mhurhangee/patent-ind-claim-en huggingface dataset:
A method of detecting potential malicious attacks in vehicles operational environment using staged machine learning, comprising: training at least one unsupervised machine learning model to detect anomalies known for at least one vehicle using a plurality of unlabeled training feature vectors indicative of operation of the at least one vehicle ; training at least one supervised machine learning model applied to detect anomaly events known for the at least one vehicle using a plurality of labeled training feature vectors indicative of failure patterns identified for the at least one vehicle ; detecting, in real-time, at least one potential cyberattack event in an operational environment of at least one vehicle , by creating a plurality of features vectors each comprising a plurality of features extracted from vehicle operational data generated by a plurality of devices deployed in the at least one vehicle , the vehicle operational data is indicative of operation of the at least one vehicle ; detecting a plurality of anomaly feature vectors using the at least one unsupervised machine learning model applied to the plurality of feature vectors; identifying at least one potential cyberattack event using the at least one supervised machine learning model applied to the plurality of anomaly feature vectors; and generating an alert indicative of the at least one potential cyberattack event. training at least one unsupervised machine learning model to detect anomalies known for at least one vehicle using a plurality of unlabeled training feature vectors indicative of operation of the at least one vehicle ; training at least one supervised machine learning model applied to detect anomaly events known for the at least one vehicle using a plurality of labeled training feature vectors indicative of failure patterns identified for the at least one vehicle ; detecting, in real-time, at least one potential cyberattack event in an operational environment of at least one vehicle , by creating a plurality of features vectors each comprising a plurality of features extracted from vehicle operational data generated by a plurality of devices deployed in the at least one vehicle , the vehicle operational data is indicative of operation of the at least one vehicle ; detecting a plurality of anomaly feature vectors using the at least one unsupervised machine learning model applied to the plurality of feature vectors; identifying at least one potential cyberattack event using the at least one supervised machine learning model applied to the plurality of anomaly feature vectors; and generating an alert indicative of the at least one potential cyberattack event.
An electronic device comprising: a display ; and a processor , the processor is configured to: playback, using the display , display data of content based on a designated field of view "FoV" ; determine whether the display data of the content based on the designated field of view "FoV" , corresponding to a designated frame number is played; and, after playback of the display data corresponding to the designated frame number based on the designated FoV, playback, using the display , display data of the content based on a determined FoV . a display ; and a processor , the processor is configured to: playback, using the display , display data of content based on a designated field of view "FoV" ; determine whether the display data of the content based on the designated field of view "FoV" , corresponding to a designated frame number is played; and, after playback of the display data corresponding to the designated frame number based on the designated FoV, playback, using the display , display data of the content based on a determined FoV . playback, using the display , display data of content based on a designated field of view "FoV" ; determine whether the display data of the content based on the designated field of view "FoV" , corresponding to a designated frame number is played; and, after playback of the display data corresponding to the designated frame number based on the designated FoV, playback, using the display , display data of the content based on a determined FoV .
An airfoil comprising: an airfoil body including a leading edge (LE) and a trailing edge (TE) and a first side wall and a second side wall that is spaced apart from the first side wall , the first side wall and the second side wall joining the leading edge (LE) and the trailing edge (TE) and at least partially defining a cavity in the airfoil body ; a damper member enclosed in the cavity , the damper member being loose within the cavity ; wherein at least one guide member includes a plurality of guide members that are longitudinally spaced apart with respect to a longitudinal axis (L) defined by the airfoil body ; and wherein the damper member includes longitudinally alternating bearing sections and non-bearing sections with respect to a longitudinal axis (L) defined by the airfoil body ; characterised in that the at least one guide member is fixed with regard to the first sidewall and the second sidewall , the at least one guide member including a bearing surface that circumscribes the damper member ; the airfoil body defines a longitudinal axis (L), and the bearing surface is inclined with regard to the longitudinal axis (L); and at least one guide member includes at least one support arm fixed to at least one of the first sidewall or the second sidewall , and a guide piece is supported on the least one support arm , the guide piece including a guide wall that defines an opening through which the damper member extends, the guide wall including the bearing surface . an airfoil body including a leading edge (LE) and a trailing edge (TE) and a first side wall and a second side wall that is spaced apart from the first side wall , the first side wall and the second side wall joining the leading edge (LE) and the trailing edge (TE) and at least partially defining a cavity in the airfoil body ; a damper member enclosed in the cavity , the damper member being loose within the cavity ; wherein at least one guide member includes a plurality of guide members that are longitudinally spaced apart with respect to a longitudinal axis (L) defined by the airfoil body ; and wherein the damper member includes longitudinally alternating bearing sections and non-bearing sections with respect to a longitudinal axis (L) defined by the airfoil body ; characterised in that the at least one guide member is fixed with regard to the first sidewall and the second sidewall , the at least one guide member including a bearing surface that circumscribes the damper member ; the airfoil body defines a longitudinal axis (L), and the bearing surface is inclined with regard to the longitudinal axis (L); and at least one guide member includes at least one support arm fixed to at least one of the first sidewall or the second sidewall , and a guide piece is supported on the least one support arm , the guide piece including a guide wall that defines an opening through which the damper member extends, the guide wall including the bearing surface .
An apparatus for generating a lung condition map, comprising: - an input unit ; and - a processing unit ; wherein the input unit is configured to provide X-ray attenuation information of a patient's chest, and to provide X-ray dark field information of a patient's chest to the processing unit; characterised in that the processing unit is configured to segment the X-ray attenuation information to provide segmented X-ray image data separated from unsegmented areas, wherein the segmented image data comprises a lung mask image corresponding to a lung structure region in the X-ray attenuation information, to provide boneless lung image data by applying a bone suppression algorithm to the lung mask image, to generate a lung depth map by applying a radiation attenuation model to the boneless lung image data, and in that the lung depth map comprises a lung thickness value for each data value of the boneless lung image data, to provide boneless lung image data by applying a bone suppression algorithm to the lung mask image, and to normalize data values of the X-ray dark field information with spatially corresponding data values of the lung depth map, to yield normalized lung dark-field information representing a lung condition map. - an input unit ; and - a processing unit ;
Crystalline 5-(4-cyclopropyl-1H-imidazol-1-yl)-N-(6-(4-isopropyl-4H-1,2,4-triazol-3-yl)pyridin-2-yl)-2-fluoro-4-methylbenzamide (Compound I Form I) characterized by an X-ray powder diffractogram comprising the following peaks: 16.7, 21.3, and 22.8 °20 ± 0.2 °2θ, as determined on a diffractometer using Cu-Kα radiation at a wavelength of 1.5406 Å.
A method for compressing and decompressing an initial program executable by a microprocessor or interpretable by an interpreter of an integrated circuit device, comprising the following steps of: providing an initial program comprising initial instructions comprising an opcode field and an instruction field; reformatting, by a function f, the initial instructions of said initial program, comprising a reorganisation of the bit fields contained in the instructions, to obtain intermediate instructions of an intermediate program in which the useful information contained in the initial instruction fields is grouped in an information field; determining repetition templates of m bits in the intermediate program and comprising m - q bits set to 0 or to 1, and q generic bits, and defining, for each repetition template, a pair formed of said repetition template and an instruction compressed by a function h; replacing intermediate instructions of the intermediate program by the compressed instructions and modifying the links of the program to obtain a compressed program by a function g; replacing the compressed instructions of the compressed program by the intermediate instructions by the function g -1 to obtain the intermediate program; and of reformatting the intermediate instructions by the function f -1 to obtain the initial program. providing an initial program comprising initial instructions comprising an opcode field and an instruction field; reformatting, by a function f, the initial instructions of said initial program, comprising a reorganisation of the bit fields contained in the instructions, to obtain intermediate instructions of an intermediate program in which the useful information contained in the initial instruction fields is grouped in an information field; determining repetition templates of m bits in the intermediate program and comprising m - q bits set to 0 or to 1, and q generic bits, and defining, for each repetition template, a pair formed of said repetition template and an instruction compressed by a function h; replacing intermediate instructions of the intermediate program by the compressed instructions and modifying the links of the program to obtain a compressed program by a function g; replacing the compressed instructions of the compressed program by the intermediate instructions by the function g -1 to obtain the intermediate program; and of reformatting the intermediate instructions by the function f -1 to obtain the initial program.
An electromechanical actuator for actuating a flight control surface of an aircraft , the actuator comprising: a motor ; a first screw configured for translation movement relative to a structure of the aircraft when driven by the motor ; a second screw mounted in series with the first screw , the first screw and the second screw defining a load path between the aircraft structure and the flight control surface ; a fuse element coupling the first screw and the second screw together to permit translation movement of the second screw together with the first screw , the fuse element permitting at least partial disengagement of the second screw from the first screw to permit translation of the second screw relative to the first screw . a motor ; a first screw configured for translation movement relative to a structure of the aircraft when driven by the motor ; a second screw mounted in series with the first screw , the first screw and the second screw defining a load path between the aircraft structure and the flight control surface ; a fuse element coupling the first screw and the second screw together to permit translation movement of the second screw together with the first screw , the fuse element permitting at least partial disengagement of the second screw from the first screw to permit translation of the second screw relative to the first screw .
Storey ceiling construction having a first lower wooden support for supporting a storey ceiling , a first upper wooden support for supporting a further storey ceiling and a first support head made of wood for introducing the forces of the storey ceiling into the first lower wooden support , wherein the first support head lies on the first lower wooden support and the first upper wooden support is supported directly on the first lower wooden support; characterized in that the first support head of wood has a first main fiber direction and a second main fiber direction different from the first main fiber direction, wherein the first main fiber direction and the second main fiber direction are arranged in the plane of the storey ceiling .
A method for affirming a pairing of Bluetooth enabled devices performed by a Bluetooth enabled peripheral computing device , the method comprising: a) advertising availability of the Bluetooth enabled peripheral computing device for pairing; b) receiving a scan request from a Bluetooth enabled central computing device ; c) transmitting a scan response to the Bluetooth enabled central computing device in response to the scan request; d) providing an affirmation value to the Bluetooth enabled central computing device , wherein the affirmation value is embedded within the scan response; e) receiving a connection request from the Bluetooth enabled central computing device ; f) establishing a connection with the Bluetooth enabled central computing device ; g) identifying an affirmation key provided by the Bluetooth enabled central computing device , wherein - the affirmation key is provided within an affirmation key characteristic, and - an affirmation algorithm modulates the affirmation value in a defined manner in order to produce the affirmation key; h) validating that the affirmation key is valid, wherein validating that the affirmation key is valid comprises: - processing the affirmation value with the affirmation algorithm to calculate a reference affirmation key, and - validating that the affirmation key matches the reference affirmation key; and i) pairing with the Bluetooth enabled central computing device . a) advertising availability of the Bluetooth enabled peripheral computing device for pairing; b) receiving a scan request from a Bluetooth enabled central computing device ; c) transmitting a scan response to the Bluetooth enabled central computing device in response to the scan request; d) providing an affirmation value to the Bluetooth enabled central computing device , wherein the affirmation value is embedded within the scan response; e) receiving a connection request from the Bluetooth enabled central computing device ; f) establishing a connection with the Bluetooth enabled central computing device ; g) identifying an affirmation key provided by the Bluetooth enabled central computing device , wherein - the affirmation key is provided within an affirmation key characteristic, and - an affirmation algorithm modulates the affirmation value in a defined manner in order to produce the affirmation key; - the affirmation key is provided within an affirmation key characteristic, and - an affirmation algorithm modulates the affirmation value in a defined manner in order to produce the affirmation key; h) validating that the affirmation key is valid, wherein validating that the affirmation key is valid comprises: - processing the affirmation value with the affirmation algorithm to calculate a reference affirmation key, and - validating that the affirmation key matches the reference affirmation key; and - processing the affirmation value with the affirmation algorithm to calculate a reference affirmation key, and - validating that the affirmation key matches the reference affirmation key; and i) pairing with the Bluetooth enabled central computing device .
A method of deriving reciprocating device component health comprising: utilizing a controller for: obtaining one or more frequencies, wherein each of the one or more frequencies corresponds to a fundamental frequency of a reciprocating device component; receiving a signal from a knock sensor coupled to the reciprocating device ; deriving total harmonic distortion (THD) from the signal at the one or more frequencies; and determining whether the derived THD exceeds a threshold value; providing a user perceptible indication of the THD exceeding the threshold value indicative of the component approaching failure. obtaining one or more frequencies, wherein each of the one or more frequencies corresponds to a fundamental frequency of a reciprocating device component; receiving a signal from a knock sensor coupled to the reciprocating device ; deriving total harmonic distortion (THD) from the signal at the one or more frequencies; and determining whether the derived THD exceeds a threshold value; providing a user perceptible indication of the THD exceeding the threshold value indicative of the component approaching failure.
A heat source unit for a refrigeration apparatus, the heat source unit comprising: a compressor ; a heat exchanger which allows a refrigerant to exchange heat with air; a fan ; an electric component box for housing an electric component; and a casing for housing the compressor , the heat exchanger , the fan , and the electric component box , wherein a lower portion of the casing is a closed space separated from an outside, and constitutes a machine chamber (31A to 31D) in which the compressor and the electric component box are housed, an upper portion of the casing is provided with the heat exchanger and the fan , and constitutes an air passage (32A to 32D) through which air flows, the heat source unit includes a drain pan disposed under the heat exchanger and receives condensed water generated in the heat exchanger , and a drain gutter which is disposed under an outflow port that is open in a bottom plate of the drain pan , and which receives water that has passed through the outflow port , the drain gutter has a depth which gradually increases from one end to the other end of the drain gutter , a main drain port is formed at an end portion of the drain gutter where the depth of the drain gutter is deepest, and the main drain port is intended to drain water in the drain gutter to an outside of the machine chamber (31A to 31D), characterized in that the heat source unit furthermore comprising: a secondary drain port is formed at an end portion of the drain gutter where the depth of the drain gutter is shallowest, the secondary drain port being intended to drain water in the drain gutter to the outside of the machine chamber (31A to 31D). a lower portion of the casing is a closed space separated from an outside, and constitutes a machine chamber (31A to 31D) in which the compressor and the electric component box are housed, an upper portion of the casing is provided with the heat exchanger and the fan , and constitutes an air passage (32A to 32D) through which air flows, the heat source unit includes a drain pan disposed under the heat exchanger and receives condensed water generated in the heat exchanger , and a drain gutter which is disposed under an outflow port that is open in a bottom plate of the drain pan , and which receives water that has passed through the outflow port , a drain pan disposed under the heat exchanger and receives condensed water generated in the heat exchanger , and a drain gutter which is disposed under an outflow port that is open in a bottom plate of the drain pan , and which receives water that has passed through the outflow port , the drain gutter has a depth which gradually increases from one end to the other end of the drain gutter , a main drain port is formed at an end portion of the drain gutter where the depth of the drain gutter is deepest, and the main drain port is intended to drain water in the drain gutter to an outside of the machine chamber (31A to 31D),
A searchable code processing system in which a registration client , a search client and a management server are connected via a network , wherein the registration client is provided with units that create secure data acquired by encrypting unciphered data for registration; the management server is provided with a storage that stores secure data including a first search tag used for a search; and the registration client further determines the length of the first search tag for the secure data according to tag length stored in a data storage and is provided with units that create the first search tag having a different length from the tag length stored in the data storage for the secure data; wherein the search client creates a secure keyword, by dividing an unciphered text keyword for a search in n divided pieces, encrypting the n divided pieces as n intermediate encrypted keywords, wherein each intermediate encrypted keyword is created utilizing the previously created intermediate encrypted keyword, acquiring a main body of an encrypted keyword utilizing the nth intermediate encrypted keyword, creating an initial vector and a second search tag, and connecting the initial vector, the main body of the encrypted keyword and the second search tag as the secure keyword, and transmits it to the management server via the network ; and the management server receives the secure keyword via the network and searches the secure data and the secure keyword.