mhurhangee/patent-ind-claim-en huggingface dataset:
A luggage compartment of an electric traction vehicle, comprising: - a floor ; - an electric/electronic unit for recharging a battery pack ; - a support structure comprising: a) a frame which carries said electric/electronic unit in a fixed position; b) an attachment portion arranged in front of said frame and fixed to said floor ; c) a deformable portion interposed between said attachment portion and said frame and adapted to bend about an axis which is horizontal and is transverse to a horizontal advancement direction of the vehicle ; characterized in that the luggage compartment further comprises: - a pushing element fixed with respect to said floor and comprising a support surface ; wherein said support structure comprises a lower surface which rests on said support surface so as to be pushed upwards when said pushing element moves towards said axis in the event of an accident. - a floor ; - an electric/electronic unit for recharging a battery pack ; - a support structure comprising: a) a frame which carries said electric/electronic unit in a fixed position; b) an attachment portion arranged in front of said frame and fixed to said floor ; c) a deformable portion interposed between said attachment portion and said frame and adapted to bend about an axis which is horizontal and is transverse to a horizontal advancement direction of the vehicle ; characterized in that the luggage compartment further comprises: a) a frame which carries said electric/electronic unit in a fixed position; b) an attachment portion arranged in front of said frame and fixed to said floor ; c) a deformable portion interposed between said attachment portion and said frame and adapted to bend about an axis which is horizontal and is transverse to a horizontal advancement direction of the vehicle ; - a pushing element fixed with respect to said floor and comprising a support surface ;
A method for producing a cast workpiece , wherein the method comprises the following method steps: - providing a mold having at least one mold core arranged in the mold ; - inserting a metal melt into the mold ; - waiting for a period of time until at least the outer contour of the metal melt has solidified and the workpiece has been formed from the metal melt ; - removing the workpiece from the mold ; - shattering the mold core , wherein for shattering the mold core , a hammer head is applied on a defined energy transmission surface of the workpiece and the energy transmission surface is acted on by means of the hammer head , characterized in that shattering the mold core by means of the hammer head is carried out at a surface temperature of the energy transmission surface of between 300° Celsius and 400° Celsius, wherein at least outward parts of the mold core are shattered. - providing a mold having at least one mold core arranged in the mold ; - inserting a metal melt into the mold ; - waiting for a period of time until at least the outer contour of the metal melt has solidified and the workpiece has been formed from the metal melt ; - removing the workpiece from the mold ; - shattering the mold core , wherein for shattering the mold core , a hammer head is applied on a defined energy transmission surface of the workpiece and the energy transmission surface is acted on by means of the hammer head , characterized in that
Telescopic sight , in particular for a shotgun, comprising a zoom adjusting device , wherein the zoom adjusting device comprises a ring which is rotatable about the optical axis of the telescopic sight , wherein the zoom adjusting device comprises at least one marking which is provided or coated at least in part with a luminous colour, characterised in that the luminous colour comprises a fluorescent colour or a phosphorescent colour. the zoom adjusting device comprises at least one marking which is provided or coated at least in part with a luminous colour, characterised in that the luminous colour comprises a fluorescent colour or a phosphorescent colour.
A method for wireless communication at a user equipment, UE, comprising: receiving , during a first transmission time interval, TTI, an uplink grant that includes an assignment of resources of a shared radio frequency spectrum band; receiving , during a second TTI, a trigger for a transmission on the assigned resources; identifying , by the UE, uplink control information comprising channel state information, CSI, based at least in part on a time difference between at least one of: the first TTI and the second TTI, the first TTI and a third TTI that precedes the first TTI, or the second TTI and a fourth TTI that is subsequent to the second TTI; determining whether the time difference between the first TTI and the second TTI exceeds a threshold; identifying a fifth TTI as a reference for the CSI when the time difference between the first TTI and the second TTI exceeds the threshold, wherein the fifth TTI precedes the second TTI; or identifying the third TTI as the reference for the CSI when the time difference between the first TTI and the second TTI is less than or equal to the threshold; and transmitting the uplink control information during the fourth TTI in response to the trigger. receiving , during a first transmission time interval, TTI, an uplink grant that includes an assignment of resources of a shared radio frequency spectrum band; receiving , during a second TTI, a trigger for a transmission on the assigned resources; identifying , by the UE, uplink control information comprising channel state information, CSI, based at least in part on a time difference between at least one of: the first TTI and the second TTI, the first TTI and a third TTI that precedes the first TTI, or the second TTI and a fourth TTI that is subsequent to the second TTI; determining whether the time difference between the first TTI and the second TTI exceeds a threshold; identifying a fifth TTI as a reference for the CSI when the time difference between the first TTI and the second TTI exceeds the threshold, wherein the fifth TTI precedes the second TTI; or identifying the third TTI as the reference for the CSI when the time difference between the first TTI and the second TTI is less than or equal to the threshold; and transmitting the uplink control information during the fourth TTI in response to the trigger.
An end effector configured to open and close a screw-type lid for closing an opening of a container body , comprising: a container gripper configured to grip the container body ; a lid gripper configured to grip the lid and be movable on a screw axis of the lid ; a rotating part configured to rotate the lid gripper ; a guiding part configured to guide the lid gripper being rotated by the rotating part to move on the screw axis; and a detector configured to detect that the lid gripper is moved to one of an opened position and a closed position of the lid , wherein the end effector is provided to a robotic arm , characterized in that the container gripper is attached to a link of the robotic arm , and the rotating part is included in a wrist part of the robotic arm , the wrist part is configured to be rotatably coupled to the link . a container gripper configured to grip the container body ; a lid gripper configured to grip the lid and be movable on a screw axis of the lid ; a rotating part configured to rotate the lid gripper ; a guiding part configured to guide the lid gripper being rotated by the rotating part to move on the screw axis; and a detector configured to detect that the lid gripper is moved to one of an opened position and a closed position of the lid , wherein the end effector is provided to a robotic arm , characterized in that the container gripper is attached to a link of the robotic arm , and the rotating part is included in a wrist part of the robotic arm , the wrist part is configured to be rotatably coupled to the link .
A method for detecting blockage of a radar system of a vehicle (V), the method comprising the steps of: collecting (S100) radar data by the radar system , and collecting camera data by a camera system of the vehicle (V); detecting (S200) a first set of objects (SO1) in the surrounding of the vehicle (V) based on the camera data, and detecting a second set of objects (SO2) in the surrounding of the vehicle (V) based on the radar data; determining (S300) a third set of objects (SO3) as an intersection of the first set of objects (SO1) and the second set of objects (SO2) ; determining a first indicator (q) based on a number of objects within the first set of objects (SO1), wherein the first indicator (q) refers to a sensor quality of the camera system ; determining a second indicator (r) based on a comparison of the number of objects within the first set of objects (SO1) with a number of objects within the third set of objects (SO3), wherein the second indicator (r) refers to a relation between the sensor quality of the camera system and a sensor quality of the radar system; detecting (S400) blockage of the radar system based on the first indicator (q) and on the second indicator (r) characterized in that blockage is detected if a mean distance of the objects within the second set of objects (SO2) is smaller than a distance threshold value, wherein the distance threshold value is adjusted based on the second indicator (r). collecting (S100) radar data by the radar system , and collecting camera data by a camera system of the vehicle (V); detecting (S200) a first set of objects (SO1) in the surrounding of the vehicle (V) based on the camera data, and detecting a second set of objects (SO2) in the surrounding of the vehicle (V) based on the radar data; determining (S300) a third set of objects (SO3) as an intersection of the first set of objects (SO1) and the second set of objects (SO2) ; determining a first indicator (q) based on a number of objects within the first set of objects (SO1), wherein the first indicator (q) refers to a sensor quality of the camera system ; determining a second indicator (r) based on a comparison of the number of objects within the first set of objects (SO1) with a number of objects within the third set of objects (SO3), wherein the second indicator (r) refers to a relation between the sensor quality of the camera system and a sensor quality of the radar system; detecting (S400) blockage of the radar system based on the first indicator (q) and on the second indicator (r) characterized in that blockage is detected if a mean distance of the objects within the second set of objects (SO2) is smaller than a distance threshold value, wherein the distance threshold value is adjusted based on the second indicator (r).
An overhead camshaft engine , comprising: a cylinder block defining a cylinder in cooperation with a cylinder head ; a crankcase attached to a lower part of the cylinder block to define a crank case chamber in cooperation with a part of the cylinder block; a first bearing provided on the cylinder block to rotatably support a first end of a crankshaft of the engine; a second bearing provided on a bearing retaining member attached to a part of the cylinder block to rotatably support a second end of the crankshaft; a camshaft rotatably supported in an upper part of the cylinder head and provided with a camshaft pulley ; a crankshaft pulley attached to a part of the second end of the crankshaft projecting outward from the second bearing; and a timing belt passed around the camshaft pulley and the crankshaft pulley, characterized by that the crankcase is attached to a lower end of the cylinder block at a parting plane that extends obliquely across the crankshaft. a cylinder block defining a cylinder in cooperation with a cylinder head ; a crankcase attached to a lower part of the cylinder block to define a crank case chamber in cooperation with a part of the cylinder block; a first bearing provided on the cylinder block to rotatably support a first end of a crankshaft of the engine; a second bearing provided on a bearing retaining member attached to a part of the cylinder block to rotatably support a second end of the crankshaft; a camshaft rotatably supported in an upper part of the cylinder head and provided with a camshaft pulley ; a crankshaft pulley attached to a part of the second end of the crankshaft projecting outward from the second bearing; and a timing belt passed around the camshaft pulley and the crankshaft pulley, characterized by that the crankcase is attached to a lower end of the cylinder block at a parting plane that extends obliquely across the crankshaft.
A first apparatus , comprising a processor , a memory , and communication circuitry , the first apparatus being an Internet of Things, IoT, device and being connected to a cellular network via its communication circuitry, the first apparatus further comprising computer-executable instructions stored in the memory of the first apparatus which, when executed by the processor of the first apparatus, cause the first apparatus to perform operations comprising: a. sending a first registration request to a first public land mobile network only if the first apparatus receives an indication from the first public land mobile network that the first public land mobile network supports public land mobile network retargeting; b. receiving a registration reject message, the registration reject message comprising an identification of a second public land mobile network; c. sending a second registration request to the second public land mobile network. a. sending a first registration request to a first public land mobile network only if the first apparatus receives an indication from the first public land mobile network that the first public land mobile network supports public land mobile network retargeting; b. receiving a registration reject message, the registration reject message comprising an identification of a second public land mobile network; c. sending a second registration request to the second public land mobile network.
Method for controlling at least one function of a vehicle by an individual present onboard this vehicle , through the completion, by this individual, of at least one control gesture (GC) associated with this function, according to which the following steps are provided: a) detection of the control gesture (GC) completed by the individual in a detection zone (D) of said vehicle , b) determination of an interaction state (EI) between said individual and his or her environment, said interaction state (EI) of the individual with the environment being determined from among a zero interaction state and an active interaction state, and c) based on the interaction state (EI) determined in step b), controlling of the function associated with the control gesture (GC) detected in step a), characterized in that when the interaction state (EI) determined in step b) is active, step c) comprises the following substeps: c1) transmission of a signal (S) to at least one individual present in the vehicle , c2) reception of a response (R) from at least one individual present in the vehicle, to said signal (S) transmitted in step c1), and, c3) based on the response (R) received in step c2), controlling of the function associated with said control gesture (GC) detected in step a). a) detection of the control gesture (GC) completed by the individual in a detection zone (D) of said vehicle , b) determination of an interaction state (EI) between said individual and his or her environment, said interaction state (EI) of the individual with the environment being determined from among a zero interaction state and an active interaction state, and c) based on the interaction state (EI) determined in step b), controlling of the function associated with the control gesture (GC) detected in step a), characterized in that c1) transmission of a signal (S) to at least one individual present in the vehicle , c2) reception of a response (R) from at least one individual present in the vehicle, to said signal (S) transmitted in step c1), and, c3) based on the response (R) received in step c2), controlling of the function associated with said control gesture (GC) detected in step a).
An energy absorbing landing gear system for attachment to a vertical landing apparatus , the energy absorbing landing gear system comprising: a linear damper assembly ; and a load limiter assembly coupled to the linear damper assembly , the load limiter assembly having: - a tubular fitting incorporating at least one deformable element to enhance an energy absorption capability , the at least one deformable element comprising two deformable elements aligned opposite each other on the tubular fitting , each of the two deformable elements having a through opening ; and - a pin inserted through each through opening of the two deformable elements , and the pin further coupled to the linear damper assembly , wherein when the energy absorbing landing gear system is configured to be attached to the vertical landing apparatus , during a landing phase , the linear damper assembly contacts a landing surface , and a piston assembly of the linear damper assembly moves a first compression distance toward the load limiter assembly , and when the linear damper assembly reaches a maximum compression , the linear damper assembly moves a second compression distance into the load limiter assembly , and the at least one deformable element deforms, and when the linear damper assembly moves into the load limiter assembly , the pin tears through the two deformable elements to deform the two deformable elements . a linear damper assembly ; and a load limiter assembly coupled to the linear damper assembly , the load limiter assembly having: - a tubular fitting incorporating at least one deformable element to enhance an energy absorption capability , the at least one deformable element comprising two deformable elements aligned opposite each other on the tubular fitting , each of the two deformable elements having a through opening ; and - a pin inserted through each through opening of the two deformable elements , and the pin further coupled to the linear damper assembly , - a tubular fitting incorporating at least one deformable element to enhance an energy absorption capability , the at least one deformable element comprising two deformable elements aligned opposite each other on the tubular fitting , each of the two deformable elements having a through opening ; and - a pin inserted through each through opening of the two deformable elements , and the pin further coupled to the linear damper assembly , wherein when the energy absorbing landing gear system is configured to be attached to the vertical landing apparatus , during a landing phase , the linear damper assembly contacts a landing surface , and a piston assembly of the linear damper assembly moves a first compression distance toward the load limiter assembly , and when the linear damper assembly reaches a maximum compression , the linear damper assembly moves a second compression distance into the load limiter assembly , and the at least one deformable element deforms, and when the linear damper assembly moves into the load limiter assembly , the pin tears through the two deformable elements to deform the two deformable elements .
An optical assembly comprising: an adapter ; a connector assembly comprising: a housing received by the adapter, said housing defining a bore ; a projection extending from the housing; and a ferrule translatable within the bore of the housing; and a sensor mounted only on the housing or only on the adapter, the sensor being configured for detecting translation of the ferrule, wherein (i) the sensor is mounted on the projection when the sensor is mounted on the housing or (ii) the sensor is configured for contacting the projection when the sensor is mounted on the adapter, and wherein an electrical characteristic of the sensor changes to indicate translation of the ferrule to a predetermined position. an adapter ; a connector assembly comprising: a housing received by the adapter, said housing defining a bore ; a projection extending from the housing; and a ferrule translatable within the bore of the housing; and a housing received by the adapter, said housing defining a bore ; a projection extending from the housing; and a ferrule translatable within the bore of the housing; and a sensor mounted only on the housing or only on the adapter, the sensor being configured for detecting translation of the ferrule, wherein (i) the sensor is mounted on the projection when the sensor is mounted on the housing or (ii) the sensor is configured for contacting the projection when the sensor is mounted on the adapter, and wherein an electrical characteristic of the sensor changes to indicate translation of the ferrule to a predetermined position.
Method for determining a distance (d ERC ) between an eye rotation center of an eye of a subject and an apex of a cornea of the eye , the method being carried out using calculation means and comprising: - providing a geometric model of an eye , whereby the eye is modeled with a first sphere (C1) for the sclera of the eye and a second sphere (C2) for the cornea of the eye , the first sphere (C1) having a first radius (R1) and a first center (P1), the second sphere (C2) having a second radius (R2) smaller than the first radius (R1) and a second center (P2), the first center (P1) and the second center (P2) being aligned on an optical axis of the eye , another distance "P1P2" between first center (P1) and the second center (P2) being such that P1P2 < (R 1 2 - R2 2 )1⁄2, "R1" referring to the first radius (R1) and "R2" referring to the second radius (R2), the eye rotation center of this eye being positioned at the center (P1) of the first sphere (C1), said distance (d ERC ) being determined based on a set of personal parameters (L E , d AC , D I , A GE , K) including at least a first geometric dimension (D I ) of the eye , each personal parameter (L E , d AC , D I , A GE , K) being distinct from said distance (dERc) ; - determining a value of each personal parameter (L E , d AC , D I , A GE , K) for the subject; and - determining a first approximate value of said distance (d ERC ) in accordance with said geometric model based on the values of the personal parameters (L E , d AC , D I , AGE, K). - providing a geometric model of an eye , whereby the eye is modeled with a first sphere (C1) for the sclera of the eye and a second sphere (C2) for the cornea of the eye , the first sphere (C1) having a first radius (R1) and a first center (P1), the second sphere (C2) having a second radius (R2) smaller than the first radius (R1) and a second center (P2), the first center (P1) and the second center (P2) being aligned on an optical axis of the eye , another distance "P1P2" between first center (P1) and the second center (P2) being such that P1P2 < (R 1 2 - R2 2 )1⁄2, "R1" referring to the first radius (R1) and "R2" referring to the second radius (R2), the eye rotation center of this eye being positioned at the center (P1) of the first sphere (C1), said distance (d ERC ) being determined based on a set of personal parameters (L E , d AC , D I , A GE , K) including at least a first geometric dimension (D I ) of the eye , each personal parameter (L E , d AC , D I , A GE , K) being distinct from said distance (dERc) ; - determining a value of each personal parameter (L E , d AC , D I , A GE , K) for the subject; and - determining a first approximate value of said distance (d ERC ) in accordance with said geometric model based on the values of the personal parameters (L E , d AC , D I , AGE, K).