mhurhangee/patent-ind-claim-en huggingface dataset:
An insect trap comprising: a trap portion including an enclosure having an adhesive surface and a first opening , wherein the adhesive surface is at least partially contained within the enclosure and is configured to adhere to an insect; and a base portion including a lighting element and a mounting portion, wherein the lighting element is configured to provide light to the trap portion, and wherein the mounting portion is configured to communicate with and receive power from a power source; and a first heating element in communication with the power source, wherein the trap portion is configured to removably engage with the base portion and receive light from the base portion when engaged therewith, and wherein the first heating element provides heat to at least a portion of the trap when the trap is engaged; characterized in that the enclosure comprises: a front housing portion having a first internal surface; and a rear housing portion having a second internal surface, wherein the front housing portion and rear housing portion are matingly engaged with each other to form the enclosure; and wherein at least one of the first or second internal surfaces is configured to manipulate light, and wherein the base portion comprises: an opening , the opening configured to allow light to emit from the base portion to the enclosure such that the light diverges over substantially the second internal surface . a trap portion including an enclosure having an adhesive surface and a first opening , wherein the adhesive surface is at least partially contained within the enclosure and is configured to adhere to an insect; and a base portion including a lighting element and a mounting portion, wherein the lighting element is configured to provide light to the trap portion, and wherein the mounting portion is configured to communicate with and receive power from a power source; and a first heating element in communication with the power source, wherein the trap portion is configured to removably engage with the base portion and receive light from the base portion when engaged therewith, and wherein the first heating element provides heat to at least a portion of the trap when the trap is engaged; a front housing portion having a first internal surface; and a rear housing portion having a second internal surface, wherein the front housing portion and rear housing portion are matingly engaged with each other to form the enclosure; and wherein at least one of the first or second internal surfaces is configured to manipulate light, and wherein the base portion comprises: an opening , the opening configured to allow light to emit from the base portion to the enclosure such that the light diverges over substantially the second internal surface .
A Controller Area Network, CAN, transceiver comprising: A receiver configured to determine a voltage differential signal from analog signaling received from a CAN bus and configured to provide a digital output signal at a receiver output to a CAN controller based on the voltage differential signal, wherein the analog signaling received from the CAN bus is capable of operating in accordance with a first defined voltage level scheme of a first CAN protocol and a second defined voltage level scheme for a second CAN protocol, the receiver comprising: a first comparator configured to compare the voltage differential signal to a first threshold (Thresh 2) which is set to a value which differentiates between a logic low bit and logic high bit in accordance with the second CAN protocol; and a second comparator configured to compare the voltage differential signal to a second threshold (Thresh 3), wherein the second threshold is less than the first threshold; a filtering circuitry configured to detect noise on the CAN bus based on an output of the first comparator and an output of the second comparator; the filtering circuitry configured to filter the output of the first comparator in response to detecting noise on the CAN bus, such that the first comparator provides a first digital signal indicative of activity on the CAN bus in accordance with the second CAN protocol; and the filtering circuitry is configured to not filtering the output of the first comparator in response to not detecting noise on the CAN bus, such that the first comparator provides the first digital signal as an output of the first comparator. a first comparator configured to compare the voltage differential signal to a first threshold (Thresh 2) which is set to a value which differentiates between a logic low bit and logic high bit in accordance with the second CAN protocol; and a second comparator configured to compare the voltage differential signal to a second threshold (Thresh 3), wherein the second threshold is less than the first threshold; a filtering circuitry configured to detect noise on the CAN bus based on an output of the first comparator and an output of the second comparator; the filtering circuitry configured to filter the output of the first comparator in response to detecting noise on the CAN bus, such that the first comparator provides a first digital signal indicative of activity on the CAN bus in accordance with the second CAN protocol; and the filtering circuitry is configured to not filtering the output of the first comparator in response to not detecting noise on the CAN bus, such that the first comparator provides the first digital signal as an output of the first comparator.
A method comprising: receiving, by a computer, at least one image or video frame; for a color space of the at least one image or video frame, partitioning, by the computer, the color space in M 1 x M 2 x M 3 non-overlapping bins; determining for each bin whether it is a valid bin, a valid bin being a bin for which the at least one image or video frame has at least one pixel with a color value falling within said bin; for each chroma channel of the color space: calculating, based on, for each non-overlapping bin, a required number of codewords necessary to observe a difference in color in said non-overlapping bin, by the computer and for each valid bin, a required number of codewords necessary for the respective chroma channel to represent, without a noticeable difference, two color values in said valid bin that have consecutive codewords for the respective chroma channel; generating, by the computer, at least one content-aware chroma forward reshaping function, based on the calculated required numbers of codewords; applying, by the computer, the at least one content-aware chroma forward reshaping function to the at least one image or video frame. receiving, by a computer, at least one image or video frame; for a color space of the at least one image or video frame, partitioning, by the computer, the color space in M 1 x M 2 x M 3 non-overlapping bins; determining for each bin whether it is a valid bin, a valid bin being a bin for which the at least one image or video frame has at least one pixel with a color value falling within said bin; for each chroma channel of the color space: calculating, based on, for each non-overlapping bin, a required number of codewords necessary to observe a difference in color in said non-overlapping bin, by the computer and for each valid bin, a required number of codewords necessary for the respective chroma channel to represent, without a noticeable difference, two color values in said valid bin that have consecutive codewords for the respective chroma channel; generating, by the computer, at least one content-aware chroma forward reshaping function, based on the calculated required numbers of codewords;
System for utilizing process heat for at least one heating process, comprising a burner , in particular a gas burner, for generating heat, comprising at least one process unit for using a first portion of the heat generated by the burner , and comprising at least one heat exchanger for transporting the first portion of the heat generated by the burner to the process unit , characterized in that the system has at least one high-temperature fuel cell system which can be heated to an operating temperature by a second portion of the heat generated by the burner .
A developing cartridge comprising: a casing configured to accommodate developing agent therein, the casing including one end portion and another end portion spaced apart from the one end portion in a first direction; a developing roller rotatable about a developing roller axis extending in the first direction; and a first cam positioned at the one end portion of the casing , the first cam being movable relative to the casing and the developing roller in the first direction between a first position and a second position, the first cam in the second position being positioned closer to the another end portion of the casing in the first direction than the first cam in the first position is to the another end portion of the casing ; a second cam positioned at the another end portion of the casing , the second cam being movable relative to the casing and the developing roller in the first direction between a third position and a fourth position, the second cam in the fourth position being positioned closer to the another end portion of the casing in the first direction than the second cam in the third position is to the another end portion of the casing ; and a connection member connecting the first cam and the second cam to each other, characterized in that the second cam is movable from the third position to the fourth position due to a tensile force of the connection member in accordance with movement of the first cam from the first position to the second position. a casing configured to accommodate developing agent therein, the casing including one end portion and another end portion spaced apart from the one end portion in a first direction; a developing roller rotatable about a developing roller axis extending in the first direction; and a first cam positioned at the one end portion of the casing , the first cam being movable relative to the casing and the developing roller in the first direction between a first position and a second position, the first cam in the second position being positioned closer to the another end portion of the casing in the first direction than the first cam in the first position is to the another end portion of the casing ; a second cam positioned at the another end portion of the casing , the second cam being movable relative to the casing and the developing roller in the first direction between a third position and a fourth position, the second cam in the fourth position being positioned closer to the another end portion of the casing in the first direction than the second cam in the third position is to the another end portion of the casing ; and a connection member connecting the first cam and the second cam to each other, characterized in that the second cam is movable from the third position to the fourth position due to a tensile force of the connection member in accordance with movement of the first cam from the first position to the second position.
An aircraft electrical actuator arrangement comprising: a plurality of electrical actuators coupled to an electrical power distribution network, the plurality of electrical actuators comprising at least one flap actuator , at least one landing gear actuator , at least one environmental control system actuator , at least one aileron actuator , at least one slat actuator , at least one thrust reverser actuator , at least one brake actuator and at least one taxiing actuator , a reconfigurable master power converter for converting electrical power from the electrical power distribution network for supply to each of the electrical actuators , and a controller coupled to the master power converter and arranged to control the reconfiguration of the master power converter to meet the individual and specific electrical power requirements of the plurality of electrical actuators , wherein the controller is further arranged to allow the supply of electrical power from the master power converter to the at least one environmental control system actuator during a first mode of operation of the aircraft , and wherein the controller is further arranged to allow the supply of electrical power from the master power converter to at least one of the at least one aileron actuator , the at least one flap actuator , the at least one slat actuator , the at least one landing gear actuator , the at least one thrust reverser actuator , the at least one brake actuator or the at least one taxiing actuator during a second mode of operation of the aircraft . a plurality of electrical actuators coupled to an electrical power distribution network, the plurality of electrical actuators comprising at least one flap actuator , at least one landing gear actuator , at least one environmental control system actuator , at least one aileron actuator , at least one slat actuator , at least one thrust reverser actuator , at least one brake actuator and at least one taxiing actuator , a reconfigurable master power converter for converting electrical power from the electrical power distribution network for supply to each of the electrical actuators , and a controller coupled to the master power converter and arranged to control the reconfiguration of the master power converter to meet the individual and specific electrical power requirements of the plurality of electrical actuators , wherein the controller is further arranged to allow the supply of electrical power from the master power converter to the at least one environmental control system actuator during a first mode of operation of the aircraft , and wherein the controller is further arranged to allow the supply of electrical power from the master power converter to at least one of the at least one aileron actuator , the at least one flap actuator , the at least one slat actuator , the at least one landing gear actuator , the at least one thrust reverser actuator , the at least one brake actuator or the at least one taxiing actuator during a second mode of operation of the aircraft .
A method for handling a radio link failure, characterized by comprising: a first base station respectively sending a first configuration message to a User Equipment, UE, and a third configuration message to a second base station ; the UE in dual-connectivity configuration receiving the first configuration message ; when a failure occurs in a first radio link of the UE, the UE sending a Radio Resource Control, RRC, connection re-establishment request message ; and in an RRC connection re-establishment process, when the UE detects that no failure occurs in a second radio link, the UE performing data transmission through the second radio link according to the first configuration message ; wherein the first radio link refers to a data transmission link established between the UE and the first base station; and the second radio link refers to a data transmission link established between the UE and the second base station; wherein the first base station is a Master eNodeB, MeNB, and the second base station is a Secondary eNodeB, SeNB; the method being further characterized by the fact that the first configuration message and the third configuration message respectively comprise a maximum allowable time for the UE to perform the data transmission with the second base station through the second radio link when the failure occurs in the first radio link of the UE with the first base station. a first base station respectively sending a first configuration message to a User Equipment, UE, and a third configuration message to a second base station ; the UE in dual-connectivity configuration receiving the first configuration message ; when a failure occurs in a first radio link of the UE, the UE sending a Radio Resource Control, RRC, connection re-establishment request message ; and in an RRC connection re-establishment process, when the UE detects that no failure occurs in a second radio link, the UE performing data transmission through the second radio link according to the first configuration message ; wherein the first radio link refers to a data transmission link established between the UE and the first base station; and the second radio link refers to a data transmission link established between the UE and the second base station; wherein the first base station is a Master eNodeB, MeNB, and the second base station is a Secondary eNodeB, SeNB; the method being further characterized by the fact that the first configuration message and the third configuration message respectively comprise a maximum allowable time for the UE to perform the data transmission with the second base station through the second radio link when the failure occurs in the first radio link of the UE with the first base station.
A self-propelled robotic work tool comprising: - a tool chassis , - a number of tool support members attached to the tool chassis and being configured to abut against a ground surface in a first plane (P1) during operation of the work tool , - a number of snap fit assemblies (s1-s4), and - a tool body attachable to the tool chassis via the number of snap fit assemblies (s1-s4), wherein the number of snap fit assemblies (s1-s4) is configured to allow movement of at least a portion the tool body relative to the tool chassis between a lowered and a raised position in directions (d1, d2) substantially perpendicular to the first plane (P1) when the tool body is attached to the tool chassis via the number of snap fit assemblies (s1-s4), characterized in that the work tool comprises a top cover attachable to the tool body through releasable attachment means , and wherein the top cover prevents access to at least one snap fit assembly (s1 - s4) of the number of snap fit assemblies (s1 - s4) when the top cover is attached to the tool body . - a tool chassis , - a number of tool support members attached to the tool chassis and being configured to abut against a ground surface in a first plane (P1) during operation of the work tool , - a number of snap fit assemblies (s1-s4), and - a tool body attachable to the tool chassis via the number of snap fit assemblies (s1-s4), wherein the number of snap fit assemblies (s1-s4) is configured to allow movement of at least a portion the tool body relative to the tool chassis between a lowered and a raised position in directions (d1, d2) substantially perpendicular to the first plane (P1) when the tool body is attached to the tool chassis via the number of snap fit assemblies (s1-s4), characterized in that the work tool comprises a top cover attachable to the tool body through releasable attachment means , and wherein the top cover prevents access to at least one snap fit assembly (s1 - s4) of the number of snap fit assemblies (s1 - s4) when the top cover is attached to the tool body . wherein the number of snap fit assemblies (s1-s4) is configured to allow movement of at least a portion the tool body relative to the tool chassis between a lowered and a raised position in directions (d1, d2) substantially perpendicular to the first plane (P1) when the tool body is attached to the tool chassis via the number of snap fit assemblies (s1-s4), characterized in that the work tool comprises a top cover attachable to the tool body through releasable attachment means , and wherein the top cover prevents access to at least one snap fit assembly (s1 - s4) of the number of snap fit assemblies (s1 - s4) when the top cover is attached to the tool body .
An accelerator comprising: a vacuum chamber comprising a beam extraction port inside said vacuum chamber; an ion source connected to said vacuum chamber and configured to inject ion beams inside said vacuum chamber at an injection point; a pair of iron cores having a central axis (C)and being arranged so as to face each other; said pair of iron cores configured to generate magnetic fields between each other; said magnetic fields configured to generate multiple annular beam turning trajectories along which the ion beams of respective different energies turn after being injected into the accelerator ; an acceleration electrode (9A-9D) configured to accelerate the ion beams; and a beam extraction path configured to extract the ion beams to the outside, characterized in that the ion source is located toward the beam extraction port with respect to the central axis (C) and is configured to inject said ion beams to a position offset to the beam extraction port, such that the gaps between the multiple annular beam turning trajectories between the ion injection point and the beam extraction port are narrower than the gaps between the multiple annular beam turning trajectories between the ion injection point and a direction passing through the ion injection point and the beam extraction port and positioned 180° opposite to the beam extraction port. a vacuum chamber comprising a beam extraction port inside said vacuum chamber; an ion source connected to said vacuum chamber and configured to inject ion beams inside said vacuum chamber at an injection point; a pair of iron cores having a central axis (C)and being arranged so as to face each other; said pair of iron cores configured to generate magnetic fields between each other; said magnetic fields configured to generate multiple annular beam turning trajectories along which the ion beams of respective different energies turn after being injected into the accelerator ; an acceleration electrode (9A-9D) configured to accelerate the ion beams; and a beam extraction path configured to extract the ion beams to the outside, characterized in that the ion source is located toward the beam extraction port with respect to the central axis (C) and is configured to inject said ion beams to a position offset to the beam extraction port, such that the gaps between the multiple annular beam turning trajectories between the ion injection point and the beam extraction port are narrower than the gaps between the multiple annular beam turning trajectories between the ion injection point and a direction passing through the ion injection point and the beam extraction port and positioned 180° opposite to the beam extraction port.