mhurhangee/ep-ind-claims huggingface dataset:
A mobile station having an end device and having a removable or hard-implemented security element operable in the end device, wherein a binding between the end device and the security element is devised, so that the end device and the security element are operable with each other only according to the binding, wherein a secret key (PrK; KST) is stored in the security element, and a verification key corresponding to the secret key (PuK; KSA) is stored in the end device, so that the binding between the end device and the security element is verifiable by means of the secret key (PrK; KST) and the verification key (PuK; KSA), wherein the end device comprises a secure runtime environment and the verification key (PuK; KST) is stored in the secure runtime environment, and that in the secure runtime environment further at least a part of a radio interface layer, RIL, driver (RIL driver) is implemented which is devised for communicating at hardware level between a security operating system in the secure runtime environment and the security element, and wherein a binding application (SIM Lock Trustlet) is devised for communicating within the secure runtime environment with the at least part of the RIL driver.
Panel element for lining a ceiling and/or wall, having a cover panel and having at least one retaining spring, in particular a leg spring, which can be moved from a transport position to a fastening position for the purpose of fastening the cover panel to a ceiling and/or wall preferably in a suspended manner, wherein the panel element has a retaining device for the at least one retaining spring, wherein the retaining spring is closer to a back side of the cover panel in its transport position than in its fastening position, characterized in that the retaining device is configured to fix the at least one retaining spring in its transport position under tension, wherein the retaining device, for the tensioned fixing of the at least one retaining spring in its transport position, is in the form of a counterbearing and the at least one retaining spring is fixed on the retaining device in the transport position by its inherent spring force.
An absorbent article (10, 20, 300, 500, 600) comprising an absorbent core (101, 501, 601) sandwiched between a liquid permeable topsheet (520, 620) and a liquid impermeable backsheet (521, 621), wherein the absorbent core (101, 501, 601) comprises absorbent material selected from the group consisting of cellulose fibers, superabsorbent polymers and combinations thereof, wherein said absorbent material is contained within at least one core wrap substrate enclosing said absorbent material, and wherein a top layer of said core wrap is adhered to a bottom layer of said core wrap to form one or more channels substantially free of said absorbent material, wherein said channels have a length extending along a longitudinal axis and the absorbent core (101, 501, 601) has a length extending along said longitudinal axis and wherein the length of said channels is from 10% to 95% of the length of said absorbent core (101, 501, 601) such that each said channels are circumscribed by absorbent material characterized in that said top layer of the core wrap is in direct contact with the topsheet, and in that said top layer of the core wrap comprises a spunbond nonwoven.
A method for an automated provision of a monitoring function for a machining process to be executed by a machine tool (150, 250), the method comprising the following steps: a. analyzing a computer-aided manufacturing, CAM, program (240, 400) of the machining process by means of a postprocessor in order to determine processing steps to be monitored; and b. inserting at least one monitoring instruction (1310, 1320, 1330, 1340) into a control program (270, 1300) of the machine tool (150, 250) by means of the postprocessor which is executed during the machining process. a. analyzing a computer-aided manufacturing, CAM, program (240, 400) of the machining process by means of a postprocessor in order to determine processing steps to be monitored; and b. inserting at least one monitoring instruction (1310, 1320, 1330, 1340) into a control program (270, 1300) of the machine tool (150, 250) by means of the postprocessor which is executed during the machining process.
An implant assembly for a hindfoot, comprising: a nail, the nail comprising a proximal portion, a distal portion, and a central longitudinal axis, the distal portion of the nail having at least a first angled, at least partially threaded fastener-receiving hole and a second angled, at least partially threaded fastener-receiving hole, each having an axis (160, 162) which is at an angle with respect to the central axis; wherein the nail comprises a third fastener-receiving hole which is at least partially threaded and which has an axis that is substantially perpendicular to the central longitudinal axis; and wherein the assembly further comprises first and second fasteners; characterised in that the first fastener is adapted to be received by the nail and achieve at least partial purchase into a patient's calcaneus and cuboid bones and the second fastener is adapted to be received by the nail and achieve at least partial purchase into a patient's calcaneus and talus bones. a nail, the nail comprising a proximal portion, a distal portion, and a central longitudinal axis, the distal portion of the nail having at least a first angled, at least partially threaded fastener-receiving hole and a second angled, at least partially threaded fastener-receiving hole, each having an axis (160, 162) which is at an angle with respect to the central axis; wherein the nail comprises a third fastener-receiving hole which is at least partially threaded and which has an axis that is substantially perpendicular to the central longitudinal axis; and wherein the assembly further comprises first and second fasteners; characterised in that
A FASTENING DEVICE which comprises a clip and a retaining element which are made of any suitable material and used for mounting self-supporting parts for the internal trim of vehicles and/or accessories for the panels thereof, it being possible to fasten another object where required, in which said clip in the rest condition has a form with a general arch-shaped and/or conical configuration, being provided with a head or rounded central surface from where both lateral wings for fastening to the panel as well as resilient lugs for fastening the retaining element to said clip extend laterally, said retaining element having an internal cavity for disassembling the clip, said device being configured for assembly with said retaining element inside said clip providing temporary fastening of said retaining element in said clip, so as to be inserted in this state inside a mounting hole or opening where final fastening of the device to the vehicle panel is performed, CHARACTERIZED IN THAT said resilient lugs have a fold from which they extend so as to form inner wings which are provided with an opening inside which, upon insertion of said retaining element, projections thereof engage.
A cognitive-driver-assist system, said system comprising: an object-detection device operable to detect when an object is proximate to a host-vehicle; an operator-detection device operable to determine when an operator of the host-vehicle is aware of the object; and a controller configured to output a warning-signal for the operator of the host-vehicle when the object-detection device detects the object, said warning-signal having a warning-intensity that is variable, wherein the controller is configured to increase the warning-intensity when the operator is not aware of the object, characterized in that the object is a traffic-signal for a travel-path of the host-vehicle, the controller is further configured to estimate a time-to-violation of the traffic-signal by the host-vehicle, and increase the warning-intensity when the time-to-violation is less than a time-threshold and the operator is not aware of the object. an object-detection device operable to detect when an object is proximate to a host-vehicle; an operator-detection device operable to determine when an operator of the host-vehicle is aware of the object; and a controller configured to output a warning-signal for the operator of the host-vehicle when the object-detection device detects the object, said warning-signal having a warning-intensity that is variable, wherein the controller is configured to increase the warning-intensity when the operator is not aware of the object, characterized in that the object is a traffic-signal for a travel-path of the host-vehicle, the controller is further configured to estimate a time-to-violation of the traffic-signal by the host-vehicle, and increase the warning-intensity when the time-to-violation is less than a time-threshold and the operator is not aware of the object.
A rotor blade assembly for a wind turbine, the rotor blade assembly comprising: a rotor blade extending lengthwise between a root and a tip, the rotor blade including a pressure side and a suction side extending between a leading edge and a trailing edge; and a chord extender (104, 106) extending spanwise between an inboard edge and an outboard edge for elongating the chord length of the rotor blade in order to enhance the operational efficiency thereof, the chord extender (104,106) including an attachment portion coupled to at least one of the pressure side or the suction side and an extension portion extending outwardly from the attachment portion beyond the trailing edge, the extension portion extending chordwise between a first end disposed adjacent to the trailing edge and a second end disposed opposite the first end, the extension portion including a surface defined between the first and second ends, the extension portion further including at least one stiffening rib projecting outwardly from the surface of the extension portion configured to provide stiffness and rigidity to the chord extender, wherein the at least one stiffening rib extends lengthwise along the surface of the extension portion between a first rib end and a second rib end, the first rib end being disposed directly adjacent to the trailing edge and wherein an end face of the first rib end is configured to be engaged against the trailing edge of the rotor blade when an aerodynamic load is applied against the extension portion, characterised in that the second end of the extension portion defines a straight outer edge extending from the inboard edge to the outboard edge. a rotor blade extending lengthwise between a root and a tip, the rotor blade including a pressure side and a suction side extending between a leading edge and a trailing edge; and a chord extender (104, 106) extending spanwise between an inboard edge and an outboard edge for elongating the chord length of the rotor blade in order to enhance the operational efficiency thereof, the chord extender (104,106) including an attachment portion coupled to at least one of the pressure side or the suction side and an extension portion extending outwardly from the attachment portion beyond the trailing edge, the extension portion extending chordwise between a first end disposed adjacent to the trailing edge and a second end disposed opposite the first end, the extension portion including a surface defined between the first and second ends, the extension portion further including at least one stiffening rib projecting outwardly from the surface of the extension portion configured to provide stiffness and rigidity to the chord extender, wherein the at least one stiffening rib extends lengthwise along the surface of the extension portion between a first rib end and a second rib end, the first rib end being disposed directly adjacent to the trailing edge and wherein an end face of the first rib end is configured to be engaged against the trailing edge of the rotor blade when an aerodynamic load is applied against the extension portion,
A method for estimating a geographical position of a point of interest, the method comprising: - marking a point of interest on an identified object of interest on a digital image, acquired by the first communication device; - acquiring, by processing image data of the digital image, estimates of a first relative distance between, and a direction from the first communication device to the point of interest, by estimating the height of the object of interest; - acquiring complementary data, suitable for estimating at least one second relative distance between, and a second direction from a respective second communication device to the point of interest, wherein the at least one second communication device has been determined based on the estimated first relative distance and direction, and - acquiring an estimate of a geographical position of the point of interest, based on the estimates of the first relative distance and direction and the acquired complementary data. - marking a point of interest on an identified object of interest on a digital image, acquired by the first communication device; - acquiring, by processing image data of the digital image, estimates of a first relative distance between, and a direction from the first communication device to the point of interest, by estimating the height of the object of interest; - acquiring complementary data, suitable for estimating at least one second relative distance between, and a second direction from a respective second communication device to the point of interest, wherein the at least one second communication device has been determined based on the estimated first relative distance and direction, and - acquiring an estimate of a geographical position of the point of interest, based on the estimates of the first relative distance and direction and the acquired complementary data.
A rotor stack assembly (25; 125) for a gas turbine engine, comprising: a first rotor assembly (26;126A) having a first airfoil, a first rim (38;138A), a first bore (40;140A) and a first web (42;142A) that extends between said first rim (38;138A) and said first bore (40;140A); a second rotor assembly (26;126B) aft of said first rotor assembly (26;126A) and having a second airfoil, a second rim (38;138B), a second bore (40;140B) and a second web (42;142B) that extends between said second rim (38;138B) and said second bore (42; 142B); a tie shaft (47;147) extending through the rotor stack assembly and positioned radially inward of said first bore (40;140A) and said second bore (40;140B), wherein said tie shaft (47;147) is preloaded to maintain a compressive load on said first rotor assembly (26;126A) and said second rotor assembly (26;126B), said compressive load is communicated through a first load path (LP;LP1) of said first rotor assembly (26;126A) and a second load path (LP;LP2) of said second rotor assembly (26;126B), wherein said first load path (LP;LP1) and said second load path (LP;LP2) are radially inboard of said first rim (38;138A) and said second rim (38; 138B), respectively, the rotor stack assembly characterized in that said tie shaft (47, 147) is threaded through a forward hub and snapped into an aft hub; said first airfoil is configured as an integrally bladed airfoil of said first rotor assembly (26; 126A); and said second airfoil is configured as a separate bladed airfoil received within a slot of said second rim (38;138B). a first rotor assembly (26;126A) having a first airfoil, a first rim (38;138A), a first bore (40;140A) and a first web (42;142A) that extends between said first rim (38;138A) and said first bore (40;140A); a second rotor assembly (26;126B) aft of said first rotor assembly (26;126A) and having a second airfoil, a second rim (38;138B), a second bore (40;140B) and a second web (42;142B) that extends between said second rim (38;138B) and said second bore (42; 142B); a tie shaft (47;147) extending through the rotor stack assembly and positioned radially inward of said first bore (40;140A) and said second bore (40;140B), wherein said tie shaft (47;147) is preloaded to maintain a compressive load on said first rotor assembly (26;126A) and said second rotor assembly (26;126B), said compressive load is communicated through a first load path (LP;LP1) of said first rotor assembly (26;126A) and a second load path (LP;LP2) of said second rotor assembly (26;126B), wherein said first load path (LP;LP1) and said second load path (LP;LP2) are radially inboard of said first rim (38;138A) and said second rim (38; 138B), respectively, the rotor stack assembly characterized in that said tie shaft (47, 147) is threaded through a forward hub and snapped into an aft hub; said first airfoil is configured as an integrally bladed airfoil of said first rotor assembly (26; 126A); and said second airfoil is configured as a separate bladed airfoil received within a slot of said second rim (38;138B).
Air spring bellows of an air spring, which air spring bellows can be fastened sealingly by way of its two open ends to connector parts (3, 4) of two components which are spaced apart from one another, and which air spring bellows, in the mounted state of the air spring, at least partially delimits a working space which is filled with compressed air, the two open ends of the air spring bellows being configured as beads (6, 10), in which in each case one annular core (7, 11) is arranged, and in the case of which air spring bellows the cores (7, 10) are connected to a woven-fabric reinforcement material which is embedded in an elastic bellows material, characterized in that the reinforcement material is turned over on itself over the entire bellows wall of the air spring bellows, as a result of which the cores (7, 11) in the beads (6, 10) are enclosed completely by the reinforcement material, and in that the two free ends (17a, 17b) of the reinforcement material are brought together and connected to one another.
A light source device comprising: a first light source (70, 70A) that is configured to emit excitation light; a second rotatable light source that includes a fluorescent area configured to emit fluorescent light by being irradiated with the excitation light; and a dichroic mirror that is disposed on an emission side of the second rotatable Z light source and that is configured to reflect the excitation light towards the second light source while transmitting the fluorescent light, wherein an intersection of the optical axis of the first light source (70, 70A) and the dichroic rotatable mirror is apart from the center of the optical axis of the second light source, and the second rotatable light source further includes a diffuse reflection area configured to diffuse and reflect the excitation light. a first light source (70, 70A) that is configured to emit excitation light; a second rotatable light source that includes a fluorescent area configured to emit fluorescent light by being irradiated with the excitation light; and a dichroic mirror that is disposed on an emission side of the second rotatable Z light source and that is configured to reflect the excitation light towards the second light source while transmitting the fluorescent light, wherein an intersection of the optical axis of the first light source (70, 70A) and the dichroic rotatable mirror is apart from the center of the optical axis of the second light source, and the second rotatable light source further includes a diffuse reflection area configured to diffuse and reflect the excitation light.
A combined luminaire and air conditioning nozzle, including: - a front panel with an opening, - a nozzle frame pivotably connected to the opening of the front panel and arranged to separate an air cavity located behind the front panel from a front side of the front panel, - a controller element with a closing mechanism mechanically coupled thereto and arranged to adjustably limit an air passage from the air cavity to the front side of the front panel in response to a movement of the controller element, - a luminaire element that is provided with a light source arranged to output light to the front side of the front panel, characterized in that - said luminaire element forms part of the closing mechanism, and - the closing mechanism is arranged to convert a movement of the controller element into a movement of the luminaire element, so that said adjustable limiting of the air passage occurs as a result of said movement of the luminaire element. - a front panel with an opening, - a nozzle frame pivotably connected to the opening of the front panel and arranged to separate an air cavity located behind the front panel from a front side of the front panel, - a controller element with a closing mechanism mechanically coupled thereto and arranged to adjustably limit an air passage from the air cavity to the front side of the front panel in response to a movement of the controller element, - a luminaire element that is provided with a light source arranged to output light to the front side of the front panel, characterized in that - said luminaire element forms part of the closing mechanism, and - the closing mechanism is arranged to convert a movement of the controller element into a movement of the luminaire element, so that said adjustable limiting of the air passage occurs as a result of said movement of the luminaire element.
Method of manufacturing a graphite bipolar plate for a fuel cell or flow battery, comprising: providing a pair of graphite monopolar plates and bonding the monopolar plates along opposing contact faces of the monopolar plates, characterised in that a 1C epoxy resin is used for bonding, and the 1C epoxy resin is adapted to have an activation temperature of at least 50°C by using aromatic amines, which act as solid hardeners, as hardeners. providing a pair of graphite monopolar plates and bonding the monopolar plates along opposing contact faces of the monopolar plates, characterised in that a 1C epoxy resin is used for bonding, and the 1C epoxy resin is adapted to have an activation temperature of at least 50°C by using aromatic amines, which act as solid hardeners, as hardeners.