mhurhangee/patent-ind-claim-en huggingface dataset:
A solar sail, comprising: a bus ; and a plurality of separate vanes , each of the plurality of separate vanes including: a reflective surface for using solar radiation pressure to propel the solar sail in space; and a support frame to support the reflective surface; wherein the support frame includes a stowed configuration and a deployed configuration; wherein each of the plurality of separate vanes is movably coupled to the bus ; and, wherein each connection between the bus and a vane of the plurality of separate vanes has a first rotational degree of freedom about the connection axis between the bus and the vane and an axis of symmetry of the vane, and a second rotational degree of freedom orthogonal to the first rotational degree of freedom in a fully deployed configuration. a bus ; and a plurality of separate vanes , each of the plurality of separate vanes including: a reflective surface for using solar radiation pressure to propel the solar sail in space; and a support frame to support the reflective surface; wherein the support frame includes a stowed configuration and a deployed configuration; wherein each of the plurality of separate vanes is movably coupled to the bus ; and, wherein each connection between the bus and a vane of the plurality of separate vanes has a first rotational degree of freedom about the connection axis between the bus and the vane and an axis of symmetry of the vane, and a second rotational degree of freedom orthogonal to the first rotational degree of freedom in a fully deployed configuration. a reflective surface for using solar radiation pressure to propel the solar sail in space; and a support frame to support the reflective surface; wherein the support frame includes a stowed configuration and a deployed configuration; wherein each of the plurality of separate vanes is movably coupled to the bus ; and, wherein each connection between the bus and a vane of the plurality of separate vanes has a first rotational degree of freedom about the connection axis between the bus and the vane and an axis of symmetry of the vane, and a second rotational degree of freedom orthogonal to the first rotational degree of freedom in a fully deployed configuration.
A push to connect fitting assembly for a conduit having a longitudinal axis, the fitting assembly comprising: a first fitting component having an outboard end that is adapted to receive a conduit end; a second fitting component joined to the first fitting component to define an interior cavity; a seal device disposed in the interior cavity, wherein the seal device seals one of the first and second fitting components with an outer surface of a conduit end (C) when the conduit end is inserted into the outboard end of the first fitting component; and a retainer assembled with at least one of the first and second fitting components, the retainer including an annular retainer body , and a gripping portion comprising a plurality of circumferentially spaced bearing members captured between the retainer body and the at least one of the first and second fitting components to engage the inserted conduit end over a first surface contact area to grip the conduit end, the retainer further including a colleting portion outboard of the gripping portion, the colleting portion comprising a plurality of axially extending, radially flexible fingers , each flexible finger at a distal end thereof projects radially outward to form an associated tab , the fingers having conduit contacting surfaces that engage the inserted conduit end over a second surface contact area greater than the first surface contact area to collet the inserted conduit end. a first fitting component having an outboard end that is adapted to receive a conduit end; a second fitting component joined to the first fitting component to define an interior cavity; a seal device disposed in the interior cavity, wherein the seal device seals one of the first and second fitting components with an outer surface of a conduit end (C) when the conduit end is inserted into the outboard end of the first fitting component; and a retainer assembled with at least one of the first and second fitting components, the retainer including an annular retainer body , and a gripping portion comprising a plurality of circumferentially spaced bearing members captured between the retainer body and the at least one of the first and second fitting components to engage the inserted conduit end over a first surface contact area to grip the conduit end,
Method for fabricating a memory device , wherein the method comprises: processing a plurality of selector devices in a semiconductor layer of a first substrate , processing an interconnect layer on a front-side of the semiconductor layer , the interconnect layer comprising an interconnect structure electrically connected to the plurality of selector devices , processing a plurality of memory elements in an oxide layer of the first substrate arranged on a back-side of the semiconductor layer , each memory element being electrically connected to one of the selector devices , and processing one or more vias through the semiconductor layer to electrically connect the memory elements to the interconnect structure , characterised in that each selector device comprises an NPN bipolar transistor with a floating base, or a PNP bipolar transistor with a floating base, or an NP diode, or a PN diode. processing a plurality of selector devices in a semiconductor layer of a first substrate , processing an interconnect layer on a front-side of the semiconductor layer , the interconnect layer comprising an interconnect structure electrically connected to the plurality of selector devices , processing a plurality of memory elements in an oxide layer of the first substrate arranged on a back-side of the semiconductor layer , each memory element being electrically connected to one of the selector devices , and processing one or more vias through the semiconductor layer to electrically connect the memory elements to the interconnect structure , characterised in that each selector device comprises an NPN bipolar transistor with a floating base, or a PNP bipolar transistor with a floating base, or an NP diode, or a PN diode.
A wireless communication method, comprising: determining , by a terminal device, a plurality of slots according to a constraint condition starting from a first slot, the plurality of slots being used for transmitting one Physical Uplink Control Channel, PUCCH; and sending , by the terminal device, the one PUCCH to a network device on the plurality of slots, wherein the constraint condition is a constraint on a physical resource available for transmitting the one PUCCH within each slot of the plurality of slots, wherein the constraint on the physical resource available for transmitting the one PUCCH within each slot of the plurality of slots comprises: a constraint on the number of the physical resources available for transmitting the one PUCCH within each slot of the plurality of slots and a constraint on a resource location of the physical resource available for transmitting the one PUCCH within each slot of the plurality of slots, and the number of time domain symbols available for transmitting the one PUCCH within each of the slots satisfying the constraint condition is greater than or equal to a first predetermined value; wherein the method further comprises: receiving, by the terminal device, second configuration information sent by the network device, the second configuration information being used for indicating the first predetermined value. determining , by a terminal device, a plurality of slots according to a constraint condition starting from a first slot, the plurality of slots being used for transmitting one Physical Uplink Control Channel, PUCCH; and sending , by the terminal device, the one PUCCH to a network device on the plurality of slots, wherein the constraint condition is a constraint on a physical resource available for transmitting the one PUCCH within each slot of the plurality of slots, wherein the constraint on the physical resource available for transmitting the one PUCCH within each slot of the plurality of slots comprises: a constraint on the number of the physical resources available for transmitting the one PUCCH within each slot of the plurality of slots and a constraint on a resource location of the physical resource available for transmitting the one PUCCH within each slot of the plurality of slots, and the number of time domain symbols available for transmitting the one PUCCH within each of the slots satisfying the constraint condition is greater than or equal to a first predetermined value; wherein the method further comprises: receiving, by the terminal device, second configuration information sent by the network device, the second configuration information being used for indicating the first predetermined value.
A method for preparing a functional test for a manufactured product , said method comprising: determining by means of a functional test computer aided manufacturing (FTCAM) system a test procedure for said product according to design data for said product; performing a process selected from at least one of: (i) automatically inducing at least one selected stimulus to an approved instance of said product according to said test procedure, and automatically recording at least one response signal of said approved instance resulting from said at least one stimulus; and (ii) creating a simulation of an input signal and a simulation of a response signal from at least one simulation tool according to said test procedure and said design data; and converting at least one of said recorded response signal and said simulation of said response signal into a reference specification. determining by means of a functional test computer aided manufacturing (FTCAM) system a test procedure for said product according to design data for said product; performing a process selected from at least one of: (i) automatically inducing at least one selected stimulus to an approved instance of said product according to said test procedure, and automatically recording at least one response signal of said approved instance resulting from said at least one stimulus; and (ii) creating a simulation of an input signal and a simulation of a response signal from at least one simulation tool according to said test procedure and said design data; and (i) automatically inducing at least one selected stimulus to an approved instance of said product according to said test procedure, and automatically recording at least one response signal of said approved instance resulting from said at least one stimulus; and (ii) creating a simulation of an input signal and a simulation of a response signal from at least one simulation tool according to said test procedure and said design data; and converting at least one of said recorded response signal and said simulation of said response signal into a reference specification.
A reflection type encoder, which receives a plurality of light-receiving signals from a single scale , including: a light source which is adapted to irradiate a plurality of wavelengths (λ 1 , λ 2 ,...); a scale having a plurality of patterns formed thereon to which light is irradiated from the light source ; and a light-receiving element for receiving light reflected from each of the plurality of patterns ; characterized in that the plurality of patterns each having different thicknesses (h 1 , h 2 ) are formed on a single track of the scale by using a dielectric substance , wherein the thickness of each of the plurality of patterns is set such that the reflected light of each wavelength has a different brightness in accordance with the differences in the thickness of the dielectric substance and a light receiving signal is obtained for the respective thicknesses of the dielectric substance. a light source which is adapted to irradiate a plurality of wavelengths (λ 1 , λ 2 ,...); a scale having a plurality of patterns formed thereon to which light is irradiated from the light source ; and a light-receiving element for receiving light reflected from each of the plurality of patterns ; characterized in that the plurality of patterns each having different thicknesses (h 1 , h 2 ) are formed on a single track of the scale by using a dielectric substance , wherein the thickness of each of the plurality of patterns is set such that the reflected light of each wavelength has a different brightness in accordance with the differences in the thickness of the dielectric substance and a light receiving signal is obtained for the respective thicknesses of the dielectric substance.
A process for treating crop kernels, comprising the steps of: a) soaking kernels to produce soaked kernels; b) grinding the soaked kernels; c) treating the soaked kernels in the presence of a polypeptide having protease activity, wherein step c) is performed before, simultaneously with or after step b), and said polypeptide is a serine protease of the peptidase family S53, selected from the group consisting of: (a) a polypeptide having at least 90% sequence identity to the polypeptide of SEQ ID NO: 5, SEQ ID NO: 6, or the mature polypeptide of SEQ ID NO: 2 or SEQ ID NO: 4; and (b) a polypeptide encoded by a polynucleotide having at least 90% sequence identity to the mature polypeptide coding sequence of SEQ ID NO: 1 or SEQ ID NO: 3. a) soaking kernels to produce soaked kernels; b) grinding the soaked kernels; c) treating the soaked kernels in the presence of a polypeptide having protease activity, wherein step c) is performed before, simultaneously with or after step b), (a) a polypeptide having at least 90% sequence identity to the polypeptide of SEQ ID NO: 5, SEQ ID NO: 6, or the mature polypeptide of SEQ ID NO: 2 or SEQ ID NO: 4; and (b) a polypeptide encoded by a polynucleotide having at least 90% sequence identity to the mature polypeptide coding sequence of SEQ ID NO: 1 or SEQ ID NO: 3.
Method for operating a pressure tank device comprising a pressure tank , a high-pressure inlet to the pressure tank and a low-pressure outlet from the pressure tank , and a control unit , wherein at least one electromechanical shut-off valve , having a shut-off valve closure body and a shut-off valve seat, is arranged in the low-pressure outlet , wherein the shut-off valve is actuated in an opening direction by a first magnet coil during an extraction operation, characterized in that , at least at the beginning of a process for filling the pressure tank device via the high-pressure inlet , the shut-off valve closure body applies a larger pressure force to the shut-off valve seat than during a rest operation of the pressure tank device, in which rest operation no medium is extracted from the pressure tank and the pressure tank is not filled, wherein, for the application of the larger pressure force of the shut-off valve closure body to the shut-off valve seat, the shut-off valve is, by means of the control unit , actuated in a closing direction by the first magnet coil or a second magnet coil .
A fitting component comprising: a threaded main body having a central axis (X) and comprising an internal bore; and a stroke resisting member including a first end portion axially fixed to the threaded main body and having a first radial thickness, a second end portion including a radially extending bearing surface having a second radial thickness, characterized in that the stroke resisting member further comprises an annular web connecting the first and second end portions (428a, 458a, 518; 428b, 458b, 528), the annular web having a third radial thickness smaller than each of the first and second radial thicknesses and including a hinge portion that facilitates controllable deformation of the annular web when the stroke resisting member is under axial load. a threaded main body having a central axis (X) and comprising an internal bore; and a stroke resisting member including a first end portion axially fixed to the threaded main body and having a first radial thickness, a second end portion including a radially extending bearing surface having a second radial thickness,
An assembly for supporting an aircraft fuselage during manufacturing comprising: a first cradle configured to receive and support a fuselage section at a first location on the fuselage section, and move only in first and second directions relative to the assembly wherein the first direction and the second direction are approximately perpendicular; a second cradle configured to receive and support the fuselage section at a second location on the fuselage section, and move only in the first and the second directions ; a first hydraulic actuator coupled to the first cradle and configured to move the first cradle only in the second direction ; a second hydraulic actuator coupled to the second cradle and configured to move the second cradle only in the second direction ; a hydrostatic system fluidly coupling the first hydraulic actuator and the second hydraulic actuator so that loads are distributed between the first cradle and the second cradle ; and a support structure configured to support the first cradle , the second cradle , the first hydraulic actuator , the second hydraulic actuator and the hydrostatic system . a first cradle configured to receive and support a fuselage section at a first location on the fuselage section, and move only in first and second directions relative to the assembly wherein the first direction and the second direction are approximately perpendicular; a second cradle configured to receive and support the fuselage section at a second location on the fuselage section, and move only in the first and the second directions ; a first hydraulic actuator coupled to the first cradle and configured to move the first cradle only in the second direction ; a second hydraulic actuator coupled to the second cradle and configured to move the second cradle only in the second direction ; a hydrostatic system fluidly coupling the first hydraulic actuator and the second hydraulic actuator so that loads are distributed between the first cradle and the second cradle ; and a support structure configured to support the first cradle , the second cradle , the first hydraulic actuator , the second hydraulic actuator and the hydrostatic system .
A method for determining the amount of one or more dihydroxyvitamin D metabolites in a sample by tandem mass spectrometry, comprising: (i) derivatizing said one or more dihydroxyvitamin D metabolites from said sample with 4-phenyl-1,2,4-triazoline-3,5-dione (PTAD); (ii) generating a precursor ion of said one or more derivatized dihydroxyvitamin D metabolites by ionizing said one or more derivatized dihydroxyvitamin D metabolites; (iii) generating one or more fragment ions of said precursor ion, wherein said one or more fragment ions include at least one ion having a mass/charge ratio of 314.12 ± 0.5; and (iv) detecting the amount of one or more of said ions generated in step (ii) or (iii) or both and relating the amount of detected ions to the amount of said one or more dihydroxyvitamin D metabolites in said sample, wherein the method comprises an immunopurifying step, wherein said one or more dihydroxyvitamin D metabolites comprise 1α,25(OH) 2 D 2 and 1α,25(OH) 2 D 3 and wherein said amount of said metabolites are determined in a single assay. (i) derivatizing said one or more dihydroxyvitamin D metabolites from said sample with 4-phenyl-1,2,4-triazoline-3,5-dione (PTAD); (ii) generating a precursor ion of said one or more derivatized dihydroxyvitamin D metabolites by ionizing said one or more derivatized dihydroxyvitamin D metabolites; (iii) generating one or more fragment ions of said precursor ion, wherein said one or more fragment ions include at least one ion having a mass/charge ratio of 314.12 ± 0.5; and (iv) detecting the amount of one or more of said ions generated in step (ii) or (iii) or both and relating the amount of detected ions to the amount of said one or more dihydroxyvitamin D metabolites in said sample, wherein the method comprises an immunopurifying step, wherein said one or more dihydroxyvitamin D metabolites comprise 1α,25(OH) 2 D 2 and 1α,25(OH) 2 D 3 and wherein said amount of said metabolites are determined in a single assay.
An injection system for an annular combustion chamber of a turbine engine, comprising: - means for supporting and centering a fuel injector head , these means comprising a frustoconical surface connected at its downstream end of smallest diameter to an upstream end of a cylindrical surface , - a bowl for mixing air and fuel arranged downstream of said means, characterized in that at least one axial swirl inducer extends at least in part around said means, said or each swirl inducer comprising vanes delimiting between them substantially axial channels for the passage of an air flow, and said channels open at their upstream ends on said frustoconical surface. - means for supporting and centering a fuel injector head , these means comprising a frustoconical surface connected at its downstream end of smallest diameter to an upstream end of a cylindrical surface , - a bowl for mixing air and fuel arranged downstream of said means, characterized in that at least one axial swirl inducer extends at least in part around said means, said or each swirl inducer comprising vanes delimiting between them substantially axial channels for the passage of an air flow, and said channels open at their upstream ends on said frustoconical surface.
Sensor arrangement for determining at least one parameter of a fluid medium flowing through a duct structure , in particular an intake air mass flow of an internal combustion engine, wherein the sensor arrangement has a sensor housing , in particular a plug-in sensor which is inserted or can be inserted into a flow pipe and in which the duct structure is formed, and at least one sensor chip for determining the parameter of the fluid medium, which sensor chip is arranged in the duct structure , wherein the sensor housing has an inlet into the duct structure , which inlet faces counter to a main flow direction of the fluid medium, and an outlet out of the duct structure , wherein the duct structure comprises a main duct and a measuring duct , wherein the measuring duct branches away from the main duct , wherein the sensor chip is arranged in the measuring duct , wherein the main duct and the measuring duct jointly issue into the outlet out of the duct structure , wherein the main duct has at least one first main duct section , in which the measuring duct branches away, and a second main duct section , wherein the second main duct section adjoins a combining section of the duct structure , in which combining section the measuring duct and the main duct are combined, wherein the second main duct section is arranged at an angle (β) of from 10° to 135° in relation to the first main duct section , characterized in that the main duct has a curved main duct section which connects the first main duct section and the second main duct section , wherein a maximum distance of the curved main duct section from the inlet in the main flow direction is from 10.0 mm to 20.0 mm, wherein the curved main duct section has at least two radii of curvature , wherein a first radius of curvature , which is located upstream of the second radius of curvature with respect to the main flow direction , is from 3.0 mm to 10.0 mm and the second radius of curvature is from 1.5 mm to 10.0 mm.