mhurhangee/patent-ind-claim-en huggingface dataset:
An antenna system designed to reduce a probability of destructive interference of signals received by the antenna system, the antenna system comprising: a first linearly polarized antenna (105; 701) oriented to detect energy along a first plane; a second linearly polarized antenna (111, 113; 702) oriented to detect energy along a second plane, wherein the second antenna is positioned generally perpendicular to the first antenna and affixed thereto such that the first plane is cross-polarized with the second plane; a first RF amplifier coupled to the first antenna and comprising a first resistor for controlling a gain of the first RF amplifier; and a second RF amplifier coupled to the second antenna and comprising a second resistor for controlling a gain of the second RF amplifier; wherein the first antenna exhibits a first gain and the second antenna exhibits a second gain that is different from the first gain, such that the different first gain and second gain are configured to reduce a probability of destructive interference of the signals arriving at the antenna system; and characterized in that the first and second resistors are configured to adjust the gain of the first RF amplifier and the gain of the second RF amplifier to match the different first gain and second gain of the first antenna and the second antenna. a first linearly polarized antenna (105; 701) oriented to detect energy along a first plane; a second linearly polarized antenna (111, 113; 702) oriented to detect energy along a second plane, wherein the second antenna is positioned generally perpendicular to the first antenna and affixed thereto such that the first plane is cross-polarized with the second plane; a first RF amplifier coupled to the first antenna and comprising a first resistor for controlling a gain of the first RF amplifier; and a second RF amplifier coupled to the second antenna and comprising a second resistor for controlling a gain of the second RF amplifier; wherein the first antenna exhibits a first gain and the second antenna exhibits a second gain that is different from the first gain, such that the different first gain and second gain are configured to reduce a probability of destructive interference of the signals arriving at the antenna system; and characterized in that the first and second resistors are configured to adjust the gain of the first RF amplifier and the gain of the second RF amplifier to match the different first gain and second gain of the first antenna and the second antenna.
Vehicle headlamp, in particular motor vehicle headlamp, comprising an adjusting device for adjusting, for example for pivoting, at least one optically relevant unit of the vehicle headlamp, which optically relevant unit , for example, is a lighting unit or a light module or comprises at least one light unit or light module, and wherein the adjusting device comprises an actuating element and a driving device , wherein the actuating element is, with a first end portion , articulately connected to the optical unit , and wherein the actuating element , at a second end portion thereof, is coupled to the driving device in such a manner in that the actuating element is rotatable about its longitudinal axis by means of the driving device and is mounted longitudinally displaceable along its longitudinal axis , wherein the actuating element comprises a threaded section by means of which the actuating element is mounted rotatable about its longitudinal axis within in a mating thread , the mating thread being arranged fixed with respect to a housing of the vehicle headlight, wherein the driving device is mounted at the housing of the vehicle headlamp, wherein the adjustment device comprises a guide element separate from the housing of the vehicle headlamp, the guide element being fixedly connected to the housing , and wherein the mating thread is fixedly connected to the guide element , characterised in that the guide element includes a guide receptacle , in which guide receptacle the at least one optically relevant unit is mounted with a bearing region being displaceable in the direction of the longitudinal axis of the actuating element , and the bearing region having a articulation section , with which the actuating element is connected in an articulated manner to its first end region .
An implantable prosthetic valve comprising: an annular frame comprising an inflow end and an outflow end and being radially collapsible and expandable between a radially collapsed configuration and a radially expanded configuration, the frame defining an axial direction extending from the inflow end to the outflow end ; a leaflet structure positioned within the frame and secured thereto; and an annular outer skirt positioned around an outer surface of the frame , wherein the outer skirt comprises: an inflow edge secured to the frame at a first location, an outflow edge secured to the frame at a second location; characterized by further comprising a plurality of axially extending creases , wherein the creases are configured to cause at least a portion of the outer skirt to retract radially within the frame when the frame is radially collapsed from the expanded configuration, wherein the annular outer skirt is positioned relative to the frame such that at least one of the creases is circumferentially disposed between struts of the frame . an annular frame comprising an inflow end and an outflow end and being radially collapsible and expandable between a radially collapsed configuration and a radially expanded configuration, the frame defining an axial direction extending from the inflow end to the outflow end ; a leaflet structure positioned within the frame and secured thereto; and an annular outer skirt positioned around an outer surface of the frame , wherein the outer skirt comprises: an inflow edge secured to the frame at a first location, an outflow edge secured to the frame at a second location; characterized by further comprising a plurality of axially extending creases , wherein the creases are configured to cause at least a portion of the outer skirt to retract radially within the frame when the frame is radially collapsed from the expanded configuration, wherein the annular outer skirt is positioned relative to the frame such that at least one of the creases is circumferentially disposed between struts of the frame . an inflow edge secured to the frame at a first location, an outflow edge secured to the frame at a second location; characterized by further comprising a plurality of axially extending creases , wherein the creases are configured to cause at least a portion of the outer skirt to retract radially within the frame when the frame is radially collapsed from the expanded configuration, wherein the annular outer skirt is positioned relative to the frame such that at least one of the creases is circumferentially disposed between struts of the frame .
A method for stabilizing a refractory carbide hot gas path component comprising: combusting a fuel in a combustor to form a gas stream comprising post-combustion gases; and delivering a high carbon activity gas to at least a portion of a hot gas path component thermally coupled to a hot gas path, wherein the component comprises rows of discrete film holes oriented at shallow angles to the surface, and wherein delivering the high carbon activity gas comprises introducing the high carbon activity gas via the rows of discrete film holes, thereby to cover at least a portion of the component with a layer of the high carbon activity gas. combusting a fuel in a combustor to form a gas stream comprising post-combustion gases; and delivering a high carbon activity gas to at least a portion of a hot gas path component thermally coupled to a hot gas path, wherein the component comprises rows of discrete film holes oriented at shallow angles to the surface, and wherein delivering the high carbon activity gas comprises introducing the high carbon activity gas via the rows of discrete film holes, thereby to cover at least a portion of the component with a layer of the high carbon activity gas.
An elevator system device , comprising: an interface configured to operate in a first mode that allows an elevator passenger to communicate with the elevator system by at least one of inputting an indication for desired elevator service and receiving an indication regarding elevator service; and a magnetically actuated switch that selectively causes the interface to operate in a second mode that allows an authorized individual to communicate with the elevator system in a manner that is different than an elevator passenger communication in the first mode, characterised in that the magnetically actuated switch includes at least one magnet and at least one switch contact that changes between an open and closed state based on an interaction between the at least one magnet and a magnetic key brought into proximity of the at least one magnet by the authorized individual. an interface configured to operate in a first mode that allows an elevator passenger to communicate with the elevator system by at least one of inputting an indication for desired elevator service and receiving an indication regarding elevator service; and a magnetically actuated switch that selectively causes the interface to operate in a second mode that allows an authorized individual to communicate with the elevator system in a manner that is different than an elevator passenger communication in the first mode, characterised in that the magnetically actuated switch includes at least one magnet and at least one switch contact that changes between an open and closed state based on an interaction between the at least one magnet and a magnetic key brought into proximity of the at least one magnet by the authorized individual.
A fluidics cassette , comprising: a housing ; an irrigation line and an aspiration line , the lines configured to provided irrigation and aspiration functions for an eye treatment probe ; a ramp configured for transferring fluid through a resilient channel when the resilient channel is engaged by a pump head , the ramp comprising: a central portion characterised by a first base curvature (C central ); an entrance portion having a base curvature (C entrance ) that is different from the first base curvature; and an exit portion having a base curvature (C exit ) that is different from the first base curvature; an arcuate extent of the entrance portion being unequal to an arcuate extent of the exit portion. a housing ; an irrigation line and an aspiration line , the lines configured to provided irrigation and aspiration functions for an eye treatment probe ; a ramp configured for transferring fluid through a resilient channel when the resilient channel is engaged by a pump head , the ramp comprising: a central portion characterised by a first base curvature (C central ); an entrance portion having a base curvature (C entrance ) that is different from the first base curvature; and an exit portion having a base curvature (C exit ) that is different from the first base curvature; an arcuate extent of the entrance portion being unequal to an arcuate extent of the exit portion. a central portion characterised by a first base curvature (C central ); an entrance portion having a base curvature (C entrance ) that is different from the first base curvature; and an exit portion having a base curvature (C exit ) that is different from the first base curvature; an arcuate extent of the entrance portion being unequal to an arcuate extent of the exit portion.
- A refrigeration apparatus, comprising a main circuit , including: - a compressor , including a compressor inlet and a compressor outlet , - a condenser , including a condenser inlet , connected to the compressor outlet , and a condenser outlet , - an expansion valve , including a valve inlet , connected to the condenser outlet and a valve outlet , and - an evaporator , including an evaporator inlet , connected to the valve outlet , and an evaporator outlet , connected to the compressor inlet , wherein the main circuit is configured for a loop circulation of a main flow of refrigerant, successively through the compressor , the condenser , the expansion valve , and the evaporator , wherein the refrigeration apparatus further comprises a lubrication branch , comprising: - a lubrication inlet , connected to a supply part of the main circuit , the supply part consisting in the condenser , the valve inlet , and any part of the main circuit between the condenser outlet and the valve inlet , the lubrication inlet being configured to derive a lubrication flow from the main flow of refrigerant circulating through the supply part ; and - a lubrication outlet , connected to the compressor so as to feed the compressor with the lubrication flow , for lubrication of said compressor with the refrigerant of the lubrication flow , wherein the main circuit comprises a low-temperature part , consisting in the evaporator , the compressor inlet , and any part of the main circuit between the evaporator outlet and the compressor inlet , characterized in that the lubrication branch further comprises a subcooling heat exchanger , which is configured for enabling an exchange of heat between the lubrication flow circulating through the lubrication branch and the main flow of refrigerant circulating through the low-temperature part , so that the lubrication flow may be cooled by the main flow of refrigerant circulating through the low-temperature part , within the subcooling heat exchanger . - a compressor , including a compressor inlet and a compressor outlet , - a condenser , including a condenser inlet , connected to the compressor outlet , and a condenser outlet , - an expansion valve , including a valve inlet , connected to the condenser outlet and a valve outlet , and - an evaporator , including an evaporator inlet , connected to the valve outlet , and an evaporator outlet , connected to the compressor inlet , - a lubrication inlet , connected to a supply part of the main circuit , the supply part consisting in the condenser , the valve inlet , and any part of the main circuit between the condenser outlet and the valve inlet , the lubrication inlet being configured to derive a lubrication flow from the main flow of refrigerant circulating through the supply part ; and - a lubrication outlet , connected to the compressor so as to feed the compressor with the lubrication flow , for lubrication of said compressor with the refrigerant of the lubrication flow ,
A glass-ceramic article comprising: a) a composition, in mole %, comprising: i) SiO 2 in a range from 60 to 75, ii) Al 2 O 3 in a range from 10 to 18, iii) Li 2 O in a range from 5 to 14, and iv) B 2 O 3 in a range from 10 to 20, wherein a ratio of the mole sum total [Li 2 O + Na 2 O + K 2 O + MgO + ZnO]/ moles of [Al 2 O 3 ] is in a range from 0.8 to 1.5; and b) a Vickers crack initiation threshold of a least 25kgf, wherein β-spodumene is the predominant crystalline phase. a) a composition, in mole %, comprising: i) SiO 2 in a range from 60 to 75, ii) Al 2 O 3 in a range from 10 to 18, iii) Li 2 O in a range from 5 to 14, and iv) B 2 O 3 in a range from 10 to 20, wherein a ratio of the mole sum total [Li 2 O + Na 2 O + K 2 O + MgO + ZnO]/ moles of [Al 2 O 3 ] is in a range from 0.8 to 1.5; and i) SiO 2 in a range from 60 to 75, ii) Al 2 O 3 in a range from 10 to 18, iii) Li 2 O in a range from 5 to 14, and iv) B 2 O 3 in a range from 10 to 20, wherein a ratio of the mole sum total [Li 2 O + Na 2 O + K 2 O + MgO + ZnO]/ moles of [Al 2 O 3 ] is in a range from 0.8 to 1.5; and b) a Vickers crack initiation threshold of a least 25kgf, wherein β-spodumene is the predominant crystalline phase.
An information recording object comprising a superimposed image including a first ink layer and a second ink layer formed on the first ink layer , wherein the first ink layer is an image of a chromatic color formed using a lustrous material, and includes a picture image (C1b) and a background image (C1a), the second ink layer is a pattern image which is formed using a transparent material and has regularity, the first ink layer includes a shading pattern image patterned by shading of colors, the shading pattern image is an image on which a process of acquiring data for code generation can be performed by a conversion application different from the conversion application to acquire data for specifying code from the pattern image of the second ink layer , and information is allowed to be read from the shading pattern image, the background image (C1a) is the shading pattern image patterned by shading of colors, the picture image (C1b) is not the shading pattern image, the transparent material is configured so that an amount of reflected light varies depending on a viewing angle, and is allowed to be recognized by a specific viewing angle different from a viewing angle by which the first ink layer is allowed to be recognized, and the superimposed image is formed so that the second ink layer is allowed to be recognized by the specific viewing angle. a superimposed image including a first ink layer and a second ink layer formed on the first ink layer , wherein the first ink layer is an image of a chromatic color formed using a lustrous material, and includes a picture image (C1b) and a background image (C1a), the second ink layer is a pattern image which is formed using a transparent material and has regularity, the first ink layer includes a shading pattern image patterned by shading of colors, the shading pattern image is an image on which a process of acquiring data for code generation can be performed by a conversion application different from the conversion application to acquire data for specifying code from the pattern image of the second ink layer , and information is allowed to be read from the shading pattern image, the background image (C1a) is the shading pattern image patterned by shading of colors, the picture image (C1b) is not the shading pattern image, the transparent material is configured so that an amount of reflected light varies depending on a viewing angle, and is allowed to be recognized by a specific viewing angle different from a viewing angle by which the first ink layer is allowed to be recognized, and the superimposed image is formed so that the second ink layer is allowed to be recognized by the specific viewing angle.
A method for making a low density foamed article, comprising: combining in an extruder a molten polymer selected from the group consisting of thermoplastic polyurethane elastomers and thermoplastic ethylene-vinyl acetate copolymers with (a) from about 0.1 to about 4 weight percent of supercritical fluid nitrogen based on polymer weight and (b) from about 0.1 to about 5 weight percent of a supercritical fluid carbon dioxide based on polymer weight to form a mixture, wherein the supercritical fluid nitrogen is added through a first port to the molten polymer and the supercritical fluid carbon dioxide is added through a second port to the molten polymer; and injection molding and foaming the mixture or extruding and foaming the mixture. combining in an extruder a molten polymer selected from the group consisting of thermoplastic polyurethane elastomers and thermoplastic ethylene-vinyl acetate copolymers with (a) from about 0.1 to about 4 weight percent of supercritical fluid nitrogen based on polymer weight and (b) from about 0.1 to about 5 weight percent of a supercritical fluid carbon dioxide based on polymer weight to form a mixture, wherein the supercritical fluid nitrogen is added through a first port to the molten polymer and the supercritical fluid carbon dioxide is added through a second port to the molten polymer; and (a) from about 0.1 to about 4 weight percent of supercritical fluid nitrogen based on polymer weight and (b) from about 0.1 to about 5 weight percent of a supercritical fluid carbon dioxide based on polymer weight to form a mixture, wherein the supercritical fluid nitrogen is added through a first port to the molten polymer and the supercritical fluid carbon dioxide is added through a second port to the molten polymer; and injection molding and foaming the mixture or extruding and foaming the mixture.
An aircraft fuselage sidewall comprising: an aircraft sidewall volume delineated by an aircraft skin forming an outboard boundary of the aircraft sidewall volume, a passenger cabin sidewall forming an inboard boundary of the aircraft sidewall volume and fuselage frame structures forming axial boundaries of the aircraft sidewall volume; a flow controller positioned at a portion of the aircraft sidewall volume to selectably control air flow through the aircraft sidewall volume, and a dividing member disposed in the aircraft sidewall volume to divide the aircraft sidewall volume into an inboard volume between the dividing member and the passenger cabin sidewall and an outboard volume between the dividing member and the aircraft skin ; wherein the flow controller is configured, during an in-flight situation in which the aircraft skin is cold, to restrict flow of air in the inboard volume to provide insulating properties in the inboard volume , and to allow unrestricted flow of air in the outboard volume ; and wherein the flow controller is configured, during a ground situation in which the aircraft skin is hot due to thermal solar energy, to restrict flow of air in the outboard volume to provide insulating properties in the outboard volume , and to allow unrestricted flow of air in the inboard volume . an aircraft sidewall volume delineated by an aircraft skin forming an outboard boundary of the aircraft sidewall volume, a passenger cabin sidewall forming an inboard boundary of the aircraft sidewall volume and fuselage frame structures forming axial boundaries of the aircraft sidewall volume; a flow controller positioned at a portion of the aircraft sidewall volume to selectably control air flow through the aircraft sidewall volume, and a dividing member disposed in the aircraft sidewall volume to divide the aircraft sidewall volume into an inboard volume between the dividing member and the passenger cabin sidewall and an outboard volume between the dividing member and the aircraft skin ; wherein the flow controller is configured, during an in-flight situation in which the aircraft skin is cold, to restrict flow of air in the inboard volume to provide insulating properties in the inboard volume , and to allow unrestricted flow of air in the outboard volume ; and wherein the flow controller is configured, during a ground situation in which the aircraft skin is hot due to thermal solar energy, to restrict flow of air in the outboard volume to provide insulating properties in the outboard volume , and to allow unrestricted flow of air in the inboard volume .