mhurhangee/ep-ind-claims huggingface dataset:
A braking system for an aircraft operable to apply one or more aircraft wheel brakes according to at least one of a plurality of wheel brake control functions, the braking system comprising: an aircraft speed indicator; a brake condition indicator comprising a brake temperature characteristic indicator; and characterised by a controller configured to: control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; select a second wheel brake control function from the plurality of wheel brake control functions based on a brake temperature characteristic of the one or more aircraft wheel breaks, wherein a thermal oxidation limiting function is selected as the second wheel brake control function if the brake temperature characteristic of at least one aircraft wheel brake meets a thermal oxidation limiting criterion; and control the wheel braking operation of the aircraft according to at least the second wheel brake control function if the aircraft speed does not exceed the speed threshold. an aircraft speed indicator; a brake condition indicator comprising a brake temperature characteristic indicator; and characterised by a controller configured to: control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; select a second wheel brake control function from the plurality of wheel brake control functions based on a brake temperature characteristic of the one or more aircraft wheel breaks, wherein a thermal oxidation limiting function is selected as the second wheel brake control function if the brake temperature characteristic of at least one aircraft wheel brake meets a thermal oxidation limiting criterion; and control the wheel braking operation of the aircraft according to at least the second wheel brake control function if the aircraft speed does not exceed the speed threshold. control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; select a second wheel brake control function from the plurality of wheel brake control functions based on a brake temperature characteristic of the one or more aircraft wheel breaks, wherein a thermal oxidation limiting function is selected as the second wheel brake control function if the brake temperature characteristic of at least one aircraft wheel brake meets a thermal oxidation limiting criterion; and control the wheel braking operation of the aircraft according to at least the second wheel brake control function if the aircraft speed does not exceed the speed threshold.
Battery sealing plug with an external thread for installation, notably to screw into the opening in the battery cover, in which the sealing plug has at least one gas-tight seal on the outside, characterised by the seal being made of a blend of polypropylene or polyethylene and polyisobutene.
Load hooking device for a lifting apparatus, including a return system, a housing and a load hook mounted so as to pivot relative to the housing, the return system including an elastic means mounted between a rod secured to said housing and a crank pin fixed to said load hook, said return system being capable of exerting a return force on the load hook in order to allow said load hook to be closed, characterised in that said return system includes a device (12, 13) for adjusting the return force of the elastic means.
A method of manufacturing a blade rubber including: a head portion formed in a cross-sectional rectangular shape; a lip portion contacting a surface of a windshield of a vehicle; and a neck portion connecting the head portion with the lip portion, the method comprising the steps of: a) molding the blade rubber with using an ethylene-propylene-diene terpolymer rubber (EPDM) wherein a content of ethylene contained in the polymer of EPDM is 62 mol% or less; b) adhering monomers on at least the lip portion in the molded blade rubber; c) performing an irradiation treatment to a portion where the monomers are adhered to generate radical active sites on the EPDM of a surface of the portion; and d) binding the monomers by graft polymerization at the generated radical active sites. a) molding the blade rubber with using an ethylene-propylene-diene terpolymer rubber (EPDM) wherein a content of ethylene contained in the polymer of EPDM is 62 mol% or less; b) adhering monomers on at least the lip portion in the molded blade rubber; c) performing an irradiation treatment to a portion where the monomers are adhered to generate radical active sites on the EPDM of a surface of the portion; and d) binding the monomers by graft polymerization at the generated radical active sites.
Wind turbine auxiliary drive system comprising a motor, a drive pinion and a bearing, the bearing comprising an outer bearing ring, an inner bearing ring and, between these two bearing rings, one or more rows of rolling elements (23a; 23b) which allow both bearing rings to rotate relative to each other, the inner bearing ring having an inner side comprising a gear which meshes with the drive pinion, wherein a height (h) of the gear in an axial direction is smaller than the height of the inner bearing ring such that a gearless portion is defined characterized in that it comprises a lubrication system wherein at least one lubricant inlet and/or at least one lubricant outlet is arranged on the gearless portion, and wherein a supporting arrangement for supporting lubrication components is provided inside the inner bearing ring of the bearing in such a way that it traverses a bearing rotational axis.
RTD assembly, with at least one substrate, and with at least one resistance element, which is arranged on the substrate, wherein the substrate is essentially made from a material whose thermal expansion coefficient is greater than 10.5 ppm/K, and wherein at least one electrically isolating separation layer is provided, said layer being arranged between the resistance element and the substrate, characterized in that at least one inner compensation layer is provided on the side of the substrate facing away from the resistance element, said layer being designed in an essentially identical manner to the separation layer in terms of a change in the expansion caused by the temperature.
A method of operating a wireless communication device (500, 1000), comprising: searching for a cell during an initial cell search period; receiving signaling from a radio network node of an identified cell; detecting a transmitter switch-off period of the radio network node based on the received signaling; adapting the initial cell search period of the wireless communication device based on the radio network node transmitter switch-off period; detecting an operating state of a radio network node based on one of: a state indicator broadcast by the radio network node, a state indicator broadcast by a neighbor cell of the radio network node, information received in a master information block, MIB, or synchronization signal patterns; and in response to detecting that the operating state is a restricted operating state during which the radio network node is switched on and off for certain periods of time, transmitting information to the radio network node during the adapted initial cell search period to initiate a transition of the radio network node from the restricted operating state to a normal operating state. searching for a cell during an initial cell search period; receiving signaling from a radio network node of an identified cell; detecting a transmitter switch-off period of the radio network node based on the received signaling; adapting the initial cell search period of the wireless communication device based on the radio network node transmitter switch-off period; detecting an operating state of a radio network node based on one of: a state indicator broadcast by the radio network node, a state indicator broadcast by a neighbor cell of the radio network node, information received in a master information block, MIB, or synchronization signal patterns; and a state indicator broadcast by the radio network node, a state indicator broadcast by a neighbor cell of the radio network node, information received in a master information block, MIB, or synchronization signal patterns; and in response to detecting that the operating state is a restricted operating state during which the radio network node is switched on and off for certain periods of time, transmitting information to the radio network node during the adapted initial cell search period to initiate a transition of the radio network node from the restricted operating state to a normal operating state.
A cooking device for commercial use, especially a combi-steamer or a baking oven, with a digital optical identification means for food to be cooked within the cooking device, wherein the optical identification means comprises a picture taking means for capturing a picture of the food, especially an electronic image sensor, and wherein the optical identification means comprises a controller having access to picture data captured of the food, characterized in that the controller is programmed to check upon identification of the food to be cooled whether already running cooking chamber conditions are suitable for cooking that food, and to show a warning.
A centrifugal fluid processing system comprising: a centrifuge assembly including upper and lower umbilicus mounts and a bearing support; and a fluid set comprising an umbilicus (24a, 24b) including a first anchor portion (60a, 60b) removably received by the lower umbilicus mount; a second anchor portion (64a, 64b) removably received by the upper umbilicus mount; at least one elongated, flexible fluid-transmitting portion supported by the bearing support for orbiting around an axis of centrifugation, comprised of at least a first material and defining a lumen (84, 98) extending between the first and second anchor portions (60a, 60b, 64a, 64b) for transmitting a fluid between the first and second anchor portions (60a, 60b, 64a, 64b); and at least one flexible, non-fluid-transmitting shaft (86, 88) comprised of at least a second material different than the first material and extending between the first and second anchor portions (60a, 60b, 64a, 64b). a centrifuge assembly including upper and lower umbilicus mounts and a bearing support; and a fluid set comprising an umbilicus (24a, 24b) including
A method for header compression of an Ethernet frame, comprising: determining, by a first device, according to configuration information, that header compression needs to be performed on the Ethernet frame; determining, by the first device, a header compression object in the Ethernet frame according to specific information, wherein the specific information is pre-defined information or indication information; and performing, by the first device, header compression on the header compression object, characterized in that the header compression object comprises tag protocol identifier, TP-ID, and/or canonical format indicator/drop eligible indicator, CFI/DEI, in a virtual local area network, VLAN, subheader of the Ethernet frame. determining, by a first device, according to configuration information, that header compression needs to be performed on the Ethernet frame; determining, by the first device, a header compression object in the Ethernet frame according to specific information, wherein the specific information is pre-defined information or indication information; and performing, by the first device, header compression on the header compression object, characterized in that the header compression object comprises tag protocol identifier, TP-ID, and/or canonical format indicator/drop eligible indicator, CFI/DEI, in a virtual local area network, VLAN, subheader of the Ethernet frame.
A method for face image recognition, comprising: generating one or more face region pairs of face images to be compared and recognized; forming a plurality of feature modes by exchanging the two face regions of each face region pair and horizontally flipping each face region of each face region pair; receiving, by one or more convolutional neural networks, the plurality of feature modes, each of which forms a plurality of input maps; extracting, by the one or more convolutional neural networks, one or more identity relational features from the input maps to form a plurality of output maps which reflect identity relations of the compared face images; and recognizing whether the face images belong to the same identity based on the identity relational features of the face images, wherein the step of generating further comprises: detecting a plurality of facial feature points of the face images to be recognized; aligning the face images to be recognized according to the detected facial feature points; and selecting one or more regions on the same position of the aligned face images to generate one or more face region pairs, respectively. generating one or more face region pairs of face images to be compared and recognized; forming a plurality of feature modes by exchanging the two face regions of each face region pair and horizontally flipping each face region of each face region pair; receiving, by one or more convolutional neural networks, the plurality of feature modes, each of which forms a plurality of input maps; extracting, by the one or more convolutional neural networks, one or more identity relational features from the input maps to form a plurality of output maps which reflect identity relations of the compared face images; and recognizing whether the face images belong to the same identity based on the identity relational features of the face images, wherein the step of generating further comprises: detecting a plurality of facial feature points of the face images to be recognized; aligning the face images to be recognized according to the detected facial feature points; and selecting one or more regions on the same position of the aligned face images to generate one or more face region pairs, respectively. detecting a plurality of facial feature points of the face images to be recognized; aligning the face images to be recognized according to the detected facial feature points; and selecting one or more regions on the same position of the aligned face images to generate one or more face region pairs, respectively.
An aircraft comprising: a fuselage having first and second rotor stations; a first rotor assembly positioned proximate the first rotor station, the first rotor assembly including a first rotor hub and first rotor blades (40a, 40b, 40c) having support arms (42a, 42b) pivotably coupled to the first rotor hub; a second rotor assembly positioned proximate the second rotor station, the second rotor assembly including a second rotor hub and second rotor blades (60a, 60b, 60c) pivotably coupled to the second rotor hub; and a cam positioned between the first and second rotor stations and coupled to the second rotor blades (60a, 60b, 60c); wherein, the first rotor blades (40a, 40b, 40c) and the second rotor blades (60a, 60b, 60c) have deployed configurations extending generally radially from the fuselage and stowed configurations extending generally parallel with the fuselage; wherein, the cam has a first orientation when the second rotor blades (60a, 60b, 60c) are in the stowed configuration; and wherein, the cam has a second orientation when the second rotor blades (60a, 60b, 60c) are in the deployed configuration in which the cam props the support arms (42a, 42b) of the first rotor blades (40a, 40b, 40c) preventing transition of the first rotor blades (40a, 40b, 40c) from the deployed configuration to the stowed configuration. a fuselage having first and second rotor stations; a first rotor assembly positioned proximate the first rotor station, the first rotor assembly including a first rotor hub and first rotor blades (40a, 40b, 40c) having support arms (42a, 42b) pivotably coupled to the first rotor hub; a second rotor assembly positioned proximate the second rotor station, the second rotor assembly including a second rotor hub and second rotor blades (60a, 60b, 60c) pivotably coupled to the second rotor hub; and a cam positioned between the first and second rotor stations and coupled to the second rotor blades (60a, 60b, 60c); wherein, the first rotor blades (40a, 40b, 40c) and the second rotor blades (60a, 60b, 60c) have deployed configurations extending generally radially from the fuselage and stowed configurations extending generally parallel with the fuselage; wherein, the cam has a first orientation when the second rotor blades (60a, 60b, 60c) are in the stowed configuration; and wherein, the cam has a second orientation when the second rotor blades (60a, 60b, 60c) are in the deployed configuration in which the cam props the support arms (42a, 42b) of the first rotor blades (40a, 40b, 40c) preventing transition of the first rotor blades (40a, 40b, 40c) from the deployed configuration to the stowed configuration.
A process for producing a conformal electroluminescent system, comprising the steps of: selecting a substrate; applying a base backplane film layer upon the substrate using an aqueous-based, electrically conductive backplane material; applying a dielectric film layer upon the backplane film layer using an aqueous-based dielectric material; applying a phosphor film layer upon the dielectric film layer using an aqueous-based phosphor material, the phosphor film layer being excited by an ultraviolet radiation source during application, the ultraviolet radiation source providing visual cues while the phosphor film layer is being applied, the application of the phosphor film layer being adjusted in response to the visual cues during the phosphor application step to apply a generally uniform distribution of the phosphor material upon the dielectric film layer; and applying an electrode film layer upon the phosphor film layer using an aqueous-based, substantially transparent, electrically conductive electrode material, the backplane film layer, dielectric film layer, phosphor film layer, and electrode film layer each being applied by spray conformal coating, wherein the phosphor film layer is excitable by an electrical field established across the phosphor film layer upon application of an electrical charge between the backplane film layer and the electrode film layer such that the phosphor film layer emits electroluminescent light. selecting a substrate; applying a base backplane film layer upon the substrate using an aqueous-based, electrically conductive backplane material; applying a dielectric film layer upon the backplane film layer using an aqueous-based dielectric material; applying a phosphor film layer upon the dielectric film layer using an aqueous-based phosphor material, the phosphor film layer being excited by an ultraviolet radiation source during application, the ultraviolet radiation source providing visual cues while the phosphor film layer is being applied, the application of the phosphor film layer being adjusted in response to the visual cues during the phosphor application step to apply a generally uniform distribution of the phosphor material upon the dielectric film layer; and applying an electrode film layer upon the phosphor film layer using an aqueous-based, substantially transparent, electrically conductive electrode material, the backplane film layer, dielectric film layer, phosphor film layer, and electrode film layer each being applied by spray conformal coating, wherein the phosphor film layer is excitable by an electrical field established across the phosphor film layer upon application of an electrical charge between the backplane film layer and the electrode film layer such that the phosphor film layer emits electroluminescent light.
A method for producing a rodent comprising inserting into a rodent ES cell genome a plurality of human light chain kappa V regions, and one or more human Ig kappa J regions upstream of the host rodent kappa constant region; the method comprising inserting the human kappa DNA between the rodent constant region and the last, 3', rodent J region; wherein the inserting is carried out in a stepwise manner; wherein the insertion is such that the rodent is able to produce a repertoire of chimaeric kappa chains having a rodent constant region and a human variable region. the method comprising inserting the human kappa DNA between the rodent constant region and the last, 3', rodent J region; wherein the inserting is carried out in a stepwise manner; wherein the insertion is such that the rodent is able to produce a repertoire of chimaeric kappa chains having a rodent constant region and a human variable region.
A composition comprising 3-[(4-biphenylyloxy)methyl]piperidine or a pharmaceutically acceptable salt thereof for use in improving the therapeutic effect of an anti-cancer agent or radiation therapy by increasing sensitivity of cancer cells to the anti-cancer agent or radiation therapy when the composition is used in combination with the anti-cancer agent or radiation therapy.