mhurhangee/ep-ind-claims huggingface dataset:
Method for correction of a trapezoidal distortion of images (2, 4, 7) in image processing for medium-image registration in a printing device, the method comprising the steps of: A) determining a trapezoidal distortion of an image (2, 4, 7) to be printed, B) calculating the amount and the positioning of linear arrays of image pixels to be omitted or to be added to correct the trapezoidal distortion determined under step A), and C) printing the image (2, 4, 7) onto a medium (1, 5, 8), wherein the multiple linear image pixel arrays (6, 9) calculated under step B) are omitted or added, wherein the omission of the linear arrays of image pixels in step C) is a deletion of said linear arrays and the addition of the linear arrays of image pixels in step C) is a duplication of pixel values of a contiguous pixel array, and the linear image pixel arrays (6, 9) extend to a side of the image (2, 4, 7) in a direction substantially perpendicular to a processing direction (y) of the medium (1, 5, 8) and have a length being smaller than the width of the image to be registered, wherein according to step A) the trapezoidal distortion of an image (2, 4, 7) to be printed is determined by determining a pressure difference between an image-carrying member and an image-receiving member in a transfer or transfuse nip of the printing device, characterized in that the lengths of the linear image pixel arrays (6, 9) are mutually substantially different and the linear image pixel arrays (6, 9) with different lengths are positioned substantially randomly. A) determining a trapezoidal distortion of an image (2, 4, 7) to be printed, B) calculating the amount and the positioning of linear arrays of image pixels to be omitted or to be added to correct the trapezoidal distortion determined under step A), and C) printing the image (2, 4, 7) onto a medium (1, 5, 8), wherein the multiple linear image pixel arrays (6, 9) calculated under step B) are omitted or added, wherein the omission of the linear arrays of image pixels in step C) is a deletion of said linear arrays and the addition of the linear arrays of image pixels in step C) is a duplication of pixel values of a contiguous pixel array, and the linear image pixel arrays (6, 9) extend to a side of the image (2, 4, 7) in a direction substantially perpendicular to a processing direction (y) of the medium (1, 5, 8) and have a length being smaller than the width of the image to be registered, wherein according to step A) the trapezoidal distortion of an image (2, 4, 7) to be printed is determined by determining a pressure difference between an image-carrying member and an image-receiving member in a transfer or transfuse nip of the printing device, characterized in that the lengths of the linear image pixel arrays (6, 9) are mutually substantially different and the linear image pixel arrays (6, 9) with different lengths are positioned substantially randomly.
A waveguide comprising first and second waveguide sections, each waveguide section comprising a main body portion and a connecting portion at its distal end, said first and second waveguide sections being longitudinally aligned to define a conduit therethrough with a butted interface therebetween, characterized in that the connecting portion of each waveguide section has: (i) a first circumferential dam on its outer surface located adjacent its distal end, (ii) a second circumferential dam on its outer surface spaced apart from the first circumferential dam, and (iii) a third circumferential dam on its outer surface located between said first and second circumferential dams, such that a first respective recess is defined between said second and third circumferential dams and a second respective recess is defined between said first and third circumferential dams; and in that the waveguide further comprises a sleeve member over said butted interface, such that a respective first cavity is defined between an inner surface of said sleeve member and each said first recess and a respective second cavity is defined between the inner surface of said sleeve member and each said second recess, each said first cavity having a chemical adhesive therein operative to join said first and second waveguide sections together by means of said sleeve member, each said second cavity being an overflow region for receiving excess adhesive from said first cavity.
A control system for an aerospace vehicle, the control system comprising: a voter; and a plurality of control blocks, wherein each of the control blocks comprises: a controller configured to receive an input signal and perform a control algorithm comprising an integral function on the input signal to provide an output signal; and a feedback controller configured to: receive the output signal from the controller, a reference signal from an external controller, and a plant feedback signal from an external plant; perform a feedback algorithm on the output signal to provide a feedback control signal; and perform a combinator algorithm using the reference signal, the plant feedback signal and the feedback control signal to provide the input signal to the controller; wherein the voter is configured to receive the output signals and perform a voting algorithm on the output signals to determine a control signal to provide to the external plant. a controller configured to receive an input signal and perform a control algorithm comprising an integral function on the input signal to provide an output signal; and a feedback controller configured to: receive the output signal from the controller, a reference signal from an external controller, and a plant feedback signal from an external plant; perform a feedback algorithm on the output signal to provide a feedback control signal; and perform a combinator algorithm using the reference signal, the plant feedback signal and the feedback control signal to provide the input signal to the controller; wherein the voter is configured to receive the output signals and perform a voting algorithm on the output signals to determine a control signal to provide to the external plant. receive the output signal from the controller, a reference signal from an external controller, and a plant feedback signal from an external plant; perform a feedback algorithm on the output signal to provide a feedback control signal; and perform a combinator algorithm using the reference signal, the plant feedback signal and the feedback control signal to provide the input signal to the controller; wherein the voter is configured to receive the output signals and perform a voting algorithm on the output signals to determine a control signal to provide to the external plant. perform a combinator algorithm using the reference signal, the plant feedback signal and the feedback control signal to provide the input signal to the controller; wherein the voter is configured to receive the output signals and perform a voting algorithm on the output signals to determine a control signal to provide to the external plant.
Filter arrangement for a combustion engine for lowering the pressure of the air that builds up in the crankcase of the engine when the engine is running for separating undesired particles from said air, said filter arrangement comprising a filter unit having a top face and a bottom face, an inlet for contamined air, an outlet for delivering clean air, and a drainage conduit, wherein the inlet is adapted to be connected to the crankcase, said outlet is adapted to be connected to the engine's inlet manifold, and the drainage conduit is adapted to lead separated particles back into the crankcase, characterized in that the filter unit having, between its top and bottom faces, one or more walls of fibrous mass, through which contamined air has to pass and wherein the fibrous mass comprises fibres which are bonded to each other.
A cosmetic puff produced using a membrane film, the cosmetic puff including: an inner skin of which at least one surface forms a liquid cosmetic material storage part made of a membrane film; a porous cushion material which entirely or partially covers the outer surface of the inner skin; an outer skin which covers the inner skin and the cushion material to block penetration of an external makeup cosmetic material or external bacteria; a liquid cosmetic material which is stored in the liquid cosmetic material storage part; and a coating film which is coated on a portion of the inner side of the inner skin, wherein the membrane film of the inner skin is porous with numerous pores having sizes approximately between 0.025 to 0.2 μ m, the stored liquid cosmetic material is discharged to the outside through the numerous pores of the membrane film by a predetermined pressurization force F. an inner skin of which at least one surface forms a liquid cosmetic material storage part made of a membrane film; a porous cushion material which entirely or partially covers the outer surface of the inner skin; an outer skin which covers the inner skin and the cushion material to block penetration of an external makeup cosmetic material or external bacteria; a liquid cosmetic material which is stored in the liquid cosmetic material storage part; and a coating film which is coated on a portion of the inner side of the inner skin, wherein the membrane film of the inner skin is porous with numerous pores having sizes approximately between 0.025 to 0.2 μ m, the stored liquid cosmetic material is discharged to the outside through the numerous pores of the membrane film by a predetermined pressurization force F.
A method for producing a sintered ferrite magnet comprising the steps of preparing raw material powders comprising metal elements of Ca, La, an element A which is Ba and/or Sr, Fe and Co, which are represented by the general formula of Ca 1-x-y La x A y Fe 2n-z Co z, wherein 1-x-y, x, y and z representing the atomic ratios of said metal elements, and n representing a molar ratio meet: 0.3 ≤ 1-x-y < 0.65, 0.3 ≤ x ≤ 0.65, 0 ≤ y ≤ 0.2, 0.25 ≤ z ≤ 0.65, and 4.5 ≤ n ≤ 7; calcining said raw material powders to obtain a calcined body; pulverizing said calcined body to powder; molding said powder to obtain a green body; and sintering said green body to obtain a sintered body; 0-1.8% by mass of SiO 2 and 0-2% by mass (as CaO) of CaCO 3 being added to 100% by mass of said calcined body after calcining and before molding; and said sintering step being conducted with a temperature-elevating speed of 1-4°C/minute in a temperature range from 1100°C to a sintering temperature, and a temperature-lowering speed of 6°C/minute or more in a temperature range from the sintering temperature to 1100°C. 0.3 ≤ 1-x-y < 0.65, 0.3 ≤ x ≤ 0.65, 0 ≤ y ≤ 0.2, 0.25 ≤ z ≤ 0.65, and 4.5 ≤ n ≤ 7;
A method for controlling at least one guide vane of a gas turbine comprising: receiving a reference signal associated with the at least one guide vane; measuring an actuator position and an angular position associated with the at least one guide vane; generating a deadband signal based at least in part on the angular position; and manipulating the at least one guide vane based at least in part on the deadband signal and the reference signal, wherein generating the deadband signal is further based on a difference between the actuator position and the angular position. receiving a reference signal associated with the at least one guide vane; measuring an actuator position and an angular position associated with the at least one guide vane; generating a deadband signal based at least in part on the angular position; and manipulating the at least one guide vane based at least in part on the deadband signal and the reference signal, wherein generating the deadband signal is further based on a difference between the actuator position and the angular position.
An information handling system, IHS, comprising: a server chassis; and a casing in which the server chassis is inserted, the casing (i) designed to be utilized as both the exterior casing of the server chassis and an external shipping carton for physically shipping the IHS to a destination and (ii) formed of a structurally rigid material to protect the server chassis and any functional compute components inserted within the server chassis, wherein the casing comprises sealable flaps that enable the server chassis to be fully enclosed within the casing and the casing is sized to closely receive the server chassis to prevent relative movement of the server chassis within the casing, wherein the chassis comprises at least one molded receptacle to engageably receive a selected modular, functional compute component. a server chassis; and a casing in which the server chassis is inserted, the casing (i) designed to be utilized as both the exterior casing of the server chassis and an external shipping carton for physically shipping the IHS to a destination and (ii) formed of a structurally rigid material to protect the server chassis and any functional compute components inserted within the server chassis, wherein the casing comprises sealable flaps that enable the server chassis to be fully enclosed within the casing and the casing is sized to closely receive the server chassis to prevent relative movement of the server chassis within the casing, wherein the chassis comprises at least one molded receptacle to engageably receive a selected modular, functional compute component.
The pyrimidylaminobenzamide derivative named 4-methyl-3-[[4-(3-pyridinyl)-2-pyrimidinyl]amino]- N -[5-(4-methyl-1H-imidazol-1-yl)-3-(trifluoromethyl)phenyl] benzamide of formula: or a N-oxide or a pharmaceutially acceptable salt thereof, for use in a method for the treatment of a myeloproliferative disease selected from hypereosinophilic syndrome, chronic eosinophilic leukemia and hypereosinophilic syndrome with resistance to imatinib.
A method for damping tower vibrations in a floating wind turbine installation, the installation comprising a floating cell, a tower arranged over the floating cell, a generator mounted on the tower that is rotatable in relation to the wind direction and fitted with a wind turbine comprising turbine blades, and an anchor line arrangement that is connectable to anchors or foundations on a sea bed; wherein the method comprises: controlling the generator in response to changes in the relative wind velocity against the turbine, by controlling the blade angle of the turbine blades by means of a controller in the constant power or RPM range of the wind turbine; and damping the tower's eigenvibrations (ω eig) by, in addition to controlling the controller in the constant power or RPM range of the wind turbine, an increment (Δβ) being added to the blade angle of the turbine blades on the basis of the tower velocities (ΔŻ), so that the eigenvibrations of the tower are counteracted; wherein the vibrations in the horizontal displacement of the top of the tower (ΔZ) that have frequency ω eig are damped by means of a stabiliser with a transfer function (H stab (s)) between the tower velocities (ΔŻ) and the blade angle increment (Δβ) and wherein the stabiliser is provided with a low pass filter that is arranged such that the stabiliser does not affect the blade angle at frequencies in a range above the tower vibrations' eigenfrequency (ω eig). controlling the generator in response to changes in the relative wind velocity against the turbine, by controlling the blade angle of the turbine blades by means of a controller in the constant power or RPM range of the wind turbine; and damping the tower's eigenvibrations (ω eig) by, in addition to controlling the controller in the constant power or RPM range of the wind turbine, an increment (Δβ) being added to the blade angle of the turbine blades on the basis of the tower velocities (ΔŻ), so that the eigenvibrations of the tower are counteracted; wherein the vibrations in the horizontal displacement of the top of the tower (ΔZ) that have frequency ω eig are damped by means of a stabiliser with a transfer function (H stab (s)) between the tower velocities (ΔŻ) and the blade angle increment (Δβ) and wherein the stabiliser is provided with a low pass filter that is arranged such that the stabiliser does not affect the blade angle at frequencies in a range above the tower vibrations' eigenfrequency (ω eig).
Method for transmitting data of a vehicle to a mobile device, characterized in that a point in time is sensed at which the mobile device leaves the vehicle, in that the mobile device is informed by an apparatus of the vehicle as soon as the mobile device leaves the vehicle, in that the transmission of the data from the device to the mobile device is started and controlled starting from the sensed point in time by the mobile device, and in that the transmission of the data takes place automatically without a user action.
Automatically controlled washing machine having, arranged at the front within the body of the machine, a dispensing mechanism for laundry treatment media, which mechanism contains a drawer which is accessible from the front having at least one container (11, 12, 16 to 18) for powdered, liquid or gel-form laundry treatment media, and having a device (15, 16) for automatically feeding each stored laundry treatment medium into the treatment process, characterised in that the drawer consists of a guide frame which has a handle at the front and at least one window-like recess (23 to 27) for housing an insertable container (11, 12, 16 to 18) for laundry treatment media, that the guide frame is supported by lateral support legs so as to be angularly stable with respect to the handle, and the window-like recess (23 to 27) has a downwardly directed flange at its edge.
A display device comprising: a base layer defining a flat area and a first bending area, the first bending area bent from the flat area according to a bending axis, wherein the first bending area comprises a display area and a peripheral area adjacent to the display area; a display element layer disposed on the base layer; a thin film encapsulation layer disposed on the display element layer; and an input sensing circuit configured to sense an external input in an electrostatic capacitive manner and directly disposed on the encapsulation layer, the input sensing circuit comprising: a conductive layer (TS-CL1, TS-CL2) disposed on the thin film encapsulation layer; an insulating layer (TS-IL1, TS-IL2) overlapping the conductive layer; and a plurality of signal lines (SPL2a, SPL2b, SPL2C, SPL2d, SPL2e) disposed in the peripheral area and connected to the conductive layer, wherein a first signal line of the signal lines comprises at least two inclined portions inclined with respect to the bending axis and at least two parallel portions parallel to the bending axis, in the peripheral area of the first bending area. a base layer defining a flat area and a first bending area, the first bending area bent from the flat area according to a bending axis, wherein the first bending area comprises a display area and a peripheral area adjacent to the display area; a display element layer disposed on the base layer; a thin film encapsulation layer disposed on the display element layer; and an input sensing circuit configured to sense an external input in an electrostatic capacitive manner and directly disposed on the encapsulation layer, the input sensing circuit comprising: a conductive layer (TS-CL1, TS-CL2) disposed on the thin film encapsulation layer; an insulating layer (TS-IL1, TS-IL2) overlapping the conductive layer; and a plurality of signal lines (SPL2a, SPL2b, SPL2C, SPL2d, SPL2e) disposed in the peripheral area and connected to the conductive layer, wherein a first signal line of the signal lines comprises at least two inclined portions inclined with respect to the bending axis and at least two parallel portions parallel to the bending axis, in the peripheral area of the first bending area. a conductive layer (TS-CL1, TS-CL2) disposed on the thin film encapsulation layer; an insulating layer (TS-IL1, TS-IL2) overlapping the conductive layer; and a plurality of signal lines (SPL2a, SPL2b, SPL2C, SPL2d, SPL2e) disposed in the peripheral area and connected to the conductive layer, wherein a first signal line of the signal lines comprises at least two inclined portions inclined with respect to the bending axis and at least two parallel portions parallel to the bending axis, in the peripheral area of the first bending area.
A method for enriching atrial myocytes or ventricular myocytes in a cardiomyocyte-containing cell population induced from stem cells, comprising a step of collecting atrial myocytes or ventricular myocytes from the cell population by using an expression level of CD151 as an index.
A design program for causing a computer to execute a process for designing a composition of a perovskite type crystal structure, the design program comprising causing a computer to determine a combination of A i and B i in the following formula created by taking a logarithm of a formula of a tolerance factor, t, represented by the following formula, in which logt is 0, by executing ground state search by an annealing method using an Ising model or QUBO, t = r A + r X 2 r B + r X = d A − X 2 d B − X log t = ∑ i = 1 n A i − ∑ i = 1 n B i wherein, in the formula, r A, r B, and rx represent ionic radii at A site, B site, and an anion site, respectively, when a general formula of the perovskite type crystal structure is represented by ABX, in which A represents a cation, B represents a cation, and X represents an anion, and d A-X = r A + rx and d B-X = r B + rx are satisfied, wherein, in the formula, A i and B i are represented by the following formulas and, respectively, 1 n log d A i − X ≡ A i 1 n log 2 d B i − X ≡ B i wherein, in the formulas,, and, n is the parameter n in a composition formula A 1 p A 2 q...B 1 r B 2 s...X n, where p + q +... = r + s +... = n and each number represents an integer, and where ions A 1, A 2,..., and A u of composition ratio p: q:... are located at the A site, and ions B 1, B 2,..., and B v of composition ratio r: s:... are located at the B site in the ABX which is the general formula, and moreover, the d A-X and d Ai-X in the formula satisfy the following formula, and the d B -x and d Bi-X in the formula satisfy the following formula, d A − X = ∏ i = 1 n r A i + r X 1 n = ∏ i = 1 n d A i − X 1 n d B − X = ∏ i = 1 n r B i + r X 1 n = ∏ i = 1 n d B i − X 1 n wherein, in the formulas and, n is the same as n in the formulas to. wherein, in the formula, r A, r B, and rx represent ionic radii at A site, B site, and an anion site, respectively, when a general formula of the perovskite type crystal structure is represented by ABX, in which A represents a cation, B represents a cation, and X represents an anion, and d A-X = r A + rx and d B-X = r B + rx are satisfied, wherein, in the formula, A i and B i are represented by the following formulas and, respectively, 1 n log d A i − X ≡ A i 1 n log 2 d B i − X ≡ B i wherein, in the formulas,, and, n is the parameter n in a composition formula A 1 p A 2 q...B 1 r B 2 s...X n, where p + q +... = r + s +... = n and each number represents an integer, and where ions A 1, A 2,..., and A u of composition ratio p: q:... are located at the A site, and ions B 1, B 2,..., and B v of composition ratio r: s:... are located at the B site in the ABX which is the general formula, and moreover, the d A-X and d Ai-X in the formula satisfy the following formula, and the d B -x and d Bi-X in the formula satisfy the following formula, d A − X = ∏ i = 1 n r A i + r X 1 n = ∏ i = 1 n d A i − X 1 n d B − X = ∏ i = 1 n r B i + r X 1 n = ∏ i = 1 n d B i − X 1 n wherein, in the formulas and, n is the same as n in the formulas to.