mhurhangee/ep-ind-claims huggingface dataset:
A regeneration stage (140, 510) of a sense amplifier, comprising: a first inverter having an input and an output; a second inverter having an input and an output; a third inverter having an input, an output, a first supply terminal, and a second supply terminal, wherein the input of the third inverter is configured to receive a clock signal, the output of the third inverter is coupled to the input of the second inverter, the first supply terminal of the third inverter is coupled to a supply rail, and the second supply terminal of the third inverter is coupled to the output of the first inverter; and a fourth inverter having an input, an output, a first supply terminal, and a second supply terminal, wherein the input of the fourth inverter is configured to receive the clock signal, the output of the fourth inverter is coupled to the input of the first inverter, the first supply terminal of the fourth inverter is coupled to the supply rail, and the second supply terminal of the fourth inverter is coupled to the output of the second inverter; and a first switch coupled between the supply rail and the input of the first inverter, the first switch having a control input coupled to the output of the third inverter; and a second switch coupled between the supply rail and the input of the second inverter, the second switch having a control input coupled to the output of the fourth inverter. a first inverter having an input and an output; a second inverter having an input and an output; a third inverter having an input, an output, a first supply terminal, and a second supply terminal, wherein the input of the third inverter is configured to receive a clock signal, the output of the third inverter is coupled to the input of the second inverter, the first supply terminal of the third inverter is coupled to a supply rail, and the second supply terminal of the third inverter is coupled to the output of the first inverter; and a fourth inverter having an input, an output, a first supply terminal, and a second supply terminal, wherein the input of the fourth inverter is configured to receive the clock signal, the output of the fourth inverter is coupled to the input of the first inverter, the first supply terminal of the fourth inverter is coupled to the supply rail, and the second supply terminal of the fourth inverter is coupled to the output of the second inverter; and a first switch coupled between the supply rail and the input of the first inverter, the first switch having a control input coupled to the output of the third inverter; and a second switch coupled between the supply rail and the input of the second inverter, the second switch having a control input coupled to the output of the fourth inverter.
A combination of a wing (104, 1104) of an aircraft (100, 1100) and a fence (108, 1108) coupled to the wing (104, 1104), the fence having a first end (302, 1302) positioned toward a leading edge (126, 1126) of the wing and a second end (312, 1312) positioned toward a trailing edge (128, 1128) of the wing, the fence being movable relative to the wing between a stowed position in which a panel (142, 1142) of the fence extends along a skin (114, 1114) of the wing, and a deployed position in which the panel extends at an upward angle away from the skin, the panel configured to impede a spanwise airflow along the wing when the fence is in the deployed position, the fence configured to move from the deployed position to the stowed position in response to an aerodynamic force exerted on the panel, the combination further comprising an actuator (316, 1316) configured to move the fence from the stowed position to the deployed position, wherein the fence is configured to move from the deployed position to the stowed position during a cruise operation of the aircraft having a first speed, wherein the fence is further configured to move from the stowed position to the deployed position during a reduced speed operation of the aircraft having a second speed less than the first speed, and wherein the actuator (316, 1316) includes a spring-loaded axle operatively coupled to the fence and mounted to the wing via a first axle mount (304, 1304) positioned toward the leading edge of the wing and a second axle mount (308, 1308) positioned toward the trailing edge of the wing, the spring-loaded axle including an axle (144, 1144) and a spring (318, 1318) coiled around the axle, the spring being located between the second end of the fence and the second axle mount. the combination further comprising an actuator (316, 1316) configured to move the fence from the stowed position to the deployed position, wherein the fence is configured to move from the deployed position to the stowed position during a cruise operation of the aircraft having a first speed, wherein the fence is further configured to move from the stowed position to the deployed position during a reduced speed operation of the aircraft having a second speed less than the first speed, and wherein the actuator (316, 1316) includes a spring-loaded axle operatively coupled to the fence and mounted to the wing via a first axle mount (304, 1304) positioned toward the leading edge of the wing and a second axle mount (308, 1308) positioned toward the trailing edge of the wing, the spring-loaded axle including an axle (144, 1144) and a spring (318, 1318) coiled around the axle, the spring being located between the second end of the fence and the second axle mount.
An isolated antibody, or an antigen-binding antibody fragment, wherein the antibody or antibody fragment binds the non-repeat region depicted in SEQ ID NO:1 or SEQ ID NO:2, wherein the non-repeat region in SEQ ID NO:1 is represented by amino acids 453 to 708 of SEQ ID NO:1 and wherein the non-repeat region in SEQ ID NO:2 is represented by amino acids 453 to 711 of SEQ ID NO:2; and wherein the antibody or antibody fragment preferentially binds cell-associated CA 125/O772P polypeptide relative to shed CA 125/O772P polypeptide, wherein the antibody or antibody fragment preferentially binds cell-associated CA 125/O772P polypeptide relative to shed CA 125/O772P polypeptide if the antibody or antibody fragment, in an ELISA Competition Assay, exhibits less than 25±2.5% inhibition of binding to the peptide of SEQ ID NO:1 in the presence of a 25-fold (weight/weight) excess of shed CA 125/O772P over the peptide of SEQ ID NO:1; and/or the antibody or antibody fragment, in a Flow Cytometry Competition Assay, exhibits an IC 50, as measured by percent-positive cells, of at least 0.05±0.005 mg/ml shed CA 125/O772P.
A discharge device for a visibility-ensuring material comprising: a syringe, wherein a gel-like viscoelastic body is filled into the syringe; and at least one of: a mesh filter having an opening of less than 1 mm, a needle having an inner diameter of less than 1 mm, and an application nozzle having a tip end having an inner diameter of less than 1 mm, wherein the gel-like viscoelastic body comprises a self-assembling peptide, and wherein the gel-like viscoelastic body is intended to be passed through the mesh filter, the needle and/or the application nozzle. a syringe, wherein a gel-like viscoelastic body is filled into the syringe; and at least one of: a mesh filter having an opening of less than 1 mm, a needle having an inner diameter of less than 1 mm, and an application nozzle having a tip end having an inner diameter of less than 1 mm,
A process for producing a ski shoe or a part of a ski shoe, comprising the steps of providing a composition comprising (i) a thermoplastic polyurethane (TPU-1) obtained or obtainable by reaction of an isocyanate composition comprising MDI with a polyol composition, wherein the polyol composition comprises at least one polyol selected from polytetrahydrofurans having an average molecular weight Mn in the range from 1200 to 2000 g/mol and a chain extender, selected from the group consisting of 1,2-ethandiol, 1,3-propanediol, 1,4-butanediol and 1,6-hexanediol; and (ii) hollow glass microspheres; wherein the composition comprises the microspheres in an amount of from 1 to 25 weight % based on the sum of the components (i) and (ii); producing a ski shoe or a part of a ski shoe from the composition provided according to step. providing a composition comprising (i) a thermoplastic polyurethane (TPU-1) obtained or obtainable by reaction of an isocyanate composition comprising MDI with a polyol composition, wherein the polyol composition comprises at least one polyol selected from polytetrahydrofurans having an average molecular weight Mn in the range from 1200 to 2000 g/mol and a chain extender, selected from the group consisting of 1,2-ethandiol, 1,3-propanediol, 1,4-butanediol and 1,6-hexanediol; and (ii) hollow glass microspheres; wherein the composition comprises the microspheres in an amount of from 1 to 25 weight % based on the sum of the components (i) and (ii); (i) a thermoplastic polyurethane (TPU-1) obtained or obtainable by reaction of an isocyanate composition comprising MDI with a polyol composition, wherein the polyol composition comprises at least one polyol selected from polytetrahydrofurans having an average molecular weight Mn in the range from 1200 to 2000 g/mol and a chain extender, selected from the group consisting of 1,2-ethandiol, 1,3-propanediol, 1,4-butanediol and 1,6-hexanediol; and (ii) hollow glass microspheres; producing a ski shoe or a part of a ski shoe from the composition provided according to step.
A computer implemented method for determining fractional fat content of tissue comprising registering thermoacoustic image coordinates to an acquired ultrasound image, the acquired ultrasound image at least comprising target tissue within a region of interest; defining a thermoacoustic voxel grid coincident with the region of interest; obtaining thermoacoustic image measurement values from tissue within the region of interest corresponding to the voxels within the defined thermoacoustic voxel grid to yield a thermoacoustic measurement matrix; normalizing the thermoacoustic image measurement values within the thermoacoustic measurement matrix; calculating a fractional fat content map for the target tissue within the region of interest based on the normalized thermoacoustic image measurement values within the thermoacoustic measurement matrix and a reference thermoacoustic measurement value; and correcting the fractional fat content map based on tissue speed-of-sound data to yield a final fractional fat content map for the target tissue within the region of interest. registering thermoacoustic image coordinates to an acquired ultrasound image, the acquired ultrasound image at least comprising target tissue within a region of interest; defining a thermoacoustic voxel grid coincident with the region of interest; obtaining thermoacoustic image measurement values from tissue within the region of interest corresponding to the voxels within the defined thermoacoustic voxel grid to yield a thermoacoustic measurement matrix; normalizing the thermoacoustic image measurement values within the thermoacoustic measurement matrix; calculating a fractional fat content map for the target tissue within the region of interest based on the normalized thermoacoustic image measurement values within the thermoacoustic measurement matrix and a reference thermoacoustic measurement value; and correcting the fractional fat content map based on tissue speed-of-sound data to yield a final fractional fat content map for the target tissue within the region of interest.
A bottom bracket shell assembly (32; 132; 232; 332; 432; 532) comprising: left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540) each including a lateral surface (44; 344) and defining a generally circular void at the lateral surfaces (44; 344); a bearing support is disposed at the voids of the left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540); characterized in that the left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540) each include a peripheral rim (42; 342); wherein the bottom bracket shell assembly (32; 132; 232; 332; 432; 532) comprises left and right first bosses (62; 162; 262; 362) projecting away from the left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540) at a periphery of the lateral surface (44; 344) and sized to connect to a first tubular member at a first boss (62; 162; 262; 362) end; wherein the left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540) are joined at the peripheral rim (42; 342) to form contiguous front and rear surfaces (52, 54; 152, 154; 252, 254). left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540) each including a lateral surface (44; 344) and defining a generally circular void at the lateral surfaces (44; 344); a bearing support is disposed at the voids of the left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540); characterized in that the left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540) each include a peripheral rim (42; 342); wherein the bottom bracket shell assembly (32; 132; 232; 332; 432; 532) comprises left and right first bosses (62; 162; 262; 362) projecting away from the left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540) at a periphery of the lateral surface (44; 344) and sized to connect to a first tubular member at a first boss (62; 162; 262; 362) end; wherein the left and right sidewalls (38, 40; 338, 340; 438, 440; 538, 540) are joined at the peripheral rim (42; 342) to form contiguous front and rear surfaces (52, 54; 152, 154; 252, 254).
A small RNA detection sensor comprising: at one end thereof, a first sensing region comprising nucleotide sequences complementary to a target small RNA; and a PCR-capable region that is coupled to the first sensing region, the small RNA detection sensor to synthesize a replication region complementary to the PCR-capable region by a DNA polymerase by using the target small RNA as a primer, and amplify the PCR-capable region and the replication region, wherein the first sensing region comprises: at least one amine modification portion that prevents non-specific PCR amplification may be caused by the self-dimer formation between two different sensors via the first sensing regions; and at least one nucleotide substitution portion for cutting the first sensing region by a nuclease, and wherein the nucleotide substitution portion comprises an ANA nucleotide substituted for a nucleotide of the first sensing region.
A configurable preconditioned channel former (200, 400, 600, 700, 800) for an antenna array, comprising N inputs designed to be connected to N antenna elements and M outputs designed to be connected to M receivers (Rx i), characterised in that it comprises means designed to route all of the signals (Sj) received by said antenna elements toward at least one receiver (Rx i) available when at most a number K of receivers is unavailable, said means being configured to implement the transfer function matrix A to N columns and M lines defined as follows: a) each column comprises K+1 coefficients, the value of which can be configured to 0 or to a non-zero value, the other coefficients of each column being set to 0; b) the K+1 configurable coefficients of a column are offset by a line relative to the K+1 configurable coefficients of the column located to its left so as to form a matrix A, referred to as "stepped" matrix. a) each column comprises K+1 coefficients, the value of which can be configured to 0 or to a non-zero value, the other coefficients of each column being set to 0; b) the K+1 configurable coefficients of a column are offset by a line relative to the K+1 configurable coefficients of the column located to its left so as to form a matrix A, referred to as "stepped" matrix.
A probe fluid analyzer system, comprising: a lid element for a container; a sensor mounted or mountable to the lid element, the sensor being configured to determine measurement data of a probe fluid to be stored in the container; an electronic circuitry electrically connected or connectable to the sensor and configured to generate a radio transmission signal carrying information based on the measurement data; and an antenna for transmitting the radio transmission signal to an external radio receiver, wherein the antenna and the electronic circuitry are mounted on a support member characterized in that the support member is permanently affixed to the lid element and acts as an intermediate holding structure to mount the sensor to the lid element. a lid element for a container; a sensor mounted or mountable to the lid element, the sensor being configured to determine measurement data of a probe fluid to be stored in the container; an electronic circuitry electrically connected or connectable to the sensor and configured to generate a radio transmission signal carrying information based on the measurement data; and an antenna for transmitting the radio transmission signal to an external radio receiver, wherein the antenna and the electronic circuitry are mounted on a support member characterized in that the support member is permanently affixed to the lid element and acts as an intermediate holding structure to mount the sensor to the lid element.
A method for detecting fixed pitch operation of a variable pitch propeller of an engine, the method comprising: outputting a command signal for maintaining a rotational speed of the propeller at a reference speed; obtaining an actual value of at least one of the rotational speed and a blade angle of the propeller; assessing, from the actual value, whether an expected change in the at least one of the rotational speed and the blade angle of the propeller has occurred in response to the command signal; and responsive to determining that the expected change in the at least one of the rotational speed and the blade angle of the propeller has not occurred in response to the command signal, detecting operation of the propeller at fixed pitch and outputting an alert accordingly. outputting a command signal for maintaining a rotational speed of the propeller at a reference speed; obtaining an actual value of at least one of the rotational speed and a blade angle of the propeller; assessing, from the actual value, whether an expected change in the at least one of the rotational speed and the blade angle of the propeller has occurred in response to the command signal; and responsive to determining that the expected change in the at least one of the rotational speed and the blade angle of the propeller has not occurred in response to the command signal, detecting operation of the propeller at fixed pitch and outputting an alert accordingly.
The use of polymers that can be obtained from the monomers N,N-diallyl-N-C 1-12 -alkyl-ammonio-N-C 1-4 -alkyl sulfonate and N-vinyl-2-pyrrolidone for increasing the primary detergency of washing or cleaning agents when washing textiles or when cleaning hard surfaces of stains.
A backlight device for a holographic display comprising: a light source configured to emit light comprising a plurality of wavelengths; a light guide plate configured to guide the light emitted by the light source; a first holographic optical element provided on a side of the light guide plate; and a second holographic optical element configured to enable light incident from the first holographic optical element to exit the light guide plate, wherein the first holographic optical element is configured to diffractively expand and reflect light from the light source that has propagated through the light guide plate toward the second holographic optical element, and wherein the second holographic optical element is configured to operate as a lens to concentrate light incident from the first holographic optical element, and characterised in that the first holographic optical element comprises a multi-layered structure, the layers of the multi-layered structure being configured to respectively respond to different wavelengths of light, and in that each layer of the multi-layered structure comprises a holographic pattern based on the wavelength of light the layer is responsive to. a light source configured to emit light comprising a plurality of wavelengths; a light guide plate configured to guide the light emitted by the light source; a first holographic optical element provided on a side of the light guide plate; and a second holographic optical element configured to enable light incident from the first holographic optical element to exit the light guide plate, wherein the first holographic optical element is configured to diffractively expand and reflect light from the light source that has propagated through the light guide plate toward the second holographic optical element, and wherein the second holographic optical element is configured to operate as a lens to concentrate light incident from the first holographic optical element, and characterised in that the first holographic optical element comprises a multi-layered structure, the layers of the multi-layered structure being configured to respectively respond to different wavelengths of light, and in that each layer of the multi-layered structure comprises a holographic pattern based on the wavelength of light the layer is responsive to.
A cover device for a household appliance, having an operational front side and an operational rear side, comprising at least one light source; a transparent volume-coloured glass ceramic exhibiting a light transmittance according to DIN EN 410 based on a thickness of 4 mm in the range from 0.5 % to 70 %; wherein the light source is arranged on the operational rear side of the cover device; and wherein a first means for reducing light transmittance according to DIN EN 410 is arranged between the light source and the glass ceramic; wherein the volume-coloured glass ceramic and the first means for reducing light transmittance together exhibit a DIN EN 410 light transmittance in the range from 0.4 % to 15 %; wherein the transmission spectrum of the glass ceramic, the transmission spectrum of the first means for reducing light transmittance and the emission spectrum of the light source are matched to one another such that the following applies for the x and y colour coordinates of the light emitted by the light source in the CIE xy Y colour space after passing through the volume-coloured glass ceramic, x 1 and y 1, and for the x and y colour coordinates of the light emitted by the light source in the CIE xy Y colour space after passing through the volume-coloured glass ceramic and the first means for reducing light transmittance, x 2 and y 2: x 1 − x 2 2 + y 1 − y 2 2 < 0.05. a transparent volume-coloured glass ceramic exhibiting a light transmittance according to DIN EN 410 based on a thickness of 4 mm in the range from 0.5 % to 70 %; wherein the light source is arranged on the operational rear side of the cover device; and wherein a first means for reducing light transmittance according to DIN EN 410 is arranged between the light source and the glass ceramic; wherein the volume-coloured glass ceramic and the first means for reducing light transmittance together exhibit a DIN EN 410 light transmittance in the range from 0.4 % to 15 %; wherein the transmission spectrum of the glass ceramic, the transmission spectrum of the first means for reducing light transmittance and the emission spectrum of the light source are matched to one another such that the following applies for the x and y colour coordinates of the light emitted by the light source in the CIE xy Y colour space after passing through the volume-coloured glass ceramic, x 1 and y 1, and for the x and y colour coordinates of the light emitted by the light source in the CIE xy Y colour space after passing through the volume-coloured glass ceramic and the first means for reducing light transmittance, x 2 and y 2: x 1 − x 2 2 + y 1 − y 2 2 < 0.05.