mhurhangee/patent-ind-claim-en huggingface dataset:
A releasably attachable gravity-fed spray gun spray head assembly comprising a liquid port for connection to a gravity-fed spray gun paint reservoir; a liquid nozzle opening for spraying a liquid; a liquid inlet passage that is fed through the liquid port and from which liquid enters a liquid passageway ; characterized in that the spray gun spray head assembly further comprises a connection tab formed in a barrel frame to assist in connection of the spray head assembly to a gravity-fed spray gun platform, wherein the connection tab comprises a lever element .
A brake pad for brake disc, which comprises: - a support plate for receiving a friction lining, with the support plate having: o a first surface (1.1), a second surface (1.2) and at least one hole that extends from the first surface (1.1) to the second surface (1.2); - at least one counterweight rigidly connected to the support plate to modify the vibration of the support plate , with the counterweight having: ∘ a first face facing the first surface (1.1); and ∘ a protrusion that projects from the first face and has a free end , with the protrusion being inserted into the hole ; characterised in that it also comprises: - at least one groove in the second surface (1.2) of the support plate in a region near the hole and extending from the hole ; wherein the protrusion is partially housed in the groove , and wherein the hole has a circular cross-section. - a support plate for receiving a friction lining, with the support plate having: o a first surface (1.1), a second surface (1.2) and at least one hole that extends from the first surface (1.1) to the second surface (1.2); - at least one counterweight rigidly connected to the support plate to modify the vibration of the support plate , with the counterweight having: ∘ a first face facing the first surface (1.1); and ∘ a protrusion that projects from the first face and has a free end , with the protrusion being inserted into the hole ; ∘ a first face facing the first surface (1.1); and ∘ a protrusion that projects from the first face and has a free end , with the protrusion being inserted into the hole ; - at least one groove in the second surface (1.2) of the support plate in a region near the hole and extending from the hole ;
Foodstuffs packaging container with an inner part and an outer part , wherein the inner part forms a shell-shaped or mug-shaped container and the outer part at least partially envelopes the inner part wherein the inner part is produced in one piece from a mouldable, i.e. thermomouldable and/or deep-drawable material, wherein the material for this is provided from a single or multi-layered material containing at least a proportion of recycled raw materials, wherein at least one proportion can be provided from renewable and/or biodegradable materials and that the outer part encompasses at least the circumference of the inner part and is produced from a renewable and/or biodegradable and/or recyclable material, wherein preferably fibrous materials can be provided, characterised in that in the inner part, the recycled material is covered with an inner layer of new plastic material and the layer of recycled material together with the inner layer form the inner part, that the inner part is retained and reinforced by the outer part and that the inner part is formed from a polymer, comprising, in particular, PS, PE, PP, PET, PVC, starch polymers, polylactic acids or other natural or synthetic polymers in single or multi-layered layers as well as in combination with barrier layers, lacquers or similar and, at least in one layer, a proportion of a recycled plastic material, containing preferably R-PET, R-PP or R-PS such that at least one edge of the outer part can be sealed and/or be protected so that it can be impervious to moisture, liquid, and/or grease wherein this sealing can be created by layering, coating and/or folding over.
A rotary cutting tool comprising: a base material including a head portion , a body portion , and a shoulder portion defining a boundary portion between the head portion and the body portion ; a first diamond layer covering the body portion and the shoulder portion and exposing the head portion ; and a second diamond layer covering the head portion and not covering the body portion , characterized in that the second diamond layer is provided on the first diamond layer in the shoulder portion . a base material including a head portion , a body portion , and a shoulder portion defining a boundary portion between the head portion and the body portion ; a first diamond layer covering the body portion and the shoulder portion and exposing the head portion ; and a second diamond layer covering the head portion and not covering the body portion , characterized in that the second diamond layer is provided on the first diamond layer in the shoulder portion .
Rotor blade for a wind power installation , having a rotor blade length, having a profile depth established between a leading edge and a trailing edge , and having a profile thickness established between a suction side and a pressure side , - wherein the rotor blade has a trailing edge region , which adjoins the trailing edge and extends with a region extent of less than 20%, in particular less than 10%, of the profile depth in the direction of the leading edge , - wherein the trailing edge region has at least one acoustic opening , characterized in that at least one section of the trailing edge region is formed by a suction-side trailing edge element and a pressure-side trailing edge element , which are arranged adjacent to one another in the direction of the profile thickness, and wherein at least one of the trailing edge elements and/or a screen between the trailing edge elements are/is arranged movably, and preferably the at least one acoustic opening is formed by a suction-side passage opening in the suction-side trailing edge element and by a pressure-side passage opening in the pressure-side trailing edge element, - wherein the at least one acoustic opening is open in an open position of the movably arranged trailing edge element and is substantially closed in a closed position of the movably arranged trailing edge element, and/or - the at least one acoustic opening is open in an open position of the screen and is substantially closed in a closed position of the screen. - wherein the rotor blade has a trailing edge region , which adjoins the trailing edge and extends with a region extent of less than 20%, in particular less than 10%, of the profile depth in the direction of the leading edge , - wherein the trailing edge region has at least one acoustic opening , characterized in that at least one section of the trailing edge region is formed by a suction-side trailing edge element and a pressure-side trailing edge element , which are arranged adjacent to one another in the direction of the profile thickness, and wherein at least one of the trailing edge elements and/or a screen between the trailing edge elements are/is arranged movably, and preferably the at least one acoustic opening is formed by a suction-side passage opening in the suction-side trailing edge element and by a pressure-side passage opening in the pressure-side trailing edge element, - wherein the at least one acoustic opening is open in an open position of the movably arranged trailing edge element and is substantially closed in a closed position of the movably arranged trailing edge element, and/or - the at least one acoustic opening is open in an open position of the screen and is substantially closed in a closed position of the screen.
A method of determining a total mass of an aircraft comprising: determining an acceleration of a pushback vehicle while moving the aircraft ; determining a pushback force applied by the pushback vehicle while moving the aircraft ; and determining the total mass of the aircraft based on the pushback force, the acceleration of the pushback vehicle , and a coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves; wherein determining the acceleration of the pushback vehicle while moving the aircraft comprises determining a first acceleration, and wherein determining the pushback force applied by the pushback vehicle while moving the aircraft comprises determining a first pushback force, and wherein the method further comprises: applying a known mass to the aircraft ; determining a second acceleration of the pushback vehicle while moving the aircraft with the known mass; determining a second pushback force applied by the pushback vehicle while moving the aircraft with the known mass; and determining the coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves based on the known mass, the first acceleration, the first pushback force, the second acceleration, and the second pushback force. determining an acceleration of a pushback vehicle while moving the aircraft ; determining a pushback force applied by the pushback vehicle while moving the aircraft ; and determining the total mass of the aircraft based on the pushback force, the acceleration of the pushback vehicle , and a coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves; wherein determining the acceleration of the pushback vehicle while moving the aircraft comprises determining a first acceleration, and wherein determining the pushback force applied by the pushback vehicle while moving the aircraft comprises determining a first pushback force, and wherein the method further comprises: applying a known mass to the aircraft ; determining a second acceleration of the pushback vehicle while moving the aircraft with the known mass; determining a second pushback force applied by the pushback vehicle while moving the aircraft with the known mass; and determining the coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves based on the known mass, the first acceleration, the first pushback force, the second acceleration, and the second pushback force. applying a known mass to the aircraft ; determining a second acceleration of the pushback vehicle while moving the aircraft with the known mass; determining a second pushback force applied by the pushback vehicle while moving the aircraft with the known mass; and determining the coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves based on the known mass, the first acceleration, the first pushback force, the second acceleration, and the second pushback force.
A brake assembly including an operating shaft configured to rotate about a first axis to actuate a brake, the first axis being defined by a body of the brake, the operating shaft including a convex bearing surface being arcuate and defining a second axis parallel to and offset from the first axis, a yoke having an arcuate concave bearing surface, the yoke being configured to move linearly relative to the body as the operating shaft rotates about the first axis, a rotating element bearing having a plurality of rotating elements retained by a cage , the cage having a first arcuate portion having a first array of apertures for receiving some of the plurality of rotating elements, the cage having a second arcuate portion having a second array of apertures for receiving some of the plurality of rotating elements, the rotating element bearing being positioned between the convex bearing surface and the concave bearing surface such that the rotating element bearing is configured to move relative to the operating shaft and relative to the yoke during actuation of the brake, characterised in that the first arcuate portion is connected to the second arcuate portion by a single elongate connecting portion .
An electronic device , comprising: a first electrode (SP1) comprising a first boundary side (SP1_BS) extending in a predetermined direction (DR3); a second electrode (SP2) comprising a second boundary side (SP2 BS) extending in the predetermined direction (DR3) and facing the first boundary side (SP1_BS), the second electrode (SP2) being spaced apart from the first electrode (SP1) in an intersecting direction (DR4) crossing the predetermined direction (DR3) and being electrically disconnected from the first electrode (SP1); and a third electrode (IMP) disposed between the first boundary side (SP1_BS) and the second boundary side (SP2 BS), and spaced apart from the first electrode (SP1) and the second electrode (SP2), the third electrode (IMP) comprising a first side (S1) facing the first boundary side (SP1_BS) and a second side (S2) facing the second boundary side (SP2_BS) at least one of the first side (S1) and the second side (S2) comprises a plurality of protruding patterns (RP-S1, RP-S2) spaced apart from each other in the predetermined direction (DR3); the first side (S1) and the second side (S2) have shapes that are asymmetric to each other with respect to a center axis (CX) extending in the predetermined direction (DR3) and the third electrode (IMP) is a floating electrode. a first electrode (SP1) comprising a first boundary side (SP1_BS) extending in a predetermined direction (DR3); a second electrode (SP2) comprising a second boundary side (SP2 BS) extending in the predetermined direction (DR3) and facing the first boundary side (SP1_BS), the second electrode (SP2) being spaced apart from the first electrode (SP1) in an intersecting direction (DR4) crossing the predetermined direction (DR3) and being electrically disconnected from the first electrode (SP1); and a third electrode (IMP) disposed between the first boundary side (SP1_BS) and the second boundary side (SP2 BS), and spaced apart from the first electrode (SP1) and the second electrode (SP2), the third electrode (IMP) comprising a first side (S1) facing the first boundary side (SP1_BS) and a second side (S2) facing the second boundary side (SP2_BS) at least one of the first side (S1) and the second side (S2) comprises a plurality of protruding patterns (RP-S1, RP-S2) spaced apart from each other in the predetermined direction (DR3); the first side (S1) and the second side (S2) have shapes that are asymmetric to each other with respect to a center axis (CX) extending in the predetermined direction (DR3) and the third electrode (IMP) is a floating electrode. at least one of the first side (S1) and the second side (S2) comprises a plurality of protruding patterns (RP-S1, RP-S2) spaced apart from each other in the predetermined direction (DR3); the first side (S1) and the second side (S2) have shapes that are asymmetric to each other with respect to a center axis (CX) extending in the predetermined direction (DR3) and the third electrode (IMP) is a floating electrode.
A cathode mixture comprising: a cathode active material including one or more composite oxides of: a metal of cobalt, manganese, nickel; and lithium; and a cathode additive of which the whole composition is represented by the following Chemical Formula 1, and wherein the cathode additive is included in the content of 1 to 30 wt%, based on the total weight of the mixture (100 wt%): [Chemical Formula 1] { x (Li 2+a Ni b M 1-b O 2+c )}·{ y (NiO)} ·{ z (Li 2 O)} wherein, in Chemical Formula 1, M is one or more metal atoms forming a divalent cation or a trivalent cation, -0.2<a<0.2, b=1.0, -0.2<c<0.2, 0.7≤x<1.0, 0<y≤0.15, 0<z≤0.15, and x+y+z=1. a cathode active material including one or more composite oxides of: a metal of cobalt, manganese, nickel; and lithium; and a cathode additive of which the whole composition is represented by the following Chemical Formula 1, and wherein the cathode additive is included in the content of 1 to 30 wt%, based on the total weight of the mixture (100 wt%): [Chemical Formula 1] { x (Li 2+a Ni b M 1-b O 2+c )}·{ y (NiO)} ·{ z (Li 2 O)} wherein, in Chemical Formula 1, M is one or more metal atoms forming a divalent cation or a trivalent cation, -0.2<a<0.2, b=1.0, -0.2<c<0.2, 0.7≤x<1.0, 0<y≤0.15, 0<z≤0.15, and x+y+z=1.
Method for operating a vehicle information system comprising at least a first display area and a second display area , in which method: an activation signal and a transition signal are received in succession; graphical data for an activation animation containing a first view and a second view is generated on the basis of the activation signal and the transition signal and displayed by the first display area and second display area ; wherein after the activation signal has been received, an appearing of the first view is output; wherein the first view comprises a first graphical object ; and after the transition signal has been received, a disappearing of the first view and an appearing of the second view are output; wherein the appearing of the second view comprises a movement effect, wherein said movement effect depicts a movement from the first display area to the second display area , characterized in that the transition signal is received when an approach action, an unlocking action, a door-opening, a user entering or sitting down or a vehicle being started is detected. an activation signal and a transition signal are received in succession; graphical data for an activation animation containing a first view and a second view is generated on the basis of the activation signal and the transition signal and displayed by the first display area and second display area ; wherein after the activation signal has been received, an appearing of the first view is output; wherein the first view comprises a first graphical object ; and after the transition signal has been received, a disappearing of the first view and an appearing of the second view are output; wherein the appearing of the second view comprises a movement effect, wherein said movement effect depicts a movement from the first display area to the second display area , characterized in that the transition signal is received when an approach action, an unlocking action, a door-opening, a user entering or sitting down or a vehicle being started is detected.
A metering apparatus comprising: a microcomputer (MCU) ; a transceiver unit coupled to the MCU , the transceiver unit to provide power line communication (PLC); memory coupled to the MCU , the memory to store data; a communication device coupled to the MCU ; analog transducers coupled to the MCU , the analog transducers to supply real time data to the MCU ; an electronically operated relay coupled to the MCU , the electronically operated relay to disconnect the line outputs from a meter, wherein the meter includes the metering apparatus; a battery coupled to the MCU , the battery to provide power to the MCU for powering a portion of a functionality of the MCU when a main power supply is turned off; characterized by cold start interrupt circuitry coupled to the MCU , the cold start interrupt circuitry to change a mode of operation of the metering apparatus between a stop mode and a normal mode, wherein all clocks used by the MCU are turned off and the battery is to provide power to the MCU when the metering apparatus is in the stop mode, and wherein the MCU generates a real-time clock when the metering apparatus is in normal mode. a microcomputer (MCU) ; a transceiver unit coupled to the MCU , the transceiver unit to provide power line communication (PLC); memory coupled to the MCU , the memory to store data; a communication device coupled to the MCU ; analog transducers coupled to the MCU , the analog transducers to supply real time data to the MCU ; an electronically operated relay coupled to the MCU , the electronically operated relay to disconnect the line outputs from a meter, wherein the meter includes the metering apparatus; a battery coupled to the MCU , the battery to provide power to the MCU for powering a portion of a functionality of the MCU when a main power supply is turned off; characterized by cold start interrupt circuitry coupled to the MCU , the cold start interrupt circuitry to change a mode of operation of the metering apparatus between a stop mode and a normal mode, wherein all clocks used by the MCU are turned off and the battery is to provide power to the MCU when the metering apparatus is in the stop mode, and wherein the MCU generates a real-time clock when the metering apparatus is in normal mode.
Electrically rechargeable redox flow battery having a first chamber and a second chamber , wherein the first chamber is separated from the second chamber by means of a membrane , wherein the first chamber comprises a cathode and the second chamber comprises an anode and wherein a first planar surface of the cathode and/or a second planar surface of the anode has raised regions to enlarge the surface area and these raised regions are suitable for forming flow channels for a first and/or second electrolyte of the redox flow battery , wherein the cathode and/or the anode comprise at least one first material comprising lead or bismuth, wherein the first material comprises lead or bismuth in a proportion by weight of at least 20%.
A respiratory apparatus comprising: a blower driven by a motor to generate a flow of breathable gas, at least one sensor (4270; 4272; 4274; 4276; 4278) configured to provide at least one input signal indicative of at least one of a physical and system parameter, a microprocessor configured to provide executable instructions to control the motor, and characterized in that the respiratory apparatus further comprises: a fault mitigation integrated circuit separate from the microprocessor and in communication with the motor and the microprocessor, the fault mitigation integrated circuit configured to: receive the at least one input signal from the at least one sensor, detect a fault based on the received at least one input signal, and generate an output signal to stop the motor based on the detected fault, wherein the fault mitigation integrated circuit is configured to monitor a motor current and/or a motor bus voltage. a blower driven by a motor to generate a flow of breathable gas, at least one sensor (4270; 4272; 4274; 4276; 4278) configured to provide at least one input signal indicative of at least one of a physical and system parameter, a microprocessor configured to provide executable instructions to control the motor, and characterized in that the respiratory apparatus further comprises: a fault mitigation integrated circuit separate from the microprocessor and in communication with the motor and the microprocessor, the fault mitigation integrated circuit configured to: receive the at least one input signal from the at least one sensor, detect a fault based on the received at least one input signal, and generate an output signal to stop the motor based on the detected fault, wherein the fault mitigation integrated circuit is configured to monitor a motor current and/or a motor bus voltage. a fault mitigation integrated circuit separate from the microprocessor and in communication with the motor and the microprocessor, the fault mitigation integrated circuit configured to: receive the at least one input signal from the at least one sensor, detect a fault based on the received at least one input signal, and generate an output signal to stop the motor based on the detected fault, receive the at least one input signal from the at least one sensor, detect a fault based on the received at least one input signal, and generate an output signal to stop the motor based on the detected fault, wherein the fault mitigation integrated circuit is configured to monitor a motor current and/or a motor bus voltage.