mhurhangee/patent-ind-claim-en huggingface dataset:
A welding equipment in which in use a plurality of annular bodies having openings at both ends in an axial direction are placed one after another in the axial direction and that forms an annular joined body by joining the corresponding openings with each other by laser welding, the welding equipment comprising: a vacuum compartment in which a vacuum atmosphere can be established; a holding member that is installed in the vacuum compartment and that in use holds the annular joined body in which a welding groove is formed by placing the openings of the plurality of the annular bodies next to each other, characterized by comprising; a window member that is installed in a wall of the vacuum compartment , which is adapted to intersect with an axial center of the annular joined body , and that forms a portion of the wall; a laser radiating member that is installed outside the vacuum compartment and that is adapted to irradiate a laser beam into an internal space of the annular joined body through the window member ; and a mirror member that is installed separately from the laser radiating member and inside the vacuum compartment so as to be positioned in use in the internal space of the annular joined body wherein the mirror member is adapted to reflect the laser beam radiated from the laser radiating member and passing through the window member , so that the laser beam is turned into a reflected laser beam , and to adjust the reflected laser beam to be oriented in a direction perpendicular to the welding groove. a vacuum compartment in which a vacuum atmosphere can be established; a holding member that is installed in the vacuum compartment and that in use holds the annular joined body in which a welding groove is formed by placing the openings of the plurality of the annular bodies next to each other, characterized by comprising; a window member that is installed in a wall of the vacuum compartment , which is adapted to intersect with an axial center of the annular joined body , and that forms a portion of the wall; a laser radiating member that is installed outside the vacuum compartment and that is adapted to irradiate a laser beam into an internal space of the annular joined body through the window member ; and a mirror member that is installed separately from the laser radiating member and inside the vacuum compartment so as to be positioned in use in the internal space of the annular joined body wherein the mirror member is adapted to reflect the laser beam radiated from the laser radiating member and passing through the window member , so that the laser beam is turned into a reflected laser beam , and to adjust the reflected laser beam to be oriented in a direction perpendicular to the welding groove.
A hair treatment product having a plurality of components (2, 4-9), comprising a first container for holding at least one first preparation component and at least one second container for holding at least one second preparation component , in order to produce a preparation mixture for use from the preparation components , having an outer packaging which contains all components (2, 4-9) of the hair treatment product , and having an insert which accommodates the components (4-9) of the hair treatment product at least in part, characterized in that one of the containers is designed as a closable mixing bowl which is tightly closed by a detachable closure element until use and is integrally formed on the insert .
A wheel bearing sealing arrangement for a vehicle , comprising: - an outboard bearing having an outboard periphery intended to face away from a central longitudinal axis of the vehicle and an inboard periphery intended to face towards the central longitudinal axis of the vehicle, wherein the outboard bearing comprises a first race-forming part and a second race-forming part which surrounds the first race-forming part, - an outboard seal arranged between the first race-forming part and an opposite part , and - a safety washer pressed against the outboard periphery of the first race-forming part, wherein the outboard seal comprises a sealing part pressed against and in direct contact with the safety washer, wherein the outboard seal comprises a supporting part which supports the sealing part , wherein the sealing part comprises a lip projecting away from the supporting part , wherein the lip is in sealing contact with the safety washer , wherein the wheel bearing sealing arrangement has a geometrical centre axis, characterized in that said lip extends radially away from the geometrical centre axis. - an outboard bearing having an outboard periphery intended to face away from a central longitudinal axis of the vehicle and an inboard periphery intended to face towards the central longitudinal axis of the vehicle, wherein the outboard bearing comprises a first race-forming part and a second race-forming part which surrounds the first race-forming part, - an outboard seal arranged between the first race-forming part and an opposite part , and - a safety washer pressed against the outboard periphery of the first race-forming part, wherein the outboard seal comprises a sealing part pressed against and in direct contact with the safety washer, wherein the outboard seal comprises a supporting part which supports the sealing part , wherein the sealing part comprises a lip projecting away from the supporting part , wherein the lip is in sealing contact with the safety washer , wherein the wheel bearing sealing arrangement has a geometrical centre axis, characterized in that said lip extends radially away from the geometrical centre axis.
A propulsion unit for an aircraft, comprising: - a nacelle , - a turbojet engine , - an annular flow path for circulating a secondary air flow, defined between an outer structure of the nacelle and an inner fixed structure of the nacelle , and - a precooler device , communicating with a motor enclosure defined by the annular space comprised between the inner fixed structure of the nacelle and a motor casing surrounding a combustion chamber of the turbojet engine , said precooler device comprising a scoop opening into said annular flow path and a valve for the intake of an air flow from said annular flow path , said propulsion unit being characterized in that it comprises a compressed air supply circuit , arranged in the propulsion unit and designed to inject a flow of compressed air into said scoop of the precooler device . - a nacelle , - a turbojet engine , - an annular flow path for circulating a secondary air flow, defined between an outer structure of the nacelle and an inner fixed structure of the nacelle , and - a precooler device , communicating with a motor enclosure defined by the annular space comprised between the inner fixed structure of the nacelle and a motor casing surrounding a combustion chamber of the turbojet engine , said precooler device comprising a scoop opening into said annular flow path and a valve for the intake of an air flow from said annular flow path ,
A method for degrading a phenolic resin-containing material, characterised in that the phenolic resin-containing material is subjected to aminolysis with a reagent containing at least one amino group.
Heat exchanger for the exchange of heat between a first and a second fluid, notably for supplying air to a motor vehicle combustion engine, comprising at least one heat exchange core bundle comprising fluid circulation plates stacked on one another, said core bundle having the first fluid passing through it, and a casing in which said heat exchange core bundle is housed so that the second fluid can pass through it, said casing being closed along one of its faces by a plate referred to as the frontal flange , to which said heat exchange core bundle is fixed in a fluidtight fashion, said core bundle having a large face secured to said frontal flange , and an opposite large face and lateral faces connecting said large faces, said heat exchanger comprising at least one seal placed between said heat exchange core bundle and said casing so as to limit the extent to which the second fluid can bypass the core bundle , characterized in that said seal extends along said large face opposite to the one secured to the frontal flange and along said lateral faces .
A method for graphics processing, comprising: receiving, by at least one processor, a source pixel value to be written to a pixel location in a render target, wherein the source pixel value is associated with a source node in a hierarchical structure having a plurality of nodes associated with a plurality of node indices, and wherein the source node is associated with a source node index made up of a first set of bits; receiving, by the at least one processor, a destination pixel value of the pixel location in the render target, wherein the destination pixel value is associated with a destination node in the hierarchical structure, and wherein the destination node is associated with a destination node index made up of a second set of bits; determining, by the at least one processor, a lowest common ancestor node of the source node and the destination node in the hierarchical structure, including determining a resulting node index associated with the lowest common ancestor node based at least in part on a common set of bits between the first set of bits and the second set of bits; and outputting, by the at least one processor, a resulting pixel value associated with the lowest common ancestor node of the source node and the destination node to the pixel location in the render target. receiving, by at least one processor, a source pixel value to be written to a pixel location in a render target, wherein the source pixel value is associated with a source node in a hierarchical structure having a plurality of nodes associated with a plurality of node indices, and wherein the source node is associated with a source node index made up of a first set of bits; receiving, by the at least one processor, a destination pixel value of the pixel location in the render target, wherein the destination pixel value is associated with a destination node in the hierarchical structure, and wherein the destination node is associated with a destination node index made up of a second set of bits; determining, by the at least one processor, a lowest common ancestor node of the source node and the destination node in the hierarchical structure, including determining a resulting node index associated with the lowest common ancestor node based at least in part on a common set of bits between the first set of bits and the second set of bits; and outputting, by the at least one processor, a resulting pixel value associated with the lowest common ancestor node of the source node and the destination node to the pixel location in the render target.
An unlocking mechanism for an actuator comprising: a base ; an unlocking element mounted to said base for rotation around an axis (A) between a first, locking position and a second, unlocking position; and an unlocking actuator for rotating said unlocking element between said first and second positions; said unlocking element has an axially facing end surface for engagement, in the first position, with an operating element , and further comprising a slot extending axially thereinto from said end surface for receiving the operating element in the second position for permitting an unlocking movement of the operating element along the slot ; and characterised in that the unlocking element comprise an annular wall portion , with the slot being formed in the annular wall portion . a base ; an unlocking element mounted to said base for rotation around an axis (A) between a first, locking position and a second, unlocking position; and an unlocking actuator for rotating said unlocking element between said first and second positions; said unlocking element has an axially facing end surface for engagement, in the first position, with an operating element , and further comprising a slot extending axially thereinto from said end surface for receiving the operating element in the second position for permitting an unlocking movement of the operating element along the slot ; and characterised in that
A pump, comprising: a piston chamber ; a port ; a piston disposed within the piston chamber and adapted to draw fluid into the piston chamber through the port as the piston moves away from the port; a valve operatively coupled to the port and configured to block the fluid from exiting the piston chamber through the port (208. 308) as the piston moves toward the port ; and characterized by a filter configured to separate gas from liquid in the fluid as the piston moves toward the filter , while retaining the liquid in the piston chamber . a piston chamber ; a port ; a piston disposed within the piston chamber and adapted to draw fluid into the piston chamber through the port as the piston moves away from the port; a valve operatively coupled to the port and configured to block the fluid from exiting the piston chamber through the port (208. 308) as the piston moves toward the port ; and characterized by a filter configured to separate gas from liquid in the fluid as the piston moves toward the filter , while retaining the liquid in the piston chamber .
A fuel pump system for a turbomachine engine, comprising: a boost pump driven by an electric motor and configured to be in fluid communication with a fuel tank ; a primary pump configured to be driven by a shaft connected to the turbomachine engine, wherein the primary pump is in fluid communication with the boost pump downstream of the boost pump by a boost branch ; a bypass flow branch that connects the boost branch to a downstream branch that is downstream of the primary pump , wherein the downstream branch is in fluid communication with one or more metering valves and/or one or more fuel nozzles; and a bypass valve disposed in the bypass flow branch and/or the downstream branch and configured to selectively directly fluidly communicate the boost branch and the downstream branch ; wherein the electric motor is controlled by a controller , characterized in that the controller is in cooling flow communication with the bypass branch , and wherein the electric motor is in cooling flow communication with both the controller and the boost pump to create loop through the boost pump . a boost pump driven by an electric motor and configured to be in fluid communication with a fuel tank ; a primary pump configured to be driven by a shaft connected to the turbomachine engine, wherein the primary pump is in fluid communication with the boost pump downstream of the boost pump by a boost branch ; a bypass flow branch that connects the boost branch to a downstream branch that is downstream of the primary pump , wherein the downstream branch is in fluid communication with one or more metering valves and/or one or more fuel nozzles; and a bypass valve disposed in the bypass flow branch and/or the downstream branch and configured to selectively directly fluidly communicate the boost branch and the downstream branch ; wherein the electric motor is controlled by a controller , characterized in that the controller is in cooling flow communication with the bypass branch , and wherein the electric motor is in cooling flow communication with both the controller and the boost pump to create loop through the boost pump .
Electronic component comprising a functional body provided with a reflection structure , wherein the reflection structure is arranged and designed to reflect radiation that impinges on the electronic component from outside away from the functional body , wherein the electronic component is radiation-passive, wherein the electronic component comprises a protective layer , which is arranged on the reflection structure , wherein the protective layer comprises a pigment , and wherein the pigment is designed to adapt the colour of the electronic component to that of surroundings of the electronic component , and wherein the electronic component comprises a barrier layer , which is arranged between the functional body and the reflection structure .
Engine mount for ventilators , having a ventilation grill with radially running struts , which connect grill rings lying coaxially relative to each other, and are fastened to an inner ring with their radially inner end , and to an outer supporting ring with their radially outer end , wherein, in order to adjust the engine mount to the oscillating behavior of the ventilator , the number and/or diameter of the struts is varied with regard to acoustic noise reduction and/or self-resonances of the engine mount, characterized in that the inner ring is an inner supporting ring , which has a planar ring portion that lies in a radial plane of the ventilation grill , and whose edge is upwardly inclined and has fastened to it the radially inner ends of the struts , and that an interface is provided at the ring portion of the inner supporting ring in the form of openings distributed over the periphery for attachment to the ventilator .
A network node for deployment in an access network, the node having a substantially cylindrical shape and comprising: a first end configured to receive an input metallic cable ; a second end configured to receive an output metallic cable ; a port configured to receive an optical fibre cable , the port being located intermediate the first and the second end of the node; a power circuit configured, in use, to receive an electrical power supply from the output metallic cable; a digital subscriber line transceiver configured, in use, to receive optical data signals from the optical fibre cable and to transmit electrical data signals on the output metallic cable; and a heat sink which comprises a heat pipe which extends along the length of the node. a first end configured to receive an input metallic cable ; a second end configured to receive an output metallic cable ; a port configured to receive an optical fibre cable , the port being located intermediate the first and the second end of the node; a power circuit configured, in use, to receive an electrical power supply from the output metallic cable; a digital subscriber line transceiver configured, in use, to receive optical data signals from the optical fibre cable and to transmit electrical data signals on the output metallic cable; and a heat sink which comprises a heat pipe which extends along the length of the node.
A cooling system for a drive train of an electric transport vehicle , the drive train comprising a power supply module for at least one electric motor, an electrical transformer and a braking rheostat , the cooling system comprising: - a first cooling device configured to at least partially remove heat dissipated by the power supply module , - a second cooling device configured to at least partially remove heat dissipated by the electrical transformer , - a third cooling device configured to at least partially remove heat dissipated by the braking rheostat , - the first , second and third cooling devices being disposed within a single air flow duct , the cooling system comprising said air flow duct and at least one fan configured to generate an air flow in said air flow duct . - a first cooling device configured to at least partially remove heat dissipated by the power supply module , - a second cooling device configured to at least partially remove heat dissipated by the electrical transformer , - a third cooling device configured to at least partially remove heat dissipated by the braking rheostat , - the first , second and third cooling devices being disposed within a single air flow duct , the cooling system comprising said air flow duct and at least one fan configured to generate an air flow in said air flow duct .
A data check method, the method characterized by : obtaining a first counter value and a second counter value, wherein the first counter value is a value obtained by performing counting by user equipment, UE, during data transmission between the UE and a user plane function, UPF, entity, and the second counter value is a value obtained by performing counting by the UPF entity during the data transmission between the UE and the UPF entity; determining whether the first counter value matches the second counter value; and if the first counter value does not match the second counter value, sending a response message to a session management network element. obtaining a first counter value and a second counter value, wherein the first counter value is a value obtained by performing counting by user equipment, UE, during data transmission between the UE and a user plane function, UPF, entity, and the second counter value is a value obtained by performing counting by the UPF entity during the data transmission between the UE and the UPF entity; determining whether the first counter value matches the second counter value; and if the first counter value does not match the second counter value, sending a response message to a session management network element.
A method for coordinating Wireless Avionics Intra-Communications (WAIC) communications with a radio altimeter signal, the method comprising: monitoring a frequency band, wherein the frequency band is an adjustable range between 4200 MHz and 4400 MHz; recording a sequence of time stamps, each time stamp of the sequence of time stamps corresponding to a time at which a strength of the radio altimeter signal exceeds a threshold signal strength in the frequency band; calculating time stamp intervals between successive time stamps in the sequence of time stamps to produce a sequence of time stamp intervals; identifying a pattern of time stamp intervals in the sequence of time stamp intervals; and coordinating the WAIC communications with the pattern of time stamp intervals to avoid interference with the radio altimeter signal; and characterized in that coordinating the WAIC communications with the pattern of time stamp intervals to avoid the interference with the altimeter signal further comprises one or more of: adjusting a packet size of the WAIC communications; and adjusting packet transmission timing of the WAIC communications. monitoring a frequency band, wherein the frequency band is an adjustable range between 4200 MHz and 4400 MHz; recording a sequence of time stamps, each time stamp of the sequence of time stamps corresponding to a time at which a strength of the radio altimeter signal exceeds a threshold signal strength in the frequency band; calculating time stamp intervals between successive time stamps in the sequence of time stamps to produce a sequence of time stamp intervals; identifying a pattern of time stamp intervals in the sequence of time stamp intervals; and coordinating the WAIC communications with the pattern of time stamp intervals to avoid interference with the radio altimeter signal; and characterized in that coordinating the WAIC communications with the pattern of time stamp intervals to avoid the interference with the altimeter signal further comprises one or more of: adjusting a packet size of the WAIC communications; and adjusting packet transmission timing of the WAIC communications.