mhurhangee/patent-ind-claim-en huggingface dataset:
Method of producing a crystalline semiconductor foil with an integrated electric field, comprising: - doping a fluid semiconductor with a doping substance having an equilibrium segregation coefficient k 0 where k 0 < 0.01, - filling a casting frame with the fluid semiconductor ; - drawing a foil from the casting frame containing said fluid semiconductor in a production direction by passing a substrate band underneath the casting frame, wherein the substrate band has a lower temperature than the fluid semiconductor in the bottom of the casting frame, so that a bottom layer of the fluid semiconductor crystallises on the substrate band as a crystallized layer and the semiconductor foil is produced on the substrate band on one side of the casting frame characterised by : - cooling said fluid semiconductor in such a way that the crystallised layer is thicker at the output end of the casting frame and the crystal growth speed decreases in a direction essentially perpendicular to the substrate band , by keeping the respective temperature of the substrate and the fluid semiconductor to be supplied constant for creating a gradient doping profile in the crystalline semiconductor foil that has a desired high value on one side of the foil. - doping a fluid semiconductor with a doping substance having an equilibrium segregation coefficient k 0 where k 0 < 0.01, - filling a casting frame with the fluid semiconductor ; - drawing a foil from the casting frame containing said fluid semiconductor in a production direction by passing a substrate band underneath the casting frame, wherein the substrate band has a lower temperature than the fluid semiconductor in the bottom of the casting frame, so that - cooling said fluid semiconductor in such a way that the crystallised layer is thicker at the output end of the casting frame and the crystal growth speed decreases in a direction essentially perpendicular to the substrate band , by keeping the respective temperature of the substrate and the fluid semiconductor to be supplied constant for creating a gradient doping profile in the crystalline semiconductor foil that has a desired high value on one side of the foil.
An image processing apparatus, comprising: a control portion configured to calculate an amount of overlapping between a first captured image and a second captured image; the control portion further configured to carry out image stabilization, wherein the image stabilization comprises: setting a first image production area for the first captured image and setting a second image production area for the second captured image, wherein the size of the first image production area and the size of the second image production area are based on the amount of overlapping, wherein the image in the first image production area and the image in the second image production area, when connected to each other, produce a panoramic image, wherein the control portion is further configured to increase the size of at least one of the first image production area and the second image production area when the amount of overlapping is equal to or smaller than an image stabilization limitation threshold value. a control portion configured to calculate an amount of overlapping between a first captured image and a second captured image; the control portion further configured to carry out image stabilization, wherein the image stabilization comprises: setting a first image production area for the first captured image and setting a second image production area for the second captured image, wherein the size of the first image production area and the size of the second image production area are based on the amount of overlapping, wherein the image in the first image production area and the image in the second image production area, when connected to each other, produce a panoramic image, wherein the control portion is further configured to increase the size of at least one of the first image production area and the second image production area when the amount of overlapping is equal to or smaller than an image stabilization limitation threshold value.
Use of Mitogen-activated protein kinase 1 (ERK2) to normalise biological variation in the expression level of one or more platelet proteins in an ex vivo diagnostic method of Alzheimer's disease which uses the quantification of proteins in a platelet sample.
A gas turbine engine comprising: a fan rotor , a first compressor rotor and a second compressor rotor , said second compressor rotor for compressing air to a higher pressure than said first compressor rotor ; a first turbine rotor , said first turbine rotor configured to drive said second compressor rotor , and a second turbine rotor , said second turbine rotor configured to drive said first compressor rotor ; and a fan drive turbine positioned downstream of said second turbine rotor , wherein said first compressor rotor and said second turbine rotor are configured to rotate as an intermediate speed spool , said second compressor rotor and said first turbine rotor are configured to rotate together as a high speed spool , said high speed spool and said fan drive turbine are configured to rotate in the same, first direction, and said intermediate speed spool is configured to rotate in an opposed, second direction, characterised in that : said fan drive turbine drives said fan rotor through a gear reduction ; and a mid-turbine frame (TMTF) is positioned between said first and second turbine rotors , and a turning vane is positioned between said mid-turbine frame (TMTF) and said second turbine rotor . a fan rotor , a first compressor rotor and a second compressor rotor , said second compressor rotor for compressing air to a higher pressure than said first compressor rotor ; a first turbine rotor , said first turbine rotor configured to drive said second compressor rotor , and a second turbine rotor , said second turbine rotor configured to drive said first compressor rotor ; and a fan drive turbine positioned downstream of said second turbine rotor , wherein said first compressor rotor and said second turbine rotor are configured to rotate as an intermediate speed spool , said second compressor rotor and said first turbine rotor are configured to rotate together as a high speed spool , said high speed spool and said fan drive turbine are configured to rotate in the same, first direction, and said intermediate speed spool is configured to rotate in an opposed, second direction, characterised in that : said fan drive turbine drives said fan rotor through a gear reduction ; and a mid-turbine frame (TMTF) is positioned between said first and second turbine rotors , and a turning vane is positioned between said mid-turbine frame (TMTF) and said second turbine rotor . said fan drive turbine drives said fan rotor through a gear reduction ; and a mid-turbine frame (TMTF) is positioned between said first and second turbine rotors , and a turning vane is positioned between said mid-turbine frame (TMTF) and said second turbine rotor .
An oxalate salt of 6-(2,4-dichlorophenyl)-5-{4-[1-(3-fluoro-propyl)-pyrrolidin-3-yloxy]-phanyl)-8,9-dihydro-7H-benzocycloheptene-2-carboxylic acid methyl ester of the formula below:
An electrical architecture for an aircraft comprising two air-conditioning systems , two converters (16, 18; 46, 48; 62L, 62R), each intended to power one of the air-conditioning systems , and comprising at least one first electric machine (24; 24L) which starts up a first main engine (42; 42L) of the aircraft, and wherein each of the two converters (16, 18; 46, 48; 62L, 62R) comprises two inverters (26, 28, 38, 40; 50, 52, 54, 56; 64L, 66L, 64R, 66R), characterized in that the electrical architecture (10; 47; 60) is configured such that the two converters (16, 18; 46, 48; 62L, 62R) can together power the first electric machine (24; 24L), in that the electrical architecture (10; 47; 60) further comprises a coupler for linking at least two first of the inverters, and in that the electric machine comprises a main winding (24-1) that can be powered by the coupler and an exciter winding (24-2) that can be powered by a second one of the inverters.
Mounting unit having at least one mounting rail to which at least one holding clip is releasably fixable, said at least one holding clip having two clip parts (4, 5; 104, 105) which (4, 5; 104, 105), by means of a clamping device , are braceable against one another in such a way that, in a holding position, the clip parts (4, 5; 104, 105) clamp the mounting rail in between them at least in a sub-region, wherein the clamping device has a clamping pin which projects from a first clip part and which extends through a passage opening in a second clip part , wherein the clamping device has a sleeve-like clamping element for subjecting the second clip part to pressure, which , by way of its sleeve interior, is rotatably mounted against or on the clamping pin , characterized in that the sleeve-like clamping element has at least one guide path with a curved or helical path profile, on which at least one guide path at least one assigned pin tooth , or clamping protrusion , held on the clamping pin is guided in such a way that a relative rotational movement between the clamping element and the clamping pin is converted into a longitudinal movement of the clamping element on the clamping pin .
A vehicle comprising a battery , a plug receiving portion for receiving a plug for supplying an electric power to be charged in said battery or a plug for receiving an electric power discharged from said battery , a lid for closing said plug receiving portion and a light for illuminating said plug receiving portion , characterized in that when the state of said vehicle becomes a running mode indicating a state that the running of said vehicle is permitted, said light is turned off.
A method for manufacturing a delaminatable container , the container comprising: an outer shell ; an inner bag configured to store contents therein and to shrink as the contents decrease; a cap configured to discharge the contents stored in the inner bag ; an air inlet formed on the outer shell ; and a hydrophobic filter (F) arranged to block the air inlet and configured to to allow permeation of air and blocking of water, wherein the hydrophobic filter (F) is a laminate of a hydrophobic microporous membrane (F1) and a nonwoven fabric (F2) ; the method comprising: providing the outer shell with a rib (R) formed around the air inlet ; subjecting the hydrophobic filter (F) placed on the rib (R) to ultrasonic sealing in a direction where the rib (R) of the outer shell is in contact with the nonwoven fabric (F2), wherein during the ultrasonic sealing the rib (R) functions as energy director; wherein a combination of Gurley number of the hydrophobic filter (F), area of the hydrophobic filter (F), and discharge pressure of the cap is selected so that an amount of air leakage through the hydrophobic filter (F) represented by the following equation would be 0.5 ml/sec to 2.4 ml/sec, the amount of air leakage being defined as: amount of air leakage ml an outer shell ; an inner bag configured to store contents therein and to shrink as the contents decrease; a cap configured to discharge the contents stored in the inner bag ; an air inlet formed on the outer shell ; and a hydrophobic filter (F) arranged to block the air inlet and configured to to allow permeation of air and blocking of water, wherein the hydrophobic filter (F) is a laminate of a hydrophobic microporous membrane (F1) and a nonwoven fabric (F2) ; the method comprising: providing the outer shell with a rib (R) formed around the air inlet ; subjecting the hydrophobic filter (F) placed on the rib (R) to ultrasonic sealing in a direction where the rib (R) of the outer shell is in contact with the nonwoven fabric (F2), wherein during the ultrasonic sealing the rib (R) functions as energy director; wherein a combination of Gurley number of the hydrophobic filter (F), area of the hydrophobic filter (F), and discharge pressure of the cap is selected so that an amount of air leakage through the hydrophobic filter (F) represented by the following equation would be 0.5 ml/sec to 2.4 ml/sec, the amount of air leakage being defined as: amount of air leakage ml providing the outer shell with a rib (R) formed around the air inlet ; subjecting the hydrophobic filter (F) placed on the rib (R) to ultrasonic sealing in a direction where the rib (R) of the outer shell is in contact with the nonwoven fabric (F2), wherein during the ultrasonic sealing the rib (R) functions as energy director; wherein a combination of Gurley number of the hydrophobic filter (F), area of the hydrophobic filter (F), and discharge pressure of the cap is selected so that an amount of air leakage through the hydrophobic filter (F) represented by the following equation would be 0.5 ml/sec to 2.4 ml/sec, the amount of air leakage being defined as: amount of air leakage ml
A sliding door stopper , which allows a sliding door (K) to be closed by being activated upon a fuel lid is opened after the sliding door (K) is opened during fuel filling, comprising - at least one stopper mechanism which is adapted to be provided between the sliding door (K) and the fuel lid on the vehicle body (G), and which is connected to at least one stopper pin wherein the stopper mechanism is adapted to detect that the fuel lid is opened and adapted to bring the stopper pin to a preventing position according to this information to prevent the sliding door (K) from opening and characterized by the stopper pin comprising - at least one lower pin which enables the connection of the stopper pin to the stopper mechanism , - at least one moving upper pin which can be bent such that the stopper pin will not prevent the sliding door (K) in open position from closing, - at least one rotating pin which enables the connection between the lower pin and the moving upper pin and enables the moving upper pin to rotate around its own axis, - at least one spring which enables the moving upper pin to become its previous vertical state after it is bent by rotating around the rotating pin after the sliding door (K) is closed. - at least one stopper mechanism which is adapted to be provided between the sliding door (K) and the fuel lid on the vehicle body (G), and which is connected to at least one stopper pin wherein the stopper mechanism is adapted to detect that the fuel lid is opened and adapted to bring the stopper pin to a preventing position according to this information to prevent the sliding door (K) from opening and characterized by the stopper pin comprising - at least one lower pin which enables the connection of the stopper pin to the stopper mechanism , - at least one moving upper pin which can be bent such that the stopper pin will not prevent the sliding door (K) in open position from closing, - at least one rotating pin which enables the connection between the lower pin and the moving upper pin and enables the moving upper pin to rotate around its own axis, - at least one spring which enables the moving upper pin to become its previous vertical state after it is bent by rotating around the rotating pin after the sliding door (K) is closed.
Humidifier for a fuel cell device , with a plurality of flow field frames , between each of which a humidifier membrane is arranged, characterized in that a plurality of cooling flow field frames being identically formed to the flow field frames , between each of which a separating plate is arranged, form an integrated charge air cooler , and in that a coupling plate is provided between the flow field frames arranged in a stack and the cooling flow field frames arranged in a stack.
A system for detection of intruding objects , including: a photographic or video device receiving an image from at least a portion of a surface; at least one illumination device with a zone of illumination directed toward the surface; and wherein an object intruding into at least a portion of the zone of illumination causes a shadow to be cast on the surface, whereby the shadow is at least a portion of the image being received by the photographic or video device , whereby presence of the object intruding into at least a portion of the zone of illumination is detected, wherein the at least one illumination device includes a first illumination device defining a first zone of illumination having a first wavelength and a second illumination device defining a second zone of illumination having a second wavelength different from the first wavelength, wherein the first zone of illumination defines a first cone , the second zone of illumination defines a second cone , and the field of view of the photographic or video device defines a third cone , and wherein the first, second and third cones at least partially intersect on the surface thereby defining an intrusion detection zone. a photographic or video device receiving an image from at least a portion of a surface; at least one illumination device with a zone of illumination directed toward the surface; and wherein an object intruding into at least a portion of the zone of illumination causes a shadow to be cast on the surface, whereby the shadow is at least a portion of the image being received by the photographic or video device , whereby presence of the object intruding into at least a portion of the zone of illumination is detected, wherein the at least one illumination device includes a first illumination device defining a first zone of illumination having a first wavelength and a second illumination device defining a second zone of illumination having a second wavelength different from the first wavelength, wherein the first zone of illumination defines a first cone , the second zone of illumination defines a second cone , and the field of view of the photographic or video device defines a third cone , and
A transmission method for transmitting transmission streams comprising: performing a signal processing to convert a first bit stream and a second bit stream into a first transmission stream including first transmission signal points z1(t) and a second transmission stream including second transmission signal points z2(t), where t is index of a signal point, the signal processing including: mapping the first bit stream into first complex signal points s1(t) using a first modulation scheme; mapping the second bit stream into second complex signal points s2(t) using a second modulation scheme; converting two complex signal points s1 and s2 to two transmission signal points z1 and z2, respectively, by multiplication with a precoding matrix F and a phase change matrix Y(t); and transmitting the first transmission stream and the second transmission stream by using antennas ; wherein the phase change matrix Y(t) is defined as Y t = 1 0 0 y t , wherein y(t) is a phase changing formula, wherein the following 8 candidate values are provided for 8 of consecutive y(t) e j 0 , e j π 4 , e j 1 π 2 , e j 3 π 4 , e jπ , e j 5 π 4 , e j 3 π 2 , e j 7 π 4 , and wherein each of 8 candidate values is periodically used for y(t). mapping the first bit stream into first complex signal points s1(t) using a first modulation scheme; mapping the second bit stream into second complex signal points s2(t) using a second modulation scheme; converting two complex signal points s1 and s2 to two transmission signal points z1 and z2, respectively, by multiplication with a precoding matrix F and a phase change matrix Y(t); and transmitting the first transmission stream and the second transmission stream by using antennas ; wherein the phase change matrix Y(t) is defined as Y t = 1 0 0 y t , wherein y(t) is a phase changing formula, wherein the following 8 candidate values are provided for 8 of consecutive y(t) e j 0 , e j π 4 , e j 1 π 2 , e j 3 π 4 , e jπ , e j 5 π 4 , e j 3 π 2 , e j 7 π 4 , and wherein each of 8 candidate values is periodically used for y(t).
A method of displaying an image, the method comprising: recognizing, by a sensor, a speed and direction of an object as the object approaches an image capture button ; capturing a plurality of frames in response to a recognized movement pattern of the object after recognizing the speed and direction of the object that approaches the image capture button; recognizing the image capture button is touched or selected by the object; automatically determining a frame from among the plurality of captured frames after recognizing that the image capture button is touched or selected by the object, based on a pattern history in which the pattern of a user selecting at least one frame that is captured at the point of time when the image capture button is touched or selected, is stored; and displaying the determined frame on a display unit . recognizing, by a sensor, a speed and direction of an object as the object approaches an image capture button ; capturing a plurality of frames in response to a recognized movement pattern of the object after recognizing the speed and direction of the object that approaches the image capture button; recognizing the image capture button is touched or selected by the object; automatically determining a frame from among the plurality of captured frames after recognizing that the image capture button is touched or selected by the object, based on a pattern history in which the pattern of a user selecting at least one frame that is captured at the point of time when the image capture button is touched or selected, is stored; and displaying the determined frame on a display unit .
An aircraft comprising a wing , wing, the wing having a fixed wing with a wing tip device , the wing tip device rotatably mounted about a hinge axis , such that the wing tip device may rotate, about the hinge axis, relative to the fixed wing, wherein the aircraft comprises an actuator assembly operable to rotate the wing tip device about the hinge axis, the actuator assembly comprising: a tubular shaft having an axis of rotation orientated non-parallel to the hinge axis, a motor , at least partially housed within the tubular shaft and operable to cause rotation of the tubular shaft, and a tip-rotating shaft arranged along the hinge axis and coupled to the tubular shaft, thereby to rotate the wing tip device about the hinge axis in response to the rotation of the tubular shaft. a tubular shaft having an axis of rotation orientated non-parallel to the hinge axis, a motor , at least partially housed within the tubular shaft and operable to cause rotation of the tubular shaft, and a tip-rotating shaft arranged along the hinge axis and coupled to the tubular shaft, thereby to rotate the wing tip device about the hinge axis in response to the rotation of the tubular shaft.