mhurhangee/ep-ind-claims huggingface dataset:
A stowable seat comprising: a seat back; a seat bottom; a legrest; an attachment knob extending from the legrest; and a suspension recline system for the stowable seat, comprising: a suspension member comprising: a first end configured to be coupled to the seat back, and a second end configured to be coupled to the legrest, an attachment aperture disposed in the second end; and wherein the suspension member is placed over the attachment knob, with the attachment knob extending through the attachment aperture to couple the suspension member to the legrest;wherein the suspension member is moveable between a stowed position and a deployed position; wherein the seat back is configured to recline in response to the suspension member being moved to the deployed position. a seat back; a seat bottom; a legrest; an attachment knob extending from the legrest; and a suspension recline system for the stowable seat, comprising: a suspension member comprising: a first end configured to be coupled to the seat back, and a second end configured to be coupled to the legrest, an attachment aperture disposed in the second end; and wherein the suspension member is placed over the attachment knob, with the attachment knob extending through the attachment aperture to couple the suspension member to the legrest;wherein the suspension member is moveable between a stowed position and a deployed position; wherein the seat back is configured to recline in response to the suspension member being moved to the deployed position. a suspension member comprising: a first end configured to be coupled to the seat back, and a second end configured to be coupled to the legrest, an attachment aperture disposed in the second end; and wherein the suspension member is placed over the attachment knob, with the attachment knob extending through the attachment aperture to couple the suspension member to the legrest;wherein the suspension member is moveable between a stowed position and a deployed position; a first end configured to be coupled to the seat back, and a second end configured to be coupled to the legrest, an attachment aperture disposed in the second end; and wherein the suspension member is placed over the attachment knob, with the attachment knob extending through the attachment aperture to couple the suspension member to the legrest;wherein the suspension member is moveable between a stowed position and a deployed position; wherein the seat back is configured to recline in response to the suspension member being moved to the deployed position.
A floor having integrated components for an aircraft fuselage, the floor comprising: a floor panel including a sandwiched structural core between and bonded to top and bottom skins (54, 56); and floor beams coupled to a bottom surface of the floor panel, wherein the floor beams are arranged to extend in a longitudinal direction when fitted within a fuselage, wherein the sandwiched structural core comprises a first structural honeycomb core sandwiched between and bonded to the bottom skin and a septum and a second structural honeycomb core sandwiched between and bonded to the septum and the top skin, wherein the first structural honeycomb core includes a low density core and the second structural honeycomb core includes a high density core, wherein the low density core and the high density core are relative terms to one another; wherein the floor further comprises outer extremities having flanges for connecting to the fuselage, characterised in that the flanges form an integral part of lateral edges of the floor panel; wherein the flanges are formed by upper and lower straps (90, 92) and a medium density core at the outer extremities, wherein the low density core transitions into the medium density core having the same thickness as that of the low density core, the medium density core having a higher density than the low density core and a lower density than the high density core, to strengthen the outer extremities of the floor panel. a floor panel including a sandwiched structural core between and bonded to top and bottom skins (54, 56); and floor beams coupled to a bottom surface of the floor panel, wherein the floor beams are arranged to extend in a longitudinal direction when fitted within a fuselage, wherein the sandwiched structural core comprises a first structural honeycomb core sandwiched between and bonded to the bottom skin and a septum and a second structural honeycomb core sandwiched between and bonded to the septum and the top skin, wherein the first structural honeycomb core includes a low density core and the second structural honeycomb core includes a high density core, wherein the low density core and the high density core are relative terms to one another; wherein the floor further comprises outer extremities having flanges for connecting to the fuselage, characterised in that the flanges form an integral part of lateral edges of the floor panel; wherein the flanges are formed by upper and lower straps (90, 92) and a medium density core at the outer extremities, wherein the low density core transitions into the medium density core having the same thickness as that of the low density core, the medium density core having a higher density than the low density core and a lower density than the high density core, to strengthen the outer extremities of the floor panel.
An effective immunogenic composition comprising an attenuated Mycoplasma bovis strain, wherein said strain is deposited with the American Type Culture Collection under accession number PTA-122167.
A polyamide resin composition for a portable electronic device, comprising: a polyamide resin, a glass fiber having an elongated cross-section with an aspect ratio of 2.5 or more, said aspect ratio being defined by the formula shown below, and optionally a glass fiber having a circular cross-section with a diameter of 3 to 30 μm, the ratio (by weight) of the component to the component being 3:7 to 10:0, the proportion of the component being 60 to 34 % by weight, and the proportion of the component or the proportion of the sum of the components and being 40 to 66 % by weight with the proviso that the total sum of the above components is 100 % by weight, which polyamide resin composition shows a tensile strength of 200 MPa or higher as measured for an ISO test piece thereof according to ISO 527-1, -2, wherein polyamide resin of component consists of of at least one polyamide resin selected from the group consisting of polyhexamethylene terephthalamide (polyamide 6T), polyhexamethylene isophthalamide (polyamide 6I), polymetaxylylene adipamide (polyamide MXD6), polymetaxylylene dodecamide (polyamide MXD10), polyamide 9T, polymetaxylylene adipamide/polyparaxylylene adipamide copolymer (polyamide MP6), polymetaxylylene adipamide/polymetaxylylene isophthalamide copolymer (polyamide MXD6/MXDI), polyhexamethylene terephthalamide/poly-2-methyl-pentamethylene terephthalamide copolymer (polyamide 6T/M5T), and polyhexamethylene terephthalamide/polyhexamethylene isophthalamide copolymer (polyamide 6T/6I); aspect ratio = Major axis length D 2 of a cross - section of the glass fiber / Minor axis length D 1 of a cross - section of the glass fiber. a polyamide resin, a glass fiber having an elongated cross-section with an aspect ratio of 2.5 or more, said aspect ratio being defined by the formula shown below, and optionally a glass fiber having a circular cross-section with a diameter of 3 to 30 μm,
A cell identifier allocation method for allocating a cell identifier to a target cell of a target base station from among a plurality of base stations in a mobile communication system, comprising: an identification step of identifying,, a first cell that has the greatest reception power or the lowest propagation loss, from among the cells of the adjacent base stations; and, an allocation step of allocating,, a cell identifier in which a code sequence number of the synchronization signal is different from that of the first cell and that has not been allocated to any of the cells of the adjacent base stations, to the target cell, wherein each of the plural base stations forms a plurality of cells, and the allocation step includes: identifying a second cell that has the lowest reception power or the greatest propagation loss, from among the plural cells of the adjacent base station that forms the first cell; and, allocating the cell identifier, in which the code sequence number of the synchronization signal is the same as that of the second cell and that has not been allocated to any of the cells of the adjacent base stations, to the target cell, wherein the method is performed either by the target base station or by a maintenance server included in the system, when the method is performed by the target base station, the method further includes a measurement step wherein the target base station receives signal inside the target cell from each of the cells of the adjacent base stations and measures the reception power or propagation loss of the received signal; and when the method is performed by the maintenance server, the method further includes a step of obtaining information on a reception power or propagation loss of signal inside the target cell from each cell of adjacent base station in neighborhood of the target base station, from a maintenance terminal. identifying a second cell that has the lowest reception power or the greatest propagation loss, from among the plural cells of the adjacent base station that forms the first cell; and, allocating the cell identifier, in which the code sequence number of the synchronization signal is the same as that of the second cell and that has not been allocated to any of the cells of the adjacent base stations, to the target cell,
A method of transmitting an uplink access signal by a terminal in a communication system, the method comprising: receiving first reference signals through wide transmitting beams and receiving beams; calculating a first path loss for each combination of the wide transmitting beams and receiving beams by using a difference between transmission power information and a measurement of the first reference signals, and selecting a combination of a wide transmitting beam and a receiving beam with the lowest path loss from among the combinations of the wide transmitting beams and receiving beams; receiving second reference signals through narrow transmitting beams corresponding to the selected wide transmitting beam by using the selected receiving beam; calculating a second path loss between the narrow transmitting beams and the selected receiving beam, and selecting a narrow transmitting beam with the lowest path loss; and transmitting an uplink access signal through a transmitting beam corresponding to the selected receiving beam at an access time or frequency assigned to an uplink narrow receiving beam that corresponds to the selected narrow transmitting beam. receiving first reference signals through wide transmitting beams and receiving beams; calculating a first path loss for each combination of the wide transmitting beams and receiving beams by using a difference between transmission power information and a measurement of the first reference signals, and selecting a combination of a wide transmitting beam and a receiving beam with the lowest path loss from among the combinations of the wide transmitting beams and receiving beams; receiving second reference signals through narrow transmitting beams corresponding to the selected wide transmitting beam by using the selected receiving beam; calculating a second path loss between the narrow transmitting beams and the selected receiving beam, and selecting a narrow transmitting beam with the lowest path loss; and transmitting an uplink access signal through a transmitting beam corresponding to the selected receiving beam at an access time or frequency assigned to an uplink narrow receiving beam that corresponds to the selected narrow transmitting beam.
A method performed by a keypad device, the method comprising: receiving data from a security panel of a property, where the keypad device receives the data by intercepting commands on a keypad bus of the security panel using an interceptor, wherein the interceptor is configured to intercept incoming communications on the keypad bus of the security panel; determining a keypad bus protocol of the security panel based on the data received from the security panel; receiving sensor data from one or more sensors located within the property; determining, based on the obtained sensor data, an emergency condition; determining a monitoring system command that is not specified within the keypad bus of the security panel, wherein: i) the monitoring system command that is not specified within the keypad bus of the security panel is determined based on the obtained sensor data, and ii) the monitoring system command adjusts a security status of the monitoring system based on the detected emergency condition; converting the monitoring system command to a panel command using the keypad bus protocol; and transmitting the panel command on the keypad bus of the security panel, wherein the panel command is processed and executed by the security panel in the same way as a command entered on the keypad device. receiving data from a security panel of a property, where the keypad device receives the data by intercepting commands on a keypad bus of the security panel using an interceptor, wherein the interceptor is configured to intercept incoming communications on the keypad bus of the security panel; determining a keypad bus protocol of the security panel based on the data received from the security panel; receiving sensor data from one or more sensors located within the property; determining, based on the obtained sensor data, an emergency condition; determining a monitoring system command that is not specified within the keypad bus of the security panel, wherein: i) the monitoring system command that is not specified within the keypad bus of the security panel is determined based on the obtained sensor data, and ii) the monitoring system command adjusts a security status of the monitoring system based on the detected emergency condition; i) the monitoring system command that is not specified within the keypad bus of the security panel is determined based on the obtained sensor data, and ii) the monitoring system command adjusts a security status of the monitoring system based on the detected emergency condition; converting the monitoring system command to a panel command using the keypad bus protocol; and transmitting the panel command on the keypad bus of the security panel, wherein the panel command is processed and executed by the security panel in the same way as a command entered on the keypad device.
A dentifrice having a pigment system which comprises one or more pigments, and titanium dioxide, wherein the level of titanium dioxide is 0.05 - 0.2% by weight of the dentifrice, wherein the one or more pigment is Pigment Blue 15: and wherein the dentifrice comprises 1.5 - 2.0% of sodium lauryl sulfate and 0.5 - 2.0% of a copolymer of methyl vinyl ether and maleic anhydride.
A device for controlling a hydraulic pump of construction machinery, the hydraulic pump having a first pump supplying working fluid through a swing control valve to a swing motor, and a second pump supplying working fluid through a work tool control valve to a work tool actuator, the device comprising: a first tilting angle control unit for controlling a discharge flow of the first pump by controlling a tilting angle of the first pump according to an input pump control signal; and a controller deducting a discharge pressure of the second pump from a discharge pressure of the first pump to calculate a pump difference pressure (P1-P2), comparing the calculated pump difference pressure (P1-P2) to a reference difference pressure and, when the calculated pump difference pressure (P1-P2) is greater than the reference difference pressure, outputting the pump control signal to the first tilting angle control unit to make the discharge pressure of the first pump equal to or less than a first reference pressure that is less than or equal to a swing relief pressure. a first tilting angle control unit for controlling a discharge flow of the first pump by controlling a tilting angle of the first pump according to an input pump control signal; and a controller deducting a discharge pressure of the second pump from a discharge pressure of the first pump to calculate a pump difference pressure (P1-P2), comparing the calculated pump difference pressure (P1-P2) to a reference difference pressure and, when the calculated pump difference pressure (P1-P2) is greater than the reference difference pressure, outputting the pump control signal to the first tilting angle control unit to make the discharge pressure of the first pump equal to or less than a first reference pressure that is less than or equal to a swing relief pressure.
A cable lockout assembly comprising: a base comprising a threaded protuberance extending centrally above the said base and a through-passage extending between two diametrically opposite pair of openings formed on outer peripheral wall of the base for inserting therethrough a cable; a rotatable piece having a first central opening for receiving the threaded protuberance of the base; the rotatable piece is rotatable about axis of the threaded protuberance wherein the rotation of the rotatable piece axially moves the rotatable piece along the axis of the threaded protuberance relative to the base; a tool, having a second central opening for receiving the threaded protuberance and a second provision engageable with a first provision of the rotatable piece wherein rotation of the tool rotates the said rotatable piece thereby adjusting the clamping force exerted on portion of the cable interposed between the rotatable piece and the base in the through-passage, wherein the base has a plurality of spaced locking apertures alignable with a plurality of spaced locking apertures ( 302, 402) disposed in the rotatable piece and tool respectively, for receiving a locking device to lock the relative rotation of the tool, the rotatable piece and the base. a base comprising a threaded protuberance extending centrally above the said base and a through-passage extending between two diametrically opposite pair of openings formed on outer peripheral wall of the base for inserting therethrough a cable; a rotatable piece having a first central opening for receiving the threaded protuberance of the base; the rotatable piece is rotatable about axis of the threaded protuberance wherein the rotation of the rotatable piece axially moves the rotatable piece along the axis of the threaded protuberance relative to the base; a tool, having a second central opening for receiving the threaded protuberance and a second provision engageable with a first provision of the rotatable piece wherein rotation of the tool rotates the said rotatable piece thereby adjusting the clamping force exerted on portion of the cable interposed between the rotatable piece and the base in the through-passage, wherein the base has a plurality of spaced locking apertures alignable with a plurality of spaced locking apertures ( 302, 402) disposed in the rotatable piece and tool respectively, for receiving a locking device to lock the relative rotation of the tool, the rotatable piece and the base.
A system for creating a plasma proximate an aerodynamic surface, the system comprising: an aircraft active flow control dielectric barrier discharge device, comprising: a machinable ceramic dielectric support (14, 110) having an aerodynamic surface (118, 36) shaped to form an exposed flush part of an airfoil surface of an aircraft (200, 300); and at least two electrodes (16, 18) configured to be oppositely charged and spaced apart from each other on the dielectric support, and characterized by a controller configured to activate the dielectric barrier device during takeoff and landing if a predetermined speed threshold is crossed or if a predetermined angle of attack for the airfoil surface is exceeded, wherein the dielectric barrier discharge device is provided in a form of a cartridge configured to plug into the airfoil structure (12, 102) and to be unplugged for replacement. a machinable ceramic dielectric support (14, 110) having an aerodynamic surface (118, 36) shaped to form an exposed flush part of an airfoil surface of an aircraft (200, 300); and at least two electrodes (16, 18) configured to be oppositely charged and spaced apart from each other on the dielectric support, and characterized by a controller configured to activate the dielectric barrier device during takeoff and landing if a predetermined speed threshold is crossed or if a predetermined angle of attack for the airfoil surface is exceeded, wherein the dielectric barrier discharge device is provided in a form of a cartridge configured to plug into the airfoil structure (12, 102) and to be unplugged for replacement.
A mold support system comprising a portal-like frame, a mold support upper part movable relative to the frame and having a first mold clamping plate, a mold support lower part having a second mold clamping plate, first locking means provided on the frame and second locking means provided on the mold support upper part for locking the mold support upper part relative to the frame in a locking position, wherein the first locking means and/or the second locking means are formed by a plurality of equally spaced locking elements (53; 63) which can be brought into engagement in different locking positions, characterized in that at least one compressed air cushion is provided for stepless fine positioning of the first mold clamping plate and/or the second mold clamping plate on the mold support upper part and/or on the mold support lower part.
A food processor, comprising: a motor base including a motor coupling; an outer vessel being removably mounted on the motor base; an inner vessel being removably mounted within the outer vessel; an inner lid including a blade and a food passage opening on a surface of the inner lid; characterized in that the inner vessel has an inner vessel coupler for engaging the motor coupling and the inner lid is secured on top of the inner vessel so that the inner vessel moves in unison with the inner lid during rotation. a motor base including a motor coupling; an outer vessel being removably mounted on the motor base; an inner vessel being removably mounted within the outer vessel; an inner lid including a blade and a food passage opening on a surface of the inner lid; characterized in that the inner vessel has an inner vessel coupler for engaging the motor coupling and the inner lid is secured on top of the inner vessel so that the inner vessel moves in unison with the inner lid during rotation.
An electric coolant pump having: a pump impeller for accelerating the coolant to be conveyed; a rotor shaft on which the pump impeller is fixed, an electric motor for driving the rotor shaft, comprising a stator and a rotor, a control circuit for controlling the electric motor, and a pump housing which accommodates at least the control circuit and the electric motor, the coolant to be conveyed being able to flow through the pump housing, characterized in that the coolant to be conveyed thereby flowing around the stator, the rotor and the control circuit, wherein the coolant to be conveyed is dielectric, and electronic components of the control circuit are in direct contact with the coolant to be conveyed. a pump impeller for accelerating the coolant to be conveyed; a rotor shaft on which the pump impeller is fixed, an electric motor for driving the rotor shaft, comprising a stator and a rotor, a control circuit for controlling the electric motor, and a pump housing which accommodates at least the control circuit and the electric motor, the coolant to be conveyed being able to flow through the pump housing, characterized in that the coolant to be conveyed thereby flowing around the stator, the rotor and the control circuit, wherein the coolant to be conveyed is dielectric, and electronic components of the control circuit are in direct contact with the coolant to be conveyed.