mhurhangee/patent-ind-claim-en huggingface dataset:
A method of delidding an integrated circuit, IC, package, comprising: directing a laser beam (L) along a cut line (C) of an integrated circuit package , the cut line defining a removable portion (R); cutting along the cut line; and removing the removable portion after the directing; wherein the integrated circuit package includes a body portion and a lid , the lid defining a hermetically sealed cavity therein, and wherein the lid includes a side wall extending from the body portion to a top surface of the lid, and wherein the removable portion includes the top surface of the lid. directing a laser beam (L) along a cut line (C) of an integrated circuit package , the cut line defining a removable portion (R); cutting along the cut line; and removing the removable portion after the directing; wherein the integrated circuit package includes a body portion and a lid , the lid defining a hermetically sealed cavity therein, and wherein the lid includes a side wall extending from the body portion to a top surface of the lid, and wherein the removable portion includes the top surface of the lid.
An operating device suitable to be used as an input device for an information processing apparatus, the operating device comprising: left and right hold sections to be held by a user; a front surface ; an upper surface; a touch sensor ; a light source (G); a plurality of operating members (11, 19, 22; 122; 222) disposed on the upper surface of the hold sections ; and a light emitting area defined in the upper surface and configured to be made luminous by the light source (G), wherein the touch sensor is provided on the upper surface, and the light emitting area on the upper surface is located along a front edge of the touch sensor . a front surface ; an upper surface; a touch sensor ; a light source (G); a plurality of operating members (11, 19, 22; 122; 222) disposed on the upper surface of the hold sections ; and a light emitting area defined in the upper surface and configured to be made luminous by the light source (G), wherein the touch sensor is provided on the upper surface, and the light emitting area on the upper surface is located along a front edge of the touch sensor .
Method for operating a combustor for a gas turbine, the combustor at least comprising in the direction of hot gas flow a first combustion chamber , a deflection unit , a sequential combustion chamber , whereby the first combustion chamber is a premix combustion chamber with at least one premixing burner for injecting a mixture of air and a gaseous and/or liquid fuel into a combustion zone , and the sequential combustion chamber is an auto-ignition combustion chamber and is connected to the first turbine rotor blade row , in the first combustion chamber the premixed fuel air mixture is combusted in a stable flame at an average flame temperature in the range between 1550 K and 1800 K, then a mass flow of additional air is injected into the hot gas flow in order to reduce the temperature below 1400 K, preferably below 1350 K, then said mixture of hot gas and additional air enters the deflection unit and is deflected there at least in a circumferential direction, then a mass flow of an additional fuel is injected downstream of said air injection , generating an hot gas-air-fuel mixture with auto ignition times between 1 ms and 10 ms, whereby said hot gas-air-fuel mixture is burned in the sequential combustion chamber by a combination of auto-ignition and recirculation of hot reaction products, and a reverse flow zone is generated at a step provided by a sudden cross-sectional enlargement of a hot gas flow channel in the inlet section of the sequential combustion chamber , characterized in that : the mass flow of additional air is injected into the hot gas flow at the downstream end of the first combustion chamber and upstream of the deflection unit , the reverse flow zone forming a reaction zone that defines a flame anchoring point at the inlet to the sequential combustion chamber ; additional fuel is injected in the reverse flow zone . the mass flow of additional air is injected into the hot gas flow at the downstream end of the first combustion chamber and upstream of the deflection unit , the reverse flow zone forming a reaction zone that defines a flame anchoring point at the inlet to the sequential combustion chamber ; additional fuel is injected in the reverse flow zone .
A data sending method, applied to a terminal, characterized by comprising: if a physical, PHY, layer has not sent first data on a first semi-persistent uplink sending resource after a media access control, MAC, layer of the terminal buffers first data to a hybrid automatic repeat request, HARQ, process, and instructs the PHY layer to send the first data on the first semi-persistent uplink sending resource, transmitting, by the PHY layer, a non-sending indication to the MAC layer; instructing, by the MAC layer, the PHY layer to transmit second data on a second semi-persistent uplink sending resource upon receiving the non-sending indication; and sending , by the PHY layer, the second data on the second semi-persistent uplink sending resource, wherein the second data is the first data buffered in the HARQ process, or the second data is data corresponding to the first data buffered in the HARQ process, and the non-sending indication is used to indicate that the PHY layer has not sent the first data on the first semi-persistent uplink sending resource. if a physical, PHY, layer has not sent first data on a first semi-persistent uplink sending resource after a media access control, MAC, layer of the terminal buffers first data to a hybrid automatic repeat request, HARQ, process, and instructs the PHY layer to send the first data on the first semi-persistent uplink sending resource, transmitting, by the PHY layer, a non-sending indication to the MAC layer; instructing, by the MAC layer, the PHY layer to transmit second data on a second semi-persistent uplink sending resource upon receiving the non-sending indication; and sending , by the PHY layer, the second data on the second semi-persistent uplink sending resource, wherein the second data is the first data buffered in the HARQ process, or the second data is data corresponding to the first data buffered in the HARQ process, and the non-sending indication is used to indicate that the PHY layer has not sent the first data on the first semi-persistent uplink sending resource.
Device for feeding of a liquid at risk of freezing into a fluid line of a motor vehicle, having a storage container, a delivery element and a line which leads from the storage container to the delivery element, the latter opening in a controlled manner, and through which it is possible to convey back into the storage container the liquid still present in and upstream of the delivery element after the motor vehicle is shut down, wherein provision is made of a venting device which is independent of the controlled opening of the delivery element and by means of which it is possible to discharge air present in the line when or after the motor vehicle is restarted, characterized in that the venting device is formed by a venting opening which is provided at the delivery element or in the stated line in the immediate vicinity of the delivery element and which is covered by an air-permeable diaphragm which is not permeable to the liquid at risk of freezing at least up to maximum pressure values prevailing in the stated line.
Method for treating the exhaust gases of a motor vehicle supercharged internal combustion engine that are partially recycled at high pressure and at low pressure to the intake, said method comprising: - a step of recirculating a high-pressure EGR gas flow (Q EGR HP ) to the engine , and - a step of recirculating a low-pressure EGR gas flow (Q EGR LP ) to the engine , the whole of these flows constituting a total EGR gas flow (Q EGR ), the ratio (α) of the low-pressure EGR gas flow (Q EGR LP ) divided by the total EGR gas flow (Q EGR ) being determined as a function of the effective efficiency (ε) of an oxidation catalyst for oxidizing unburned hydrocarbons and carbon monoxide of the exhaust gases of the engine , CHARACTERIZED IN THAT said ratio (α) assumes: - the value 0 when the effective efficiency (ε) is less than a first threshold (ε 1 ), - the value 1 when the effective efficiency (ε) is greater than a second threshold (ε 2 ) which is greater than the first threshold (ε 1 ), and - a value between 0 and 1 when the effective efficiency (ε) is between the first threshold (ε 1 ) and the second threshold (ε 2 ). - a step of recirculating a high-pressure EGR gas flow (Q EGR HP ) to the engine , and - a step of recirculating a low-pressure EGR gas flow (Q EGR LP ) to the engine , the whole of these flows constituting a total EGR gas flow (Q EGR ), - the value 0 when the effective efficiency (ε) is less than a first threshold (ε 1 ), - the value 1 when the effective efficiency (ε) is greater than a second threshold (ε 2 ) which is greater than the first threshold (ε 1 ), and - a value between 0 and 1 when the effective efficiency (ε) is between the first threshold (ε 1 ) and the second threshold (ε 2 ).
Target for physical vapour deposition with the following chemical composition: - at least 95 mol% of a mixture of at least two of the following compounds: titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ) - 0.01 mol% to 5 mol% of carbon (C) - less than 0.01 mol% of borides other than titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ) wherein, in relation to metallic purity, the sum of the mixture of titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ) and the carbon (C) is at least 99.8 mol%, and with the following physical properties: - a density greater than 90%, preferably greater than 95%, of the theoretical density of the chemical composition defined above - a d50 value, as the average grain size, of grains of the mixture of titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ), of less than 10 μm, preferably less than 3 μm. - at least 95 mol% of a mixture of at least two of the following compounds: titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ) - 0.01 mol% to 5 mol% of carbon (C) - less than 0.01 mol% of borides other than titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ) wherein, in relation to metallic purity, the sum of the mixture of titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ) and the carbon (C) is at least 99.8 mol%, and with the following physical properties: - a density greater than 90%, preferably greater than 95%, of the theoretical density of the chemical composition defined above - a d50 value, as the average grain size, of grains of the mixture of titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ), of less than 10 μm, preferably less than 3 μm. - a density greater than 90%, preferably greater than 95%, of the theoretical density of the chemical composition defined above - a d50 value, as the average grain size, of grains of the mixture of titanium diboride (TiB 2 ) and/or vanadium diboride (VB 2 ) and/or mixed phases ((Ti,V)B 2 ) of titanium diboride (TiB 2 ) and vanadium diboride (VB 2 ), of less than 10 μm, preferably less than 3 μm.
A soldered product manufacturing device comprising: a stage on which a substrate (W) is placed, solder being arranged on the substrate; a cover configured to cover at least an entire upper part of the substrate placed on the stage at a predetermined distance, the predetermined distance being a shortest distance between the solder arranged on the substrate (W) and the cover ; a chamber configured to house the stage and the cover; a heating portion configured to heat the substrate placed on the stage; and a reducing gas supply device configured to supply a reducing gas (F) for reducing oxide into the chamber. a stage on which a substrate (W) is placed, solder being arranged on the substrate; a cover configured to cover at least an entire upper part of the substrate placed on the stage at a predetermined distance, the predetermined distance being a shortest distance between the solder arranged on the substrate (W) and the cover ; a chamber configured to house the stage and the cover; a heating portion configured to heat the substrate placed on the stage; and a reducing gas supply device configured to supply a reducing gas (F) for reducing oxide into the chamber.
Tampon applicator wherein the tampon applicator comprises cellulose pulp and discrete areas of polymeric material.
A method for smoothing a surface of an object , the method comprising: receiving the object in a chamber ; and being characterized by : generating a mist by a nebulizer assembly from a liquid held in a reservoir into the chamber; and surrounding the object with the mist ; wherein the nebulizer assembly comprises a mesh , a vibrating element , and a wick . generating a mist by a nebulizer assembly from a liquid held in a reservoir into the chamber; and surrounding the object with the mist ; wherein the nebulizer assembly comprises a mesh , a vibrating element , and a wick .
A finger-print data (FP) preparing method comprising: a FP preparing step preparing a FP configured by peaks and retention time points of the peaks detected from a chromatogram of an evaluation target, the chromatogram being a 3D chromatogram including retention time points, detection wavelengths, and peaks as data, characterized in that the FP preparing step prepares the FP by two-dimensionelly indicating maximum values or area values in signal strength of the peaks, as heights at the respective retention time points and including ultraviolet absorbance spectrum information for each respective heights, the peaks being detected from the 3D chromatogram at a specific wavelength. a FP preparing step preparing a FP configured by peaks and retention time points of the peaks detected from a chromatogram of an evaluation target, the chromatogram being a 3D chromatogram including retention time points, detection wavelengths, and peaks as data,
An ultrasound production source comprising a body containing an ultrasound transducer presenting in front an emission face , the body including an opening defined by a tubular wall and arranged so that the emission face of the ultrasound transducer faces towards the opening , the tubular wall being provided externally with at least one thread of a screw thread assembly system for co-operating with at least one complementary thread either of a fastener ring for fastening a flexible membrane on the body, or of a protective cover , or of a ring fitted with an alignment system , wherein the fastener ring possesses a central passage for passing a portion of the flexible membrane , the fastener ring , when screwed onto the body, serving to hold the flexible membrane pressed in sealed manner against the body .
A switching element for creating a short-circuit connection with two busbars arranged spaced apart from one another and at least one power semiconductor arranged between the two busbars and respectively abutting the busbars , wherein the power semiconductor is switchable between an electrically non-conducting and an electrically conducting state, wherein a means for pressing the power semiconductor to the busbars is provided and wherein the means for pressing the power semiconductor to the busbars comprises a spring acting on the one busbar , characterised in that the means for pressing the power semiconductor to the busbars comprises a wedge acting on the other busbar for adjusting a contact force.
A video adaptation method, comprising: receiving indication information sent by a video receiving device, wherein the indication information indicates an image super-resolution capability of the video receiving device, wherein the indication information comprises an image super-resolution multiplier that has a positive correlation with a video definition enhancement capability of the video receiving device, and wherein the indication information indicates whether the image super-resolution capability of the video receiving device is enabled or not; if the indication information indicates that the image super-resolution capability of the video receiving device is enabled, obtaining a video having a target frame rate and a target resolution based on a network status and the indication information; and sending the video having the target frame rate and the target resolution to the video receiving device. receiving indication information sent by a video receiving device, wherein the indication information indicates an image super-resolution capability of the video receiving device, wherein the indication information comprises an image super-resolution multiplier that has a positive correlation with a video definition enhancement capability of the video receiving device, and wherein the indication information indicates whether the image super-resolution capability of the video receiving device is enabled or not; if the indication information indicates that the image super-resolution capability of the video receiving device is enabled, obtaining a video having a target frame rate and a target resolution based on a network status and the indication information; and sending the video having the target frame rate and the target resolution to the video receiving device.
An enteral preterm infant formula comprising a proteinaceous composition, wherein the preterm infant formula: a) comprises 2.0-2.29 g phenylalanine per 100 g protein; b) comprises 64.00-82.29 mg phenylalanine per 100 kcal; and/or c) provides, or is formulated to provide phenylalanine in an amount of 80-96 mg / kg body weight per day. a) comprises 2.0-2.29 g phenylalanine per 100 g protein; b) comprises 64.00-82.29 mg phenylalanine per 100 kcal; and/or c) provides, or is formulated to provide phenylalanine in an amount of 80-96 mg / kg body weight per day.
A water-based composition comprising: an aqueous medium in an amount of 40% by mass or more; (A) fine cellulose fibers having a number-average fiber diameter of 0.5 nm or more and 200 nm or less, and having a carboxy group content of 0.1 mmol/g or more, wherein the carboxy group forms a salt with an alkali metal; and (B) an additive comprising one or more compounds having carbon atoms and nitrogen atom or atoms, wherein a ratio thereof per molecule of the compound (number of carbon atoms/number of nitrogen atoms) is 3 or more and 45 or less, wherein the content of the component (A) is 0.2% by mass or more and 10% by mass or less, and wherein the content of the component (B) is 3 parts by mass or more and 150 parts by mass or less, based on 100 parts by mass of the component (A), and wherein the water-based composition has a viscosity at 80°C at a rotational speed of 30 rpm of 80 mPa·s or more. an aqueous medium in an amount of 40% by mass or more; (A) fine cellulose fibers having a number-average fiber diameter of 0.5 nm or more and 200 nm or less, and having a carboxy group content of 0.1 mmol/g or more, wherein the carboxy group forms a salt with an alkali metal; and (B) an additive comprising one or more compounds having carbon atoms and nitrogen atom or atoms, wherein a ratio thereof per molecule of the compound (number of carbon atoms/number of nitrogen atoms) is 3 or more and 45 or less, (A) fine cellulose fibers having a number-average fiber diameter of 0.5 nm or more and 200 nm or less, and having a carboxy group content of 0.1 mmol/g or more, wherein the carboxy group forms a salt with an alkali metal; and (B) an additive comprising one or more compounds having carbon atoms and nitrogen atom or atoms, wherein a ratio thereof per molecule of the compound (number of carbon atoms/number of nitrogen atoms) is 3 or more and 45 or less, wherein the content of the component (A) is 0.2% by mass or more and 10% by mass or less, and wherein the content of the component (B) is 3 parts by mass or more and 150 parts by mass or less, based on 100 parts by mass of the component (A), and wherein the water-based composition has a viscosity at 80°C at a rotational speed of 30 rpm of 80 mPa·s or more.
A gas turbine engine comprising: a core engine within a core nacelle (C) that houses a low spool and high spool which rotate about an engine axis of rotation (A), the low spool including a low pressure compressor and low pressure turbine , the high spool 24 including a high pressure compressor and high pressure turbine , a combustor being arranged between the high pressure compressor and high pressure turbine ; a fan connected to and driven by the low spool ; a fan case section defined about the engine axis of rotation (A); and a core case section defined about said axis of rotation (A) and having a rear structural wall which at least partially supports a multiple of fan exit guide vanes ; said multiple of fan exit guide vanes being mounted to said fan case section and said core case section ; characterized by further comprising: a multitude of discreet radial extending 2.5 bleed ducts located between the low pressure compressor and the high pressure compressor and defined at least in part by said rear structural wall , wherein said multitude of discreet radial extending 2.5 bleed ducts are raked generally forward to define a respective multitude of exits just aft of said multiple of fan exit guide vanes . a core engine within a core nacelle (C) that houses a low spool and high spool which rotate about an engine axis of rotation (A), the low spool including a low pressure compressor and low pressure turbine , the high spool 24 including a high pressure compressor and high pressure turbine , a combustor being arranged between the high pressure compressor and high pressure turbine ; a fan connected to and driven by the low spool ; a fan case section defined about the engine axis of rotation (A); and a core case section defined about said axis of rotation (A) and having a rear structural wall which at least partially supports a multiple of fan exit guide vanes ; said multiple of fan exit guide vanes being mounted to said fan case section and said core case section ; characterized by further comprising: a multitude of discreet radial extending 2.5 bleed ducts located between the low pressure compressor and the high pressure compressor and defined at least in part by said rear structural wall , wherein said multitude of discreet radial extending 2.5 bleed ducts are raked generally forward to define a respective multitude of exits just aft of said multiple of fan exit guide vanes .