mhurhangee/ep-ind-claims huggingface dataset:
A blade for a rotor of a wind turbine having a substantially horizontal rotor shaft, said rotor comprising a hub, from which the blade extends substantially in a radial direction when mounted to the hub, the blade having a longitudinal direction (r) with a tip end and a root end and a transverse direction as well as having a blade length, the blade further comprising: - a profiled contour including a pressure side and a suction side, as well as a leading edge and a trailing edge with a chord having a chord length (c) extending there between, the profiled contour, when being impacted by an incident airflow, generating a lift, wherein - the blade is assembled from an inboard blade part closest to the hub and an outboard blade part farthest from the hub, wherein - the inboard part comprises the root end of the blade and comprises a load carrying structure with a first aerodynamic shell fitted to the load carrying structure, wherein the load carrying structure of the inboard blade part is a spar or a beam, and - the outboard part comprises a blade shell (141, 142) with a load carrying structure (143, 144) integrated in the blade shell (141, 142), wherein the load carrying structure (143, 144) of the outboard blade part is a principal laminate integrated in the shell, wherein the outboard blade part comprises a first blade part comprising a pressure side shell part with a pressure side principal laminate, and a suction side shell part with a suction side principal laminate, and wherein at least one shear web is mounted between the pressure side principal laminate and the suction side principal laminate. - a profiled contour including a pressure side and a suction side, as well as a leading edge and a trailing edge with a chord having a chord length (c) extending there between, the profiled contour, when being impacted by an incident airflow, generating a lift, wherein - the blade is assembled from an inboard blade part closest to the hub and an outboard blade part farthest from the hub, wherein - the inboard part comprises the root end of the blade and comprises a load carrying structure with a first aerodynamic shell fitted to the load carrying structure, wherein the load carrying structure of the inboard blade part is a spar or a beam, and - the outboard part comprises a blade shell (141, 142) with a load carrying structure (143, 144) integrated in the blade shell (141, 142), wherein the load carrying structure (143, 144) of the outboard blade part is a principal laminate integrated in the shell, wherein the outboard blade part comprises a first blade part comprising a pressure side shell part with a pressure side principal laminate, and a suction side shell part with a suction side principal laminate, and wherein at least one shear web is mounted between the pressure side principal laminate and the suction side principal laminate.
An article having a surface patterned to enhance retention of deposited films, comprising: a processing chamber component having a macro textured surface formed from engineered features arranged to prevent formation of a line of sight surface across the macro textured surface, wherein one or more of the engineered features has a concave surface, wherein the macro textured surface comprises one or more structures defined between the engineered features, the one or more structures comprising: a top surface; and an overhang, having a rounded edge, located along a sidewall of the one or more structures, wherein the overhang originates from the top surface of the one or more structures and a recess is formed within a center area of the top surface of each of the one or more structures located radially inward from the overhang. a top surface; and an overhang, having a rounded edge, located along a sidewall of the one or more structures, wherein the overhang originates from the top surface of the one or more structures and a recess is formed within a center area of the top surface of each of the one or more structures located radially inward from the overhang.
A curtain airbag module for a vehicle occupant restraint system comprising at least one airbag for mounting on a vehicle body, wherein the airbag is in the form of a lateral head airbag and, on its upper edge area in the installed state, includes a plurality of fastening points for mounting on an inner roof area of the vehicle body, wherein at least one holding element on the one hand to be fastened on the vehicle side and on the other hand fastened on the airbag side is provided for positioning the airbag when activated, wherein the holding element is fastened on an additional non-inflatable surface portion (5a, 5b) that is connected to an inflatable portion of the airbag, wherein the at least one additional non-inflatable surface portion (5a, 5b) is arranged on a front edge area in the installed state and/or on a rear edge area in the installed state of the inflatable portion of the airbag, and wherein the holding element is fastened to a free edge area of the additional non-inflatable surface portion (5a, 5b), characterized in that the surface portion (5a, 5b) has a triangular design und with one side is fastened over a predetermined length to the front and/or rear edge area (3a, 3b) of the inflatable surface portion of the airbag, and the holding element is fastened to the tip of the triangular surface portion (5a, 5b) facing away from the airbag, and wherein the fastening of the holding element on the free edge area is provided in the middle third of a height of the airbag and a length L A of the additional non-inflatable surface portion (5a, 5b) level with the holding element amounts to more than one third of the free length L H of the holding element.
An adjustment arrangement for rear view mirrors for vehicles, in particular commercial vehicles, with a vehicle-side first element and a movable second element that can be adjusted by at least one pivot support opposite the vehicle-side element about at least one axis and which comprises at least one reflecting surface, wherein one of the two elements (4, 6) comprises at least in a partial area a concave surface in particular with the shape of a spherical shell and the other element (6, 4) has a complementary convex surface, in particular with the shape of a spherical shell at least in a partial area, wherein both surfaces (20, 16) slide over one another during the adjustment, and at least one of the two elements (4, 6) comprises a sealing means that has at least partially a sliding contact with the corresponding other element, and the sealing means seals a joining slot of the pivot support against environmental influences, characterized in that the sealing means is arranged in the area of a housing opening through which the vehicle-side element projects from a housing associated with the movable element and that can move with the latter, wherein the sealing means acts directly between the housing opening and a section of the vehicle-side element, wherein this section defines the concave surface that is in particular shaped like a spherical shell, and acts indirectly on the joining slot between the two elements (4, 6).
A probe system for an aircraft comprising: a heater comprising a resistive heating element routed through the probe system, wherein an operational voltage is provided to the resistive heating element to provide heating for the probe system, and wherein the resistive heating element has an element capacitance and wherein the resistive heating element is configured to provide an antenna response indicative of dielectric properties of the resistive heating element upon receiving a radio-frequency signal that comprises a plurality of signal frequencies; and characterised by comprising a control circuit configured to determine the antenna response of the resistive heating element and a resonant frequency from the antenna response and to determine a remaining useful life of the probe system based on the antenna response and resonant frequency over time. a heater comprising a resistive heating element routed through the probe system, wherein an operational voltage is provided to the resistive heating element to provide heating for the probe system, and wherein the resistive heating element has an element capacitance and wherein the resistive heating element is configured to provide an antenna response indicative of dielectric properties of the resistive heating element upon receiving a radio-frequency signal that comprises a plurality of signal frequencies; and characterised by comprising a control circuit configured to determine the antenna response of the resistive heating element and a resonant frequency from the antenna response and to determine a remaining useful life of the probe system based on the antenna response and resonant frequency over time.
An anti-CD38 antibody, for use in treatment of a subject having a CD38-positive hematological malignancy, wherein the anti-CD38 antibody is administered in combination with cyclophosphamide, doxorubicin, vincristine and prednisone (CHOP), wherein the anti-CD38 antibody: i. induces in vitro killing of CD38-expressing cells by antibody-dependent cell-mediated cytotoxicity (ADCC), antibody-dependent cellular phagocytosis (ADCP), complement dependent cytotoxicity, apoptosis, or in vitro modulation of CD38 enzymatic activity; ii. comprises the heavy chain complementarity determining regions (HCDR) 1 (HCDR1), 2 (HCDR2) and 3 (HCDR3) sequences of SEQ ID NOs: 6, 7 and 8, respectively; and iii. comprises the light chain complementarity determining regions (LCDR) 1 (LCDR1), 2 (LCDR2) and 3 (LCDR3) sequences of SEQ ID NOs: 9, 10 and 11, respectively. i. induces in vitro killing of CD38-expressing cells by antibody-dependent cell-mediated cytotoxicity (ADCC), antibody-dependent cellular phagocytosis (ADCP), complement dependent cytotoxicity, apoptosis, or in vitro modulation of CD38 enzymatic activity; ii. comprises the heavy chain complementarity determining regions (HCDR) 1 (HCDR1), 2 (HCDR2) and 3 (HCDR3) sequences of SEQ ID NOs: 6, 7 and 8, respectively; and iii. comprises the light chain complementarity determining regions (LCDR) 1 (LCDR1), 2 (LCDR2) and 3 (LCDR3) sequences of SEQ ID NOs: 9, 10 and 11, respectively.
An electronic inductance circuit for the power supply of a 2-wire bus intercom system, wherein said electronic inductance circuit comprises: a main circuit path along an inductor and a source terminal and a drain terminal of a FET between the input terminal and the output terminal of said electronic inductance circuit, in which said inductor is connected to said source terminal of said FET; a resistor and a freewheeling diode individually connected to said inductor in parallel; and a secondary circuit path along a capacitor connected with a second resistor in series between said input terminal and said output terminal, which is connected to said main circuit path in parallel. a main circuit path along an inductor and a source terminal and a drain terminal of a FET between the input terminal and the output terminal of said electronic inductance circuit, in which said inductor is connected to said source terminal of said FET; a resistor and a freewheeling diode individually connected to said inductor in parallel; and a secondary circuit path along a capacitor connected with a second resistor in series between said input terminal and said output terminal, which is connected to said main circuit path in parallel.
Plasmalysis apparatus (100; 100`; 100") for corona discharge-induced cracking of hydrogen-containing gas into molecular hydrogen and at least one by-product (14; 14`; 14") or for producing molecular hydrogen and at least one by-product (14; 14`; 14"), comprising: - a gas-tight reaction chamber (18; 18`; 18"); - a gas supply line for the hydrogen-containing gas into the reaction chamber (18; 18`; 18"); - exactly one plasma electrode (22; 22`; 22") for generating corona discharges in the reaction chamber (18; 18`; 18") by means of a high-frequency alternating voltage; and - a gas discharge line for the molecular hydrogen from the reaction chamber (18; 18`; 18"); wherein the gas-tight reaction chamber (18; 18`; 18") is enclosed by a wall (28; 28") that is designed to electrically insulate the plasma electrode (22; 22`; 22") from an outside of the wall, and wherein the plasma electrode (22; 22`; 22") is connected to a high-frequency generator for generating the high-frequency alternating voltage. - a gas-tight reaction chamber (18; 18`; 18"); - a gas supply line for the hydrogen-containing gas into the reaction chamber (18; 18`; 18"); - exactly one plasma electrode (22; 22`; 22") for generating corona discharges in the reaction chamber (18; 18`; 18") by means of a high-frequency alternating voltage; and - a gas discharge line for the molecular hydrogen from the reaction chamber (18; 18`; 18"); wherein the gas-tight reaction chamber (18; 18`; 18") is enclosed by a wall (28; 28") that is designed to electrically insulate the plasma electrode (22; 22`; 22") from an outside of the wall, and wherein the plasma electrode (22; 22`; 22") is connected to a high-frequency generator for generating the high-frequency alternating voltage.
Packaging for transporting and/or storing radioactive material comprising a radiation protection structure that comprises a portion for shielding from radiation emitted by the radioactive material, having an inner surface that defines a cavity intended to house the radioactive material, the radiation protection structure comprising, furthermore, a portion (7, 70) that has an effect of distancing the radioactive material from the outside of the packaging, the shielding portion having a mean density of more than 8 and the distancing-effect portion having a mean density of less than 0.5, with the distancing-effect portion (7, 70) directly enclosing the shielding portion, and having an outer surface which is the outer surface of the packaging, the radiation protection structure having a thickness e belonging to a straight line segment connecting a point on the outer surface of the packaging to the center of gravity of the cavity, characterized in that the thickness e satisfies, for any point: e = e 1 + e 2 and 0.05 < e 1 / e < 0.25 with e1 the thickness of the shielding portion, e2 the thickness of the distancing-effect portion, with the thicknesses e1, e2 belonging to the straight line segment.
A method comprising: drawing ink into a printhead assembly by operating a pump in fluid communication with the printhead assembly for a first period of time at a first speed, characterised in that an amount of ink drawn into the printhead assembly during the first period is sufficient to cover nozzles of a die at an outlet of the printhead assembly; and in that the method further comprises: evacuating air within the printhead assembly by operating the pump for a second period of time after the first period of time at a second speed greater than the first speed.
An on-press development type lithographic printing plate precursor comprising: an aluminum support; an image-recording layer on the aluminum support; and a protective layer as an outermost layer on the image-recording layer, wherein the protective layer contains a discoloring compound, wherein the discoloring compound is an infrared absorber, wherein discoloring compound refers to a compound which undergoes change in absorption in the visible light region, meaning a wavelength of 400 nm or more and less than 750 nm, due to the exposure to infrared, and infrared is a ray having a wavelength of 750 nm to 1 mm; wherein the image-recording layer contains an infrared-absorbing polymethine colorant having HOMO of -5.2 eV or less, a polymerization initiator, and a polymerizable compound having 7 or more polymerizable functional groups, wherein the polymerizable compound has a molecular weight of less than 10,000, and wherein when the image-recording layer contains a polymer having a molecular weight of 10,000 or more, then a ratio Wp/Wm by mass of a content Wp of the polymer having a molecular weight 10,000 or more to a content Wm of the polymerizable compound having 7 or more polymerizable functional groups is 1.00 or less. an aluminum support; an image-recording layer on the aluminum support; and a protective layer as an outermost layer on the image-recording layer, wherein the protective layer contains a discoloring compound, wherein the discoloring compound is an infrared absorber, wherein discoloring compound refers to a compound which undergoes change in absorption in the visible light region, meaning a wavelength of 400 nm or more and less than 750 nm, due to the exposure to infrared, and infrared is a ray having a wavelength of 750 nm to 1 mm; wherein the image-recording layer contains an infrared-absorbing polymethine colorant having HOMO of -5.2 eV or less, a polymerization initiator, and a polymerizable compound having 7 or more polymerizable functional groups, wherein the polymerizable compound has a molecular weight of less than 10,000, and wherein when the image-recording layer contains a polymer having a molecular weight of 10,000 or more, then a ratio Wp/Wm by mass of a content Wp of the polymer having a molecular weight 10,000 or more to a content Wm of the polymerizable compound having 7 or more polymerizable functional groups is 1.00 or less.
A method of determining the error in the period of one or more teeth of a rotating toothed wheel having N teeth comprising: i) generating a periodic signal corresponding to the tooth periods of said teeth passing a point; ii) in respect of each tooth period Ti, for each tooth i, determining the value of the centered sum Ti (N-1) of the flanking N-1 periods; iii) determining a measure of the local gradient ΔT i N-1 of each centered sum Ti (N-1); iv) computing the mean value of gradient ΔT i N-1 with respect to all centred sums Ti (N-1) v) computing an error value τ in respect of tooth angle period based on the difference between said mean value of gradient ΔT i N-1 and the local gradient ΔT i N-1 calculated with respect of the tooth in step iii) i) generating a periodic signal corresponding to the tooth periods of said teeth passing a point; ii) in respect of each tooth period Ti, for each tooth i, determining the value of the centered sum Ti (N-1) of the flanking N-1 periods; iii) determining a measure of the local gradient ΔT i N-1 of each centered sum Ti (N-1); iv) computing the mean value of gradient ΔT i N-1 with respect to all centred sums Ti (N-1) v) computing an error value τ in respect of tooth angle period based on the difference between said mean value of gradient ΔT i N-1 and the local gradient ΔT i N-1 calculated with respect of the tooth in step iii)
A machine arrangement having several processing stations for the processing of sheets, wherein in the transport direction of the sheets several processing stations (01; 02; 03; 04; 06; 07; 08; 09; 11; 12) are arranged consecutively for the inline-processing of these sheets, wherein at least one of these processing stations is configured as a non-impact printing device, wherein a transfer device arranged directly upstream of the operating region of the non-impact printing device for transferring the sheets from a first processing station (01; 02; 03; 04; 06; 07; 08; 09; 11; 12) arranged upstream of the non-impact printing device to the non-impact printing device is provided, wherein the transfer device aligns in each case the sheets in their axial register in register relative to the printing position of the non-impact printing device, wherein, in addition to the axial register, the transfer device aligns in each case the sheets in their circumferential register and/or in their diagonal register in register relative to the printing position of the non-impact printing device, characterized in that a first processing station arranged upstream in the transport direction of the non-impact printing device is configured as a sheet feeder or as a magazine feeder, wherein a processing station (02; 03; 08) arranged between the first processing station and the non-impact printing device is configured as a first coating device (02; 03; 08), wherein the coating device (02; 03; 08) is configured as a primer application device or a cold foil application device or a lacquer application device, wherein in the transport direction of the sheets an alignment device is arranged between the non-impact printing device and a processing station (02; 03; 04; 07; 08; 09; 11; 12) arranged downstream from the non-impact printing device, wherein this alignment device aligns in each case the sheets at least in their axial register and/or in their circumferential register in register relative to a processing position of the processing station (02; 03; 04; 07; 08; 09; 11; 12) arranged downstream from the non-impact printing device.
A GAD autoantigen for use in a method for treatment or prevention of autoimmune diabetes in an individual, comprising - Determining the HLA haplotype of the individual; and - Subjecting the individual to a treatment regimen based on said haplotype, wherein an individual having an HLA DR3-DQ2 haplotype is subjected to treatment with at least a GAD-autoantigen. - Determining the HLA haplotype of the individual; and - Subjecting the individual to a treatment regimen based on said haplotype,
Insulating triple glazing, the faces of the glass sheets being numbered from the face turned towards the outside, the sheet whose faces are in the 5 and 6 position being coated on each with a set of low-e layers, the face in the 5 position being coated with layers produced by cathode sputtering and comprising at least one infrared-reflecting silver-based metal layer, the face in the 6 position comprising one or more layers of metal oxides deposited by gas pyrolysis, including a layer of tin oxide doped with antimony or with fluorine, the thickness of which is not less than 200 nm, this glazing exhibiting a light transmission which is not less than 60% (for thicknesses of the sheets of clear glass of 4 mm according to Standard E410 illuminant D65 under 2°) and a haze of less than 0.5% obtained by polishing the surface of the pyrolytic layer such that it exhibits a roughness Ra of less than 10 nm and additionally comprising an underlayer of oxides which is deposited by pyrolysis, formed of silicon oxide SiO x, of silicon oxycarbide SiO x C y or of combinations of layers of oxides, in particular of sets of layers of titanium oxide and of silicon oxide, or of tin oxide and of silicon oxide, the underlayer being inserted between the glass sheet and the layer of doped tin oxide.