mhurhangee/patent-ind-claim-en huggingface dataset:
An aluminium extrusion framing system , the framing system comprising: a first wedge member made of resilient material for securing and sealing a panel in the framing system ; an aluminium extrusion having a channel adapted to receive an edge of a panel therein, the channel being formed by a pair of opposing side walls, a first side wall having a first elongate retention means extending the full length of the extrusion for receiving the first wedge member in connection therewith, characterised in that said extrusion also has a cavity provided adjacent to the channel between a side wall of the extrusion and the first side wall of the channel; and in that the framing system further comprises a removable cover plate adapted to be secured to the extrusion and received in close proximity to a top edge of the first side wall of the channel so as to cover the cavity to a top edge of the side wall of the extrusion when secured to the extrusion whereby, in use, when a panel is installed in the channel with the first wedge member received in connection with the first retention means , the first wedge member does not protrude above the cover plate and is substantially concealed when the removable cover plate is secured to the extrusion . a first wedge member made of resilient material for securing and sealing a panel in the framing system ; an aluminium extrusion having a channel adapted to receive an edge of a panel therein, the channel being formed by a pair of opposing side walls, a first side wall having a first elongate retention means extending the full length of the extrusion for receiving the first wedge member in connection therewith, characterised in that said extrusion also has a cavity provided adjacent to the channel between a side wall of the extrusion and the first side wall of the channel; and in that the framing system further comprises a removable cover plate adapted to be secured to the extrusion and received in close proximity to a top edge of the first side wall of the channel so as to cover the cavity to a top edge of the side wall of the extrusion when secured to the extrusion whereby, in use, when a panel is installed in the channel with the first wedge member received in connection with the first retention means , the first wedge member does not protrude above the cover plate and is substantially concealed when the removable cover plate is secured to the extrusion .
Granules comprising a fiber reinforced composition (C), comprising i) an at least bimodal propylene polymer (PP), ii) an elastomeric ethylene copolymer (E) being a copolymer of ethylene and a C 4 -C 10 α-olefin, iii) an adhesion promoter (AP), and iv) long fibers (LF), wherein said fiber reinforced composition (C) fulfils in-equation (I) w PP w E > 4.2 wherein w(PP) is the weight fraction [in wt.-%] of the propylene polymer (PP), based on the overall weight of the polypropylene composition (C), and w(E) is the weight fraction [in wt.-%] of the elastomeric ethylene copolymer (E), based on the overall weight of the fiber reinforced composition (C) i) an at least bimodal propylene polymer (PP), ii) an elastomeric ethylene copolymer (E) being a copolymer of ethylene and a C 4 -C 10 α-olefin, iii) an adhesion promoter (AP), and iv) long fibers (LF),
Method for controlling a hill-start assist (RSP) for a vehicle, in particular a commercial vehicle, having a power-assisted brake system and having electronic brake control (EBS), wherein the vehicle can be kept at a standstill on a flat or inclined road by its service brake system, even without driver operation of the brake pedal, by automatically introducing a hill-start assist pressure into the wheel brakes, wherein the hill-start assist pressure is a function of the road inclination and at least one variable derived from the weight of the vehicle, and the hill-start assist pressure is proportional to the product of the absolute value of the road inclination and the weight of the vehicle, characterized in that the hill-start assist pressure is calculated internally in the vehicle using the formula RSP _ pressure = RSP _ inclination × U _ F , where RSP_pressure = hill-start assist pressure RSP_inclination = verified vehicle inclination U_F = function of the vehicle braking pressure level from earlier braking operations. RSP_pressure = hill-start assist pressure RSP_inclination = verified vehicle inclination U_F = function of the vehicle braking pressure level from earlier braking operations.
In vitro method for prognosis of the susceptibility to environmental stress of an individual, the method comprising : a. a step of determining the translation initiation sequence, or KOZAK sequence, of Ccnd1 gene, from a biological sample of said individual and comparing with the corresponding reference sequence in order to identify mutations, b. a step of quantifying the expression of the protein coded by said gene the KOZAK sequence of which was determined in the previous step, and comparing with the expression level of the protein obtained from a reference sample, such that if the KOZAK sequence comprises a mutation and the expression level of the protein is modified relative to the reference level, said individual will be likelier to develop a pathology related to an environmental stress. a. a step of determining the translation initiation sequence, or KOZAK sequence, of Ccnd1 gene, from a biological sample of said individual and comparing with the corresponding reference sequence in order to identify mutations, b. a step of quantifying the expression of the protein coded by said gene the KOZAK sequence of which was determined in the previous step, and comparing with the expression level of the protein obtained from a reference sample,
A computer-implemented method for identifying a first three-dimensional, 3D, plane corresponding to a floor and being perpendicular to a gravity vector , the method comprising: receiving a first image taken at a first location and a second image taken at a second location different from the first location; evaluating a plurality of second 3D planes (106A-C) perpendicular to the gravity vector by mapping the first image onto a second 3D plane to create a texture-mapped 3D plane, the second 3D plane being perpendicular to the gravity vector, creating an artificial second image from the texture-mapped 3D plane , and computing a score of image similarity based upon a similarity between the second image and the artificial second image; and selecting one of the plurality of second 3D planes having a highest score of image similarity between the second image and the artificial second image as the first 3D plane corresponding to the floor. receiving a first image taken at a first location and a second image taken at a second location different from the first location; evaluating a plurality of second 3D planes (106A-C) perpendicular to the gravity vector by mapping the first image onto a second 3D plane to create a texture-mapped 3D plane, the second 3D plane being perpendicular to the gravity vector, creating an artificial second image from the texture-mapped 3D plane , and computing a score of image similarity based upon a similarity between the second image and the artificial second image; and selecting one of the plurality of second 3D planes having a highest score of image similarity between the second image and the artificial second image as the first 3D plane corresponding to the floor.
A bladed rotor system for a turbomachine, comprising: a circumferential row of blades mounted on a rotor disc , each blade comprising an airfoil having an outer wall delimiting an airfoil interior, the airfoil interior comprising one or more internal cavities , the row of blades comprising a first set (H) of blades and a second set (L) of blades , wherein: the airfoils of both the first and second sets (H, L) of blades have identical outer shapes defined by an outer surface of the outer wall of the respective airfoils , and the airfoils of the first set (H) of blades are distinguished from the airfoils of the second set (L) of blades by a geometry and/or position of at least one internal cavity , which is unique to blades of a given set (H, L), said at least one cavity being a trailing edge cooling passage, whereby the natural frequency of a blade of the first set (H) differs from the natural frequency of a blade of the second set (L) by a predetermined amount, wherein blades of the first set (H) and the second set (L) are alternately arranged in a periodic fashion in said circumferential row, to provide a frequency mistuning to stabilize flutter of the blades . a circumferential row of blades mounted on a rotor disc , each blade comprising an airfoil having an outer wall delimiting an airfoil interior, the airfoil interior comprising one or more internal cavities , the row of blades comprising a first set (H) of blades and a second set (L) of blades , wherein: the airfoils of both the first and second sets (H, L) of blades have identical outer shapes defined by an outer surface of the outer wall of the respective airfoils , and the airfoils of the first set (H) of blades are distinguished from the airfoils of the second set (L) of blades by a geometry and/or position of at least one internal cavity , which is unique to blades of a given set (H, L), said at least one cavity being a trailing edge cooling passage, the airfoils of both the first and second sets (H, L) of blades have identical outer shapes defined by an outer surface of the outer wall of the respective airfoils , and the airfoils of the first set (H) of blades are distinguished from the airfoils of the second set (L) of blades by a geometry and/or position of at least one internal cavity , which is unique to blades of a given set (H, L), said at least one cavity being a trailing edge cooling passage, whereby the natural frequency of a blade of the first set (H) differs from the natural frequency of a blade of the second set (L) by a predetermined amount, wherein blades of the first set (H) and the second set (L) are alternately arranged in a periodic fashion in said circumferential row, to provide a frequency mistuning to stabilize flutter of the blades .
High pressure cleaning appliance having a pump for conveying a cleaning liquid, wherein the pump comprises a suction conduit and a pressure conduit and a check valve is arranged in the pressure conduit , and wherein the pump comprises an overflow valve which, in dependence on the pressure of the cleaning liquid prevailing in the pressure conduit , unblocks a flow path via an overflow conduit for discharging cleaning liquid from the pressure conduit , wherein the overflow valve comprises a closing body which, in a closing position, abuts in a liquid-tight manner against a valve seat , and which is moveable against the closing force of a closing spring into an open position at a distance from the valve seat and which is connected by way of a valve rod to a control piston that is displaceably held in a control chamber and is able to be acted upon with pressurized cleaning liquid, and wherein the control piston subdivides the control chamber into an outlet pressure chamber and an overflow chamber , wherein the outlet pressure chamber is connected by way of a pressure channel to a region of the pressure conduit arranged downstream from the check valve and has a first passage opening , and wherein the overflow chamber is connected by way of a conduit portion of the overflow conduit to a region of the pressure conduit arranged upstream from the check valve and has a second passage opening that forms the valve seat , wherein the two passage openings are of different size, characterized in that the first passage opening is passed through in a liquid-tight manner by a piston rod fixed to the control piston and the control piston is able to be acted upon on its side facing toward the larger passage opening by the closing force of the closing spring .
Hybrid drive , comprising a power-split, power-shiftable transmission , which has a shiftable transmission , such as a spur gear countershaft transmission , with a coaxial central shaft (25, 125, 225, 325, 525, 625, 825, 1125, 1125 I ) configured as a hollow shaft/inner shaft pair, and a power-split transmission arranged in drive terms upstream of the shiftable transmission , such as the spur gear countershaft transmission , wherein the hybrid drive includes at least three power-generating machines (3, 5, 7; 103, 105, 107; 203, 205, 207; 303, 305, 307), of which at least two are electric machines (5, 7; 105, 107; 205, 207; 305, 307) that can be used as drive motors and/or as generators, and two of the power-generating machines (3, 5, 7; 103, 105, 107; 203, 205, 207; 303, 305, 307), of which at least one can be operated both as a drive motor and as an electric generator, are each connected or able to be connected to a shaft of the coaxial central shaft (25, 125, 225, 325, 525, 625, 825, 1125, 1125 I ) in a rotatable and/or rotationally fixed manner, wherein a first claw shift element having at least four shift positions is arranged as a power flow connector between a rotating body of the power-split transmission , such as a sun gear, and one of the shafts of the central shaft (25, 125, 225, 325, 525, 625, 825, 1125, 1125 I ), which first claw shift element can make shift changes even under load, without tractive power being interrupted due to the shift change. comprising a power-split, power-shiftable transmission , which has a shiftable transmission , such as a spur gear countershaft transmission , with a coaxial central shaft (25, 125, 225, 325, 525, 625, 825, 1125, 1125 I ) configured as a hollow shaft/inner shaft pair, and a power-split transmission arranged in drive terms upstream of the shiftable transmission , such as the spur gear countershaft transmission , wherein the hybrid drive includes at least three power-generating machines (3, 5, 7; 103, 105, 107; 203, 205, 207; 303, 305, 307), of which at least two are electric machines (5, 7; 105, 107; 205, 207; 305, 307) that can be used as drive motors and/or as generators, and two of the power-generating machines (3, 5, 7; 103, 105, 107; 203, 205, 207; 303, 305, 307), of which at least one can be operated both as a drive motor and as an electric generator, are each connected or able to be connected to a shaft of the coaxial central shaft (25, 125, 225, 325, 525, 625, 825, 1125, 1125 I ) in a rotatable and/or rotationally fixed manner, wherein a first claw shift element having at least four shift positions is arranged as a power flow connector between a rotating body of the power-split transmission , such as a sun gear, and one of the shafts of the central shaft (25, 125, 225, 325, 525, 625, 825, 1125, 1125 I ), which first claw shift element can make shift changes even under load, without tractive power being interrupted due to the shift change.
A toolpath evaluation method evaluating a toolpath when a rotary tool moves relative to a workpiece while processing the workpiece, the toolpath evaluation method comprising: a calculation step of using a predetermined target toolpath and a shape of the workpiece before processing by the target toolpath as a basis to calculate a size of a contact area predicted to actually be in contact with the workpiece during processing by the target toolpath; and a judging step of judging that the target toolpath is unsuitable when the size of the contact area exceeds a predetermined threshold value; wherein: the calculated contact area is on a bottom surface portion of the rotary tool intersecting a rotational axis of the tool, and in that the bottom surface portion of the rotary tool is in the form of a flat shaped end face or is in the form of a curved end face included within a virtual cone having a vertex on the rotational axis of the rotary tool. a calculation step of using a predetermined target toolpath and a shape of the workpiece before processing by the target toolpath as a basis to calculate a size of a contact area predicted to actually be in contact with the workpiece during processing by the target toolpath; and a judging step of judging that the target toolpath is unsuitable when the size of the contact area exceeds a predetermined threshold value; wherein: the calculated contact area is on a bottom surface portion of the rotary tool intersecting a rotational axis of the tool, and in that the bottom surface portion of the rotary tool is in the form of a flat shaped end face or is in the form of a curved end face included within a virtual cone having a vertex on the rotational axis of the rotary tool.
A method of routing misbehavior detection reports from vehicle-to-everything, V2X, onboard equipment to an entity associated with the V2X onboard equipment, the method comprising: routing a misbehavior detection report to the entity associated with the V2X onboard equipment based on a combination of: information stored in a misbehavior report router, MRR, resulting from a provisioning of a certificate to the V2X onboard equipment; and information included in the misbehavior detection report received from the V2X onboard equipment. information stored in a misbehavior report router, MRR, resulting from a provisioning of a certificate to the V2X onboard equipment; and information included in the misbehavior detection report received from the V2X onboard equipment.
Fluid connection , comprising a connection fitting which has an opening pin , and a valve and/or measurement coupling for fluidic systems for detecting operating pressures of fluidic media, which comprises a coupling bushing that in the installed state is under the operating pressure and has a connection part , and having a bore in which a springloaded and mechanically activatable check valve is disposed, the valve member of the latter in the non-activated state being supported on a valve seat and being able to be contacted by the contact face of the opening pin , wherein the connection fitting is conceived to be screwed to the connection part of the valve and/or measurement coupling , and wherein the opening pin has an in particular circular closed contact face for the valve , and at least one passage which runs laterally in relation to the contact face by way of which a connection between the connection fitting and the valve and/or measurement coupling can be established, characterized in that the valve and/or measurement coupling comprises an annular seal which is disposed in a groove of the valve member , wherein the groove has a trapezoidal cross section which tapers in the radial direction.
A vent hole cleaning apparatus for cleaning a vent hole provided on a molding surface of a mold for vulcanizing a rubber product comprising: a detecting means for detecting a shape of the molding surface ; and a cleaning means for cleaning the vent hole , characterized in that the vent hole cleaning apparatus further comprises: a controlling means for storing in advance molding surface information including shape information of the molding surface including a position of the vent hole and for calculating the position of the vent hole by comparing the shape of the molding surface obtained by the detecting means with the molding surface information; and a guiding means for moving the cleaning means based on the calculated position of the vent hole . a detecting means for detecting a shape of the molding surface ; and a cleaning means for cleaning the vent hole , characterized in that the vent hole cleaning apparatus further comprises: a controlling means for storing in advance molding surface information including shape information of the molding surface including a position of the vent hole and for calculating the position of the vent hole by comparing the shape of the molding surface obtained by the detecting means with the molding surface information; and a guiding means for moving the cleaning means based on the calculated position of the vent hole . a controlling means for storing in advance molding surface information including shape information of the molding surface including a position of the vent hole and for calculating the position of the vent hole by comparing the shape of the molding surface obtained by the detecting means with the molding surface information; and a guiding means for moving the cleaning means based on the calculated position of the vent hole .
Device for carrying out a method for joining two plastic parts along a predefinable common joint using infrared radiation (IR), wherein both plastic parts to be joined together are heated at least along the joint without contacting the other plastic part by means of an assignable radiation source with infrared radiation, wherein the respective one radiation source is operated independently and spatially separated from the further radiation source, wherein the radiation sources emit the respective infrared radiation to the respectively assignable plastic part without contact and following the contour of the joint and wherein the degree of heating by means of the respective infrared radiation is selected in such a manner that, when the plastic parts are brought together, the joint is formed, the device being configured in such a manner that the respective radiation source is formed of an IR radiation element which is arranged in a respectively associated heating element and follows the contour to be irradiated without contact of an assignable plastic part , and characterised in that the respective IR radiation element has at least two radiating surfaces oriented differently from each other.
A method , comprising: monitoring a vertical speed and a forward speed of a rotorcraft; determining whether to perform vortex ring state (VRS) avoidance according to at least one of the vertical speed and the forward airspeed of the rotorcraft; and performing , in response to determining to perform the VRS avoidance, control of one or more flight parameters of the rotorcraft; wherein the performing is carried out according to a relationship between a power margin available from one or more engines of the rotorcraft and a power margin threshold. monitoring a vertical speed and a forward speed of a rotorcraft; determining whether to perform vortex ring state (VRS) avoidance according to at least one of the vertical speed and the forward airspeed of the rotorcraft; and performing , in response to determining to perform the VRS avoidance, control of one or more flight parameters of the rotorcraft; wherein the performing is carried out according to a relationship between a power margin available from one or more engines of the rotorcraft and a power margin threshold.