mhurhangee/patent-ind-claim-en huggingface dataset:
A method comprising: sending commands, wherein the commands include a command to a movement system to move a folding wing tip to a first position and a command to each of a latch system and a lock system to secure the folding wing tip in the first position ; determining with a sensor system whether each of the movement system , the latch system , and the lock system is responsive to the respective command; and in response to determining the movement system is not responsive, sending a command to utilize a backup actuator to perform an operation of the folding wing tip with the movement system , wherein the backup actuator is an electric motor or a hydraulic motor connected to the movement system . sending commands, wherein the commands include a command to a movement system to move a folding wing tip to a first position and a command to each of a latch system and a lock system to secure the folding wing tip in the first position ; determining with a sensor system whether each of the movement system , the latch system , and the lock system is responsive to the respective command; and in response to determining the movement system is not responsive, sending a command to utilize a backup actuator to perform an operation of the folding wing tip with the movement system , wherein the backup actuator is an electric motor or a hydraulic motor connected to the movement system .
A dual-clutch mechanism intended to be installed between an engine and a transmission of a motor vehicle, the dual-clutch mechanism comprising: - a subassembly comprising: - a first clutch with axis of rotation (O); - a second clutch situated radially on the inside of the first clutch ; - an axially extending sleeve rotationally coupled to an input disks carrier of the first and second clutches at a connection zone ; - an actuating system comprising a housing which houses: - a first cylindrical actuator designed to move axially so as to engage or to disengage the first clutch ; - a second cylindrical actuator designed to move axially so as to engage or to disengage the second clutch ; - a first force-transmission member designed to transmit axial load to the first clutch and generated by the first actuator ; - a second force-transmission member designed to transmit axial load to the second clutch and generated by the second actuator ; characterized in that , at a given radial distance from the axis of rotation (O), a face of the second force-transmission member is designed to be able to intersect a facing face belonging to the first force-transmission member . - a subassembly comprising: - a first clutch with axis of rotation (O); - a second clutch situated radially on the inside of the first clutch ; - an axially extending sleeve rotationally coupled to an input disks carrier of the first and second clutches at a connection zone ; - a first clutch with axis of rotation (O); - a second clutch situated radially on the inside of the first clutch ; - an axially extending sleeve rotationally coupled to an input disks carrier of the first and second clutches at a connection zone ; - an actuating system comprising a housing which houses: - a first cylindrical actuator designed to move axially so as to engage or to disengage the first clutch ; - a second cylindrical actuator designed to move axially so as to engage or to disengage the second clutch ; - a first cylindrical actuator designed to move axially so as to engage or to disengage the first clutch ; - a second cylindrical actuator designed to move axially so as to engage or to disengage the second clutch ; - a first force-transmission member designed to transmit axial load to the first clutch and generated by the first actuator ; - a second force-transmission member designed to transmit axial load to the second clutch and generated by the second actuator ;
A method for enhancing wake situational awareness comprising: receiving, by a transceiver of a trailing aircraft, a plurality of flight information transmissions from a lead aircraft; creating, by a processor of the trailing aircraft electronically connected to the transceiver, from the plurality of flight information transmissions, a positional history of the lead aircraft; determining, by said processor, from the positional history and the plurality of flight information transmissions, a differential flight parameter; and presenting on a display in a cockpit of the trailing aircraft coupled to the processor an indicia of the current position of the trailing aircraft, an indicia of the leading aircraft relative to the trailing aircraft, and the differential flight parameter for the trailing aircraft characterized in that wherein determining a differential flight parameter from the positional history and the plurality of flight information transmissions further comprises: - analyzing the positional history to determine a closest previous location of the lead aircraft based upon minimum distance to the current position of the trailing aircraft; and - computing the differential flight parameter from a difference between an altitude of the lead aircraft at the closest previous location and a current altitude of the trailing aircraft. receiving, by a transceiver of a trailing aircraft, a plurality of flight information transmissions from a lead aircraft; creating, by a processor of the trailing aircraft electronically connected to the transceiver, from the plurality of flight information transmissions, a positional history of the lead aircraft; determining, by said processor, from the positional history and the plurality of flight information transmissions, a differential flight parameter; and presenting on a display in a cockpit of the trailing aircraft coupled to the processor an indicia of the current position of the trailing aircraft, an indicia of the leading aircraft relative to the trailing aircraft, and the differential flight parameter for the trailing aircraft characterized in that wherein determining a differential flight parameter from the positional history and the plurality of flight information transmissions further comprises: - analyzing the positional history to determine a closest previous location of the lead aircraft based upon minimum distance to the current position of the trailing aircraft; and - computing the differential flight parameter from a difference between an altitude of the lead aircraft at the closest previous location and a current altitude of the trailing aircraft. - analyzing the positional history to determine a closest previous location of the lead aircraft based upon minimum distance to the current position of the trailing aircraft; and - computing the differential flight parameter from a difference between an altitude of the lead aircraft at the closest previous location and a current altitude of the trailing aircraft.
A display device comprising: display pixels (SPX) comprising light emitting elements arranged in a display area (DA) of a display panel and pixel drivers (DDU1, DDU2, DDU3) connected to the light emitting elements; light sensing pixels (LSP) comprising light sensing elements (PD) arranged in the display area (DA) and sensing drivers (FDU) connected to the light sensing elements (PD); a display scan driver configured to sequentially supply display scan signals to the pixel drivers (DDU1, DDU2, DDU3); a light sensing driver configured to sequentially supply sensing scan signals (FSp) to the sensing drivers (FDU); a blood pressure detection circuit configured to measure a blood pressure of a user using light sensing signals received from the sensing drivers (FDU); and a display driving circuit configured to supply control signals to the display scan driver and the light sensing driver to control a light sensing signal detection timing of the light sensing pixels (LSP) when a mode of the display device is switched to a blood pressure measurement mode. display pixels (SPX) comprising light emitting elements arranged in a display area (DA) of a display panel and pixel drivers (DDU1, DDU2, DDU3) connected to the light emitting elements; light sensing pixels (LSP) comprising light sensing elements (PD) arranged in the display area (DA) and sensing drivers (FDU) connected to the light sensing elements (PD); a display scan driver configured to sequentially supply display scan signals to the pixel drivers (DDU1, DDU2, DDU3); a light sensing driver configured to sequentially supply sensing scan signals (FSp) to the sensing drivers (FDU); a blood pressure detection circuit configured to measure a blood pressure of a user using light sensing signals received from the sensing drivers (FDU); and a display driving circuit configured to supply control signals to the display scan driver and the light sensing driver to control a light sensing signal detection timing of the light sensing pixels (LSP) when a mode of the display device is switched to a blood pressure measurement mode.
Load carrier foot for supporting a load bar on a vehicle , said load carrier foot comprising a support member for supporting the load bar thereon and a locking mechanism for releasably locking said load bar on said load carrier foot , characterized in that said locking mechanism is configured to automatically return into a locking state in which said load bar is locked on said load carrier foot , wherein said locking mechanism comprises a locking member configured to engage with said load bar and a biasing member for continuously applying an engaging force on said locking member , wherein said locking mechanism further comprising an operating member for transferring said locking mechanism into a release state in which said load bar is unlocked from said load carrier foot , wherein: (I) said locking member comprises an engaging section adapted to contact said load bar and force transmittingly coupled to a first portion of said operating member , wherein said support member comprises a supporting portion adapted to contact an outer surface of said load bar , said supporting portion and said engaging section forming a clamping section for fixedly holding a wall portion of said load bar between them, and/or (II) said locking mechanism is configured to take a securing state in which a movement of said locking member or a movement of said operating member is blocked. (I) said locking member comprises an engaging section adapted to contact said load bar and force transmittingly coupled to a first portion of said operating member , wherein said support member comprises a supporting portion adapted to contact an outer surface of said load bar , said supporting portion and said engaging section forming a clamping section for fixedly holding a wall portion of said load bar between them, and/or (II) said locking mechanism is configured to take a securing state in which a movement of said locking member or a movement of said operating member is blocked.
An apparatus for extracting power comprising a track comprising first and second elongate sections and a terminal connecting the first and second elongate sections, wherein the first elongate section is positioned behind the second elongate section; multiple towers, each tower supporting the track; an airfoil comprising a suction surface and a pressure surface , wherein the airfoil is coupled to the track so that the pressure surface lies between the suction surface and the track or the suction surface lies between the pressure surface and the track as the airfoil travels along the track, wherein the airfoil is moveable in opposite directions when alternately coupled to the first elongate section and second elongate section, wherein the airfoil pitches as it travels along the terminal; a power generator to harvest power from an atmospheric wind through the movement of the airfoil; and a bridle system coupling at least one of the first and second elongate sections to an anchor , wherein the bridle system balances the force of gravity on the at least one of the first and second elongate sections. a track comprising first and second elongate sections and a terminal connecting the first and second elongate sections, wherein the first elongate section is positioned behind the second elongate section; multiple towers, each tower supporting the track; an airfoil comprising a suction surface and a pressure surface , wherein the airfoil is coupled to the track so that the pressure surface lies between the suction surface and the track or the suction surface lies between the pressure surface and the track as the airfoil travels along the track, wherein the airfoil is moveable in opposite directions when alternately coupled to the first elongate section and second elongate section, wherein the airfoil pitches as it travels along the terminal; a power generator to harvest power from an atmospheric wind through the movement of the airfoil; and a bridle system coupling at least one of the first and second elongate sections to an anchor , wherein the bridle system balances the force of gravity on the at least one of the first and second elongate sections.
Method for producing a rod-shaped element wherein the method has the steps of providing a pipe made of a metal, wherein the pipe has an outer diameter and a longitudinal direction, providing at least one strand having a plurality of yarns, wherein at least one of the yarns has carbon fibres, introducing the at least one strand into the pipe such that the at least one strand extends in the longitudinal direction in the pipe , and cold-forming the pipe having the at least one strand introduced therein using a forming tool, such that the outer diameter of the pipe prior to the cold-forming is greater than the outer diameter of the pipe after the cold-forming. providing a pipe made of a metal, wherein the pipe has an outer diameter and a longitudinal direction, providing at least one strand having a plurality of yarns, wherein at least one of the yarns has carbon fibres, introducing the at least one strand into the pipe such that the at least one strand extends in the longitudinal direction in the pipe , and cold-forming the pipe having the at least one strand introduced therein using a forming tool, such that the outer diameter of the pipe prior to the cold-forming is greater than the outer diameter of the pipe after the cold-forming.
A medical device , comprising: an enclosure defining a cavity for containing agent; a lumen for receiving a pressurized gas; a source of the pressurized gas; and a barrier positioned between the cavity and the lumen, the barrier including a passage extending through the barrier for storing agent, wherein rotation of the barrier relative to the lumen establishes fluid communication between the passage and the lumen for delivering agent from the passage to the lumen, wherein the barrier includes a first opening and a second opening located on opposite ends of the barrier and connected via the passage; the device characterized in that the lumen is a flexible catheter capable of traversing a tortuous body lumen. an enclosure defining a cavity for containing agent; a lumen for receiving a pressurized gas; a source of the pressurized gas; and a barrier positioned between the cavity and the lumen, the barrier including a passage extending through the barrier for storing agent, wherein rotation of the barrier relative to the lumen establishes fluid communication between the passage and the lumen for delivering agent from the passage to the lumen, wherein the barrier includes a first opening and a second opening located on opposite ends of the barrier and connected via the passage; the device characterized in that the lumen is a flexible catheter capable of traversing a tortuous body lumen.
A burner cap base for a burner of a gas cooktop, comprising an outer ring gas inlet and a groove used for accommodating gas, wherein the outer ring gas inlet is used for allowing gas supplied by an outer ring gas injector to enter the burner cap base , the burner cap base further comprises a plurality of gas guide slots , wherein each gas guide slot communicates the groove and the outer ring gas inlet , wherein the burner cap base further comprises a plurality of flow division portions , the outer ring gas inlet is divided into a plurality of gas division openings by the flow division portion , characterized in that each gas guide slot corresponds to at least one flow division portion , and wherein each flow division portion directly faces toward the center location of one of the gas guide slots .
Modified Cas9 nuclease comprising a substantial part of a Cas9 nuclease which is required for the biological activity Z and fused thereto at least one of a functional Z protein domain of a HDR factor selected from the group consisting of RAD51, RAD52, and/or MRE11, characterized in that it further comprises CtBP interacting protein (CtIP).
A heater for heating and vaporizing droplets in a gas stream, comprising a heater housing and a heater body located inside the heater housing, the heater housing is provided with an airflow inlet and an airflow outlet, an airflow enters into the heater housing via the airflow inlet, flows through the heater body, and then is discharged via the airflow outlet; the heater body comprises a stereoscopic network structure formed by interweaving one or more electrical heating wires; wherein the gas stream is an amine gas stream, the droplets are amine droplets, the heater is a vertical type heater, the amine airflow inlet is located on the heater housing below the heater body, the amine airflow outlet is located on the heater housing above the heater body, and the bottom of the heater housing is provided with a drain port.
Seal carrier for a turbomachine, in particular a gas turbine, comprising a carrier base and at least one sealing body , wherein the at least one sealing body is connected to the carrier base and the at least one sealing body is formed by a plurality of cavities arranged next to one another in the circumferential direction (UR) and in the axial direction (AR), in particular regularly, wherein the cavities extend from the carrier base in the radial direction (RR), wherein at least one stiffening element which extends along the circumferential direction (UR) is provided on the carrier base , which stiffening element at least partially covers the at least one sealing body at one of the axial end regions thereof, wherein the carrier base , the at least one sealing body and the at least one stiffening element are produced by an additive manufacturing method and are formed in one piece.
Acoustic attenuation device for propagated sound through surfaces, said acoustic attenuation device being of the layered type and comprising: - an innermost connection layer , adapted to associate said acoustic attenuation device with at least one surface; - an intermediate layer , comprising a plurality of attenuation modules , each of said attenuation modules comprising at least one movable element defined by at least one first opening , said at least one movable element being adapted to vibrate relative to said at least one first opening in a resonant manner when hit by said propagated sound, to attenuate said propagated sound by mechanical dissipation; - an outermost layer , comprising at least one closure surface defining at least one cavity facing said movable elements and adapted to encapsulate said movable elements of said attenuation modules of said intermediate layer , to further attenuate said propagated sound by sound-absorbing effect; characterized in that at least one movable element of said intermediate layer is at least partially hollow inside and comprises at least one entrance hole facing from its inside said innermost layer , so as to further attenuate said propagated sound when said entrance hole is hit by said propagated sound. - an innermost connection layer , adapted to associate said acoustic attenuation device with at least one surface; - an intermediate layer , comprising a plurality of attenuation modules , each of said attenuation modules comprising at least one movable element defined by at least one first opening , said at least one movable element being adapted to vibrate relative to said at least one first opening in a resonant manner when hit by said propagated sound, to attenuate said propagated sound by mechanical dissipation; - an outermost layer , comprising at least one closure surface defining at least one cavity facing said movable elements and adapted to encapsulate said movable elements of said attenuation modules of said intermediate layer , to further attenuate said propagated sound by sound-absorbing effect;
An encryption method using homomorphic encryption, the encryption method comprising: generating a ciphertext by encrypting data; and bootstrapping the ciphertext by performing a modular reduction, wherein the bootstrapping is performed by approximating the modular reduction based on a trigonometric function for a modulus corresponding to the generated ciphertext and an inverse function of the trigonometric function. generating a ciphertext by encrypting data; and bootstrapping the ciphertext by performing a modular reduction, wherein the bootstrapping is performed by approximating the modular reduction based on a trigonometric function for a modulus corresponding to the generated ciphertext and an inverse function of the trigonometric function.
Method for producing a rotor for a synchronous reluctance machine, wherein, in a first step, a magnetically non-conductive, prepolymeric or polymeric base compound is interspersed with magnetically conductive particles , and, in a second step, the particles are aligned by applying a magnetic field in order to create at least one magnetic pole pair, wherein the base compound and the particles are filled into a rotor mould , in particular into a cylindrical or square rotor mould , before the field is applied, wherein at least one placeholder, or the later motor shaft , or an auxiliary shaft is introduced into the rotor mould before it is filled, characterized in that one or more particles are manufactured from an insulating wire, wherein the wire is cut up into wire segments, as a result of which particles form that have non-insulated cut surfaces and are mixed into the base compound, and therefore one or more magnetically conductive chains of multiple particles form when the magnetic field is applied.
A connecting hook for a wiper which is characterized in that , a) it has a first hooking portion and a second hooking portion which are formed integrally, b) the first hooking portion has a first contacting surface , the second hooking portion has a second contacting surface , c) the first contacting surface is in a straight line in a cross section of the connecting hook ; d) wherein the second contacting surface is in a circular arc in a cross section of the connecting hook ; and e) wherein the connecting hook transitions to the second contacting surface smoothly from the first contacting surface . a) it has a first hooking portion and a second hooking portion which are formed integrally, b) the first hooking portion has a first contacting surface , the second hooking portion has a second contacting surface , c) the first contacting surface is in a straight line in a cross section of the connecting hook ; d) wherein the second contacting surface is in a circular arc in a cross section of the connecting hook ; and e) wherein the connecting hook transitions to the second contacting surface smoothly from the first contacting surface .
Household appliance (1; 31; 41), in particular a refrigeration appliance, having a door (3; 32; 43, 44) with a recessed handle (4; 33; 45, 46, 48) and an illumination device for shining light (L) onto the recessed handle (4; 33; 45, 46, 48), wherein the illumination device has a projection device (5; 47) for projecting information (IF1-IF8; IF19; IF20) onto the recessed handle (4; 33; 45, 46, 48), characterised in that the recessed handle (4; 33; 45, 46, 48) is set up as an operating device with at least one actuation region (B1-B8, B 19) for operating the household appliance (1; 32; 41), wherein labelling information (IF1-IF8; IF19; IF20) can be projected, by means of the projection device (5; 47), onto a respective actuation region (B1-B8, B19) for the labelling thereof.