mhurhangee/ep-ind-claims huggingface dataset:
A method of determining turn faults in a stator of a motor, comprising: determining a residual voltage (V base); determining a residual impedance (Z base); and calculating a normalized cross-coupled impedance (Z np /Z pp, Z np /Z nn) of the motor based on one of the residual voltage; the residual impedance or a combination thereof; wherein the value of the normalized cross-coupled impedance is indicative of the number of turn faults in the stator. determining a residual voltage (V base); determining a residual impedance (Z base); and calculating a normalized cross-coupled impedance (Z np /Z pp, Z np /Z nn) of the motor based on one of the residual voltage; the residual impedance or a combination thereof;
Electrical plug-in connection comprising a plug-in connector, a mating plug and an electrically conductive body, wherein the plug-in connector and the mating plug are connected to one another through a cutout of the electrically conductive body, wherein the electrical plug-in connector comprises - a housing for accommodating electrical plug elements, and - a pulling aid which is composed of an electrically insulating material, by means of which the plug-in connector can be removed from a mating plug and which projects in the form of a lug from the housing of the plug-in connector, wherein the pulling aid is provided with an electrically conductive section, wherein the electrically conductive section is fixed in an interlocking manner to the pulling aid, characterized in that the electrically conductive section is designed and provided as a shield support for the shield of an electrical connection cable which is to be connected to the electrical plug-in connector, and in that the electrically conductive section comprises at least one fastening section which engages around a free end of the pulling aid, wherein the electrically conductive section further forms a surface section against which the shield of the electrical connection cable can be placed, and in that electrical connecting means (4, 5, 6, 7, 8, 9) are provided, by means of which the metal section, which is provided on the pulling aid, can be contacted by the electrically conductive body for potential equalization when the plug-in connector is connected to the mating plug as intended. - a housing for accommodating electrical plug elements, and - a pulling aid which is composed of an electrically insulating material, by means of which the plug-in connector can be removed from a mating plug and which projects in the form of a lug from the housing of the plug-in connector, wherein the pulling aid is provided with an electrically conductive section, wherein the electrically conductive section is fixed in an interlocking manner to the pulling aid,
Apparatus for the additive manufacturing of three-dimensional objects by successive, selective layer-by-layer exposure and thereby successive, selective compacting of building material layers, which consist of building material solidifiable by means of a laser beam, comprising at least one temperature controller, which is provided to regulate, at least by sections, the temperature of a construction material layer arranged on a construction plane, wherein the temperature controller comprises at least one temperature control element, which is provided to generate a temperature beam, in particular an electromagnetic beam, wherein the at least one temperature control element is embodied as or comprises a temperature control diode, wherein the temperature controller comprises several temperature control diodes, wherein the at least one temperature control diode is arranged on or in a restraint, embodied in particular as a housing, wherein the restraint is arranged within a process chamber wall of a process chamber on the side of the apparatus inside of a process chamber, within which the successive, selective layer-by-layer exposure and thereby the compacting of building material, which is solidifiable by means of an energy beam, takes place in building material layers arranged on a construction plane, characterised in that the restraint is arranged to be movable at least to a degree of freedom relative to the process chamber on the apparatus side, wherein it is arranged motion-coupled with a functions component, in particular a coating unit, which is arranged within the process chamber on the apparatus side to be movable at least to a degree of freedom and which is provided to form building material layers on the construction plane that are to be selectively compacted.
A non-transitory computer readable storage device comprising: a storage medium having an application stored therein, the application having instructions that when executed by processing circuitry configure the processing circuitry to receive sensor data indicating a behavior of a person from a sensor, the sensor being attached to the person or attached to an object used by the person; analyze a motion pattern in the sensor data to identify a predetermined event in the motion pattern, the predetermined event being captured in a series of images by an image capture device; synchronize the sensor data and the series of images; and select a portion of a series of consecutive images captured before and after the predetermined event by skipping some images of the series of consecutive images before and after the predetermined event, such that the lengths of the skipped intervals are proportional to the distance between the skipped interval and the predetermined event. receive sensor data indicating a behavior of a person from a sensor, the sensor being attached to the person or attached to an object used by the person; analyze a motion pattern in the sensor data to identify a predetermined event in the motion pattern, the predetermined event being captured in a series of images by an image capture device; synchronize the sensor data and the series of images; and select a portion of a series of consecutive images captured before and after the predetermined event by skipping some images of the series of consecutive images before and after the predetermined event, such that the lengths of the skipped intervals are proportional to the distance between the skipped interval and the predetermined event.
An aircraft, comprising: an electrical power system (6b; 32) requiring electrical power; at least one hydraulic power system (6c; 34a; 34b) requiring hydraulic power; at least two main engines (20a, 20b); a plurality of main engine generators (24a, 24b; 70a, 70b) each coupled to one of the at least two main engines, wherein the main engine generators are configured to be redundant electrical power sources; at least two non-propulsive utility power (NPUP) generation systems that are each configured to provide full-time secondary power during operation of the aircraft wherein the at least two NPUP generation systems are configured to provide at least a portion of the hydraulic power required by the at least one hydraulic power system; at least two NPUP generation sources (22a, 22b), wherein the at least two NPUP generation systems each include one of the at least two NPUP generation sources; and at least two NPUP generators (72a, 72b) each coupled to one of the at least two NPUP generation sources wherein the NPUP generators are rated to generate substantially all of the power required by the electrical power system as well as all essential and non-essential electrical loads on the aircraft. an electrical power system (6b; 32) requiring electrical power; at least one hydraulic power system (6c; 34a; 34b) requiring hydraulic power; at least two main engines (20a, 20b); a plurality of main engine generators (24a, 24b; 70a, 70b) each coupled to one of the at least two main engines, wherein the main engine generators are configured to be redundant electrical power sources; at least two non-propulsive utility power (NPUP) generation systems that are each configured to provide full-time secondary power during operation of the aircraft wherein the at least two NPUP generation systems are configured to provide at least a portion of the hydraulic power required by the at least one hydraulic power system; at least two NPUP generation sources (22a, 22b), wherein the at least two NPUP generation systems each include one of the at least two NPUP generation sources; and at least two NPUP generators (72a, 72b) each coupled to one of the at least two NPUP generation sources wherein the NPUP generators are rated to generate substantially all of the power required by the electrical power system as well as all essential and non-essential electrical loads on the aircraft.
Method for detecting a motor phase fault (R7a..d; X) of a motor arrangement (12, 18), the motor phases (U, V, W) of which are connected to a drive circuit having a DC voltage intermediate circuit and an inverter, wherein at least one motor phase (U, V, W) is connected to a first reference potential via first resistors (R1, R2) and is connected to a second reference potential via further resistors (R8, R9), or a first motor phase of the motor phases (U, V, W) is connected to a first reference potential via first resistors (R1, R2) and the other motor phases (U, V) of the motor phases (U, V, W) are each connected to a second reference potential via further resistors (R3, R4; R5, R6); a divided motor phase voltage (Uu, Uv, Uw) of one motor phase (U, V, W) or a divided motor phase voltage (Uw) of the first motor phase with respect to the first reference potential is captured while the inverter is switched off; and a voltage profile of the captured divided motor phase voltage (Uu, Uv, Uw) is used to determine whether there is a motor phase fault (R7a..d; X) on one of the motor phases (U, V, W) of the motor arrangement (12, 18), the divided motor phase voltage (Uu, Uv, Uw) of one motor phase (U, V, W) or the divided motor phase voltage (Uw) of the first motor phase is captured by means of a voltage divider (R1, R2), characterized in that a fault current value (I R7) of an insulation fault (R7a..d) during the fault check and/or a resistance value of the insulation fault (R7a..d) and/or a maximum possible fault current value (I R7,max) of the insulation fault (R7a..d) are/is quantitatively calculated during operation with the inverter switched on on the basis of the captured motor phase voltage (Uu, Uv, Uw); and the fault current value (I R7) of the insulation fault (R7a..d) during the fault check and/or the resistance value of the insulation fault (R7a..d) and/or the maximum possible fault current value (I R7,max) of the insulation fault (R7a..d) are/is calculated solely on the basis of the resistance values of the first resistors (R1, R2) and the further resistors (R3, R4; R5, R6; R8, R9), a measurement voltage (Um) of the divided motor phase voltage (Uu, Uv, Uw), as captured by means of the voltage divider (R1, R2), a network voltage (U Netz) of a supply network and an intermediate circuit voltage (U+HV) across the DC voltage intermediate circuit.
A method for preparation a glycolide polyester by ring opening polymerization characterized in that glycolide monomer with optional co-monomer(s) of cyclic ester(s) is/are subjected to ring opening polymerization in the presence of a dispersion stabilizer and a catalyst, said catalyst being selected for precipitating glycolide homopolymer or co-polymer from solvent, said solvent being selected so that said glycolide monomer and said optional co-monomer(s), said dispersion stabilizer and said catalyst are soluble therein but resulting glycolide homopolymer or co-polymer is non-soluble.
A method for anchor master, AM, selection, where the method comprises: receiving (101, 301, 401), by a device, a neighbor awareness networking beacon, NAN Beacon, frame, wherein the NAN Beacon frame carries first AM information and first time synchronization function, TSF, information, and the first AM information comprises: a first anchor master rank, AMR, a first hop count, HC, and a first anchor master beacon transmission time, AMBTT; and second AM information and second TSF information are recorded in the device, wherein the second AM information comprises: a second AMR, a second HC, and a second AMBTT; if the NAN Beacon frame is used for AM selection, when the first AMR is less than the second AMR, and a master rank, MR, of the device is greater than the first AMR, switching (102, 303, 402), by the device, a role of the device to an AM; and if the NAN Beacon frame is used for AM selection, when the first AMR is less than the second AMR, and the MR of the device is less than the first AMR, updating (103, 304, 403), by the device according to the NAN Beacon frame, the second AM information and the second TSF information that are recorded in the device. receiving (101, 301, 401), by a device, a neighbor awareness networking beacon, NAN Beacon, frame, wherein the NAN Beacon frame carries first AM information and first time synchronization function, TSF, information, and the first AM information comprises: a first anchor master rank, AMR, a first hop count, HC, and a first anchor master beacon transmission time, AMBTT; and second AM information and second TSF information are recorded in the device, wherein the second AM information comprises: a second AMR, a second HC, and a second AMBTT; if the NAN Beacon frame is used for AM selection, when the first AMR is less than the second AMR, and a master rank, MR, of the device is greater than the first AMR, switching (102, 303, 402), by the device, a role of the device to an AM; and if the NAN Beacon frame is used for AM selection, when the first AMR is less than the second AMR, and the MR of the device is less than the first AMR, updating (103, 304, 403), by the device according to the NAN Beacon frame, the second AM information and the second TSF information that are recorded in the device.
A gas turbine engine comprising: a manifold assembly, comprising: a manifold including a plurality of manifold channels (64A, 64B) disposed therethrough, each manifold channel (64A, 64B) including a manifold channel opening; and a seal plate, including a plurality of seal plate apertures extending therethrough, operably coupled to the manifold, wherein the seal plate includes at least one seal plate channel extending between at least two of the plurality of seal plate apertures; wherein: each of the plurality of seal plate apertures is aligned with a respective one of the plurality of manifold channel openings; and the manifold assembly is a first manifold assembly and the engine further comprises a second manifold assembly operably coupled to the seal plate to create a fluid circuit between the first manifold assembly and the second manifold assembly. a manifold assembly, comprising: a manifold including a plurality of manifold channels (64A, 64B) disposed therethrough, each manifold channel (64A, 64B) including a manifold channel opening; and a seal plate, including a plurality of seal plate apertures extending therethrough, operably coupled to the manifold, wherein the seal plate includes at least one seal plate channel extending between at least two of the plurality of seal plate apertures; a manifold including a plurality of manifold channels (64A, 64B) disposed therethrough, each manifold channel (64A, 64B) including a manifold channel opening; and a seal plate, including a plurality of seal plate apertures extending therethrough, operably coupled to the manifold, wherein the seal plate includes at least one seal plate channel extending between at least two of the plurality of seal plate apertures; wherein: each of the plurality of seal plate apertures is aligned with a respective one of the plurality of manifold channel openings; and the manifold assembly is a first manifold assembly and the engine further comprises a second manifold assembly operably coupled to the seal plate to create a fluid circuit between the first manifold assembly and the second manifold assembly. each of the plurality of seal plate apertures is aligned with a respective one of the plurality of manifold channel openings; and the manifold assembly is a first manifold assembly and the engine further comprises a second manifold assembly operably coupled to the seal plate to create a fluid circuit between the first manifold assembly and the second manifold assembly.
A method of fabricating an integrated optical arrayed waveguide grating device on a substrate, at least a face of the substrate providing a first cladding layer, the method comprising the steps of: (i) forming a core material layer on the first cladding layer; (ii) etching the device in regions forming the complement of an array of desired waveguide cores, the etching step removing material from the core material layer and at least some material from the first cladding layer so that the first cladding layer forms an array of mesa formations substantially covered by the array of waveguide cores; and (iii) forming a second cladding layer over the first cladding layer and the array of waveguide cores; wherein the core material layer and the first and second cladding layers are glass layers, whereby the height of each mesa formation is selected so as to give a substantially zero birefringence in the waveguide cores. (i) forming a core material layer on the first cladding layer; (ii) etching the device in regions forming the complement of an array of desired waveguide cores, the etching step removing material from the core material layer and at least some material from the first cladding layer so that the first cladding layer forms an array of mesa formations substantially covered by the array of waveguide cores; and (iii) forming a second cladding layer over the first cladding layer and the array of waveguide cores; wherein
A shoe with shoe eyelet structure, comprising: a flexible substrate for cladding foot, which has a sock like shape that is an integrate structure made of braided fabric or textile fabric; a plastic protective layer formed on an outer side of the flexible substrate; a shoe sole connected to a bottom of the flexible substrate; and a plurality of shoe eyelet structures formed on an upper side between a shoe toe portion and a shoe throat portion of the flexible structure, one end of each shoe eyelet structure being fixed to the flexible substrate, and the shoe eyelet structures being protruded from the flexible substrate and suspended, thereby a shoe lace runs through the shoe eyelet structures so as to adjust the tightness of the flexible substrate; and the shoe eyelet structures are made of plastic materials and molded on the outer side of the flexible substrate. a flexible substrate for cladding foot, which has a sock like shape that is an integrate structure made of braided fabric or textile fabric; a plastic protective layer formed on an outer side of the flexible substrate; a shoe sole connected to a bottom of the flexible substrate; and a plurality of shoe eyelet structures formed on an upper side between a shoe toe portion and a shoe throat portion of the flexible structure, one end of each shoe eyelet structure being fixed to the flexible substrate, and the shoe eyelet structures being protruded from the flexible substrate and suspended, thereby a shoe lace runs through the shoe eyelet structures so as to adjust the tightness of the flexible substrate; and the shoe eyelet structures are made of plastic materials and molded on the outer side of the flexible substrate.
A reflector antenna device comprising: a main reflector that has a rectangular aperture shape; a primary radiator that is configured to radiate a beam having an amplitude distribution with a circular shape; and a subreflector (10; 11); characterized in that the subreflector (10; 11) has a mirror surface on which asperities are formed, to convert the shape of the amplitude distribution of the beam radiated by said primary radiator from said circular shape to a rectangular shape similar to the aperture shape of said main reflector, and is configured to reflect the beam and radiate the beam having said amplitude distribution with said rectangular shape onto said main reflector. a main reflector that has a rectangular aperture shape; a primary radiator that is configured to radiate a beam having an amplitude distribution with a circular shape; and a subreflector (10; 11); characterized in that the subreflector (10; 11) has a mirror surface on which asperities are formed, to convert the shape of the amplitude distribution of the beam radiated by said primary radiator from said circular shape to a rectangular shape similar to the aperture shape of said main reflector, and is configured to reflect the beam and radiate the beam having said amplitude distribution with said rectangular shape onto said main reflector.
A vinyl chloride resin composition comprising a vinyl chloride resin (a), a plasticizer (b), and a heat-shielding pigment (c), wherein the content of plasticizer (b) per 100 parts by mass of the vinyl chloride resin (a) is 60 parts by mass or more, and wherein the heat-shielding pigment (c) has an L* value of not lower than 18.0 and not higher than 70.0 in the L*a*b* color system, measured as described in the description, and exhibits a spectral reflectance curve, measured as described in the description, on which a wavelength where reflectance is 20% or more is present in a wavelength region of 800 nm to 2400 nm, and wherein the heat-shielding pigment (c) is a Mn-Bi complex oxide. wherein the content of plasticizer (b) per 100 parts by mass of the vinyl chloride resin (a) is 60 parts by mass or more, and wherein the heat-shielding pigment (c) has an L* value of not lower than 18.0 and not higher than 70.0 in the L*a*b* color system, measured as described in the description, and exhibits a spectral reflectance curve, measured as described in the description, on which a wavelength where reflectance is 20% or more is present in a wavelength region of 800 nm to 2400 nm, and wherein the heat-shielding pigment (c) is a Mn-Bi complex oxide.
A transmitter-receiver chain comprising a differentially encoding transmitter and a differentially decoding receiver, the differentially encoding transmitter comprising a baseband modulator arranged to modulate a complex baseband signal and to output, at point n1 in time, a complex modulated signal x1 in with amplitude g1 and phase q1, i.e. x1 in =g1 e jq1, to the input port of a first filter, the first filter in turn having its output coupled to a transmit unit, said first filter being arranged to output, at point n1 in time, a filtered complex output signal x1 out with amplitude g1 but phase m1, i.e. x1 out =g1 e jm1, so that the first filter is arranged to affect the phase but not the amplitude of its input signal, the first filter being arranged to have as its transfer function for the phase of its input signal the z-transform F(z)=1+wz -1, the differentially decoding receiver comprising a receive unit whose output is connected to a second filter, the second filter in turn having its output coupled to a detector unit which is connected to a demodulator, said second filter being arranged to receive from the receiver unit at point n2 in time a complex input signal x2 in =g2 e jq2, and to output, at point n2 in time, a filtered complex output signal x 2 out =g2 e jm2, i.e. the second filter is arranged to affect the phase but not the amplitude of its input signal, the second filter being arranged to have as its transfer function for the phase of its input signal the inverse of the z-transform F(z)=1+wz -1, w being a weighting function whose value is determined based on the additive noise autocorrelation, the phase noise autocorrelation and the signal amplitude of x1 in.
A compound of formula wherein n is 0; R 1 is hydrogen; R 2 is selected from saturated or unsaturated, branched or unbranched C 1-10 alkyl or C 3-12 cycloalkyl, and substituted or non-substituted phenyl or benzyl; R 3 is hydrogen; R 4 is substituted or non-substituted C 6 -C 10 aryl or C 1 -C 9 heteroaryl wherein the heteroatoms independently are selected from N, O and S; or substituted or non-substituted mono- or bicyclic C 3-12 cycloalkyl or C 1 -C 9 heterocyclyl wherein the heteroatoms are independently selected from N, O and S; and pharmaceutically acceptable salts thereof.