mhurhangee/patent-ind-claim-en huggingface dataset:
An airfield light comprising: a first support ; a first light source connected to the first support ; and a first baffle (46; 346) proximate the first light source , the first baffle (46; 346) including: a first generally opaque baffle body (110; 310) defining a first window having a first closed portion and a first open portion through which light emitted from the first light source may pass, and a first generally opaque baffle member (112; 312) secured to the first baffle body (110; 310) and inhibiting light emitted from the first light source from passing through the first closed portion of the first window, wherein the first generally opaque baffle member (112; 312) is removable from the first baffle body (110; 310) to create a second open portion of the first window. a first support ; a first light source connected to the first support ; and a first baffle (46; 346) proximate the first light source , the first baffle (46; 346) including: a first generally opaque baffle body (110; 310) defining a first window having a first closed portion and a first open portion through which light emitted from the first light source may pass, and a first generally opaque baffle member (112; 312) secured to the first baffle body (110; 310) and inhibiting light emitted from the first light source from passing through the first closed portion of the first window, wherein the first generally opaque baffle member (112; 312) is removable from the first baffle body (110; 310) to create a second open portion of the first window. a first generally opaque baffle body (110; 310) defining a first window having a first closed portion and a first open portion through which light emitted from the first light source may pass, and a first generally opaque baffle member (112; 312) secured to the first baffle body (110; 310) and inhibiting light emitted from the first light source from passing through the first closed portion of the first window, wherein the first generally opaque baffle member (112; 312) is removable from the first baffle body (110; 310) to create a second open portion of the first window.
A computer implemented method for pre-operatively optimizing a fit of an orthopaedic implant relative to a particular individual's anatomy, the method comprising: a. receiving information including a three-dimensional anatomic model of the individual's anatomy; b. computing a periphery of a simulated resection portion of the three dimensional anatomic model without reference to any abnormal morphology using a processor; c. identifying an orthopaedic implant model having a preliminary size for an orthopaedic implant component for use on the simulated resection surface; d. positioning the identified orthopaedic implant model relative to the simulated resection portion of three-dimensional bone model; e. generating random point sets around the peripheries of the simulated resection portion and the orthopaedic implant model; f. calculating minimum distances between point sets; g. utilizing a position optimizer to determine whether the position of the orthopaedic implant periphery relative to the simulated resection portion periphery is optimal based on the minimum distances and the orthopaedic implant model; h. determining whether the selected orthopaedic implant model results in overhang relative to the three dimensional anatomic model; and i. verifying the position of the orthopaedic implant and/or the size of the orthopaedic implant. a. receiving information including a three-dimensional anatomic model of the individual's anatomy; b. computing a periphery of a simulated resection portion of the three dimensional anatomic model without reference to any abnormal morphology using a processor; c. identifying an orthopaedic implant model having a preliminary size for an orthopaedic implant component for use on the simulated resection surface; d. positioning the identified orthopaedic implant model relative to the simulated resection portion of three-dimensional bone model; e. generating random point sets around the peripheries of the simulated resection portion and the orthopaedic implant model; f. calculating minimum distances between point sets; g. utilizing a position optimizer to determine whether the position of the orthopaedic implant periphery relative to the simulated resection portion periphery is optimal based on the minimum distances and the orthopaedic implant model; h. determining whether the selected orthopaedic implant model results in overhang relative to the three dimensional anatomic model; and i. verifying the position of the orthopaedic implant and/or the size of the orthopaedic implant.
Sensor switch comprising in a common plane a first sensor electrode and a second sensor electrode at least partially surrounding the first sensor electrode, the sensor switch further comprising: - a first signal generator capacitively coupled to the first sensor electrode and capacitively coupled to the second sensor electrode , - a first sensor circuit coupled to the first sensor electrode , - a second sensor circuit coupled to the second sensor electrode , - an evaluation and control circuit connected to the first sensor circuit and the second sensor circuit , the evaluation and control circuit being configured to receive signals from the first and second sensor circuits, wherein the evaluation and control circuit is configured to derive - a first sensor electrode attenuation signal indicating a signal attenuation at the first sensor electrode, - a second sensor electrode attenuation signal indicating a signal attenuation at the second sensor electrode, and the evaluation and control circuit is configured to generate a switch output signal if the first sensor electrode attenuation signal indicates a higher attenuation than the attenuation indicated by the second sensor electrode attenuation signal . - a first signal generator capacitively coupled to the first sensor electrode and capacitively coupled to the second sensor electrode , - a first sensor circuit coupled to the first sensor electrode , - a second sensor circuit coupled to the second sensor electrode , - an evaluation and control circuit connected to the first sensor circuit and the second sensor circuit , the evaluation and control circuit being configured to receive signals from the first and second sensor circuits, - a first sensor electrode attenuation signal indicating a signal attenuation at the first sensor electrode, - a second sensor electrode attenuation signal indicating a signal attenuation at the second sensor electrode, and
A degradation-determination system for a secondary battery comprising: four strain gauges that are respectively installed at four corners of an approximately rectangularly shaped principal surface of one or more surfaces of the secondary battery and each of which is configured to detect pressure of a battery surface at a corresponding installation position; and a degradation determining unit configured to determine degradation of the secondary battery based on measured values (S1, S2, S3, S4) at the four strain gauges, wherein the degradation determining unit is configured to estimate a maximum expansion position (G) where volume expansion is maximal in a region defined by the four strain gauges, of the one or more surfaces of the secondary battery, wherein the maximum expansion position (G) is associated with coordinates, on a two-dimensional coordinate system, on the primary surface of the secondary battery , and wherein the degradation determining unit is configured to determine coordinates of the maximum expansion position (G) on the two-dimensional coordinate system, based on the measured values (S1 to S4) at the four strain gauges, the maximum expansion position (G) being single. a degradation determining unit configured to determine degradation of the secondary battery based on measured values (S1, S2, S3, S4) at the four strain gauges, wherein the degradation determining unit is configured to estimate a maximum expansion position (G) where volume expansion is maximal in a region defined by the four strain gauges, of the one or more surfaces of the secondary battery, wherein the maximum expansion position (G) is associated with coordinates, on a two-dimensional coordinate system, on the primary surface of the secondary battery , and wherein the degradation determining unit is configured to determine coordinates of the maximum expansion position (G) on the two-dimensional coordinate system, based on the measured values (S1 to S4) at the four strain gauges, the maximum expansion position (G) being single.
A package , comprising: an elongated sheet having first and second side panels , and upper and lower panels , the sheet being wrapped into a shape that defines a three-dimensional cavity wherein the first and second side panels are in confronting relation to one another to define a fin having a longitudinal free edge and opposed end free edges ; at least a portion of the side panels parallel to the longitudinal free edge of the fin being adhered to one another to define a fin seal extending between the longitudinal free edge to a fin seal terminal line which is parallel to the longitudinal free edge , portions of the upper and lower panels being placed in confronting relation and said portions of the upper and lower panels being adhered to one another to define first and second end seals ; and a starter line formed in the fin at a location between the end free edges , the starter line extending from the longitudinal free edge of the fin toward the upper panels wherein the starter line directs tearing of the package along the terminal line . an elongated sheet having first and second side panels , and upper and lower panels , the sheet being wrapped into a shape that defines a three-dimensional cavity wherein the first and second side panels are in confronting relation to one another to define a fin having a longitudinal free edge and opposed end free edges ; at least a portion of the side panels parallel to the longitudinal free edge of the fin being adhered to one another to define a fin seal extending between the longitudinal free edge to a fin seal terminal line which is parallel to the longitudinal free edge , portions of the upper and lower panels being placed in confronting relation and said portions of the upper and lower panels being adhered to one another to define first and second end seals ; and a starter line formed in the fin at a location between the end free edges , the starter line extending from the longitudinal free edge of the fin toward the upper panels wherein the starter line directs tearing of the package along the terminal line .
A high-pressure fuel pump, comprising: a metal damper ; a pump body in which a damper housing that houses the metal damper is formed; a damper cover attached to the pump body , covering the damper housing , and holding the metal damper between the pump body and damper cover ; and a holding member fixed to the damper cover and holding the metal damper from a lower side, which is a side opposite to the damper cover ; and a communication path (CP) formed along an outer periphery of the holding member to allow communication of an upper side of the metal damper with the lower side of the metal damper ; the high pressure fuel pump characterized in further comprisimg: a fuel path (FP) formed through the holding member ; wherein the holding member is provided with an elastic portion (E) formed in the fuel path (FP) for urging the pump body so that the metal damper is urged toward the damper cover . a metal damper ; a pump body in which a damper housing that houses the metal damper is formed; a damper cover attached to the pump body , covering the damper housing , and holding the metal damper between the pump body and damper cover ; and a holding member fixed to the damper cover and holding the metal damper from a lower side, which is a side opposite to the damper cover ; and a communication path (CP) formed along an outer periphery of the holding member to allow communication of an upper side of the metal damper with the lower side of the metal damper ; the high pressure fuel pump characterized in further comprisimg: a fuel path (FP) formed through the holding member ; wherein the holding member is provided with an elastic portion (E) formed in the fuel path (FP) for urging the pump body so that the metal damper is urged toward the damper cover .
A ground fault circuit interrupter self-test circuit comprising: a silicon controlled rectifier, SCR, test loop coupled to a single controller including an SCR, wherein the SCR test loop runs from the SCR test pin through a diode (D6), through the SCR and to an SCR pin of the SCR; a ground fault test loop comprising a fault test pin and a switch coupled to the single controller; and a solenoid coupled to the single controller; wherein the SCR test loop is configured to conduct an SCR self-test during a first half wave portion of a phase using the SCR test loop and the ground fault test loop is configured to conduct a ground fault self-test during a second half wave portion of a phase using the ground fault test loop; and wherein the SCR is configured to activate the solenoid to deny power to a load upon one of the SCR self-test or the ground fault self-test being identified as failing. a silicon controlled rectifier, SCR, test loop coupled to a single controller including an SCR, wherein the SCR test loop runs from the SCR test pin through a diode (D6), through the SCR and to an SCR pin of the SCR; a ground fault test loop comprising a fault test pin and a switch coupled to the single controller; and a solenoid coupled to the single controller; wherein the SCR test loop is configured to conduct an SCR self-test during a first half wave portion of a phase using the SCR test loop and the ground fault test loop is configured to conduct a ground fault self-test during a second half wave portion of a phase using the ground fault test loop; and wherein the SCR is configured to activate the solenoid to deny power to a load upon one of the SCR self-test or the ground fault self-test being identified as failing.
A separator assembly for removing dirt from an air flow in a suction cleaner , the separator assembly including a plurality of cyclone separators arranged fluidly in parallel for separating fine dirt from an air flow, each providing: a body defining a central lengthwise axis (X), having a first portion at a first end that is substantially cylindrical, adjoining a second portion at a second end that is substantially frustoconical, the first and second portions defining a volume; a cyclone inlet towards the first end, configured to receive a swirling flow of air within the volume, a dirt outlet formed at the second end, and an end wall closing the volume at the first end around an annular vortex finder that extends coaxially with the lengthwise axis, defining a passage from a vortex finder inlet disposed within the volume of the body to a vortex finder outlet formed in the end wall, the dimensions of the cyclone separators conforming to the rule 0.3 ≤ D x / D ≤ 0.42 , wherein D represents the diameter of the first portion of the cyclone body, and D x represents the diameter of vortex finder. a body defining a central lengthwise axis (X), having a first portion at a first end that is substantially cylindrical, adjoining a second portion at a second end that is substantially frustoconical, the first and second portions defining a volume; a cyclone inlet towards the first end, configured to receive a swirling flow of air within the volume, a dirt outlet formed at the second end, and an end wall closing the volume at the first end around an annular vortex finder that extends coaxially with the lengthwise axis, defining a passage from a vortex finder inlet disposed within the volume of the body to a vortex finder outlet formed in the end wall, the dimensions of the cyclone separators conforming to the rule 0.3 ≤ D x / D ≤ 0.42 , wherein D represents the diameter of the first portion of the cyclone body, and D x represents the diameter of vortex finder. D represents the diameter of the first portion of the cyclone body, and D x represents the diameter of vortex finder.
A warning device for providing an alert to persons operating an aircraft ground support equipment , of the kind having a connector that is connected in use to an aircraft and occupies a stowed position when not so connected, the ground support equipment being provided with a first coupler adapted to couple with a second coupler mounted on a towing device to allow the ground support equipment to be towed by the towing device away from the aircraft; the warning device comprising: an alert mechanism, an actuator and a backplate , the actuator comprising an actuator body and a piston , the actuator body being biased in a forward direction away from the backplate , and the actuator being provided with a drive means providing drive to the actuator to extend the piston out of the actuator body in said forward direction towards said first coupler to occlude or obstruct it; the drive means being disabled when the connector is in the stowed position, and the actuator body being caused to move against the bias towards the backplate in the opposite direction to said forward direction if the piston engages an obstruction such as the second coupler indicating that the ground support equipment is coupled to the towing device, and the actuator continues to operate, which backwards motion triggers said alert mechanism.
A compound of formula (II): or a pharmaceutically acceptable salt thereof, wherein R 1a is selected from the group consisting of hydrogen; optionally substituted C 1 -C 6 alkyl; optionally substituted C 2 -C 6 alkenyl; optionally substituted C 2 -C 6 alkynyl; optionally substituted C 3 -C 10 cycloalkyl; ((C 1 -C 6 alkylsulfonyl)amino)C 1 -C 6 alkyl; optionally substituted C 3 -C 10 heterocyclyl; optionally substituted C 3 -C 10 aryl; optionally substituted C 3 -C 10 heteroaryl; C 1 -C 6 perfluoroalkyl; halo; cyano; nitro; optionally substituted amino;-C(O)NHR 5 ; -C(O)NR 5 R 6 ; -C(O)H; -C(O)R 7 ; -C(O)OH; and -C(O)OR 5 ; R 2 is selected from hydrogen; C(O)NR 5 R 6 ; C(O)R 7 ; -P(O)(OH) 2 ; and -P(O)(ONa) 2 ; alternatively, R 2 and R 3 taken together are a carbonyl group and together with the atoms to which they are attached, form a six-membered heterocyclic carbamate; R 3 is hydrogen, or alternatively, R 2 and R 3 taken together are a carbonyl group and together with the atoms to which they are attached, form a six-membered heterocyclic carbamate; each of R 4b , and R 4d is independently selected from the group consisting of hydrogen; C 1 -C 6 perfluoroalkyl; cyano; nitro; -CHF 2 , C 1 -C 6 alkyl, -OC 1 -C 6 -alkyl, -OCF 3 , C 3 -C 10 cycloalkyl, -CF 3 , -SO 2 CH 3 and halo; R 5 and R 6 taken together with the nitrogen to which they are attached form an optionally substituted C 3 -C 6 heterocyclyl; and R 7 is selected from the group consisting of (dimethylamino)methyl, and 2-pyrrolidinyl with the proviso that R 1a and R 2 are not both hydrogen. R 1a is selected from the group consisting of hydrogen; optionally substituted C 1 -C 6 alkyl; optionally substituted C 2 -C 6 alkenyl; optionally substituted C 2 -C 6 alkynyl; optionally substituted C 3 -C 10 cycloalkyl; ((C 1 -C 6 alkylsulfonyl)amino)C 1 -C 6 alkyl; optionally substituted C 3 -C 10 heterocyclyl; optionally substituted C 3 -C 10 aryl; optionally substituted C 3 -C 10 heteroaryl; C 1 -C 6 perfluoroalkyl; halo; cyano; nitro; optionally substituted amino;-C(O)NHR 5 ; -C(O)NR 5 R 6 ; -C(O)H; -C(O)R 7 ; -C(O)OH; and -C(O)OR 5 ; R 2 is selected from hydrogen; C(O)NR 5 R 6 ; C(O)R 7 ; -P(O)(OH) 2 ; and -P(O)(ONa) 2 ; alternatively, R 2 and R 3 taken together are a carbonyl group and together with the atoms to which they are attached, form a six-membered heterocyclic carbamate; R 3 is hydrogen, or alternatively, R 2 and R 3 taken together are a carbonyl group and together with the atoms to which they are attached, form a six-membered heterocyclic carbamate; each of R 4b , and R 4d is independently selected from the group consisting of hydrogen; C 1 -C 6 perfluoroalkyl; cyano; nitro; -CHF 2 , C 1 -C 6 alkyl, -OC 1 -C 6 -alkyl, -OCF 3 , C 3 -C 10 cycloalkyl, -CF 3 , -SO 2 CH 3 and halo; R 5 and R 6 taken together with the nitrogen to which they are attached form an optionally substituted C 3 -C 6 heterocyclyl; and R 7 is selected from the group consisting of (dimethylamino)methyl, and 2-pyrrolidinyl with the proviso that R 1a and R 2 are not both hydrogen.
A lubrication system for a gas turbine engine comprising: a tank configured to store a volume of lubricant; a circulation pump for generating a flow of lubricant from the tank to a component of the gas turbine engine ; a flowrate control valve in fluid communication with the flow of lubricant generated by the circulation pump and defining a flow inlet and a flow outlet , the flowrate control valve also defining a variable throughput between the flow inlet and the flow outlet for controlling a flowrate of lubricant to the component of the gas turbine engine ; and a heat exchanger positioned in thermal communication with the flow of lubricant generated by the circulation pump for controlling a temperature of the lubricant prior to the lubricant reaching the component ; characterized in that : the heat exchanger is positioned at a location downstream of the flowrate control valve ; wherein the flow of lubricant generated by the circulation pump is split downstream of the circulation pump between a first flow path and a second flow path, wherein the second flow path is configured to provide the flow of lubricant to the component of the gas turbine engine , and wherein the flowrate control valve is in fluid communication with the second flow path, wherein the circulation pump is further configured to generate a flow of lubricant from the tank through the first flow path to one or more other components of the gas turbine engine, the one or more other components comprising one or more of a compressor section of the gas turbine engine and a turbine section of the gas turbine engine . a tank configured to store a volume of lubricant; a circulation pump for generating a flow of lubricant from the tank to a component of the gas turbine engine ; a flowrate control valve in fluid communication with the flow of lubricant generated by the circulation pump and defining a flow inlet and a flow outlet , the flowrate control valve also defining a variable throughput between the flow inlet and the flow outlet for controlling a flowrate of lubricant to the component of the gas turbine engine ; and a heat exchanger positioned in thermal communication with the flow of lubricant generated by the circulation pump for controlling a temperature of the lubricant prior to the lubricant reaching the component ; the heat exchanger is positioned at a location downstream of the flowrate control valve ; wherein the flow of lubricant generated by the circulation pump is split downstream of the circulation pump between a first flow path and a second flow path, wherein the second flow path is configured to provide the flow of lubricant to the component of the gas turbine engine , and wherein the flowrate control valve is in fluid communication with the second flow path, wherein the circulation pump is further configured to generate a flow of lubricant from the tank through the first flow path to one or more other components of the gas turbine engine, the one or more other components comprising one or more of a compressor section of the gas turbine engine and a turbine section of the gas turbine engine .