mhurhangee/ep-ind-claims huggingface dataset:
Screw anchor, in particular expansion or cavity anchor, with an anchor shaft having an expansion section, wherein a sleeve is arranged at the anchor shaft for sealing the screw anchor against a wall, which sleeve comprises a flat wall abutment portion, in which a substantially circular opening is inserted, wherein a circumferential collar framing the opening is moulded-on on at least one side of the wall abutment portion and wherein the wall abutment portion and the at least one circumferential collar is produced in one piece from an elastic, waterproof sealing material, in particular a silicone or rubber material, wherein a collar merges into a bag-shaped section moulded thereon, wherein the anchor shaft is substantially arranged within the bag-shaped section, whereby a complete encapsulation of the screw anchor against the wall is achievable, characterised in that the sleeve is non-detachably connected to the anchor shaft.
Method for setting a clearance of an electromechanical brake, in particular a commercial vehicle brake, comprising the steps of: - activating a clearance test cycle for the brake; - applying at least one brake pad of the brake in the direction of a brake disc and ascertaining a contact position (K ist) in which the brake pad comes into contact with the brake disc during the application; - determining the clearance (L ist) and a degree of pad wear (V B) on the basis of the ascertained contact position (K ist); - calculating a clearance (L Soll) required for the brake and a required contact position (K Soll) of the brake pad and brake disc depending on the degree of pad wear (V B) using predefined parameters, wherein the predefined parameters comprise: - a brake characteristic curve and/or - a stiffness characteristic map in which condition-dependent stiffness values are stored. - activating a clearance test cycle for the brake; - applying at least one brake pad of the brake in the direction of a brake disc and ascertaining a contact position (K ist) in which the brake pad comes into contact with the brake disc during the application; - determining the clearance (L ist) and a degree of pad wear (V B) on the basis of the ascertained contact position (K ist); - calculating a clearance (L Soll) required for the brake and a required contact position (K Soll) of the brake pad and brake disc depending on the degree of pad wear (V B) using predefined parameters, wherein the predefined parameters comprise: - a brake characteristic curve and/or - a stiffness characteristic map in which condition-dependent stiffness values are stored. - a brake characteristic curve and/or - a stiffness characteristic map in which condition-dependent stiffness values are stored.
A manufacturing method of a sintered magnet, the method comprising: preparing NdFeB-based powders by using a reduction-diffusion method; mixing the NdFeB-based powders and rare-earth hydride powders; heat-treating the mixture at a temperature of 600 to 850 °C; and sintering the heat-treated mixture at a temperature of 1000 to 1100 °C, wherein the rare earth hydride powders are NdH 2 powders or mixed powders of NdH 2 and PrH 2, wherein in the mixing of the NdFeB-based powders and rare-earth hydride powders, Cu powders are further contained, characterized in that a content ratio of the rare earth hydride powders and the Cu powders is 7:3 by weight. preparing NdFeB-based powders by using a reduction-diffusion method; mixing the NdFeB-based powders and rare-earth hydride powders; heat-treating the mixture at a temperature of 600 to 850 °C; and sintering the heat-treated mixture at a temperature of 1000 to 1100 °C, wherein the rare earth hydride powders are NdH 2 powders or mixed powders of NdH 2 and PrH 2, wherein in the mixing of the NdFeB-based powders and rare-earth hydride powders, Cu powders are further contained, characterized in that a content ratio of the rare earth hydride powders and the Cu powders is 7:3 by weight.
Test device for screwers, comprising an adapter or joint simulator (12, 12') and a transducer having a body and a head with a seat for receiving the coupling end of the adapter or joint simulator (12, 12'), the adapter or joint simulator having an opposite working end intended for coupling with a screwer to be tested, characterized in that the coupling end is made with a side wall (21, 21') polygonally-fashioned in order to be received in the seat, achieved in a complementary polygonal manner, the head being made tightenable to act as a clamp in order to releasably lock, in the seat, the coupling end of the adapter or joint simulator.
A nuclear power plant control system (1; 2) comprising: an operation unit configured to receive an operation for controlling a specific portion of a nuclear power plant; a notification unit configured to notify that a control signal corresponding to the operation received by the operation unit arrives at a predetermined position on a path connected to the portion; and an inhabitation unit configured to inhibit the control signal from arriving at the portion when a signal indicating a state of being on test is received and is in a position between the predetermined position on the path and the portion; the nuclear power plant control system is characterized in that the inhabitation unit is a majority circuit that causes a control signal to arrive at the portion only when a plurality of control signals are received through different paths. an operation unit configured to receive an operation for controlling a specific portion of a nuclear power plant; a notification unit configured to notify that a control signal corresponding to the operation received by the operation unit arrives at a predetermined position on a path connected to the portion; and an inhabitation unit configured to inhibit the control signal from arriving at the portion when a signal indicating a state of being on test is received and is in a position between the predetermined position on the path and the portion; the nuclear power plant control system is characterized in that the inhabitation unit is a majority circuit that causes a control signal to arrive at the portion only when a plurality of control signals are received through different paths.
A security method in a telecommunications network comprising a radio access network system and a core network system, wherein the radio access network system is configured to provide a wireless radio interface for at least one user device, wherein a shared secret key is stored in both the user device and the core network system, wherein the core network system pre-stores a RAN only indication associated with the user device to transmit at least one vector to the radio access network system, the method comprising the steps in the radio access network system of: only receiving from the core network system for a user device for which the RAN only indication has been pre-stored, the at least one vector comprising one or more values derived from the shared secret key; storing the at least one vector in the radio access network system; after storing the at least one vector, performing at least one of an authentication procedure and a key agreement procedure for the user device over the wireless radio interface using the one or more values of the received vector for establishing a connection between the user device and the radio access network system. only receiving from the core network system for a user device for which the RAN only indication has been pre-stored, the at least one vector comprising one or more values derived from the shared secret key; storing the at least one vector in the radio access network system; after storing the at least one vector, performing at least one of an authentication procedure and a key agreement procedure for the user device over the wireless radio interface using the one or more values of the received vector for establishing a connection between the user device and the radio access network system.
An array camera module (100, 100A), comprising at least two optical lenses (10, 10A) and a circuit board assembly (20, 20A), wherein the circuit board assembly further comprises: at least one circuit board (21, 21A); at least two photosensitive chips (22, 22A), wherein each of the photosensitive chips is conductively connected to the circuit board respectively, and each of the optical lenses is held in a photosensitive path of each of the photosensitive chips respectively; and at least one electronic component (23, 23A), wherein each of the electronic components is conductively connected to the circuit board respectively, and at least one of the electronic components is located on a back face (212, 212A) of the circuit board (21, 21A); wherein the circuit board assembly (20, 20A) comprises at least one embedding portion (27, 27A) bonded to the back face (212, 212A) of the circuit board (21, 21A) integrally; wherein the circuit board (21, 21A) has at least one through-hole shaped accommodation space (215, 215A), wherein at least one of the photosensitive chips (22, 22A) is attached to the front face (211, 211A) of the circuit board, and at least one of the photosensitive chips (22, 22A) is attached to the embedding portion (27, 27A) via the accommodation space of the circuit board, wherein a part of the embedding portion (27, 27A) is exposed to the accommodation space of the circuit board. at least one circuit board (21, 21A); at least two photosensitive chips (22, 22A), wherein each of the photosensitive chips is conductively connected to the circuit board respectively, and each of the optical lenses is held in a photosensitive path of each of the photosensitive chips respectively; and at least one electronic component (23, 23A), wherein each of the electronic components is conductively connected to the circuit board respectively, and at least one of the electronic components is located on a back face (212, 212A) of the circuit board (21, 21A); wherein the circuit board assembly (20, 20A) comprises at least one embedding portion (27, 27A) bonded to the back face (212, 212A) of the circuit board (21, 21A) integrally; wherein the circuit board (21, 21A) has at least one through-hole shaped accommodation space (215, 215A), wherein at least one of the photosensitive chips (22, 22A) is attached to the front face (211, 211A) of the circuit board, and at least one of the photosensitive chips (22, 22A) is attached to the embedding portion (27, 27A) via the accommodation space of the circuit board, wherein a part of the embedding portion (27, 27A) is exposed to the accommodation space of the circuit board.
An aerial survey image capture system for a survey aircraft navigable using navigation parameters that include altitude, speed and direction, the system comprising: a camera system arranged to capture successive images of ground beneath a survey aircraft as the survey aircraft travels on a defined flight path; the camera system having associated camera parameters indicative of image capture characteristics of the camera system including defined image overlap between captured images; the defined flight path and the camera parameters being such that sufficient multiple images are obtained of ground features that a bundle adjustment process can be carried out on the ground images and a photogrammetric solution produced based on the images; characterised in that the aerial survey image capture system comprises: a camera parameter modifier arranged to produce modified camera system parameters in response to a change in at least one navigation parameter, including altitude or speed, actually made to the aircraft, the modified camera system parameters modifying characteristics of image capture by the camera system so as to substantially maintain the defined image overlap between captured images and thereby at least partially compensate for a change in survey efficiency when the changed at least one navigation parameter is used to navigate the survey aircraft without modifying the defined flight path. a camera system arranged to capture successive images of ground beneath a survey aircraft as the survey aircraft travels on a defined flight path; the camera system having associated camera parameters indicative of image capture characteristics of the camera system including defined image overlap between captured images; the defined flight path and the camera parameters being such that sufficient multiple images are obtained of ground features that a bundle adjustment process can be carried out on the ground images and a photogrammetric solution produced based on the images;
A method of wireless communication, comprising: transmitting, from a user equipment, UE, a message to notify a base station of a radio link failure on a current downlink channel; retuning to a first pre-agreed downlink channel with a pre-negotiated bandwidth, wherein the first pre-agreed downlink channel with the pre-negotiated bandwidth refers to a new downlink channel to be used for communication between the base station and the UE that is pre-agreed between the base station and the UE to facilitate communication during radio link failure; and setting, by the UE, a time period to synchronize with the base station on the first pre-agreed downlink channel. transmitting, from a user equipment, UE, a message to notify a base station of a radio link failure on a current downlink channel; retuning to a first pre-agreed downlink channel with a pre-negotiated bandwidth, wherein the first pre-agreed downlink channel with the pre-negotiated bandwidth refers to a new downlink channel to be used for communication between the base station and the UE that is pre-agreed between the base station and the UE to facilitate communication during radio link failure; and setting, by the UE, a time period to synchronize with the base station on the first pre-agreed downlink channel.
Warp knit net, comprising a plurality of net meshes, each of which is defined by a polygon with at least three sides and as many knots which connect a net mesh to adjacent meshes, each side being formed by a chain of loops comprising at least a first yarn that forms first yarn mutually interlaced turns so as to form a primary interlacement of the chain of loops, and at least a second yarn that passes through said primary interlacement of the chain of loops, characterized in that said second yarn, in at least one portion of the chain of loops before and immediately after the knots of the warp knit net forms second yarn mutually interlaced turns which are also interlaced with first yarn mutually interlaced turns of adjacent courses so as to form at least one reinforcing interlacement of the chain of loops.
Fuel tank for a motor vehicle, - comprising a plastics wall (4, 84) which delimits a storage volume for storing a fuel, - comprising one or more reinforcing elements (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) for reinforcing the plastics wall (4, 84), - at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) being connected to an outer side of the plastics wall (4, 84) that faces away from the storage volume, - a maximum thickness of at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) measured normal to the plastics wall (4, 84) being greater than the wall thickness of the plastics wall (4, 84), characterized in that the at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) is tapered on two sides starting from a region of maximum thickness and the - at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) is arranged in a transition from a side wall to a tank top and/or the at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) is arranged in a transition from a side wall to a tank bottom. - comprising a plastics wall (4, 84) which delimits a storage volume for storing a fuel, - comprising one or more reinforcing elements (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) for reinforcing the plastics wall (4, 84), - at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) being connected to an outer side of the plastics wall (4, 84) that faces away from the storage volume, - a maximum thickness of at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) measured normal to the plastics wall (4, 84) being greater than the wall thickness of the plastics wall (4, 84), - at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) is arranged in a transition from a side wall to a tank top and/or the at least one reinforcing element (8, 38, 42, 56, 60, 66, 74, 82, 96, 98) is arranged in a transition from a side wall to a tank bottom.
A robotic surgical system, comprising: a robotic arm (100, 500) comprising a first arm segment (110, 510) comprising a first plurality of links operable to rotate around a plurality of axes to provide the robotic arm with at least five degrees of freedom, wherein the plurality of axes comprise at least three pitch axes and at least one roll axis between each of the pitch axes; and a second arm segment (150, 550) comprising a second plurality of links providing the robotic arm with at least two degrees of freedom, wherein the second plurality of links comprises a roll link, a first link rotatable within a first plane and having a proximal end coupled to a distal end of the roll link, and a second link rotatable within a second plane and having a proximal end coupled to a distal end of the first link; and an instrument driver (180, 580) configured to hold a surgical instrument, wherein the instrument driver is coupled to a distal end of the second link such that the instrument driver is not parallel to at least one of the first and second planes. a robotic arm (100, 500) comprising a first arm segment (110, 510) comprising a first plurality of links operable to rotate around a plurality of axes to provide the robotic arm with at least five degrees of freedom, wherein the plurality of axes comprise at least three pitch axes and at least one roll axis between each of the pitch axes; and a second arm segment (150, 550) comprising a second plurality of links providing the robotic arm with at least two degrees of freedom, wherein the second plurality of links comprises a roll link, a first link rotatable within a first plane and having a proximal end coupled to a distal end of the roll link, and a second link rotatable within a second plane and having a proximal end coupled to a distal end of the first link; and a first arm segment (110, 510) comprising a first plurality of links operable to rotate around a plurality of axes to provide the robotic arm with at least five degrees of freedom, wherein the plurality of axes comprise at least three pitch axes and at least one roll axis between each of the pitch axes; and a second arm segment (150, 550) comprising a second plurality of links providing the robotic arm with at least two degrees of freedom, wherein the second plurality of links comprises a roll link, a first link rotatable within a first plane and having a proximal end coupled to a distal end of the roll link, and a second link rotatable within a second plane and having a proximal end coupled to a distal end of the first link; and an instrument driver (180, 580) configured to hold a surgical instrument, wherein the instrument driver is coupled to a distal end of the second link such that the instrument driver is not parallel to at least one of the first and second planes.
System for monitoring the insulation in a network comprising a transformer and a plurality of tappings (Bj) downstream of the transformer, said monitoring system (10, 20) comprising a permanent insulation monitor at the level of the transformer, with means for injecting an alternating current signal of predetermined voltage (U 0) at a first frequency (f 1), means for measuring the intensity (I f) of the first current signal, and means for determining whether the impedance (Z f) calculated as a function of the intensity (I f) of the first injected current signal is below a first threshold, and at least one locator at the level of a tapping (Bj), the locator comprising: means (22 j) for measuring the intensity of the current signal at the first frequency (f 1) at the level of the tapping (B j), processing and calculation means for calculating the impedance (Z fj) as a function of the measured intensity of the current signal, means for determining whether the calculated impedance (Z fj) is below a respective threshold (D j), said system furthermore comprising indicator means for indicating whether one of the respective thresholds (D j) is attained; characterized in that the monitoring system further comprises: - global measurement means for measuring the intensity of the global current signal at the first frequency (f 1) in the network downstream of the transformer; said global measurement means being at the output of said transformer; - means (26") for determining whether the intensity of the downstream global current signal at the first frequency (f 1) is above a threshold value; - processing and calculation means for giving a second impedance value (Z f0) as a function of the intensity of the downstream global current signal at the first frequency (f 1); - means for determining whether the second impedance value (Z f0) is below the first threshold; - indicator means for indicating whether the first threshold is not attained and/or whether the threshold value is exceeded. - global measurement means for measuring the intensity of the global current signal at the first frequency (f 1) in the network downstream of the transformer; said global measurement means being at the output of said transformer; - means (26") for determining whether the intensity of the downstream global current signal at the first frequency (f 1) is above a threshold value; - processing and calculation means for giving a second impedance value (Z f0) as a function of the intensity of the downstream global current signal at the first frequency (f 1); - means for determining whether the second impedance value (Z f0) is below the first threshold; - indicator means for indicating whether the first threshold is not attained and/or whether the threshold value is exceeded.