networked cameras once the step of sending the storage instruction to each camera has been performed. connecting a separate client computer to the plurality of networked cameras to set an initial configuration of the plurality of cameras upon installation, sending, by the client computer, a request to the plurality of networked cameras, wherein said request is requesting information relating to enabled storage type of each networked camera, receiving, at the client computer, a response from networked cameras, the response includes information relating to storage type enabled in each responsive networked camera, wherein the information relating to the storage type indicates whether the networked camera is able to store information on a camera located memory card or at a Networked Storage Device, NSD, determining, at the client computer, storage type to use for each networked camera that is enabled to autonomously store images at a storage means, wherein the determining of storage type to use for a networked camera is performed based on the information relating to enabled storage types in that networked camera, and sending, from the client computer, a storage instruction to each camera for which a storage type has been determined, wherein the storage instruction instructs a camera to store captured images on the storage type determined for that networked camera, and disconnecting the client computer from the plurality of networked cameras once the step of sending the storage instruction to each camera has been performed.
A processor implemented method for automatic speech recognition in resource constrained devices, the method comprising: receiving , by one or more hardware processors , an audio file as input; transcribing , by the one or more hardware processors , each of a plurality of utterances in the audio file using an acoustic model to generate an Intermediate Greedy Transcript; marking , by the one or more hardware processors , one or more splitting locations in the Intermediate Greedy Transcript, comprising: splitting the Intermediate Greedy Transcript based on a space symbol to generate a plurality of pieces of Intermediate Greedy Transcript; determining acoustically distinct and indistinct words in each of the plurality of pieces of Intermediate Greedy Transcript; and labeling space after the acoustically distinct words with a marker; splicing , by the one or more hardware processors , the audio file at locations where corresponding Intermediate Greedy Transcript has the marker, to get a set of audio segments; associating , by the one or more hardware processors , each audio segment from the set of audio segments with corresponding transcript from the Intermediate Greedy Transcript to get a training dataset; and training , by the one or more hardware processors , a size-constrained neural network model with the training dataset to get a trained model for recognizing short bursts of words. receiving , by one or more hardware processors , an audio file as input; transcribing , by the one or more hardware processors , each of a plurality of utterances in the audio file using an acoustic model to generate an Intermediate Greedy Transcript; marking , by the one or more hardware processors , one or more splitting locations in the Intermediate Greedy Transcript, comprising: splitting the Intermediate Greedy Transcript based on a space symbol to generate a plurality of pieces of Intermediate Greedy Transcript; determining acoustically distinct and indistinct words in each of the plurality of pieces of Intermediate Greedy Transcript; and labeling space after the acoustically distinct words with a marker; splitting the Intermediate Greedy Transcript based on a space symbol to generate a plurality of pieces of Intermediate Greedy Transcript; determining acoustically distinct and indistinct words in each of the plurality of pieces of Intermediate Greedy Transcript; and labeling space after the acoustically distinct words with a marker; splicing , by the one or more hardware processors , the audio file at locations where corresponding Intermediate Greedy Transcript has the marker, to get a set of audio segments; associating , by the one or more hardware processors , each audio segment from the set of audio segments with corresponding transcript from the Intermediate Greedy Transcript to get a training dataset; and training , by the one or more hardware processors , a size-constrained neural network model with the training dataset to get a trained model for recognizing short bursts of words.
A gas turbine engine (100;200;300) comprising a compressor section having a downstream most end and a cooling air tap at a location spaced upstream from said downstream most end , said cooling air tap being passed through at least one boost compressor and at least one heat exchanger , said boost compressor being driven by a driveshaft which is driven by said turbine section, and a boost turbine for selectively driving said boost compressor , characterised in that : a clutch is positioned between said boost turbine and said boost compressor , said clutch being selectively opened or closed to provide said selective drive of said boost compressor by said boost turbine ; and the at least one heat exchanger is configured to pass air to a turbine section to cool said turbine section. a clutch is positioned between said boost turbine and said boost compressor , said clutch being selectively opened or closed to provide said selective drive of said boost compressor by said boost turbine ; and the at least one heat exchanger is configured to pass air to a turbine section to cool said turbine section.
A high-lift device comprising - an airfoil shaped body having a leading edge (LE) and a trailing edge (TE) and extending in a longitudinal direction (A) mainly configured to generate aerodynamic force; - a profile structure arranged to be mounted inside of the airfoil shaped body and extending in longitudinal direction (A) of the airfoil shaped body , wherein the profile structure is approximately as long as the airfoil shaped body wherein the profile structure is configured to provide most of the required mechanical strength and stiffness and the airfoil shaped body is a fairing-like structure to provide for the aerodynamic shape; - wherein the airfoil shaped body is provided with a longitudinally extending opening extending over the whole length of the airfoil shaped body at a side through which the profile structure is accessible inside of the airfoil shaped body , wherein the longitudinally extending opening is at the lower side of the airfoil shaped body , characterized in that device mounting structures for mounting the high-lift device to a further aerodynamic lift device, such as a wing, are provided to the profile structure only. - an airfoil shaped body having a leading edge (LE) and a trailing edge (TE) and extending in a longitudinal direction (A) mainly configured to generate aerodynamic force; - a profile structure arranged to be mounted inside of the airfoil shaped body and extending in longitudinal direction (A) of the airfoil shaped body , wherein the profile structure is approximately as long as the airfoil shaped body wherein the profile structure is configured to provide most of the required mechanical strength and stiffness and the airfoil shaped body is a fairing-like structure to provide for the aerodynamic shape; - wherein the airfoil shaped body is provided with a longitudinally extending opening extending over the whole length of the airfoil shaped body at a side through which the profile structure is accessible inside of the airfoil shaped body , wherein the longitudinally extending opening is at the lower side of the airfoil shaped body , characterized in that device mounting structures for mounting the high-lift device to a further aerodynamic lift device, such as a wing, are provided to the profile structure only.