mhurhangee/ep-ind-claims huggingface dataset:
A fluid bearing for a wind turbine comprising: a bearing housing, a plurality of bearing pads inside the bearing housing and circumferentially distributed around a longitudinal axis of the fluid bearing, a plurality of supporting structures, each supporting structure having at least a first interface detachably connected to a respective seat provided in the bearing housing and at least a second interface detachably connected to a respective bearing pad of the plurality of bearing pads, wherein the supporting structure allows tilting of the respective bearing pad with respect to the bearing housing and wherein at least an anti-fretting layer is interposed between the first interface and the respective seat. a bearing housing, a plurality of bearing pads inside the bearing housing and circumferentially distributed around a longitudinal axis of the fluid bearing, a plurality of supporting structures, each supporting structure having at least a first interface detachably connected to a respective seat provided in the bearing housing and at least a second interface detachably connected to a respective bearing pad of the plurality of bearing pads, wherein the supporting structure allows tilting of the respective bearing pad with respect to the bearing housing and wherein at least an anti-fretting layer is interposed between the first interface and the respective seat.
A method for adjusting a handling machine, including the following steps: a) moving the control member (2, 3) of an actuator (7, 9, 11, 13, 15) or a motor to adjust a maximum operating speed of said actuator or said motor (7, 9, 11, 13, 15); characterized in that the adjusting method further includes the following steps: b) storing a maximum speed adjustment performed in step a) in an appropriate memory; c) making the work of the handling machine subject to an appropriate control law while not exceeding the storage maximum operating speed(s). a) moving the control member (2, 3) of an actuator (7, 9, 11, 13, 15) or a motor to adjust a maximum operating speed of said actuator or said motor (7, 9, 11, 13, 15); b) storing a maximum speed adjustment performed in step a) in an appropriate memory; c) making the work of the handling machine subject to an appropriate control law while not exceeding the storage maximum operating speed(s).
A method for monitoring combustion of a natural gas burner at a combustion controller, the method comprising: acquiring a measurement result for natural gas in a gas supply line of the natural gas burner, wherein the measurement result comprises a gas component in the natural gas and a corresponding content; inputting the measurement result into a preset control model, to determine control information corresponding to the measurement result, wherein the control model is related to the gas component in the natural gas and the corresponding content; adjusting a flow rate of natural gas in the gas supply line of the natural gas burner according to the control information; and characterized in that the method further comprises: acquiring a dynamic signal of a dynamic sensor of the natural gas burner, an emission signal of an emission sensor and a temperature signal of a temperature sensor (701, 702), to serve as a feedback signal; and in that the step of determining control information comprises: inputting the measurement result and the feedback signal into the preset control model, to acquire control information corresponding to the measurement result and the feedback signal, wherein the control model is related to the gas component in the natural gas and the corresponding content, and the feedback signal. acquiring a measurement result for natural gas in a gas supply line of the natural gas burner, wherein the measurement result comprises a gas component in the natural gas and a corresponding content; inputting the measurement result into a preset control model, to determine control information corresponding to the measurement result, wherein the control model is related to the gas component in the natural gas and the corresponding content; adjusting a flow rate of natural gas in the gas supply line of the natural gas burner according to the control information; and acquiring a dynamic signal of a dynamic sensor of the natural gas burner, an emission signal of an emission sensor and a temperature signal of a temperature sensor (701, 702), to serve as a feedback signal; and in that the step of determining control information comprises: inputting the measurement result and the feedback signal into the preset control model, to acquire control information corresponding to the measurement result and the feedback signal, wherein the control model is related to the gas component in the natural gas and the corresponding content, and the feedback signal.
A computer-implemented method of providing user account data, executed at an external user account system; wherein the computer-implemented method comprising: by one or more hardware processors executing program instructions: receiving, from a first computing device, information associated with an authorization request, wherein the information includes at least: account credentials associated with one or more user accounts; generating at least: an electronic record of the information, and a token associated with the electronic record; providing the token to the first computing device; receiving, from a second computing device, at least: the token, and a request for user account data associated with at least one of the one or more user accounts; accessing the user account data associated with at least one of the one or more user accounts, using the account credentials in the electronic record associated with the token; and providing, to the second computing device, the accessed user account data associated with the at least one of the one or more user accounts. receiving, from a first computing device, information associated with an authorization request, wherein the information includes at least: account credentials associated with one or more user accounts; generating at least: an electronic record of the information, and a token associated with the electronic record; an electronic record of the information, and a token associated with the electronic record; providing the token to the first computing device; receiving, from a second computing device, at least: the token, and a request for user account data associated with at least one of the one or more user accounts; the token, and a request for user account data associated with at least one of the one or more user accounts; accessing the user account data associated with at least one of the one or more user accounts, using the account credentials in the electronic record associated with the token; and providing, to the second computing device, the accessed user account data associated with the at least one of the one or more user accounts.
Road finishing machine with a screed for producing a paving layer on a subsoil on which the road finishing machine is moving in the laying direction during a pavement drive, wherein the road finishing machine comprises a leveling system (10A, 10B) for the height adjustment of the screed for compensating irregularities in the subsoil, wherein the leveling system (10A, 10B) includes a cascade control (100A, 100B) comprising an outer control loop which includes a first control unit (C bo) which is embodied to determine, on the basis of a detected actual value of a screed height (z bo) of the screed relative to a predetermined reference, and on the basis of a desired value of the screed height (r bo) relative to the predetermined reference which can be held available for it, a desired value of a pulling point position (r zp) of a pulling point of the screed relative to the predetermined reference, and which comprises an inner control loop which includes a second control unit (C nz) which is embodied to determine, on the basis of a detected actual value of a leveling cylinder position (s nz) of an extendable piston of a leveling cylinder attached to the pulling point, and on the basis of a desired value of the leveling cylinder position (r nz) held available for the second control unit (C nz), a control signal (u nz) for the leveling cylinder by means of which the leveling cylinder can be controlled, characterized in that the cascade control either comprises a central control loop between the outer and the inner control loops (11, 13) that includes a third control unit (C zp) which is embodied to determine, on the basis of a detected actual value of the pulling point position (z zp) of the pulling point of the screed to the predetermined reference, and on the basis of the desired value of the pulling point position (r zp) determined by means of the first control unit (C bo), the desired value of the leveling cylinder position (r nz) for the second control unit (C zp), or that the cascade control includes a pulling point control (C' zp) between the outer and the inner control loops (11, 13) which is embodied to determine, on the basis of the desired value of the pulling point position (r zp) of the pulling point of the screed determined by means of the first control unit (C bo), and in particular on the basis of a digital terrain model of the subsoil on which the road finishing machine is moving for producing the paving layer, which model is held available for the pulling point control (C' zp), the desired value of the leveling cylinder position (r nz) for the second control unit (C nz).
An optical lens, comprising: a first lens component comprising a first lens barrel and at least one first lens sheet mounted in the first lens barrel; a second lens component comprising a second lens barrel and at least one second lens sheet mounted in the second lens barrel, the at least one second lens sheet and the at least one first lens sheet together constituting an imageable optical system; and an adhesive, bonding the first lens component and the second lens component together, at least a part of the adhesive being interposed between and directly bonding the second lens barrel and the first lens sheet, or between and directly bonding the first lens barrel and the second lens sheet; characterised in that there are a first gap and a second gap between the first lens component and the second lens component, and the first gap is closer to an outer side of the optical lens than the second gap; the adhesive includes a first adhesive located in the first gap and a second adhesive located in the second gap; and arrangement positions and materials of the first adhesive and the second adhesive are suitable for making the first adhesive and the second adhesive be cured successively at different times; wherein the first adhesive and the second adhesive are of different materials, and an adhesion force provided by the second adhesive after curing is greater than an adhesion force provided by the first adhesive after curing. a first lens component comprising a first lens barrel and at least one first lens sheet mounted in the first lens barrel; a second lens component comprising a second lens barrel and at least one second lens sheet mounted in the second lens barrel, the at least one second lens sheet and the at least one first lens sheet together constituting an imageable optical system; and an adhesive, bonding the first lens component and the second lens component together, at least a part of the adhesive being interposed between and directly bonding the second lens barrel and the first lens sheet, or between and directly bonding the first lens barrel and the second lens sheet; characterised in that there are a first gap and a second gap between the first lens component and the second lens component, and the first gap is closer to an outer side of the optical lens than the second gap; the adhesive includes a first adhesive located in the first gap and a second adhesive located in the second gap; and arrangement positions and materials of the first adhesive and the second adhesive are suitable for making the first adhesive and the second adhesive be cured successively at different times; wherein the first adhesive and the second adhesive are of different materials, and an adhesion force provided by the second adhesive after curing is greater than an adhesion force provided by the first adhesive after curing.
A process for the preparation of a dispersion of microcapsules, wherein the microcapsules have a volume average diameter d 50 of 15 to 90 μm and a percentage of the shell weight of 3 to 40%, with reference to the total weight of capsules, wherein the shell of the microcapsules comprises at least one polyurea and the core comprises at least one lipophilic component with the proviso that the core does not contain a fragrance, comprising the steps of: a) providing a premix comprising at least one protective colloid different from hydroxyalkylcellulose in an aqueous solution, b) providing a premix comprising at least one polyisocyanate and at least one lipophilic component, c) mixing premix and premix until an emulsion is formed, d) adding an aqueous solution containing at least one polyfunctional amine to the emulsion formed in step c), e) forming a dispersion of microcapsules by heating the mixture obtained in step d) to a temperature of at least 50°C until microcapsules are formed, and f) adding hydroxyalkylcellulose to the dispersion obtained in step e). a) providing a premix comprising at least one protective colloid different from hydroxyalkylcellulose in an aqueous solution, b) providing a premix comprising at least one polyisocyanate and at least one lipophilic component, c) mixing premix and premix until an emulsion is formed, d) adding an aqueous solution containing at least one polyfunctional amine to the emulsion formed in step c), e) forming a dispersion of microcapsules by heating the mixture obtained in step d) to a temperature of at least 50°C until microcapsules are formed, and f) adding hydroxyalkylcellulose to the dispersion obtained in step e).
A method of sealing a plurality of geomembrane panels (16,18) together along adjacent edges, at least a first one of said panels having an electrically conductive lower surface for testing said sealed panels for leaks, comprising the step of: laying a second one of said panels on a surface; breaking the conductivity of the first panel bottom surface across a line adjacent the side of the second panel; heating the bottom surface of the first panel along the line by sliding the bottom of said first panel against a heated element along said line, and said heated element includes a raised projection which interrupts the conductive lower surface of said first panel; and pressing said first and second panels together along said line to heat seal the bottom of the first panel on top of the second panel. laying a second one of said panels on a surface; breaking the conductivity of the first panel bottom surface across a line adjacent the side of the second panel; heating the bottom surface of the first panel along the line by sliding the bottom of said first panel against a heated element along said line, and said heated element includes a raised projection which interrupts the conductive lower surface of said first panel; and pressing said first and second panels together along said line to heat seal the bottom of the first panel on top of the second panel.
A blade outer air seal assembly for a gas turbine engine, comprising: a main body portion extending axially along an axis, the main body portion having a radially inward facing surface and at least one radially outward facing surface; a passage provided in the main body portion between the at least one radially inward facing surface and the at least one radially outward facing surface, the passage having a first portion extending generally circumferentially, wherein the first portion has a floor, wherein at least one airflow inlet is provided by the at least one radially outward facing surface, and at least one fluid outlet is disposed at a circumferential end of the main body portion radially outward of the radially inward facing surface; and at least one rib disposed along the axis radially outward of the first portion, the passage has a second portion extending generally radially transverse to the first portion to provide fluid communication between the airflow inlet and the first portion; characterised in that the blade outer air seal further comprising a thermal barrier coating disposed adjacent the radially inward facing surface, wherein a thickness of the thermal barrier coating is substantially equal to a thickness of an inner wall of the main body portion defined between the floor of the first portion and the radially inward facing surface. a main body portion extending axially along an axis, the main body portion having a radially inward facing surface and at least one radially outward facing surface; a passage provided in the main body portion between the at least one radially inward facing surface and the at least one radially outward facing surface, the passage having a first portion extending generally circumferentially, wherein the first portion has a floor, wherein at least one airflow inlet is provided by the at least one radially outward facing surface, and at least one fluid outlet is disposed at a circumferential end of the main body portion radially outward of the radially inward facing surface; and at least one rib disposed along the axis radially outward of the first portion, the passage has a second portion extending generally radially transverse to the first portion to provide fluid communication between the airflow inlet and the first portion; characterised in that the blade outer air seal further comprising a thermal barrier coating disposed adjacent the radially inward facing surface, wherein a thickness of the thermal barrier coating is substantially equal to a thickness of an inner wall of the main body portion defined between the floor of the first portion and the radially inward facing surface.
Sensor unit for the measurement of a current in a conductor comprising at least one magnetoresistive sensor (5, 6) located at a radial distance from the outer surface of the conductor, wherein the conductor has a circular cross-section, wherein the sensor unit comprises at least one auxiliary coil for the generation of a bias magnetic field (H bias) to the at least one magnetoresistive sensor (5, 6) strong enough for inducing magnetic saturation in the at least one magnetoresistive sensor (5, 6) continuously during the whole current measurement process, wherein the direction of the bias magnetic field (H bias) provided by the auxiliary coil is oriented at an angle of 88-92° with respect to the direction of the magnetic field (H curr) produced by the current in the conductor, wherein the auxiliary coil is provided as one multiturn winding around and coaxial with the conductor, and wherein the at least one magnetoresistive sensor (5, 6) is sandwiched between the conductor and the windings of the auxiliary coil, characterized in that the magnetic field produced by the current in the conductor is directly measured by the at least one magnetoresistive sensor (5, 6) using a resulting magnetic field (H resul) which acts on said at least one magnetoresistive sensor (5, 6) and which is given by the vector sum of the magnetic field (H curr) produced by the current in the conductor and the bias magnetic field (H bias).
An implantable prosthesis comprising: a strut having a lumen and metal layer surrounding the lumen; a passivating coating within the lumen and on an interior surface of the metal layer; and a therapeutic agent in the lumen; wherein the passivating coating absorbs less than 5% moisture by weight, comprises glass or a fluoropolymer, and is disposed between the interior surface and the therapeutic agent. a strut having a lumen and metal layer surrounding the lumen; a passivating coating within the lumen and on an interior surface of the metal layer; and a therapeutic agent in the lumen;
A well tool system, comprising: multiple explosive assemblies, each explosive assembly comprising: (a) an outer housing; (b) first and second explosive components (22,24) that are rotatable relative to, and within, the outer housing, when the explosive assembly is installed in a well; (c) a connector (30,30a,30b) coupled to the outer housing (d) a third explosive component positioned in the connector (30,30a,30b), the third explosive component being non-rotatable relative to the outer housing and being explosively coupled to the second explosive component by a rotary detonation coupling; (e) a selective firing module which causes detonation of the explosive components (22,24,40) in response to a predetermined signal associated with the selective firing module; and characterized in that (f) the selective firing module is arranged in the connector (30,30a,30b) and there is a rotary detonation coupling between the selective firing module and the first and second explosive components to allow said first and second explosive components to rotate relative to the outer housing while the selective firing module does not rotate relative to the outer housing; (g) a rotary electrical connection coupled to the selective firing module, the rotary electrical connection comprising an electrical contact wherein the electrical contact is rotatable with the second explosive component when the second explosive component rotates relative to the outer housing. (a) an outer housing; (b) first and second explosive components (22,24) that are rotatable relative to, and within, the outer housing, when the explosive assembly is installed in a well; (c) a connector (30,30a,30b) coupled to the outer housing (d) a third explosive component positioned in the connector (30,30a,30b), the third explosive component being non-rotatable relative to the outer housing and being explosively coupled to the second explosive component by a rotary detonation coupling; (e) a selective firing module which causes detonation of the explosive components (22,24,40) in response to a predetermined signal associated with the selective firing module; and characterized in that (f) the selective firing module is arranged in the connector (30,30a,30b) and there is a rotary detonation coupling between the selective firing module and the first and second explosive components to allow said first and second explosive components to rotate relative to the outer housing while the selective firing module does not rotate relative to the outer housing; (g) a rotary electrical connection coupled to the selective firing module, the rotary electrical connection comprising an electrical contact wherein the electrical contact is rotatable with the second explosive component when the second explosive component rotates relative to the outer housing.
Method for making an electroluminescent marking on an exterior wall of an aircraft, said exterior wall comprising a panel with an exterior face and an interior face and being bounded by an edge, characterized in that it involves a step of superpositioning of layers (56, 58, 36, 62 and 64) designed to produce the electroluminescent marking on a first face of a flexible backing distinct from the aircraft to obtain a marking tape, and a step of affixing the marking tape to the exterior wall of the aircraft and a step of affixing at least one connection tape to the exterior face of the panel as far as the edge of the panel to connect the electroluminescent marking to an electrical control and power supply system positioned inside the aircraft, the edge of the panel being disposed downstream from the electroluminescent marking in the direction of movement of an air flow which moves on the outside of the aircraft when the aircraft is in flight.