mhurhangee/ep-ind-claims huggingface dataset:
A generator set comprising an internal combustion piston engine, an electric generator mechanically coupled with the internal combustion piston engine so as to receive power to rotate the electric generator and a common base frame is constructed of suitable steel such that it comprises at least two parallel longitudinal beams (18.1, 18.2) substantially parallel with the longitudinal direction of the engine, and the at least two parallel longitudinal beams (18.1, 18.2) are coupled with each other at least at the ends of the longitudinal beams (18.1,18.2) by means of cross beams (18.3) of suitable length providing suitable distance between the longitudinal beams (18.1, 18.2), which common base frame the internal combustion piston engine and the electric generator are supported on and attached to, characterized in that the base frame of the generator set is provided with plurality of resonator units (20, 20') comprising a bordered resonator space, which resonator space is provided with at least one communication port so as to allow communication between the resonator space and its surroundings, and wherein the resonator space is inside the longitudinal beam (18.1, 18.2, 18.3) under the engine and the electric generator.
A beam for suspending a turboshaft engine from the structure of an aircraft, extending overall in a direction and comprising at least one first attachment means (12, 32, 112, 212) designed to be fixed to said aircraft structure and at least one second attachment means designed to be fixed to the engine, said first attachment means (12, 32, 112, 215, 215') comprising a mounting plate in which housings (12a, 112a, 219, 219') are arranged for fixing means to the structure of the aircraft, characterized in that the beam (11; 111; 211; 213') is made at least in part of metal matrix composite incorporating reinforcing fibers, notably parallel to said direction.
A gas turbine engine comprising: a fan; a fan drive gear system coupled to drive the fan about an engine central axis; a compressor section including a first compressor and a second compressor; a turbine section including: a first turbine coupled to drive a first spool, the first spool being coupled at a first axial position (A 1) to a compressor hub that is coupled to drive the first compressor and the first spool being coupled at a second, different axial position (A 2) to a fan drive input shaft that is coupled to drive the fan drive gear system, at least one sensor target coupled to rotate with the first spool, and a second turbine coupled through a second spool to drive the second compressor; and characterized by a sensor probe operable together with the sensor target to determine a rotational speed of the first spool, the sensor probe being located at a third axial position (A 3) that is axially forward of the first axial position and axially aft of the second axial position. a fan; a fan drive gear system coupled to drive the fan about an engine central axis; a compressor section including a first compressor and a second compressor; a turbine section including: a first turbine coupled to drive a first spool, the first spool being coupled at a first axial position (A 1) to a compressor hub that is coupled to drive the first compressor and the first spool being coupled at a second, different axial position (A 2) to a fan drive input shaft that is coupled to drive the fan drive gear system, at least one sensor target coupled to rotate with the first spool, and a second turbine coupled through a second spool to drive the second compressor; and characterized by a sensor probe operable together with the sensor target to determine a rotational speed of the first spool, the sensor probe being located at a third axial position (A 3) that is axially forward of the first axial position and axially aft of the second axial position. a first turbine coupled to drive a first spool, the first spool being coupled at a first axial position (A 1) to a compressor hub that is coupled to drive the first compressor and the first spool being coupled at a second, different axial position (A 2) to a fan drive input shaft that is coupled to drive the fan drive gear system, at least one sensor target coupled to rotate with the first spool, and a second turbine coupled through a second spool to drive the second compressor; and characterized by a sensor probe operable together with the sensor target to determine a rotational speed of the first spool, the sensor probe being located at a third axial position (A 3) that is axially forward of the first axial position and axially aft of the second axial position.
An optical waveguide system, comprising a waveguide; an input coupler (300A, 300B, 300C), provided at an input side of the waveguide and coupling a light into the waveguide; and an output coupler, provided at an output side of the waveguide and coupling the light out of the waveguide, wherein the input coupler (300A, 300B, 300C) includes a right portion and a left portion, wherein the right portion is located at the right side of the input coupler (300A, 300B, 300C) and the left portion is located at the left side of the input coupler (300A, 300B, 300C), from light incident direction, wherein the right portion includes a first polarization volume grating and a second polarization volume grating stacked under the first polarization volume grating, wherein the left portion includes a third polarization volume grating and a fourth polarization volume grating stacked under the third polarization volume grating, wherein the first polarization volume grating and the fourth polarization volume grating are polarization volume gratings optimized for a right-hand-side field of view of the light, and wherein the third polarization volume grating and the second polarization volume grating are polarization volume gratings optimized for a left-hand-side field of view of the light. a waveguide; an input coupler (300A, 300B, 300C), provided at an input side of the waveguide and coupling a light into the waveguide; and an output coupler, provided at an output side of the waveguide and coupling the light out of the waveguide, wherein the input coupler (300A, 300B, 300C) includes a right portion and a left portion, wherein the right portion is located at the right side of the input coupler (300A, 300B, 300C) and the left portion is located at the left side of the input coupler (300A, 300B, 300C), from light incident direction, wherein the right portion includes a first polarization volume grating and a second polarization volume grating stacked under the first polarization volume grating, wherein the left portion includes a third polarization volume grating and a fourth polarization volume grating stacked under the third polarization volume grating, wherein the first polarization volume grating and the fourth polarization volume grating are polarization volume gratings optimized for a right-hand-side field of view of the light, and wherein the third polarization volume grating and the second polarization volume grating are polarization volume gratings optimized for a left-hand-side field of view of the light.
A display apparatus having a uniformity adjustment function, the display apparatus comprising: a display unit which is divided into a plurality of local areas; a signal receiver which receives from a sensor light intensity data of each local area of the plurality of local areas of the display unit; and characterised by a controller configured to analyze the plurality of local areas for non-uniformity correction by comparing a first light intensity data of a first area of the plurality of local areas, which is currently analyzed for the non-uniformity correction, with second light intensity data of at least one second area of the plurality of local areas which has been previously analyzed for the non-uniformity correction, and, in response to the at least one second area being determined to have the second light intensity data within an error range of the first light intensity data of the first local area, the controller is further configured to skip a calibration process with respect to the first area and to use previously stored calibration information of the at least one second area as calibration information for the first area, and, in response to none of the at least one second area being determined to have the second light intensity data within the error range of the first light intensity data of the first area, the controller is configured to perform the calibration process to generate the calibration information of the first area, and to output an image signal to the display unit, wherein the first area and the at least one second area are different areas of the plurality of local areas. a display unit which is divided into a plurality of local areas; a signal receiver which receives from a sensor light intensity data of each local area of the plurality of local areas of the display unit; and characterised by a controller configured to analyze the plurality of local areas for non-uniformity correction by comparing a first light intensity data of a first area of the plurality of local areas, which is currently analyzed for the non-uniformity correction, with second light intensity data of at least one second area of the plurality of local areas which has been previously analyzed for the non-uniformity correction, and, in response to the at least one second area being determined to have the second light intensity data within an error range of the first light intensity data of the first local area, the controller is further configured to skip a calibration process with respect to the first area and to use previously stored calibration information of the at least one second area as calibration information for the first area, and, in response to none of the at least one second area being determined to have the second light intensity data within the error range of the first light intensity data of the first area, the controller is configured to perform the calibration process to generate the calibration information of the first area, and to output an image signal to the display unit, wherein the first area and the at least one second area are different areas of the plurality of local areas.
A method of forming an absorbent core, the method comprising: providing a first material layer; coupling elastic strands under tension to the first material layer to form an elastic and material layer combination; performing a first tension let-off to partially relax the elastic strands, wherein the partial relaxing of the elastic strands deforms the first material layer to form a plurality of valleys in the first material layer for capturing a superabsorbent polymer material; applying the superabsorbent polymer material onto the first material layer; and coupling a second material layer to the elastic and first material layer combination. providing a first material layer; coupling elastic strands under tension to the first material layer to form an elastic and material layer combination; performing a first tension let-off to partially relax the elastic strands, wherein the partial relaxing of the elastic strands deforms the first material layer to form a plurality of valleys in the first material layer for capturing a superabsorbent polymer material; applying the superabsorbent polymer material onto the first material layer; and coupling a second material layer to the elastic and first material layer combination.
A method to facilitate prevention of malicious attacks on a web service, the method comprising: intercepting, by a redirection system, a web request from a client computing system directed to a web server providing the web service; identifying, by the redirection system, whether or not the web request is malicious; in the redirection system, when the web request is identified as malicious, preventing the web request from reaching the web server and instead redirecting the web request to an isolated mitigation server configured to mimic responses of the web server; in the isolated mitigation server, processing the web request to generate artificial content based on the web request that mimics legitimate response behavior of the web server by using a page template associated with a web page targeted by the web request and filling in data values in the page template with false information to dynamically generate the artificial content; and presenting, by the isolated mitigation server, the artificial content to the client computing system in response to the web request. intercepting, by a redirection system, a web request from a client computing system directed to a web server providing the web service; identifying, by the redirection system, whether or not the web request is malicious; in the redirection system, when the web request is identified as malicious, preventing the web request from reaching the web server and instead redirecting the web request to an isolated mitigation server configured to mimic responses of the web server; in the isolated mitigation server, processing the web request to generate artificial content based on the web request that mimics legitimate response behavior of the web server by using a page template associated with a web page targeted by the web request and filling in data values in the page template with false information to dynamically generate the artificial content; and presenting, by the isolated mitigation server, the artificial content to the client computing system in response to the web request.
A valve reading and adjustment tool for use with a valve having a pressure or flow setting adjustable to a plurality of pressure or flow settings, comprising: a signal generator, comprising: an adjustment interface configured to generate an adjustment signal to adjust the pressure or flow setting of the valve; a reading interface configured to generate a reading signal to read the pressure or flow setting of the valve; and at least one excitation coil connected to the signal generator; characterized by the excitation coil being configured to generate an oscillating electromagnetic field based on at least one of the adjustment signal and the reading signal; and further characterized by a sense coil, comprising: a first sense coil portion positioned on a first side of the excitation coil; and a second sense coil portion positioned on an opposite side of the excitation coil than the first portion. a signal generator, comprising: an adjustment interface configured to generate an adjustment signal to adjust the pressure or flow setting of the valve; a reading interface configured to generate a reading signal to read the pressure or flow setting of the valve; and an adjustment interface configured to generate an adjustment signal to adjust the pressure or flow setting of the valve; a reading interface configured to generate a reading signal to read the pressure or flow setting of the valve; at least one excitation coil connected to the signal generator; characterized by the excitation coil being configured to generate an oscillating electromagnetic field based on at least one of the adjustment signal and the reading signal; and further characterized by a sense coil, comprising: a first sense coil portion positioned on a first side of the excitation coil; and a second sense coil portion positioned on an opposite side of the excitation coil than the first portion. a first sense coil portion positioned on a first side of the excitation coil; and a second sense coil portion positioned on an opposite side of the excitation coil than the first portion.
Method for determining a state of a component in a high lift system of an aircraft, the high lift system comprising a central power control unit for providing rotational power by means of a transmission shaft (8, 10); drive stations coupled with the power control unit; movable high lift surfaces; and a control unit (20, 22), wherein each high lift surface is coupled with at least two of the drive stations by means of drive struts (14, 14a), wherein at each high lift surface at least one of the associated drive struts (14, 14a) is a load sensing drive strut; the method comprising the steps of: - extending at least one high lift surface to a first extended position, - acquiring a first load sensed by at least one load sensing drive strut associated with the at least one high lift surface at a first flight state having a first speed, - identifying a nominal load for the acquired first load, which nominal load is to be expected during a normal operation of the aircraft, - acquiring a second load sensed by the at least one load sensing drive strut associated with the at least one high lift surface at a second extended position substantially equal to the first extended position at a second flight state of the aircraft having a second speed, which is lower than the first flight speed and less than 60 knots, - adjusting the value of the first load through subtracting the value of the second load, - comparing the adjusted first load value with the nominal load for the first extended position and the first flight state under consideration of predetermined thresholds (30, 36), and - producing an alarm signal in case the adjusted load is above the nominal load further than an upper predetermined threshold or below the nominal load further than a lower predetermined threshold. - extending at least one high lift surface to a first extended position, - acquiring a first load sensed by at least one load sensing drive strut associated with the at least one high lift surface at a first flight state having a first speed, - identifying a nominal load for the acquired first load, which nominal load is to be expected during a normal operation of the aircraft, - acquiring a second load sensed by the at least one load sensing drive strut associated with the at least one high lift surface at a second extended position substantially equal to the first extended position at a second flight state of the aircraft having a second speed, which is lower than the first flight speed and less than 60 knots, - adjusting the value of the first load through subtracting the value of the second load, - comparing the adjusted first load value with the nominal load for the first extended position and the first flight state under consideration of predetermined thresholds (30, 36), and - producing an alarm signal in case the adjusted load is above the nominal load further than an upper predetermined threshold or below the nominal load further than a lower predetermined threshold.
A packaging machine for packaging products or product groups, in particular paper material or thin cardboard material, wherein the packaging machine comprises the following: - a packaging infeed for feeding flat paper or cardboard blanks; and - a separating device for individually separating the supplied paper or cardboard blanks and for transferring the separated paper or cardboard blanks to a product or a product group to be packaged, wherein the separating device comprises at least one gripper head and preferably exactly two gripper heads opposite one another and a mechanism associated with the at least one gripper head for preferably continuously moving the at least one gripper head on an orbit between the packaging infeed and a transfer region, in which the individual paper or cardboard blanks are transferred from the at least one gripper head to the product or product group to be packaged, wherein the mechanism associated with the at least one gripper head is configured so as to drive the at least one gripper head in a non-uniform orbital movement such that the at least one gripper head is moved more slowly in the region of the packaging infeed and in the transfer region than during the transition of the at least one gripper head from the packaging infeed to the transfer region, characterized in that the at least one gripper head is rotatably supported about a rotational axis, and wherein the mechanism associated with the at least one gripper head is configured so as to drive the at least one gripper head in a cycloidal or cycloid-like orbital movement, wherein the cycloidal or cycloid-like orbital movement is selected such that the at least one gripper head passes through a total of three repeating and consecutive cycloidal or cycloid-like path sections per 360° revolution. - a packaging infeed for feeding flat paper or cardboard blanks; and - a separating device for individually separating the supplied paper or cardboard blanks and for transferring the separated paper or cardboard blanks to a product or a product group to be packaged,
A rare earth-containing Y zeolite, which has a rare earth content as rare earth oxide of 10-25wt%, preferably 11-23wt%; a unit cell size of 2.440-2.472nm, preferably 2.450-2.470nm; a crystallinity of 35-65%, preferably 40-60%; a Si/Al atom ratio in the skeleton of 2.5-5.0; and a product of the ratio of the strength I 1 of the peak at 2θ=11.8±0.1° to the strength I 2 of the peak at 2θ=12.3±0.1° in the X-ray diffraction spectrogram of the zeolite and the weight percent of rare earth as rare earth oxide in the zeolite of higher than 55, wherein the rare earth is selected from lanthanum and cerium or a mixture thereof.