mhurhangee/ep-ind-claims huggingface dataset:
A system (100, 108) for conducting performance analysis on a frame of a multi-frame video sequence generated during execution of an application, comprising: (i) a hardware engine configured to execute the application; (ii) a library capture module being configured to obtain command buffer ('push buffer') data from the hardware engine, the push buffer data being for the frame of the multi-frame video sequence; (iii) a graphical user interface for presenting an interactive display of contents of the push buffer data, the contents defining a plurality of commands and data associated with each of the plurality of commands, the graphical user interface enabling access to make changes to the contents of the push buffer,; and (iv) a replay module enabling re-execution of the push buffer data with any changes made through the graphical user interface; wherein the graphical user interface provides a plurality of performance analysis measurements that quantify differences in execution of the push buffer when changes to the push buffer are made, char acterised in that the graphical user interface enables access to an option for the removal of off-screen objects from the push buffer; and wherein push buffer data with any changes made may be used as the reference point for performance analysis measurements when making additional modifications to push buffer data. (i) a hardware engine configured to execute the application; (ii) a library capture module being configured to obtain command buffer ('push buffer') data from the hardware engine, the push buffer data being for the frame of the multi-frame video sequence; (iii) a graphical user interface for presenting an interactive display of contents of the push buffer data, the contents defining a plurality of commands and data associated with each of the plurality of commands, the graphical user interface enabling access to make changes to the contents of the push buffer,; and (iv) a replay module enabling re-execution of the push buffer data with any changes made through the graphical user interface; wherein the graphical user interface provides a plurality of performance analysis measurements that quantify differences in execution of the push buffer when changes to the push buffer are made, char acterised in that the graphical user interface enables access to an option for the removal of off-screen objects from the push buffer; and wherein push buffer data with any changes made may be used as the reference point for performance analysis measurements when making additional modifications to push buffer data.
A gas turbine engine comprising: a core engine housing; a nacelle positioned radially outwardly of said core engine housing, and an outer bypass housing positioned outwardly of said nacelle; there being at least one accessory to be cooled positioned in a chamber radially between said core engine housing and said nacelle; and a manifold for delivering cooling air into said chamber, said manifold extending circumferentially about a central axis of said core engine, and said manifold having an asymmetric flow cross-section across a circumferential extent; wherein an inlet tube for said manifold captures air from a bypass duct defined between said outer bypass housing and said nacelle, characterised in that said manifold has a greater cross-sectional area associated with a circumferential location where said inlet tube enters said manifold, and having a lesser cross-sectional area at locations spaced circumferentially from said area of greater flow cross-sectional area. a core engine housing; a nacelle positioned radially outwardly of said core engine housing, and an outer bypass housing positioned outwardly of said nacelle; there being at least one accessory to be cooled positioned in a chamber radially between said core engine housing and said nacelle; and a manifold for delivering cooling air into said chamber, said manifold extending circumferentially about a central axis of said core engine, and said manifold having an asymmetric flow cross-section across a circumferential extent; wherein an inlet tube for said manifold captures air from a bypass duct defined between said outer bypass housing and said nacelle, characterised in that said manifold has a greater cross-sectional area associated with a circumferential location where said inlet tube enters said manifold, and having a lesser cross-sectional area at locations spaced circumferentially from said area of greater flow cross-sectional area.
A method in a multi-carrier transmitter comprising: receiving a timing adjustment value; determining from the received timing adjustment value an integer portion and a fractional portion; in the frequency domain, applying the determined fractional portion by rotating a signal; and in the time domain, applying the determined integer portion by one of inserting samples in the rotated signal or removing samples from the rotated signal in an amount corresponding to the determined integer portion, wherein rotating the signal comprises: X ε k = { X k exp j 2 π N k − N a 2 1 − ε, ε > 0 X k exp − j 2 π N k + N a 2 ε, ε ≤ 0; wherein -1 ≤ ε ≤ 1 is the determined fractional portion, X [ k] is the signal prior to rotation, k =0,1,..., N a -1, N a is a number of active sub-carriers, and N is a total number of sub-carriers; and subsequently, transmitting the signal. receiving a timing adjustment value; determining from the received timing adjustment value an integer portion and a fractional portion; in the frequency domain, applying the determined fractional portion by rotating a signal; and in the time domain, applying the determined integer portion by one of inserting samples in the rotated signal or removing samples from the rotated signal in an amount corresponding to the determined integer portion,
A developer carrying member comprising a base member and a surface layer, wherein the surface layer includes a urethane resin, and the urethane resin has a carbonate bond and includes a tertiary amine structure. wherein the surface layer includes a urethane resin, and the urethane resin has a carbonate bond and includes a tertiary amine structure.
A resonator device (101, 301) for damping a pressure oscillation within a combustion chamber, the resonator device comprising: • a container (102, 302) filled with a gas; • an opening (106, 306) in the container; and • a heating element (103, 303), characterised in that the heating element is adapted to generate a flame, wherein the flame is arranged to heat the gas within the container. • a container (102, 302) filled with a gas; • an opening (106, 306) in the container; and • a heating element (103, 303), characterised in that the heating element is adapted to generate a flame,
A rare-cutting endonuclease suitable to contract highly repetitive triplet motives in a gene comprising triplet repeats, characterized in that said rare-cutting endonuclease is a chimeric endonuclease which comprises (i) a binding domain that recognizes a target sequence spanning at least 10 nucleic acid bases adjacent to a triplet repeat sequence responsible for a triplet repeat disease and at least 5 nucleic acid bases inside the triplet repeat sequence, and (ii) an endonuclease domain that specifically cleaves within said triplet repeat sequence.
A power transmission device comprising: a motor; a first planetary reduction gear connected downstream of the motor; a second planetary reduction gear connected downstream of the first planetary reduction gear; a differential gear connected downstream of the second planetary reduction gear; and a drive shaft connected downstream of the differential gear, wherein the drive shaft is arranged penetrating an inner circumference of a rotor of the motor, an inner circumference of a sun gear of the first planetary reduction gear, and an inner circumference of a sun gear of the second planetary reduction gear, and a pinion of the first planetary reduction gear is a stepless pinion, and a pinion of the second planetary reduction gear is a stepped pinion, characterized in that the carrier of the first planetary reduction gear overlaps with the sun gear of the first planetary reduction gear in an axial direction, and the carrier of the first planetary reduction gear is supported by a part that integrally rotates with the sun gear of the first planetary reduction gear via a thrust bearing. a motor; a first planetary reduction gear connected downstream of the motor; a second planetary reduction gear connected downstream of the first planetary reduction gear; a differential gear connected downstream of the second planetary reduction gear; and a drive shaft connected downstream of the differential gear, wherein the drive shaft is arranged penetrating an inner circumference of a rotor of the motor, an inner circumference of a sun gear of the first planetary reduction gear, and an inner circumference of a sun gear of the second planetary reduction gear, and a pinion of the first planetary reduction gear is a stepless pinion, and a pinion of the second planetary reduction gear is a stepped pinion, characterized in that the carrier of the first planetary reduction gear overlaps with the sun gear of the first planetary reduction gear in an axial direction, and the carrier of the first planetary reduction gear is supported by a part that integrally rotates with the sun gear of the first planetary reduction gear via a thrust bearing.
A feeding arrangement for feeding biomass having a material density of not more than 200 kg/m 3 to a treatment vessel, the feeding arrangement comprising: • a plug screw feeder for feeding the biomass to the treatment vessel, the plug screw feeder comprising a plug screw and a corresponding plug screw housing surrounding the plug screw; • a force-feeding screw for feeding the biomass to the plug screw feeder and a corresponding force-feeding screw housing surrounding the force feeding screw; and • a feeding device being arranged to feed incoming biomass to the force-feeding screw; wherein the force feeding screw is arranged to provide the biomass to an inlet section of the plug screw feeder; the longitudinal axis of the force-feeding screw is arranged essentially perpendicular to the longitudinal axis of the plug screw; and the plug screw is adapted to be able to be rotated at variable speed in relation to a production flow rate set by the feeding device; characterized in that the feeding arrangement further comprises • a monitoring device configured to monitoring at least one parameter related to the load of the force-feeding screw, which is a parameter which is connected to the energy consumption of the force-feeding screw; and • an adjustment device configured to adjusting the rotational speed of the plug screw to the at least one parameter related to the load of the force-feeding screw. • a plug screw feeder for feeding the biomass to the treatment vessel, the plug screw feeder comprising a plug screw and a corresponding plug screw housing surrounding the plug screw; • a force-feeding screw for feeding the biomass to the plug screw feeder and a corresponding force-feeding screw housing surrounding the force feeding screw; and • a feeding device being arranged to feed incoming biomass to the force-feeding screw; wherein the force feeding screw is arranged to provide the biomass to an inlet section of the plug screw feeder; the longitudinal axis of the force-feeding screw is arranged essentially perpendicular to the longitudinal axis of the plug screw; and the plug screw is adapted to be able to be rotated at variable speed in relation to a production flow rate set by the feeding device; characterized in that the feeding arrangement further comprises wherein the force feeding screw is arranged to provide the biomass to an inlet section of the plug screw feeder; the longitudinal axis of the force-feeding screw is arranged essentially perpendicular to the longitudinal axis of the plug screw; and the plug screw is adapted to be able to be rotated at variable speed in relation to a production flow rate set by the feeding device; characterized in that the feeding arrangement further comprises • a monitoring device configured to monitoring at least one parameter related to the load of the force-feeding screw, which is a parameter which is connected to the energy consumption of the force-feeding screw; and • an adjustment device configured to adjusting the rotational speed of the plug screw to the at least one parameter related to the load of the force-feeding screw.
A electric jigsaw, comprising: a motor; a plunger driven by the motor and reciprocating between a top dead center and a bottom dead center, a cutting blade mounted to one end of the plunger in a reciprocating direction, the cutting blade being mounted on the plunger such that the cutting teeth section faces upward and forward in the cutting direction and the back section faces rearward in the cutting direction; and a trigger switch that is operable by a user, characterised in that the motor is a brushless motor and in that the jigsaw further comprises control means for controlling the brushless motor to stop the plunger in a predetermined stop area when the control means receives a stop signal through the trigger switch, wherein the predetermined stop area is in proximity to the top dead center. a motor; a plunger driven by the motor and reciprocating between a top dead center and a bottom dead center, a cutting blade mounted to one end of the plunger in a reciprocating direction, the cutting blade being mounted on the plunger such that the cutting teeth section faces upward and forward in the cutting direction and the back section faces rearward in the cutting direction; and a trigger switch that is operable by a user,
Control system for a technical plant, wherein the control system has control units (4.1 to 4.5) on the plant side for controlling, maintaining and/or monitoring the technical plant, has a management system external to the plant for remote control, remotely maintaining and/or remotely monitoring the technical plant and a data link between the management system and the control units (4.1 to 4.5), and wherein the control units (4.1 to 4.5) are controlled and configured by remote access by means of the management system, characterised by a first demilitarised zone, via which the data link is routed between the management system and the control units (4.1 to 4.5).
A virtual card downloading method, the method comprising: establishing, by a terminal, a near field communication connection to an intermediate device connected to a server, wherein the near field communication connection comprises a Bluetooth connection or WiFi connection, and wherein the terminal is not directly connected to the server through a communications network; reporting, by the terminal, terminal information to the server using the intermediate device, wherein the terminal information is used to enable the server to create an account for the terminal, the account is associated with a virtual card data for providing virtual card service, the virtual card data is provided for the terminal by an operator; accessing, by the terminal, the intermediate device by using the account, and downloading the virtual card data, associated with the account created at the server, by the near field communication connection; using, by the terminal, the virtual card service by invoking the virtual card data. establishing, by a terminal, a near field communication connection to an intermediate device connected to a server, wherein the near field communication connection comprises a Bluetooth connection or WiFi connection, and wherein the terminal is not directly connected to the server through a communications network; reporting, by the terminal, terminal information to the server using the intermediate device, wherein the terminal information is used to enable the server to create an account for the terminal, the account is associated with a virtual card data for providing virtual card service, the virtual card data is provided for the terminal by an operator; accessing, by the terminal, the intermediate device by using the account, and downloading the virtual card data, associated with the account created at the server, by the near field communication connection; using, by the terminal, the virtual card service by invoking the virtual card data.
A thrust reverser device for a turbojet engine nacelle comprising at least: - a fixed support structure for a thrust reverser, comprising a longitudinal support half-beam arranged to be pivotally mounted on a suspension pylon and capable of supporting a thrust reverser half-cowl, - the thrust reverser half-cowl slidably mounted on the fixed structure along a direction substantially parallel to a longitudinal axis of the device, by a guide assembly, between a direct jet position and a thrust reversal position, the device being characterized in that the fixed structure further comprises means adapted to circumferentially offset (100, 120, 130), in a plane radial to the longitudinal axis, the guide assembly of the half-cowl between its different positions relative to the half-beam on which the half-cowl is mounted. - a fixed support structure for a thrust reverser, comprising a longitudinal support half-beam arranged to be pivotally mounted on a suspension pylon and capable of supporting a thrust reverser half-cowl, - the thrust reverser half-cowl slidably mounted on the fixed structure along a direction substantially parallel to a longitudinal axis of the device, by a guide assembly, between a direct jet position and a thrust reversal position,
A hollow container manufacturing method, comprising: an injection molding step of forming a preform having a neck portion and a barrel portion, at least a part of the barrel portion being solid, by injection molding; an intermediate product formation step of inserting a boring rod (134, 144) from a side of the neck portion into the barrel portion to form a space part of at least a predetermined depth in the barrel portion, thereby converting the preform into an intermediate molded product; and a final blow molding step of blow molding the intermediate molded product to form a hollow container which is a final molded product; characterized in that during the intermediate product formation step, the space part is formed with the predetermined depth by inserting the boring rod (134, 144) into the barrel portion while jetting air from at least a leading end of the boring rod (134, 144). an injection molding step of forming a preform having a neck portion and a barrel portion, at least a part of the barrel portion being solid, by injection molding; an intermediate product formation step of inserting a boring rod (134, 144) from a side of the neck portion into the barrel portion to form a space part of at least a predetermined depth in the barrel portion, thereby converting the preform into an intermediate molded product; and a final blow molding step of blow molding the intermediate molded product to form a hollow container which is a final molded product; characterized in that during the intermediate product formation step, the space part is formed with the predetermined depth by inserting the boring rod (134, 144) into the barrel portion while jetting air from at least a leading end of the boring rod (134, 144).
Device for generating active haptic feedback, having a piezoelectric actuator which comprises a flat piezoelectric base body with plane-parallel main surfaces as well as first and second actuator electrodes (E 1, E 2), wherein the base body is configured to generate active haptic feedback if a force which is applied to the base body is detected, wherein the haptic feedback is generated by virtue of the fact that an electrical actuator voltage is applied between the first and second actuator electrodes, said volage bringing about, by means of a piezoelectric actuator effect, a change in length of the base body along a line which is perpendicular to one of the main surfaces, wherein a truncated-cone-shaped piece of sheet metal - cymbal- is attached to each of the two main surfaces of the base body in such a way that the obtuse tip of the cone points away from the base body in each case, wherein the base body with the obtuse tips of the cone is secured between a base and an activation means (BP, MB), wherein the activation means is connected to the base and is secured thereto by means of a prestress which is set as a tensile stress or compressive stress, characterized in that a measuring electrode is arranged in the base body, wherein a measuring unit is provided for measuring a measuring volage which is generated between the measuring electrode and one of the actuator electrodes and arises owing to a force which is applied to the base body, and wherein the component is configured to detect this applied force as soon as the measuring voltage which is sensed by the measuring unit exceeds a threshold value which is assigned to a triggering force, wherein when the triggering force is reached by means of a voltage generator an actuator voltage is generated and applied to the actuator electrodes, and at the same time a further action is triggered which serves to operate the device or an electrical component which is connected thereto.
A compound semiconductor laminated substrate (10,20,30,40,50) comprising: two single-crystalline compound semiconductor substrates (1a,1b,2a,2b,3a,3b,4a, 4b,5a,5b) each containing A and B as constituent elements and both having the same composition and the same atomic arrangement, which substrates are directly bonded together and laminated, wherein a front surface and a back surface of the laminated substrate (10,20,30, 40,50) are polar faces made of atoms of the same kind of A or B, and the laminated interface is a unipolar antiphase boundary (1ab,2ab,3ab,4ab,5eb) constituted by bonds of atoms either of A atom to A atom, or B atom to B atom, with coherency of the crystal lattices, wherein the crystal lattice of one single-crystalline compound semiconductor substrate side and the crystal lattice of the other single-crystalline compound semiconductor substrate side are continuously connected together over the entire laminated interface, and the density of incoherent interfaces is less than or equal to 0.1% of the density of atoms constituting the interface over the entire laminated interface, and wherein the crystal orientation of the bonded two single-crystalline compound semiconductor substrates are aligned. two single-crystalline compound semiconductor substrates (1a,1b,2a,2b,3a,3b,4a, 4b,5a,5b) each containing A and B as constituent elements and both having the same composition and the same atomic arrangement, which substrates are directly bonded together and laminated, wherein a front surface and a back surface of the laminated substrate (10,20,30, 40,50) are polar faces made of atoms of the same kind of A or B, and the laminated interface is a unipolar antiphase boundary (1ab,2ab,3ab,4ab,5eb) constituted by bonds of atoms either of A atom to A atom, or B atom to B atom, with coherency of the crystal lattices, wherein the crystal lattice of one single-crystalline compound semiconductor substrate side and the crystal lattice of the other single-crystalline compound semiconductor substrate side are continuously connected together over the entire laminated interface, and the density of incoherent interfaces is less than or equal to 0.1% of the density of atoms constituting the interface over the entire laminated interface, and wherein the crystal orientation of the bonded two single-crystalline compound semiconductor substrates are aligned.