mhurhangee/ep-ind-claims huggingface dataset:
A frame-attached anti-reflection glass (10,10A,10B) comprising: a plate-shaped member (12,12A,12B) including an anti-reflection film (14,14a) formed on at least one surface of a plate-shaped glass; and a frame-shaped member made of silicon joined to a peripheral portion on one surface side of the plate-shaped member, characterised in that: the anti-reflection film includes two partial films (15,16;15a,16a) having different compositions, one of the two partial films being a light-absorbent film (16, 16a), the two partial films are continuously formed on at least one surface of the plate-shaped glass, and respective surfaces of each partial film are on a level with each other, the plate-shaped glass is a borosilicate glass which contains at least sodium or lithium, the anti-reflection film (15,15a) includes a film containing tantalum pentaoxide as a main component, and the light-absorbent film (16,16a) is a film containing sodium tantalate or lithium tantalate. a plate-shaped member (12,12A,12B) including an anti-reflection film (14,14a) formed on at least one surface of a plate-shaped glass; and a frame-shaped member made of silicon joined to a peripheral portion on one surface side of the plate-shaped member, the anti-reflection film includes two partial films (15,16;15a,16a) having different compositions, one of the two partial films being a light-absorbent film (16, 16a), the two partial films are continuously formed on at least one surface of the plate-shaped glass, and respective surfaces of each partial film are on a level with each other, the plate-shaped glass is a borosilicate glass which contains at least sodium or lithium, the anti-reflection film (15,15a) includes a film containing tantalum pentaoxide as a main component, and the light-absorbent film (16,16a) is a film containing sodium tantalate or lithium tantalate.
An aircraft comprising: an airframe having an extending tail; a counter rotating, coaxial main rotor assembly disposed at the airframe including an upper rotor assembly and a lower rotor assembly; a translational thrust system positioned at the extending tail and providing translational thrust to the airframe; and a flight control system including a flight control computer configured to control a rotational speed of the upper and the lower rotor assemblies (28, 32) of the main rotor assembly, characterized in that the flight control system includes an engine controller configured to control the rotational speed of the upper and the lower rotor assemblies (28, 32) of the main rotor assembly as a function of airspeed of the aircraft to maintain rotor blade tip speed of the upper and lower rotor assemblies (28, 32) below a threshold rotor tip speed, wherein the flight control computer further utilizes one or more of outside air temperature, airspeed, wind speed and/or direction to determine the threshold rotor tip speed of the main rotor assembly. an airframe having an extending tail; a counter rotating, coaxial main rotor assembly disposed at the airframe including an upper rotor assembly and a lower rotor assembly; a translational thrust system positioned at the extending tail and providing translational thrust to the airframe; and a flight control system including a flight control computer configured to control a rotational speed of the upper and the lower rotor assemblies (28, 32) of the main rotor assembly, characterized in that the flight control system includes an engine controller configured to control the rotational speed of the upper and the lower rotor assemblies (28, 32) of the main rotor assembly as a function of airspeed of the aircraft to maintain rotor blade tip speed of the upper and lower rotor assemblies (28, 32) below a threshold rotor tip speed, wherein the flight control computer further utilizes one or more of outside air temperature, airspeed, wind speed and/or direction to determine the threshold rotor tip speed of the main rotor assembly.
A process for use in a transport refrigeration unit having a compressor, a condenser, an evaporator, an economizer, a second expansion valve coupled between the economizer and the compressor, and a controller, and a first expansion valve upstream of the evaporator, the process comprising: detecting a capacity increase mode transition for the economizer and adaptively controlling an injection flow rate for the economizer during at least a portion of the capacity increase mode transition in response to one of available pressure, available power or available current to the transport refrigeration unit, where the adaptively controlling comprises selectively operating the second expansion valve through a transition from a first flow rate to a second higher flow rate using system conditions to control a rate of transition from the first flow rate to the second higher flow rate responsive to the capacity increase mode transition, where the system conditions set a prescribed time period for the transition, where the first flow rate is a non-zero injection flow rate less than 100%, the second flow rate is 100% injection flow rate, and the prescribed time period is greater than ten seconds. detecting a capacity increase mode transition for the economizer and adaptively controlling an injection flow rate for the economizer during at least a portion of the capacity increase mode transition in response to one of available pressure, available power or available current to the transport refrigeration unit, where the adaptively controlling comprises selectively operating the second expansion valve through a transition from a first flow rate to a second higher flow rate using system conditions to control a rate of transition from the first flow rate to the second higher flow rate responsive to the capacity increase mode transition, where the system conditions set a prescribed time period for the transition, where the first flow rate is a non-zero injection flow rate less than 100%, the second flow rate is 100% injection flow rate, and the prescribed time period is greater than ten seconds.
Method for producing three-dimensional components by successively solidifying layers of a powdery construction material, which can be solidified by means of electromagnetic radiation, in particular bundled radiation such as laser radiation or electron radiation, at the points corresponding to the relevant cross section of the component, in particular selective laser melting or selective laser sintering methods, wherein a device is provided with a supporting device that is height-adjustable within a construction chamber for supporting the component, comprising a coating device for applying layers of the construction material to the supporting device or a previously formed layer, and comprising an irradiation apparatus for irradiating layers of the construction material in regions in order to solidify said layers, wherein a portion of the surface to be coated is scanned for its evenness before another layer is applied and, if there is unevenness that exceeds a certain tolerance range, this unevenness is removed, characterised in that a portion of the surface to be coated is scanned using a sensor with unevenness coordinates being recorded, wherein the locally identified unevenness is locally mechanical removed in a targeted manner using the identified unevenness coordinates, wherein a removal element having a relatively small surface area is guided to an upwardly protruding point on the layer and the removal process is carried out here.
A computer-implemented method of extracting irradiation field areas in an X-ray image represented by a digital signal representation comprising the steps of: a. Segmenting said image in multiple regions of pixels which have similar local image characteristics per region; b. Fitting line segments to the boundaries of said regions whereby said line segments correspond with candidate irradiation field boundaries and constitute a segmentation map; and c. Classifying regions in said segmentation map into two classes, one class being irradiation field and the other class being collimated region, on the basis of at least one of local, regional and global image characteristics, wherein said segmentation of the image in multiple regions is based on multi-scale watershed segmentation. a. Segmenting said image in multiple regions of pixels which have similar local image characteristics per region; b. Fitting line segments to the boundaries of said regions whereby said line segments correspond with candidate irradiation field boundaries and constitute a segmentation map; and c. Classifying regions in said segmentation map into two classes, one class being irradiation field and the other class being collimated region, on the basis of at least one of local, regional and global image characteristics, wherein said segmentation of the image in multiple regions is based on multi-scale watershed segmentation.
A semiconductor light-emitting device, comprising: a substrate; and multiple epitaxial units on the substrate; wherein each of the multiple epitaxial units comprises: a first semiconductor layer having a first surface and a sidewall; a second semiconductor layer having a second surface opposite to the first surface; an active layer between the second semiconductor layer and the first semiconductor layer; a first electrode directly contacting the first surface and the substrate; and characterized by a transparent adhesive layer between the first surface and the substrate; and an insulative layer covering the sidewall and the transparent adhesive layer and without covering the first surface. a substrate; and multiple epitaxial units on the substrate; a first semiconductor layer having a first surface and a sidewall; a second semiconductor layer having a second surface opposite to the first surface; an active layer between the second semiconductor layer and the first semiconductor layer; a first electrode directly contacting the first surface and the substrate; and characterized by a transparent adhesive layer between the first surface and the substrate; and an insulative layer covering the sidewall and the transparent adhesive layer and without covering the first surface.
Compositions comprising, 1) as component I the: compound I-3 2-[4-(4-chlorophenoxy)-2-(trifluoromethyl)phenyl]-1-(1,2,4-triazol-1-yl)propan-2-ol; and 2) as component II a biopesticide selected from: Bacillus amyloliquefaciens ssp. plantarum MBI 600 (II-27), Bacillus pumilus INR-7 (II-29), Bacillus subtilis FB17 (II-176). 1) as component I the: compound I-3 2-[4-(4-chlorophenoxy)-2-(trifluoromethyl)phenyl]-1-(1,2,4-triazol-1-yl)propan-2-ol; and 2) as component II a biopesticide selected from: Bacillus amyloliquefaciens ssp. plantarum MBI 600 (II-27), Bacillus pumilus INR-7 (II-29), Bacillus subtilis FB17 (II-176). Bacillus amyloliquefaciens ssp. plantarum MBI 600 (II-27), Bacillus pumilus INR-7 (II-29), Bacillus subtilis FB17 (II-176).
An insert for guiding a part of an optical cable with an outer jacket comprising at least one optical fiber element and accommodated in a housing of an optical fiber assembly, said part of the optical cable has a cut-out portion in the outer jacket exposing said at least one optical fiber element, wherein said insert comprises an optical cable guidance means for guiding said optical cable across the insert, a recess surrounding the exposed optical fiber element, a bend element having a curved portion along which the optical fiber element is guided, while pulling out the optical fiber element from the optical fiber cable, which bend element is arranged at an end portion of the recess and projecting from the recess in a curved manner, the insert being characterised in that it comprises a crosslink bridging the cut-out portion of the optical cable and extending transverse to the running direction of the optical cable and, wherein said bend element is fixed to said crosslink, wherein the crosslink is arranged adjacent to said guidance means and wherein the guidance means is adapted to receive said jacket of the optical cable in a form fit manner.
A wrinkle detection apparatus for detecting a wrinkle area (304, 313) of facial skin included in an image (301, 315), comprising: a first threshold processing unit that detects a first edge area (302, 311) included in the image (301, 315) by performing first threshold processing for comparing a gradient value that indicates a degree of change in pixel values in the image (301, 315) including skin with a first threshold, the first edge area (302, 311) including a first continuous area and a second continuous area; a second threshold processing unit that detects a second edge area (303, 312) included in the image by performing second threshold processing for comparing the gradient value with a second threshold; wherein the second threshold is higher than the first threshold; and an edge selection processing unit that determines the wrinkle area (304, 313) based on an overlapping area in which the first edge area and the second edge area are overlapped, wherein the edge selection processing unit determines that the first continuous area is included in the overlapping area and that the second continuous area is not included in the overlapping area, and wherein the edge selection processing unit extracts the first continuous area as the wrinkle area (304, 313) and excludes the second continuous area from the wrinkle area (304, 313). a first threshold processing unit that detects a first edge area (302, 311) included in the image (301, 315) by performing first threshold processing for comparing a gradient value that indicates a degree of change in pixel values in the image (301, 315) including skin with a first threshold, the first edge area (302, 311) including a first continuous area and a second continuous area; a second threshold processing unit that detects a second edge area (303, 312) included in the image by performing second threshold processing for comparing the gradient value with a second threshold; wherein the second threshold is higher than the first threshold; and an edge selection processing unit that determines the wrinkle area (304, 313) based on an overlapping area in which the first edge area and the second edge area are overlapped, wherein the edge selection processing unit determines that the first continuous area is included in the overlapping area and that the second continuous area is not included in the overlapping area, and wherein the edge selection processing unit extracts the first continuous area as the wrinkle area (304, 313) and excludes the second continuous area from the wrinkle area (304, 313).
An information notification method used in a mobile communication system including a first base station and a second base station that perform communication with a user apparatus by inter-base station carrier aggregation, comprising: a step in which the first base station notifies the second base station of a configuration change request including first desired setting information; a second desired setting information notification step in which the second base station notifies the first base station of second desired setting information; a setting step (S103, S104) in which the first base station determines first setting information and second setting information to be set to the user apparatus based on the first desired setting information and the second desired setting information, and notifies the user apparatus of the first setting information and the second setting information; characterized by a difference notification step of, after completion of setting of the first setting information and the second setting information to the user apparatus, notifying the second base station of a difference between the first and second desired setting information before the setting step and the first and second setting information after the setting step. a step in which the first base station notifies the second base station of a configuration change request including first desired setting information; a second desired setting information notification step in which the second base station notifies the first base station of second desired setting information; a setting step (S103, S104) in which the first base station determines first setting information and second setting information to be set to the user apparatus based on the first desired setting information and the second desired setting information, and notifies the user apparatus of the first setting information and the second setting information; characterized by a difference notification step of, after completion of setting of the first setting information and the second setting information to the user apparatus, notifying the second base station of a difference between the first and second desired setting information before the setting step and the first and second setting information after the setting step.
A method of constructing a multi-material mold using additive manufacturing comprising: defining a structure of said mold; within said structure defining at least two sub-regions (18,20,22,24,32,34,36,40,42); associating said sub- regions with respective specific materials and printing said sub-regions with said respective associated specific material; wherein a first of said sub-regions comprises an internal sub-region (18, 32) that allows dissipation of heat accumulating during use of the mold, the associated first sub-region specific material being a heat conductive material, the second of said sub-regions comprising an embedded heat sink sub-region (20, 34) for conducting heat away from said internal sub-region allowing dissipation, the respective second sub-region associated specific material being a relatively non- conductive bulk mold material embedded with relatively high heat-conductive material; wherein said second sub-region further comprises a heat sink printed with polymeric ink, said polymeric ink forming conductive lines and layers designed to dissipate the heat from the internal mold surface. defining a structure of said mold; within said structure defining at least two sub-regions (18,20,22,24,32,34,36,40,42); associating said sub- regions with respective specific materials and printing said sub-regions with said respective associated specific material; wherein a first of said sub-regions comprises an internal sub-region (18, 32) that allows dissipation of heat accumulating during use of the mold, the associated first sub-region specific material being a heat conductive material, the second of said sub-regions comprising an embedded heat sink sub-region (20, 34) for conducting heat away from said internal sub-region allowing dissipation, the respective second sub-region associated specific material being a relatively non- conductive bulk mold material embedded with relatively high heat-conductive material; wherein said second sub-region further comprises a heat sink printed with polymeric ink, said polymeric ink forming conductive lines and layers designed to dissipate the heat from the internal mold surface.
A light-emitting device comprising: a first electrode; a first layer (111B, 111a); a first light-emitting layer (112B, 112a) over the first layer (111B, 111a); a second layer (111G, 111b) over the first light-emitting layer (112B, 112a), wherein the second layer (111G, 111b) is a layer including a hole transporting material and a material which exhibits an electron accepting property to the hole transporting material; a second light-emitting layer (112G, 112b) over the second layer(111G, 111b); and a second electrode over the second light-emitting layer (112G, 112b, wherein the first electrode is a reflective electrode; characterized in that the first layer (111B, 111a) is in contact with the first electrode, and comprises indium tin oxide containing silicon oxide. a first electrode; a first layer (111B, 111a); a first light-emitting layer (112B, 112a) over the first layer (111B, 111a); a second layer (111G, 111b) over the first light-emitting layer (112B, 112a), wherein the second layer (111G, 111b) is a layer including a hole transporting material and a material which exhibits an electron accepting property to the hole transporting material; a second light-emitting layer (112G, 112b) over the second layer(111G, 111b); and a second electrode over the second light-emitting layer (112G, 112b, wherein the first electrode is a reflective electrode; characterized in that the first layer (111B, 111a) is in contact with the first electrode, and comprises indium tin oxide containing silicon oxide.
A gas turbine engine comprising: a main reservoir for holding a fluid; an auxiliary reservoir located inside the main reservoir, the auxiliary reservoir comprising: an auxiliary reservoir shell comprising a shell top and a shell bottom; at least one fill passage through the auxiliary reservoir shell at or near the shell bottom; and at least one vent passage through the auxiliary reservoir shell at or near the shell top, wherein the auxiliary reservoir is fluidically connected to the main reservoir by the fill passage and the vent passage; a fluid inlet located inside the main reservoir and outside of the auxiliary reservoir; a fluid outlet located inside the auxiliary reservoir between the fill passage and the vent passage; a first supply passage in fluid communication with the fluid outlet and a first pump operably connected to the first supply passage for pumping the fluid from the auxiliary reservoir to a first engine component; a second supply passage connected to the main reservoir; and a second pump operably connected to the second supply passage for pumping the fluid from the main reservoir to a second engine component; wherein: the vent passage has a smaller flow area than the fill passage. a main reservoir for holding a fluid; an auxiliary reservoir located inside the main reservoir, the auxiliary reservoir comprising: an auxiliary reservoir shell comprising a shell top and a shell bottom; at least one fill passage through the auxiliary reservoir shell at or near the shell bottom; and at least one vent passage through the auxiliary reservoir shell at or near the shell top, wherein the auxiliary reservoir is fluidically connected to the main reservoir by the fill passage and the vent passage; an auxiliary reservoir shell comprising a shell top and a shell bottom; at least one fill passage through the auxiliary reservoir shell at or near the shell bottom; and at least one vent passage through the auxiliary reservoir shell at or near the shell top, wherein the auxiliary reservoir is fluidically connected to the main reservoir by the fill passage and the vent passage; a fluid inlet located inside the main reservoir and outside of the auxiliary reservoir; a fluid outlet located inside the auxiliary reservoir between the fill passage and the vent passage; a first supply passage in fluid communication with the fluid outlet and a first pump operably connected to the first supply passage for pumping the fluid from the auxiliary reservoir to a first engine component; a second supply passage connected to the main reservoir; and a second pump operably connected to the second supply passage for pumping the fluid from the main reservoir to a second engine component; wherein: the vent passage has a smaller flow area than the fill passage. the vent passage has a smaller flow area than the fill passage.
Nutritional composition comprising: - a protein fraction, - a carbohydrate fraction, - a lipid fraction comprising at least one fatty acid from the omega-3 group, - at least one mineral element, including iron, - at least one vitamin, including vitamin B6, - a combination of powdered ginger and an extract of the shoot system of the artichoke, said extract being obtained by extraction with water or with a water/alcohol mixture. - a protein fraction, - a carbohydrate fraction, - a lipid fraction comprising at least one fatty acid from the omega-3 group, - at least one mineral element, including iron, - at least one vitamin, including vitamin B6, - a combination of powdered ginger and an extract of the shoot system of the artichoke, said extract being obtained by extraction with water or with a water/alcohol mixture.