mhurhangee/ep-ind-claims huggingface dataset:
An apparatus to facilitate control flow in a graphics processing system, the apparatus comprising: a graphics processor including: a plurality of processing resources to execute single instruction, multiple data, SIMD; flow control logic configured to detect a diverging control flow in a plurality of SIMD channels, to detect SIMD channels that are active comprising to detect whether the active SIMD channels are spread over multiple SIMD sections, and to identify a code region impacted by the diverging control flow, wherein the control flow logic is further configured to detect whether the active SIMD channels are lower in number than a predetermined threshold percentage of the plurality of SIMD channels, and to pack input to the active SIMD channels into a subset of the SIMD channels upon a determination that the number of active SIMD channels is below the predetermined threshold percentage; and shoot down logic configured to prevent packing input to the active SIMD channels into a subset of the SIMD channels upon detecting that the active SIMD channels are not spread over multiple SIMD sections. a plurality of processing resources to execute single instruction, multiple data, SIMD; flow control logic configured to detect a diverging control flow in a plurality of SIMD channels, to detect SIMD channels that are active comprising to detect whether the active SIMD channels are spread over multiple SIMD sections, and to identify a code region impacted by the diverging control flow, wherein the control flow logic is further configured to detect whether the active SIMD channels are lower in number than a predetermined threshold percentage of the plurality of SIMD channels, and to pack input to the active SIMD channels into a subset of the SIMD channels upon a determination that the number of active SIMD channels is below the predetermined threshold percentage; and shoot down logic configured to prevent packing input to the active SIMD channels into a subset of the SIMD channels upon detecting that the active SIMD channels are not spread over multiple SIMD sections.
Tread profile of a pneumatic vehicle tyre - in particular a commercial vehicle tyre - comprising at least one row of profile blocks, which is delimited in the axial direction A of the tyre by two circumferential grooves (2, 3) and is formed in the circumferential direction U of the tyre by profile block elements arranged one behind the other and respectively spaced apart from one another by transverse grooves, wherein the profile block elements are delimited outwardly in the radial direction R by a radially outer surface forming the ground contact surface, wherein one profile block element is arranged between two transverse grooves that are adjacent in the circumferential direction U and is delimited by them in the circumferential direction U of the tyre, wherein at least one transversely running sipe is respectively formed in the radial outer surface of the profile block element, wherein the sipe is delimited inwardly in the radial direction R respectively by a sipe base and each of the two transverse grooves is delimited inwardly in the radial direction R respectively by a groove base, characterized in that, along their main direction of extent from circumferential groove to circumferential groove, both transverse grooves follow at least in a portion (c Q) of their extent a zigzag- or wave-shaped path, wherein the amplitude A Q of the zigzag or wave shape has its maximum in the groove base and, starting from the groove base, steadily decreases outwards along the radial extent R to the radially outer surface, and in that, along its main direction of extent from circumferential groove to circumferential groove, at least one transversely running sipe of the profile block element follows at least in a portion (c F) of its extent a zigzag- or wave-shaped path, wherein the amplitude A F of the zigzag or wave shape has its maximum in the radial outer surface and, starting from the radially outer surface, steadily decreases inwards along the radial extent R.
An uplink signal power reduction method in a carrier aggregation system, an UE being configured with multiple timing advances, when symbols in uplink channels carried on different carriers are not aligned in the time domain and symbols on different carriers are overlapped in the time domain, if a sum of the transmission power of each uplink channel of said UE is determined to be bigger than a maximum transmission power configured for said UE, then an eNB instructing said UE to reduce a transmission power of said uplink channels in which symbols are overlapped in the time domain on different carriers; wherein said eNB instructing said UE of predefined rules for power reduction; according to said predefined rule instructed by said eNB, said UE reducing said transmission power of said uplink channels in which symbols are overlapped in the time domain on different carriers, wherein, said predefined rules comprises: reducing said transmission power of said uplink channels on each uplink carrier by a same ratio, until the transmission power of said UE does not exceed the maximum transmission power configured for said UE; or, according to a low to high order of priorities of said uplink channels reducing power of each uplink channel, until the transmission power of said UE does not exceed said maximum transmission power configured by said UE; or, only reducing the transmission power of said symbols that are overlapped on said different channels; wherein the priorities of the uplink channels are determined according to: prioritizing in accordance with subframe indexes, and their priorities from high to low being: uplink channels in a former subframe, and uplink channels in a latter subframe; and/or, prioritizing in accordance with the subframe indexes, and its priorities from high to low being: uplink channels in said latter subframe, uplink channels in said former subframe.
A printable substrate comprising a base sheet defining a first surface and a second surface; and a printable coating on the first surface, wherein the printable coating comprises a film-forming binder mixture, a crosslinking agent, a partially hydrolyzed polyvinyl alcohol, a first plurality of first silicon dioxide microparticles, a second plurality of second silicon dioxide microparticles, and a cationic polyelectrolyte serving as a cationic dye fixative, wherein the film-forming binder mixture and the crosslinking agent are capable of reacting to form a 3-dimensional crosslinked material, and wherein the first silicon dioxide microparticles have an average diameter that is smaller than an average diameter of the second silicon dioxide microparticles, characterized in that the printable coating comprises 1% by weight to 10% by weight of inorganic microparticles. a base sheet defining a first surface and a second surface; and a printable coating on the first surface, wherein the printable coating comprises a film-forming binder mixture, a crosslinking agent, a partially hydrolyzed polyvinyl alcohol, a first plurality of first silicon dioxide microparticles, a second plurality of second silicon dioxide microparticles, and a cationic polyelectrolyte serving as a cationic dye fixative, wherein the film-forming binder mixture and the crosslinking agent are capable of reacting to form a 3-dimensional crosslinked material, and wherein the first silicon dioxide microparticles have an average diameter that is smaller than an average diameter of the second silicon dioxide microparticles, characterized in that the printable coating comprises 1% by weight to 10% by weight of inorganic microparticles.
Luminaire for connection in an elongate mounting rail, comprising: a luminaire body for emitting light by means of a lamp, an elongate fastening part extending along a longitudinal axis for mechanical fastening in an elongate mounting rail, wherein the luminaire body is connected to the fastening part in a load-bearing manner, wherein the elongate fastening part comprises a latching element having a latching wing which extends along the longitudinal axis and can be deflected transversely to the longitudinal axis in a deflection direction (R1, R2), wherein the latching wing comprises a coupling projection protruding in the deflection direction (R1, R2), and wherein the elongate fastening part further comprises a wedge element having a wedge portion, characterized in that the latching wing further comprises a deflection angle at the end, with respect to the longitudinal axis, in that the wedge portion is directed toward the deflection angle, and in that the latching element having the latching wing is arranged so as to be movable along the longitudinal axis, relative to the wedge element, so that the wedge portion deflects the latching wing in the deflection direction (R1, R2) by contact with its deflection angle, and thus extends the coupling projection in the deflection direction (R1, R2). a luminaire body for emitting light by means of a lamp, an elongate fastening part extending along a longitudinal axis for mechanical fastening in an elongate mounting rail, wherein the luminaire body is connected to the fastening part in a load-bearing manner, wherein the elongate fastening part comprises a latching element having a latching wing which extends along the longitudinal axis and can be deflected transversely to the longitudinal axis in a deflection direction (R1, R2), wherein the latching wing comprises a coupling projection protruding in the deflection direction (R1, R2), and wherein the elongate fastening part further comprises a wedge element having a wedge portion, characterized in that the latching wing further comprises a deflection angle at the end, with respect to the longitudinal axis, in that the wedge portion is directed toward the deflection angle, and in that the latching element having the latching wing is arranged so as to be movable along the longitudinal axis, relative to the wedge element, so that the wedge portion deflects the latching wing in the deflection direction (R1, R2) by contact with its deflection angle, and thus extends the coupling projection in the deflection direction (R1, R2).
A method of forming a heterojunction transistor, the method comprising: forming an energy barrier (30, 32, 34) comprising a layer of a Group III nitride including indium; forming a channel layer comprising a Group III nitride on the energy barrier wherein a concentration of indium (In) in the energy barrier is greater than a concentration of indium (In) in the channel layer; forming a barrier layer comprising a Group III nitride on the channel layer so that the channel layer is between the barrier layer and the energy barrier wherein the barrier layer has a bandgap greater than a bandgap of the channel layer; and characterized in that forming the channel layer comprises: forming a first portion of the channel layer on the energy barrier at a first temperature; and after forming the first portion of the channel layer, forming a second portion of the channel layer at a second temperature on the first portion of the channel layer wherein the first temperature is less than the second temperature. forming an energy barrier (30, 32, 34) comprising a layer of a Group III nitride including indium; forming a channel layer comprising a Group III nitride on the energy barrier wherein a concentration of indium (In) in the energy barrier is greater than a concentration of indium (In) in the channel layer; forming a barrier layer comprising a Group III nitride on the channel layer so that the channel layer is between the barrier layer and the energy barrier wherein the barrier layer has a bandgap greater than a bandgap of the channel layer; and characterized in that forming the channel layer comprises: forming a first portion of the channel layer on the energy barrier at a first temperature; and after forming the first portion of the channel layer, forming a second portion of the channel layer at a second temperature on the first portion of the channel layer wherein the first temperature is less than the second temperature. forming a first portion of the channel layer on the energy barrier at a first temperature; and after forming the first portion of the channel layer, forming a second portion of the channel layer at a second temperature on the first portion of the channel layer wherein the first temperature is less than the second temperature.
Rotor blade for an aircraft gas turbine, comprising a blade root element and a stream deflection portion which adjoins the blade root element in a radial direction, respective centers of gravity (24, 24') of blade cross-sectional areas of the stream deflection portion lying on a common thread axis, the thread axis being inclined, in the attached state of the rotor blade on the gas turbine relative to the radial direction in the gas flow direction, in the axial direction and/or in the circumferential direction of the gas turbine, and the rotor blade being suitable for use in a high-speed low-pressure turbine which is connected to a fan of the aircraft gas turbine by means of a reduction gear, characterized in that the thread axis, starting from a first center of gravity of a first blade cross-sectional area adjoining the blade root element, extending within a cone, the cone tip of which lies in the first center of gravity and the cone height of which extends orthogonally to the plane of the blade cross-sectional areas, the cone height, in the attached state of the rotor blade on the aircraft gas turbine, extending in the radial direction of the aircraft gas turbine, which radial direction extends through the first center of gravity, the opening angle (β) of the cone being greaterthan or equal to 0.5° and smaller than or equal to 2°, and the thread axis, starting from the first center of gravity of a first blade cross-sectional area adjoining the blade root element, extending within a lateral surface of the cone. a blade root element and a stream deflection portion which adjoins the blade root element in a radial direction, respective centers of gravity (24, 24') of blade cross-sectional areas of the stream deflection portion lying on a common thread axis, the thread axis being inclined, in the attached state of the rotor blade on the gas turbine relative to the radial direction in the gas flow direction, in the axial direction and/or in the circumferential direction of the gas turbine, and the rotor blade being suitable for use in a high-speed low-pressure turbine which is connected to a fan of the aircraft gas turbine by means of a reduction gear, characterized in that the thread axis, starting from a first center of gravity of a first blade cross-sectional area adjoining the blade root element, extending within a cone, the cone tip of which lies in the first center of gravity and the cone height of which extends orthogonally to the plane of the blade cross-sectional areas, the cone height, in the attached state of the rotor blade on the aircraft gas turbine, extending in the radial direction of the aircraft gas turbine, which radial direction extends through the first center of gravity, the opening angle (β) of the cone being greaterthan or equal to 0.5° and smaller than or equal to 2°, and the thread axis, starting from the first center of gravity of a first blade cross-sectional area adjoining the blade root element, extending within a lateral surface of the cone.
A method of generating a medical image by using a medical imaging apparatus, the method comprising: transmitting ultrasound signals to an object and receiving ultrasound echo signals reflected from the object; acquiring a B-mode ultrasound image based on the ultrasound echo signals and displaying the B-mode ultrasound image; acquiring a first user input for setting a location of a sample volume on the B-mode ultrasound image; wherein after the sample volume location is set, the method further comprises selecting a Doppler signal corresponding to the sample volume and generating Doppler data based on the Doppler signal; generating a Doppler image based on the Doppler data to be displayed while suspending generation of the B-mode ultrasound image and a B-mode ultrasound image that was last generated is displayed; the method characterized in that if a second user input is received for changing a location of the sample volume, the generation of the Doppler data is suspended, and the B-mode ultrasound image is updated and displayed; and thereafter if a time period during which a user input is not received is greater than or equal to a threshold value, the updating of the B-mode ultrasound image is suspended and the generation and display of the Doppler data is repeated. transmitting ultrasound signals to an object and receiving ultrasound echo signals reflected from the object; acquiring a B-mode ultrasound image based on the ultrasound echo signals and displaying the B-mode ultrasound image; acquiring a first user input for setting a location of a sample volume on the B-mode ultrasound image; wherein after the sample volume location is set, the method further comprises selecting a Doppler signal corresponding to the sample volume and generating Doppler data based on the Doppler signal; generating a Doppler image based on the Doppler data to be displayed while suspending generation of the B-mode ultrasound image and a B-mode ultrasound image that was last generated is displayed; the method characterized in that if a second user input is received for changing a location of the sample volume, the generation of the Doppler data is suspended, and the B-mode ultrasound image is updated and displayed; and thereafter if a time period during which a user input is not received is greater than or equal to a threshold value, the updating of the B-mode ultrasound image is suspended and the generation and display of the Doppler data is repeated.
Method for the self-testing of a reactive radio interferer comprising a plurality of time-synchronized transmission/reception paths (C1, C2,....CN), wherein a transmission/reception path consists of a receiver connected to an antenna, signal processing for spectral analysis, signal processing for transmission signal generation and a transmitter with a downstream power amplifier and a transmitting antenna, each arranged to alternately run through - observation phases for reception of the radio spectrum and - interference phases for the transmission of an interference signal based on the radio spectrum received in the observation phase, characterized in that one of the transmission/reception paths (C1, C2,....CN) transmits a test signal within an observation phase that is received and analyzed by at least one other transmission/reception path, and the self-testing is carried out without additional hardware. - observation phases for reception of the radio spectrum and - interference phases for the transmission of an interference signal based on the radio spectrum received in the observation phase,
A pivoting turbine vane comprising an airfoil, an inner bearing race and an outer bearing race, with said inner and outer bearing races (110, 108) on a pivot axis of the pivoting turbine vane, wherein a radial direction is defined relative to the pivot axis; and cooling air passages through at least one of said inner and outer bearing races (110, 108) to provide cooling air from a remote facing face of said at least one of said inner and outer bearing races (110, 108) to an airfoil facing face of said at least one of said inner and outer bearing races (110, 108), said cooling air passages include an inlet extending into said remote facing face and an outlet in said airfoil facing face, characterised in that: at least one of said inner and outer bearing races (110, 108) includes a first radially thicker portion adjacent said airfoil and including said airfoil facing face, a radially thinner portion, and a second radially thicker portion spaced in a direction away from said airfoil from said first radially thicker portion, such that the thinner portion is located between the first and second radially thicker portions (136, 140), with said cooling air passages extending through both said first and second radially thicker portions (136, 140). cooling air passages through at least one of said inner and outer bearing races (110, 108) to provide cooling air from a remote facing face of said at least one of said inner and outer bearing races (110, 108) to an airfoil facing face of said at least one of said inner and outer bearing races (110, 108), said cooling air passages include an inlet extending into said remote facing face and an outlet in said airfoil facing face, characterised in that: at least one of said inner and outer bearing races (110, 108) includes a first radially thicker portion adjacent said airfoil and including said airfoil facing face, a radially thinner portion, and a second radially thicker portion spaced in a direction away from said airfoil from said first radially thicker portion, such that the thinner portion is located between the first and second radially thicker portions (136, 140), with said cooling air passages extending through both said first and second radially thicker portions (136, 140).
A pipeline apparatus comprising a filter (10, 110) attached to a pipeline (30, 40, 130, 140, 240), a reducing bush (26, 134) for connecting the filter into a suitable socket in the pipeline, so that the filter extends into the pipeline, the filter comprising: a tube (12, 112) extending from a first end to a second end, the tube having a bore with an internal cross-sectional area; a first inlet (18, 118) to the tube (12, 112), the first inlet being positioned through the first end of the tube (12, 112) and the first inlet having a first inlet cross-sectional area; an outlet (16, 116) from the tube (12, 112) the outlet having an outlet cross-sectional area; a plurality of further inlets (20,120) in the tube (12, 112) between an outside thereof and the bore; wherein the first inlet cross-sectional area is less than the outlet cross-sectional area; wherein the filter (10, 110) is mounted to one end of the reducing bush (26, 134) via pipeline mounting means (22, 122) such that the tube (12,112) extends through the reducing bush (26, 134) and beyond an opposite end thereof. a tube (12, 112) extending from a first end to a second end, the tube having a bore with an internal cross-sectional area; a first inlet (18, 118) to the tube (12, 112), the first inlet being positioned through the first end of the tube (12, 112) and the first inlet having a first inlet cross-sectional area; an outlet (16, 116) from the tube (12, 112) the outlet having an outlet cross-sectional area; a plurality of further inlets (20,120) in the tube (12, 112) between an outside thereof and the bore; wherein the first inlet cross-sectional area is less than the outlet cross-sectional area; wherein the filter (10, 110) is mounted to one end of the reducing bush (26, 134) via pipeline mounting means (22, 122) such that the tube (12,112) extends through the reducing bush (26, 134) and beyond an opposite end thereof.