mhurhangee/ep-ind-claims huggingface dataset:
Lid configuration for a bioreactor, comprising: - a lid configured for connection with a vessel of the bioreactor, the vessel during use containing a bioreactor fluid, the lid being provided with one or more 3D-printed sensor or controller elements for, during use, sensing or controlling one or more parameters of the bioreactor, in particular the bioreactor fluid, characterized, in that the one or more 3D-printed sensor or controller elements comprise one or more 3D-printed inlets or outlets. - a lid configured for connection with a vessel of the bioreactor, the vessel during use containing a bioreactor fluid, the lid being provided with one or more 3D-printed sensor or controller elements for, during use, sensing or controlling one or more parameters of the bioreactor, in particular the bioreactor fluid, characterized, in that the one or more 3D-printed sensor or controller elements comprise one or more 3D-printed inlets or outlets.
Electrically actuable valve for controlling the flow of a fluidic pressure medium, with a valve member which may be driven relative to a valve casing of the valve to an axial switchover movement between a closed position and an open position and which, in the closed position, makes sealing contact with a front side at an annular valve seat framing a passage orifice of a first valve passage, and which in the open position is lifted from the valve seat, so that the first valve passage is connected with an annular space framing the valve seat and constantly communicating with a second valve passage, wherein the valve member extends with axial movement facility in a guide recess defined by a guide wall which is stationary relative to the valve casing, and wherein the valve member makes sliding contact with the guide wall at its outer periphery and under sealing, and forms an axially movable boundary wall of a pressure compensation chamber located on its rear side and communicating at least in the closed position of the valve member through at least one pressure compensation passage with the first valve passage, wherein the cross-section of the guide recess corresponds to the cross-section encompassed by the valve seat, and the valve member is biased by spring means in the direction of its closed position, characterised in that the valve member, viewed in the axial direction, has an elongated external contour, wherein it has two straight long sides and two bow-shaped, rounded narrow sides, and that the valve seat, viewed in the axial direction, has an elongated shape, wherein it has two straight long sides (33a, 33b) and two bow-shaped, rounded narrow sides (33c, 33d).
Rear fuselage of an aircraft comprising - a tail cone end and - a rest of the rear fuselage where the tail cone end is attached to the rest of the rear fuselage by means of an attachment system comprising - two upper lugs, - two lower lugs and - a detachable balancer fitting at an interface point of said tail cone end and said rest of the rear fuselage, wherein the balancer fitting comprises means to modify the interface point by allowing an adjustment in the Z and Y direction of Cartesian axis and is movable along an X direction of a Cartesian axis, said balancer fitting provides guidance for alignment of the tail cone end and the rest of the rear fuselage during the assembly of the rear fuselage, wherein the balancer fitting is a two parts fitting comprising - a first fitting having a first concentric hole, - a second fitting having a second concentric hole and - a bearing inside the second concentric hole, the first and the second fittings (51 and 52) are independent and are mounted on a frame, the second fitting has the bearing inside its concentric hole in a way that when the first fitting and the second fitting are mounted together, the bearing of the second fitting fits into the concentric hole of the first fitting. - a tail cone end and - a rest of the rear fuselage where the tail cone end is attached to the rest of the rear fuselage by means of an attachment system comprising - two upper lugs, - two lower lugs and - a detachable balancer fitting at an interface point of said tail cone end and said rest of the rear fuselage, wherein the balancer fitting comprises means to modify the interface point by allowing an adjustment in the Z and Y direction of Cartesian axis and is movable along an X direction of a Cartesian axis, said balancer fitting provides guidance for alignment of the tail cone end and the rest of the rear fuselage during the assembly of the rear fuselage, - two upper lugs, - two lower lugs and - a detachable balancer fitting at an interface point of said tail cone end and said rest of the rear fuselage, wherein the balancer fitting comprises means to modify the interface point by allowing an adjustment in the Z and Y direction of Cartesian axis and is movable along an X direction of a Cartesian axis, said balancer fitting provides guidance for alignment of the tail cone end and the rest of the rear fuselage during the assembly of the rear fuselage, - a first fitting having a first concentric hole, - a second fitting having a second concentric hole and - a bearing inside the second concentric hole, the first and the second fittings (51 and 52) are independent and are mounted on a frame, the second fitting has the bearing inside its concentric hole in a way that when the first fitting and the second fitting are mounted together, the bearing of the second fitting fits into the concentric hole of the first fitting.
Optical component, being configured for modulating a light field incident on the optical component, wherein the light field has a predetermined centre wavelength in near-infrared or infrared spectral range, comprising - a stack of refractive layers (12, 13) being arranged on a substrate, being made of at least one of dielectric and semiconductor materials having a third-order nonlinearity, and having alternatingly varying refractive indices n including a linear contribution n 0 and a non-linear contribution n 2, and determining reflectance and transmittance spectra of the optical component, wherein - the refractive layers (12, 13) are configured such that reflectance and transmittance of the optical component have a Kerr effect based dependency on the intensity I of the incident light field with n = n 0 + I·n 2, - the incident light field has an intensity such that the stack of the refractive layers provides an optically non-linear response to the incident light such that the reflected or transmitted light has an intensity and/or phase which depends on this intensity, - the refractive layers (12, 13) are configured such that the reflectance and transmittance spectra of the optical component have a plateau section including the centre wavelength of the light field, - the non-linear contribution (n 2) is below 10 -12 cm 2 /W, characterized in that - the dielectric layers are made of at least one of Ta 2 O 5, Nb 2 O 5,HfO 2, TiO 2, ZrO 2, Al 2 O 3 and SiO 2, and - the semiconductor layers are made of at least one of Ge, Si and ZnSe. - a stack of refractive layers (12, 13) being arranged on a substrate, being made of at least one of dielectric and semiconductor materials having a third-order nonlinearity, and having alternatingly varying refractive indices n including a linear contribution n 0 and a non-linear contribution n 2, and determining reflectance and transmittance spectra of the optical component, wherein - the refractive layers (12, 13) are configured such that reflectance and transmittance of the optical component have a Kerr effect based dependency on the intensity I of the incident light field with n = n 0 + I·n 2, - the incident light field has an intensity such that the stack of the refractive layers provides an optically non-linear response to the incident light such that the reflected or transmitted light has an intensity and/or phase which depends on this intensity, - the refractive layers (12, 13) are configured such that the reflectance and transmittance spectra of the optical component have a plateau section including the centre wavelength of the light field, - the non-linear contribution (n 2) is below 10 -12 cm 2 /W, characterized in that - the dielectric layers are made of at least one of Ta 2 O 5, Nb 2 O 5,HfO 2, TiO 2, ZrO 2, Al 2 O 3 and SiO 2, and - the semiconductor layers are made of at least one of Ge, Si and ZnSe.
An electronic apparatus comprising: an exterior body having a sidewall (11R, 11L); a pressure-sensitive sensor having a sensing face, wherein the pressure-sensitive sensor includes an electrostatic-capacity-type sensor electrode unit having an elongated rectangular shape and a plurality of sensing units; a first reference electrode layer opposed to a first main face of the sensor electrode unit; a second reference electrode layer opposed to a second main face of the sensor electrode unit; and a deformable layer (23, 24) provided at least either between the first reference electrode layer and the sensor electrode unit or between the second reference electrode layer and the sensor electrode unit, the deformable layer (23, 24) being elastically deformed by application of pressure; and a support supporting the pressure-sensitive sensor such that an inner face (11SR, 11SL) of the sidewall (11R, 11L) of the exterior body is opposed to the sensing face, wherein the sidewall (11R, 11L) of the exterior body is capable of pressing the sensing face such that the exterior body presses against the sensing face. an exterior body having a sidewall (11R, 11L); a pressure-sensitive sensor having a sensing face, wherein the pressure-sensitive sensor includes an electrostatic-capacity-type sensor electrode unit having an elongated rectangular shape and a plurality of sensing units; a first reference electrode layer opposed to a first main face of the sensor electrode unit; a second reference electrode layer opposed to a second main face of the sensor electrode unit; and a deformable layer (23, 24) provided at least either between the first reference electrode layer and the sensor electrode unit or between the second reference electrode layer and the sensor electrode unit, the deformable layer (23, 24) being elastically deformed by application of pressure; and an electrostatic-capacity-type sensor electrode unit having an elongated rectangular shape and a plurality of sensing units; a first reference electrode layer opposed to a first main face of the sensor electrode unit; a second reference electrode layer opposed to a second main face of the sensor electrode unit; and a deformable layer (23, 24) provided at least either between the first reference electrode layer and the sensor electrode unit or between the second reference electrode layer and the sensor electrode unit, the deformable layer (23, 24) being elastically deformed by application of pressure; and a support supporting the pressure-sensitive sensor such that an inner face (11SR, 11SL) of the sidewall (11R, 11L) of the exterior body is opposed to the sensing face, wherein the sidewall (11R, 11L) of the exterior body is capable of pressing the sensing face such that the exterior body presses against the sensing face.
A tunnel wind turbine with a horizontal axis of the rotor rotation, including: - a diffuser in the form of a rotational body the wall of which has, in its axial section, the shape of a convex-concave aeronautical profile with a nose designed to be directed towards inflowing air and which is supported by a wind direction bearing set of a vertical rotation axis on the turbine mast, and - a rotor with blades rotating in the plane of a throat (R t) of the diffuser and lower ends are connected with a hub bearing mounted coaxially with the diffuser and having a contour consistent with an aerodynamic profile of a nacelle which is connected by ribs with the diffuser, characterised in that the lower ends of the blades are set away from the surface of the hub by the dimension of the lower gap, the dimension being determined by the height of the connectors mounted to the lower ends of the blades and to the hub, the dimensions of the upper gap between the upper ends of the blades and the surface of the throat (R t) and the lower gap range from 0.5 to 15% of the radius of the throat (R t), preferably from 3 to 8%. - a diffuser in the form of a rotational body the wall of which has, in its axial section, the shape of a convex-concave aeronautical profile with a nose designed to be directed towards inflowing air and which is supported by a wind direction bearing set of a vertical rotation axis on the turbine mast, and - a rotor with blades rotating in the plane of a throat (R t) of the diffuser and lower ends are connected with a hub bearing mounted coaxially with the diffuser and having a contour consistent with an aerodynamic profile of a nacelle which is connected by ribs with the diffuser, characterised in that the lower ends of the blades are set away from the surface of the hub by the dimension of the lower gap, the dimension being determined by the height of the connectors mounted to the lower ends of the blades and to the hub, the dimensions of the upper gap between the upper ends of the blades and the surface of the throat (R t) and the lower gap range from 0.5 to 15% of the radius of the throat (R t), preferably from 3 to 8%.
A method for threading spokes into a hub with two flanges (6, 7) of a wheel with spokes, wherein each of the flanges (6, 7) is provided with a ring of holes for receiving the spokes, the spokes being threaded by means of two to four spoke ejection devices (9, 10, 11, 12), each successively ejecting a spoke into a hole of a flange (6, 7), the method being characterized in that the ejection devices (9, 10, 11, 12) remain fixed and the hub is gripped, displaced and driven in rotation about its axis by a polyarticulated system controlled to successively position the holes of the flanges (6, 7) in front of the corresponding ejection devices (9, 10, 11, 12) for ejecting and threading the spokes.
A conformal antenna, comprising: a non-planar substrate; a first conductive region disposed on a first side of the substrate; a second conductive region disposed on a second side of the substrate; and a coaxial transmission line, an inner conductor of the coaxial transmission line electrically coupled to the first conductive region and an outer conductor of the coaxial transmission line electrically coupled to the second conductive region, wherein the first conductive region includes one or more first slots, wherein the second conductive region includes at least one structural feature configured to function as a choke when the first and second conductive regions (420,430) are operated together as an antenna and wherein the at least one structural feature comprises one or more second slots configured to inhibit current flow on an exterior of the outer conductor of the coaxial transmission line. a non-planar substrate; a first conductive region disposed on a first side of the substrate; a second conductive region disposed on a second side of the substrate; and a coaxial transmission line, an inner conductor of the coaxial transmission line electrically coupled to the first conductive region and an outer conductor of the coaxial transmission line electrically coupled to the second conductive region, wherein the first conductive region includes one or more first slots, wherein the second conductive region includes at least one structural feature configured to function as a choke when the first and second conductive regions (420,430) are operated together as an antenna and wherein the at least one structural feature comprises one or more second slots configured to inhibit current flow on an exterior of the outer conductor of the coaxial transmission line.
A dispensing screen for dispensing, by evaporation, volatile materials applied thereto, the screen comprising: a sheet of material (20, 108, 203); and diverting means (30, 123, 207) formed on or in the material of the sheet, characterized in that the diverting means form a minimum path length of the sheet for volatile material flowing along it between at least a portion of a first edge and an opposing second edge of the sheet, which minimum path length is longer than the distance between the first and second edges along the surface of the sheet. a sheet of material (20, 108, 203); and diverting means (30, 123, 207) formed on or in the material of the sheet, characterized in that the diverting means form a minimum path length of the sheet for volatile material flowing along it between at least a portion of a first edge and an opposing second edge of the sheet, which minimum path length is longer than the distance between the first and second edges along the surface of the sheet.
A locking device for a component, in particular for an electronic component of a vehicle, the locking device comprising: - at least one housing element of the component; - at least one operation element rotatable about a rotation axis in relation to the housing element; - at least one spring element configured to be supported on the operation element at least indirectly; and - at least one pin configured to be supported on the spring element at least indirectly, the pin being translationally movable in relation to the operation element thereby loading and unloading the spring element; wherein the operation element is rotatable about the rotation axis in relation to the housing element between: - at least one supporting position in which the operation element is supported on the housing element thereby supporting, on the housing element via the operation element, a spring force exerted on the operation element by the loaded spring element and securing the operation element against a translational movement away from the pin in relation to the housing element, and - at least one release position; characterized in that in said release position the operation element is translationally movable in relation to the housing element by the spring force. - at least one housing element of the component; - at least one operation element rotatable about a rotation axis in relation to the housing element; - at least one spring element configured to be supported on the operation element at least indirectly; and - at least one pin configured to be supported on the spring element at least indirectly, the pin being translationally movable in relation to the operation element thereby loading and unloading the spring element; - at least one supporting position in which the operation element is supported on the housing element thereby supporting, on the housing element via the operation element, a spring force exerted on the operation element by the loaded spring element and securing the operation element against a translational movement away from the pin in relation to the housing element, and - at least one release position;
A motion simulating apparatus comprising: a support base; a coupling part, pivotally connected to the support base about a first pivot axis; an occupant platform adapted to carry one or more occupants, the occupant platform being disposed above the support base and pivotally connected to the coupling part about a second pivot axis, the first pivot axis being substantially orthogonal to the second pivot axis; and an actuating system connected with the occupant platform, the actuating system being operable to cause the occupant platform to rotate about the first pivot axis and the second pivot axis, characterised in that the first pivot axis is located at an underside of the second pivot axis. a support base; a coupling part, pivotally connected to the support base about a first pivot axis; an occupant platform adapted to carry one or more occupants, the occupant platform being disposed above the support base and pivotally connected to the coupling part about a second pivot axis, the first pivot axis being substantially orthogonal to the second pivot axis; and an actuating system connected with the occupant platform, the actuating system being operable to cause the occupant platform to rotate about the first pivot axis and the second pivot axis, characterised in that the first pivot axis is located at an underside of the second pivot axis.
A heat exchanger comprising - a bundle of at least two heat exchanger tubes, wherein the bundle of heat exchanger tubes has been vertically oriented and is terminated at the bottom by a heat exchanger tube plate, - a heat exchanger housing surrounding the bundle of heat exchanger tubes, wherein a liquid heat-transfer medium is passed around the bundle of heat exchanger tubes in the heat exchanger housing, - a heat exchanger cap sealing the top of the heat exchanger housing, - a heat exchanger bottom sealing the bottom of the heat exchanger housing, - a feed point for the heat-transfer medium, wherein said feed point is provided on the heat exchanger housing and leads into the heat exchanger, - an outlet for the heat-transfer medium, wherein said outlet is provided on the heat exchanger housing and leads out of the heat exchanger, - an emergency relief port disposed in proximity to the heat exchanger cap, wherein the heat exchanger comprises a second safety device disposed in proximity to the heat exchanger bottom, wherein the second safety device is an emergency depressurization means. - a bundle of at least two heat exchanger tubes, wherein the bundle of heat exchanger tubes has been vertically oriented and is terminated at the bottom by a heat exchanger tube plate, - a heat exchanger housing surrounding the bundle of heat exchanger tubes, wherein a liquid heat-transfer medium is passed around the bundle of heat exchanger tubes in the heat exchanger housing, - a heat exchanger cap sealing the top of the heat exchanger housing, - a heat exchanger bottom sealing the bottom of the heat exchanger housing, - a feed point for the heat-transfer medium, wherein said feed point is provided on the heat exchanger housing and leads into the heat exchanger, - an outlet for the heat-transfer medium, wherein said outlet is provided on the heat exchanger housing and leads out of the heat exchanger, - an emergency relief port disposed in proximity to the heat exchanger cap,