mhurhangee/ep-ind-claims huggingface dataset:
A monolithic integrated bulk acoustic wave BAW resonator production method, wherein the method comprises: preparing an imprint template, wherein the imprint template comprises an imprint plate and a plurality of imprint dies (121, 122) protruding from a surface of the imprint plate, and at least two imprint dies out of the plurality of imprint dies have different protruding heights relative to the surface of the imprint plate; forming a mask material layer on a substrate; pressing the mask material layer in a direction of the substrate with the imprint template, to form, on the mask material layer through imprinting, a mask pattern layer, wherein the mask pattern layer comprises a plurality of mask grooves (211, 212) with depths consistent with heights of the imprint dies; performing plasma etching on the substrate by using the mask material layer as a mask, to form, on a surface of the substrate, a plurality of grooves (23a, 23b) that one-to-one correspond to positions of the plurality of mask grooves (211, 212), wherein depths of at least two grooves out of the plurality of grooves (23a, 23b) are different; and forming, in the plurality of grooves, bottom electrode layers, piezoelectric layers, and top electrode layers that are sequentially stacked to form resonators (24A, 24B) at positions of the grooves, wherein in a direction perpendicular to the substrate, thicknesses of the bottom electrode layers are the same and are all less than depths of the grooves, and piezoelectric layer thicknesses of at least two resonators are different, or top electrode layer thicknesses of at least two resonators are different preparing an imprint template, wherein the imprint template comprises an imprint plate and a plurality of imprint dies (121, 122) protruding from a surface of the imprint plate, and at least two imprint dies out of the plurality of imprint dies have different protruding heights relative to the surface of the imprint plate; forming a mask material layer on a substrate; pressing the mask material layer in a direction of the substrate with the imprint template, to form, on the mask material layer through imprinting, a mask pattern layer, wherein the mask pattern layer comprises a plurality of mask grooves (211, 212) with depths consistent with heights of the imprint dies; performing plasma etching on the substrate by using the mask material layer as a mask, to form, on a surface of the substrate, a plurality of grooves (23a, 23b) that one-to-one correspond to positions of the plurality of mask grooves (211, 212), wherein depths of at least two grooves out of the plurality of grooves (23a, 23b) are different; and forming, in the plurality of grooves, bottom electrode layers, piezoelectric layers, and top electrode layers that are sequentially stacked to form resonators (24A, 24B) at positions of the grooves, wherein in a direction perpendicular to the substrate, thicknesses of the bottom electrode layers are the same and are all less than depths of the grooves, and piezoelectric layer thicknesses of at least two resonators are different, or top electrode layer thicknesses of at least two resonators are different
An apparatus comprising: a first number of layers of a composite material for a wing; a second number of layers of the composite material for the wing; and a metal layer located between the first number of layers and the second number of layers in the wing, wherein the metal layer has a first thickness at a first area configured to receive a number of fasteners and wherein the metal layer has a second thickness at a second area that is not configured to receive the number of fasteners, wherein the second area is configured to transfer loads carried by the metal layer to the first number of layers and the second number of layers in the second area, wherein the metal layer changes in thickness by changing from the first thickness to the second thickness with a stair-step shape. a first number of layers of a composite material for a wing; a second number of layers of the composite material for the wing; and a metal layer located between the first number of layers and the second number of layers in the wing, wherein the metal layer has a first thickness at a first area configured to receive a number of fasteners and wherein the metal layer has a second thickness at a second area that is not configured to receive the number of fasteners, wherein the second area is configured to transfer loads carried by the metal layer to the first number of layers and the second number of layers in the second area, wherein the metal layer changes in thickness by changing from the first thickness to the second thickness with a stair-step shape.
A process for manufacturing disodium salt of pamidronic acid characterized in - that the acid is titrated with ammonia unto a pH of 7.50-7.60, - the resulting solution is passed over the sodium form of an ion-exchange column at elevated temperature, - the resulting eluate containing disodium pamidronate is cooled down to lower temperature until the disodium salt of pamidronic acid is crystallizing, - and the crystals are harvested by centrifugation or vacuum filtration and dried in vacuum at 25°C. - that the acid is titrated with ammonia unto a pH of 7.50-7.60, - the resulting solution is passed over the sodium form of an ion-exchange column at elevated temperature, - the resulting eluate containing disodium pamidronate is cooled down to lower temperature until the disodium salt of pamidronic acid is crystallizing, - and the crystals are harvested by centrifugation or vacuum filtration and dried in vacuum at 25°C.
A data center network, comprising: one core switch group, m cyclic arrayed waveguide grating, CAWG, groups (2 a to 2 m), and m edge switch groups (4 a to 4 m), wherein the m CAWG groups (2 a to 2 m) and the m edge switch groups (4 a to 4 m) are in a one-to-one correspondence, the m CAWG groups (2 a to 2 m) comprise a first CAWG group, and the m edge switch groups (4 a to 4 m) comprise a first edge switch group, wherein the first edge switch group is any one of the m edge switch groups, and the first CAWG group is a CAWG group corresponding to the first edge switch group; the core switch group comprises k core switches; the first CAWG group (2 a to 2 m) comprises 2*Y N*N CAWGs, wherein the 2*Y CAWGs comprise Y uplink CAWGs and Y downlink CAWGs, the Y uplink CAWGs are connected to each core switch in the core switch group separately by using an optical uplink, and the Y downlink CAWGs are connected to each core switch in the core switch group separately by using an optical downlink; and the first edge switch group (4 a to 4 m) comprises multiple edge switches; each edge switch of the multiple edge switches is connected to an uplink CAWG and a downlink CAWG in the first CAWG group separately; where each of, a number of edge switches in the first edge switch group, a number of ports of each edge switch in the first edge switch group and k, is less than or equal to N.
A method comprising: determining whether to establish an ad hoc wireless network based on an estimated time duration of a wireless connection; establishing the ad hoc wireless network comprising a plurality of vehicles, if the estimated time duration exceeds a predefined minimum time of connection; obtaining road information using sensors of a first vehicle of the plurality of vehicles; and sending the road information to other vehicles of the plurality of vehicles using the ad hoc wireless network. determining whether to establish an ad hoc wireless network based on an estimated time duration of a wireless connection; establishing the ad hoc wireless network comprising a plurality of vehicles, if the estimated time duration exceeds a predefined minimum time of connection; obtaining road information using sensors of a first vehicle of the plurality of vehicles; and sending the road information to other vehicles of the plurality of vehicles using the ad hoc wireless network.
A device comprising an absorption article, a pump, and a venting device in, under or on the absorption article, wherein the venting device comprises a flexible container (1, 1a), an air-conducting inner space, a connection, and a surface with air-impermeable zones and air-permeable zones in the form of perforations, in order to suction air from the absorption article through the perforations via the connection into the inner space of the container (1, 1 a), and the venting device is a separately manageable unit and is slid into, or inserted into or placed on the absorption article, wherein the venting device is connected via the connection to the pump, and the pump is a pump in suction operation, so that the contaminated air can be discharged to the outside from the container via the connection by suctioning.
Article of clothing comprising: at least two conductive wires (14a-14c) adapted to transmit an electric current, at least one conductive wire (14a-14c) being incorporated into at least one flat seam (12a-12b); and at least one electrical interconnection between said at least two conductive wires (14a- 14c); said electrical interconnection incorporates a weld between said at least two conductive wires (14a-14c); said article of clothing being characterized in that in that said electrical interconnection is protected by two layers of fabric respectively attached above and below said electrical interconnection: a lower layer of fabric bonded to said article of clothing over which said at least two conductive wires (14a-14c) extend; and an upper layer of fabric secured to said lower layer of fabric (21- 22) so as to form, with said lower layer of fabric (21- 22), a protective barrier around said electrical interconnection. at least two conductive wires (14a-14c) adapted to transmit an electric current, at least one conductive wire (14a-14c) being incorporated into at least one flat seam (12a-12b); and at least one electrical interconnection between said at least two conductive wires (14a- 14c); said electrical interconnection incorporates a weld between said at least two conductive wires (14a-14c); said article of clothing being characterized in that in that said electrical interconnection is protected by two layers of fabric respectively attached above and below said electrical interconnection: a lower layer of fabric bonded to said article of clothing over which said at least two conductive wires (14a-14c) extend; and an upper layer of fabric secured to said lower layer of fabric (21- 22) so as to form, with said lower layer of fabric (21- 22), a protective barrier around said electrical interconnection. a lower layer of fabric bonded to said article of clothing over which said at least two conductive wires (14a-14c) extend; and an upper layer of fabric secured to said lower layer of fabric (21- 22) so as to form, with said lower layer of fabric (21- 22), a protective barrier around said electrical interconnection.
A method of plant control comprising: topically applying to a surface of a plant a composition comprising a double-stranded RNA (dsRNA) polynucleotide and a transfer agent, wherein said dsRNA polynucleotide is identical or complementary to an RNA sequence of a 5-enolpyruvylshikimate-3-phosphate synthase (EPSPS) gene sequence selected from the group consisting of SEQ ID NOs: 11, 18, 19, 21, 22, 53-55, 61, 72, 74, 75, 84, 88, 99, 101, 110, 115, 119, and an at least 18 contiguous nucleotides polynucleotide fragment thereof, wherein said transfer agent is an organosilicone surfactant composition or an organosilicone compound contained therein and conditions said surface of said plant for permeation by said dsRNA polynucleotide, and whereby said plant's growth, development, or reproductive ability is reduced or said plant is more sensitive to an EPSPS inhibitor herbicide relative, to an untreated plant.
A method for producing a chemical reactor device based on a fluid flow, the method comprising: - obtaining a substrate with a fluid channel defined by a channel wall, in which an ordered set of microfabricated silicon pillar structures is positioned in the fluid channel, - electrochemically anodising at least the silicon pillar structures to make the silicon pillar structures porous at least to a certain depth, - after anodising, performing thermal treatment and, after the thermal treatment, performing functionalisation of the substrate and pillar structures to condition at least a part of the silanol groups on the substrate and/or pillar structures, wherein the thermal treatment is being carried out at a temperature, with a duration and in an atmosphere such that any silicon oxide layer formed has a thickness of less than 20 nm. - obtaining a substrate with a fluid channel defined by a channel wall, in which an ordered set of microfabricated silicon pillar structures is positioned in the fluid channel, - electrochemically anodising at least the silicon pillar structures to make the silicon pillar structures porous at least to a certain depth, - after anodising, performing thermal treatment and, after the thermal treatment, performing functionalisation of the substrate and pillar structures to condition at least a part of the silanol groups on the substrate and/or pillar structures,
Machine for cutting vegetables into different shapes lines, said machine comprising: holding means which are configured to receive and hold at least one vegetable; cutting means for cutting said at least one vegetable into lines, said cutting means being located downstream from said holding means; and thrust means which are movable according to a predetermined direction, to push at least one vegetable through said holding means against said cutting means; wherein said thrust means, said holding means and said cutting means are substantially aligned along said predetermined direction; and wherein said holding means are movable in rotation relative to said cutting means, such that said cutting means operate on said at least one vegetable, forming at least one substantially filiform vegetable portion when said thrust means push, when in use, said at least one vegetable against said cutting means. characterized in that said thrust means comprise a head which is idle rotatable and comprises engaging means configured to engage with said holding means such that said head passes through said holding means and rotates together with said holding means when said holding means rotate. holding means which are configured to receive and hold at least one vegetable; cutting means for cutting said at least one vegetable into lines, said cutting means being located downstream from said holding means; and thrust means which are movable according to a predetermined direction, to push at least one vegetable through said holding means against said cutting means; wherein said thrust means, said holding means and said cutting means are substantially aligned along said predetermined direction; and wherein said holding means are movable in rotation relative to said cutting means, such that said cutting means operate on said at least one vegetable, forming at least one substantially filiform vegetable portion when said thrust means push, when in use, said at least one vegetable against said cutting means. characterized in that said thrust means comprise a head which is idle rotatable and comprises engaging means configured to engage with said holding means such that said head passes through said holding means and rotates together with said holding means when said holding means rotate.
A surgical device for essentially synchronous automatic activating and deactivating of a functional device (14, 56, 58) and a surgical generator of a surgical device, comprising: - the surgical generator configured to provide energy for an energy based surgical instrument (34, 50, 52); - the functional device (14, 56, 58) configured to provide a function in an activated condition; - a switch for activating and deactivating the surgical generator - a capacitive sensor including at least one measuring electrode (26, 26a, 26b) that is arranged at the switch, wherein the capacitive sensor is configured to measure a capacity change or a capacity at the measuring electrode (26, 26a, 26b) and activate or deactivate the functional device (14, 56, 58) as a function of a measured capacity change or capacity. - the surgical generator configured to provide energy for an energy based surgical instrument (34, 50, 52); - the functional device (14, 56, 58) configured to provide a function in an activated condition; - a switch for activating and deactivating the surgical generator - a capacitive sensor including at least one measuring electrode (26, 26a, 26b) that is arranged at the switch,
A variable bandwidth electrocardiogram high pass filter, comprising: a baseline low pass filter including a finite impulse response filter and an infinite impulse response low pass filter cooperatively structurally configured and operably connected for low pass filtering a baseline unfiltered electrocardiogram signal (ECG bu) to output a filtered baseline signal (BSE f), wherein the baseline low pass filter further includes a baseline wander estimator operably connected to at least one of the finite impulse response filter and the infinite impulse response low pass filter for dynamically adjusting a corner frequency of the baseline low pass filter as a function of an estimation of any baseline wander within the baseline unfiltered electrocardiogram signal (ECG bu); a signal delay operable for time delaying the baseline unfiltered electrocardiogram signal (ECG bu) to output a delayed baseline unfiltered electrocardiogram signal (ECG dbu); and a signal extractor operably connected to the baseline low pass filter and the signal delay for extracting the filtered baseline signal (BSE f) from the delayed baseline unfiltered electrocardiogram signal (ECG dbu) to output a baseline filtered electrocardiogram signal (ECG bf). a baseline low pass filter including a finite impulse response filter and an infinite impulse response low pass filter cooperatively structurally configured and operably connected for low pass filtering a baseline unfiltered electrocardiogram signal (ECG bu) to output a filtered baseline signal (BSE f), wherein the baseline low pass filter further includes a baseline wander estimator operably connected to at least one of the finite impulse response filter and the infinite impulse response low pass filter for dynamically adjusting a corner frequency of the baseline low pass filter as a function of an estimation of any baseline wander within the baseline unfiltered electrocardiogram signal (ECG bu); wherein the baseline low pass filter further includes a baseline wander estimator operably connected to at least one of the finite impulse response filter and the infinite impulse response low pass filter for dynamically adjusting a corner frequency of the baseline low pass filter as a function of an estimation of any baseline wander within the baseline unfiltered electrocardiogram signal (ECG bu); a signal delay operable for time delaying the baseline unfiltered electrocardiogram signal (ECG bu) to output a delayed baseline unfiltered electrocardiogram signal (ECG dbu); and a signal extractor operably connected to the baseline low pass filter and the signal delay for extracting the filtered baseline signal (BSE f) from the delayed baseline unfiltered electrocardiogram signal (ECG dbu) to output a baseline filtered electrocardiogram signal (ECG bf).
A guide fitting of a piece of sliding door furniture, comprising at least one sliding door (2, 3) that can be guided along a guide profile and a running rail, having a fitting housing (101, 201, 301) arranged on the sliding door (2, 3), on which a guide bolt which can be guided in the guide profile is arranged, wherein the guide bolt can reversibly be moved from a mounting position in which the sliding door (2, 3) can be pivoted without obstruction under the guide profile to an operating position in which the guide bolt protrudes into the guide profile and can be latched in the operating position, characterized in that the guide fitting comprises a driver which is arranged on the fitting housing (101, 201, 301) and is coupled to a damping unit and/or a self-retracting unit, wherein the damping unit and/or the self-retracting unit, the driver and the guide bolt are formed as a modular unit, wherein the modular unit comprises a housing (112, 211, 306) on which the guide bolt is integrally formed and the damping unit and/or the self-retracting unit and the driver are mounted, and at least the guide bolt and the driver can reversibly be moved from a mounting position in which the sliding door (2, 3) can be pivoted without obstruction under the guide profile to an operating position in which the guide bolt and the driver protrude into the guide profile, and can be latched in the operating position.
A process for forming a turbine engine component comprising the steps of: providing a non-ceramic core formed from a refractory metal material and shaped to provide more than one as cast cooling circuit within the turbine engine component; providing a mold having a shape of said turbine engine component; positioning only said non-ceramic core within said mold; introducing a molten metal material into said mold and allowing said molten metal material to solidify and form said turbine engine component; and removing said non-ceramic core from said solidified turbine engine component; wherein said non-ceramic core providing step comprises providing a refractory metal material core having: a first portion for forming at least one internal cooling passage in said turbine engine component; an integral second portion which forms a serpentine cooling circuit in said turbine engine component; and an integral third portion which forms a trailing edge cooling circuit in said turbine engine component. providing a non-ceramic core formed from a refractory metal material and shaped to provide more than one as cast cooling circuit within the turbine engine component; providing a mold having a shape of said turbine engine component; positioning only said non-ceramic core within said mold; introducing a molten metal material into said mold and allowing said molten metal material to solidify and form said turbine engine component; and removing said non-ceramic core from said solidified turbine engine component; wherein said non-ceramic core providing step comprises providing a refractory metal material core having: a first portion for forming at least one internal cooling passage in said turbine engine component; an integral second portion which forms a serpentine cooling circuit in said turbine engine component; and an integral third portion which forms a trailing edge cooling circuit in said turbine engine component. a first portion for forming at least one internal cooling passage in said turbine engine component; an integral second portion which forms a serpentine cooling circuit in said turbine engine component; and an integral third portion which forms a trailing edge cooling circuit in said turbine engine component.