mhurhangee/ep-ind-claims huggingface dataset:
"SYSTEM FOR ACQUISITION OF DATA AND MULTIPLICATION OF SIGNALLING AND PROTECTION CONTACTS IN EQUIPMENTS OF SUBSTATIONS AND ELECTRIC POWER PLANTS AND SIMILAR", comprising: - auxiliary relays for the multiplication of contacts, wherein each auxiliary relay has a spool connected to a respective equipment contact and several outlet contacts, where said spool activates said several outlet contacts based on the status of the equipment contact, thus the information on the contact statuses is already available in the auxiliary relays; and - an acquisition system of contact status data, wherein the system is characterised in that said acquisition system of contact status data is a data acquisition equipment integrating the auxiliary relays by means of a respective two wire outlet specifically implemented for that function in the auxiliary relays, wherein the two terminals of each of said two wires outlets are respectively connected in parallel in all auxiliary relays and connected to two respective inlets of the data acquisition equipment, making up a data acquisition network that uses only two wires. - auxiliary relays for the multiplication of contacts, wherein each auxiliary relay has a spool connected to a respective equipment contact and several outlet contacts, where said spool activates said several outlet contacts based on the status of the equipment contact, thus the information on the contact statuses is already available in the auxiliary relays; and - an acquisition system of contact status data, wherein the system is characterised in that said acquisition system of contact status data is a data acquisition equipment integrating the auxiliary relays by means of a respective two wire outlet specifically implemented for that function in the auxiliary relays, wherein the two terminals of each of said two wires outlets are respectively connected in parallel in all auxiliary relays and connected to two respective inlets of the data acquisition equipment, making up a data acquisition network that uses only two wires.
An output circuit for an output module used in an industrial controller, wherein the output module includes a plurality of output terminals, the output circuit comprising: for each of the plurality of output terminals: an isolation circuit having: an input configured to receive power from a power source, and an output configured to provide power electrically isolated from the power source to the corresponding output terminal; a terminal control circuit operative to: receive power from the output of the isolation circuit, and selectively connect the output of the isolation circuit to the corresponding output terminal, a switching circuit comprising a field-effect transistor operatively connected between the output of the corresponding isolation circuit and corresponding output terminal to selectively connect the output of the corresponding isolation circuit to the corresponding output terminal; and a current limit circuit (40; 46) connected to the gate of the field-effect transistor and operative to limit a current conducted between the output of the isolation circuit and the corresponding output terminal to a predefined threshold. an isolation circuit having: an input configured to receive power from a power source, and an output configured to provide power electrically isolated from the power source to the corresponding output terminal; an input configured to receive power from a power source, and an output configured to provide power electrically isolated from the power source to the corresponding output terminal; a terminal control circuit operative to: receive power from the output of the isolation circuit, and selectively connect the output of the isolation circuit to the corresponding output terminal, receive power from the output of the isolation circuit, and selectively connect the output of the isolation circuit to the corresponding output terminal, a switching circuit comprising a field-effect transistor operatively connected between the output of the corresponding isolation circuit and corresponding output terminal to selectively connect the output of the corresponding isolation circuit to the corresponding output terminal; and a current limit circuit (40; 46) connected to the gate of the field-effect transistor and operative to limit a current conducted between the output of the isolation circuit and the corresponding output terminal to a predefined threshold.
A compression ratio control device (180, 180a), comprising: a detector (184, 186, 188, 190, 192) configured to detect a signal correlating with the maximum combustion pressure (Pmax) in a combustion chamber in a cylinder; and a controller configured to control a compression ratio of the combustion chamber, wherein the controller controls the compression ratio to be closer to a lowest compression ratio (ε0) at an engine full load, characterized in that the controller changes the compression ratio, in a first engine load region including the engine full load, in a range between the lowest compression ratio (ε0) and a highest compression ratio (εn) so that the maximum combustion pressure (Pmax) is maintained to a cylinder internal-pressure upper limit value (Pmax Limit) defined from the view point of durability of the cylinder, and the controller maintains the compression ratio to be closer to the highest compression ratio (εn), in a second engine load region in which the engine load is smaller than that in the first engine load region and the maximum combustion pressure (Pmax) is less than the cylinder-internal-pressure upper limit value (Pmax Limit). a detector (184, 186, 188, 190, 192) configured to detect a signal correlating with the maximum combustion pressure (Pmax) in a combustion chamber in a cylinder; and a controller configured to control a compression ratio of the combustion chamber, wherein the controller controls the compression ratio to be closer to a lowest compression ratio (ε0) at an engine full load, characterized in that the controller changes the compression ratio, in a first engine load region including the engine full load, in a range between the lowest compression ratio (ε0) and a highest compression ratio (εn) so that the maximum combustion pressure (Pmax) is maintained to a cylinder internal-pressure upper limit value (Pmax Limit) defined from the view point of durability of the cylinder, and the controller maintains the compression ratio to be closer to the highest compression ratio (εn), in a second engine load region in which the engine load is smaller than that in the first engine load region and the maximum combustion pressure (Pmax) is less than the cylinder-internal-pressure upper limit value (Pmax Limit).
An adhesion layer composition for forming an adhesion layer between a substrate and a photocurable composition, the adhesion layer composition comprising: a compound containing at least two binding functional groups including at least one functional group directly bound to a hydrocarbon or an aromatic hydrocarbon and capable of being bound to the substrate, and at least one functional group directly bound to a hydrocarbon or an aromatic hydrocarbon and capable of being bound to the photocurable composition; and a solvent, wherein the functional group capable of being bound to the substrate is at least one selected from the group consisting of hydroxy, carboxy, thiol, amino, epoxy, and (blocked) isocyanate, and the functional group capable of being bound to the photocurable composition is a hydrogen donating functional group, characterized in that the compound is at least one selected from the group consisting of 1,3,5-tris(3-mercaptobutyryloxyethyl)-1,3,5-triazine-2,4,6(1H,3H,5H)-trione, pentaerythritol tetrakis(3-mercaptobutylate), pentaerythritol tris(3-mercaptobutylate), N-phenylglycine, and N,N,N',N",N"-pentakis(2-hydroxypropyl)diethylenetriamine. a compound containing at least two binding functional groups including at least one functional group directly bound to a hydrocarbon or an aromatic hydrocarbon and capable of being bound to the substrate, and at least one functional group directly bound to a hydrocarbon or an aromatic hydrocarbon and capable of being bound to the photocurable composition; and a solvent, wherein the functional group capable of being bound to the substrate is at least one selected from the group consisting of hydroxy, carboxy, thiol, amino, epoxy, and (blocked) isocyanate, and the functional group capable of being bound to the photocurable composition is a hydrogen donating functional group, characterized in that the compound is at least one selected from the group consisting of 1,3,5-tris(3-mercaptobutyryloxyethyl)-1,3,5-triazine-2,4,6(1H,3H,5H)-trione, pentaerythritol tetrakis(3-mercaptobutylate), pentaerythritol tris(3-mercaptobutylate), N-phenylglycine, and N,N,N',N",N"-pentakis(2-hydroxypropyl)diethylenetriamine.
An ink-jet ink composition, comprising: (a) from 3% by mass to 10% by mass of polymer compound particles that include a first copolymer including at least one repeating unit derived from a hydrophilic monomer in an amount of from 1% by mass to 15% by mass relative to the first copolymer, that have a volume average diameter of from 100 nm to 300 nm, and that have no cross-linked structure; (b) from 5% by mass to 20% by mass of at least one water soluble polymer that comprises a second copolymer including at least one repeating unit derived from a hydrophilic monomer in an amount of from 8% by mass to 50% by mass relative to the second copolymer; (c) from 0.1% by mass to 10% by mass of at least one colorant; (d) from 5% by mass to 40% by mass of at least one water soluble organic solvent; and (e) water. (a) from 3% by mass to 10% by mass of polymer compound particles that include a first copolymer including at least one repeating unit derived from a hydrophilic monomer in an amount of from 1% by mass to 15% by mass relative to the first copolymer, that have a volume average diameter of from 100 nm to 300 nm, and that have no cross-linked structure; (b) from 5% by mass to 20% by mass of at least one water soluble polymer that comprises a second copolymer including at least one repeating unit derived from a hydrophilic monomer in an amount of from 8% by mass to 50% by mass relative to the second copolymer; (c) from 0.1% by mass to 10% by mass of at least one colorant; (d) from 5% by mass to 40% by mass of at least one water soluble organic solvent; and (e) water.
Composite of a roller shutter box (1, 2), a frame, such as a window frame or door frame, and a fitting strip, the roller shutter box (1, 2) having a width and a length and having a head piece extending in a width direction (r), the roller shutter box (1, 2) also being attached to the frame (3, 4), a receiving formation being formed on the head piece for fixing the roller shutter box (1, 2) relative to the frame (3, 4) in a variable manner in the width direction (r), in which receiving formation a part of the fitting strip extending from the frame (3, 4) is received, the receiving formation allowing, in the width direction (r), a different arrangement of the part and, by adaptation to the part of the fitting strip to be received, a stepless transfer of the roller shutter box (1, 2) in the width direction (r) by a corresponding transfer of the part of the fitting strip in the receiving formation, the fixing being achieved by a material displacement on the head piece taking place in the course of the insertion of the part of the fitting strip into the receiving recess, characterised in that the material displacement is achieved by a cutting edge, a tip or a hooking formation (18, 19) formed on the part of the fitting strip.
A strain gauge (1, 1A) comprising: a substrate formed of resin and having flexibility; and a resistor, characterized by further comprising a functional layer formed from a metal, an alloy, or a metal compound, directly on one surface of the substrate, wherein the resistor is formed as a film containing Cr, CrN, and Cr 2 N into which an element contained in the functional layer is diffused, on one surface of the functional layer, wherein a first substance having a function of controlling growth of crystal grains as a main component of the resistor, is added to the resistor, and wherein the functional layer includes a material that promotes crystal growth of the resistor, the crystal growth causing the film formed with the main component of the resistor to be deposited. a substrate formed of resin and having flexibility; and a resistor, characterized by further comprising a functional layer formed from a metal, an alloy, or a metal compound, directly on one surface of the substrate, wherein the resistor is formed as a film containing Cr, CrN, and Cr 2 N into which an element contained in the functional layer is diffused, on one surface of the functional layer, wherein a first substance having a function of controlling growth of crystal grains as a main component of the resistor, is added to the resistor, and wherein the functional layer includes a material that promotes crystal growth of the resistor, the crystal growth causing the film formed with the main component of the resistor to be deposited.
Self-sealing pneumatic vehicle tyre comprising a breaker belt assembly, a tread arranged radially above the breaker belt assembly, and an air-tight inner layer arranged radially inside, wherein the self-sealing of the pneumatic vehicle tyre is obtained by a sealant layer subsequently applied radially inside after the vulcanization of the pneumatic vehicle tyre, wherein the sealant layer has substantially the width of the breaker belt assembly and is arranged substantially in the projection thereof and has a cross section, formed in the cross-sectional plane containing the tyre axis, with a surface running substantially parallel to the breaker belt assembly in the axial direction and a surface running substantially in the radial direction, characterized in that at least the surface of the sealant layer running substantially parallel to the breaker belt assembly in the axial direction comprises around it a coating which contains at least sand.
A testing device for determining the particulate load of hydrogen (H 2) subject to high pressure, comprising a housing that contains a sample chamber in which a filter holder for a testing filter is provided through which hydrogen can flow prior to a sample quantity during a testing operation, and after the end of the testing operation can be removed from the sample chamber in order to evaluate particulate accumulation, characterised in that an adjustable throttle element is present which enables the flow entering the sample chamber to be throttled to different degrees.
A method for the operating assistance of a nuclear reactor including the steps of: - setting a request for the operating assistance of said reactor by means of a man/machine interface interacting with an operating assistance calculator dedicated to said operating assistance and using a three-dimensional neutron calculator code solving the diffusion equation, referred to as an operating assistance code, - transmitting from a system for monitoring the operation of the reactor core to said operating assistance calculator and in a unidirectional way, a set of data representative of the material, geometric and neutron characteristics of the core, as well as the operation conditions of the core, said data being determined by a three-dimensional neutron code updating the isotope balance of the core during the fuel burnup and periodically solving on line the diffusion equation, referred to as a the monitoring code, said monitoring code being integrated in a second distinct calculator, referred to as a monitoring calculator, dedicated to said monitoring system; - determining a change over time of the behaviour of the reactor core by using said operating assistance code, said data representative of the material, geometric and neutron characteristics of the core, as well as the operation conditions of the core, and said request for the operating assistance being used as input data of said operating assistance code. - setting a request for the operating assistance of said reactor by means of a man/machine interface interacting with an operating assistance calculator dedicated to said operating assistance and using a three-dimensional neutron calculator code solving the diffusion equation, referred to as an operating assistance code, - transmitting from a system for monitoring the operation of the reactor core to said operating assistance calculator and in a unidirectional way, a set of data representative of the material, geometric and neutron characteristics of the core, as well as the operation conditions of the core, said data being determined by a three-dimensional neutron code updating the isotope balance of the core during the fuel burnup and periodically solving on line the diffusion equation, referred to as a the monitoring code, said monitoring code being integrated in a second distinct calculator, referred to as a monitoring calculator, dedicated to said monitoring system; - determining a change over time of the behaviour of the reactor core by using said operating assistance code, said data representative of the material, geometric and neutron characteristics of the core, as well as the operation conditions of the core, and said request for the operating assistance being used as input data of said operating assistance code.
Gearbox with a gearbox housing and at least one gearbox element rotating in the gearbox housing and, in doing so, immersing in a lubricant, wherein, below a lubricant level, a first and a second lubricant line connector (20, 22) are coupled to the gearbox housing, wherein the first and the second lubricant line connector (20, 22) are interconnected outside the gearbox housing by means of a lubricant line and the lubricant line is provided with at least one surface-enlarging device (26, 28) and the first lubricant line connector is coupled to the gearbox housing in a region in which, during operation of the gearbox, and as a result of a direction of rotation of the at least one gearbox element immersing in the lubricant, an overpressure arises locally in the lubricant, characterised in that the second lubricant line connector is coupled to the gearbox housing in a region between the at least one gearbox element immersing in the lubricant and a retaining edge in the interior of the gearbox housing.
A Method for quantifying the elasticity of biologic tissues by ultrasound, comprising the following: a) acquiring an ultrasound image; b) defining a region of interest in the image, the region of interest including image pixels; c) generating a first acoustic disturbance ultrasound beam directed at a first excitation point, the first acoustic disturbance ultrasound beam configured to produce a first shear wave that has a direction of propagation extending laterally from a direction of propagation of the first acoustic disturbance ultrasound beam; d) measuring a first displacement of the image pixels induced by the first shear wave; wherein the method further comprises: e) generating a second acoustic disturbance ultrasound beam directed at a second excitation point, the second acoustic disturbance ultrasound beam configured to produce a second shear wave that has a direction of propagation extending laterally from a direction of propagation of the second acoustic disturbance ultrasound beam; f) defining the first and second excitation points and to be positioned such that the region of interest is interposed between the first excitation point and the second excitation point and that the first and second shear waves pass through the region of interest; g) measuring a second displacement of the image pixels induced by the second shear wave; and h) assessing a stiffness value of tissue in the region of interest based on the first and second displacements measured at d) and g). a) acquiring an ultrasound image; b) defining a region of interest in the image, the region of interest including image pixels; c) generating a first acoustic disturbance ultrasound beam directed at a first excitation point, the first acoustic disturbance ultrasound beam configured to produce a first shear wave that has a direction of propagation extending laterally from a direction of propagation of the first acoustic disturbance ultrasound beam; d) measuring a first displacement of the image pixels induced by the first shear wave; e) generating a second acoustic disturbance ultrasound beam directed at a second excitation point, the second acoustic disturbance ultrasound beam configured to produce a second shear wave that has a direction of propagation extending laterally from a direction of propagation of the second acoustic disturbance ultrasound beam; f) defining the first and second excitation points and to be positioned such that the region of interest is interposed between the first excitation point and the second excitation point and that the first and second shear waves pass through the region of interest; g) measuring a second displacement of the image pixels induced by the second shear wave; and h) assessing a stiffness value of tissue in the region of interest based on the first and second displacements measured at d) and g).
A method of folding a wing (102, 104) of an aircraft, the method comprising: moving, via a fold actuator, an unfixed portion (120, 122) of the wing (102, 104) with respect to a fixed portion (124, 126) of the wing (102, 104) between a flight position and a folded position; preventing, via a latch, movement of the unfixed portion (120, 122) of the wing (102, 104) with respect to the fixed portion (124, 126) of the wing (102, 104), the latch comprising: a first lock configured to prevent movement of a latch pin of the latch, and a first cam configured to, via contact with a second cam comprising a second lock, prevent the second lock from transitioning to a second engaged position until the first lock is in a first engaged position; and preventing, via the second cam, the first lock from transitioning away from the first engaged position until the second lock transitions away from the second engaged position; wherein each latch pin is oriented in a generally horizontal alignment and wherein a central axis of each latch pin is parallel to an axis of rotation of the unfixed portion (120, 122) of the wing (102, 104) with respect to the fixed portion (124, 126) of the wing (102, 104). moving, via a fold actuator, an unfixed portion (120, 122) of the wing (102, 104) with respect to a fixed portion (124, 126) of the wing (102, 104) between a flight position and a folded position; preventing, via a latch, movement of the unfixed portion (120, 122) of the wing (102, 104) with respect to the fixed portion (124, 126) of the wing (102, 104), the latch comprising: a first lock configured to prevent movement of a latch pin of the latch, and a first cam configured to, via contact with a second cam comprising a second lock, prevent the second lock from transitioning to a second engaged position until the first lock is in a first engaged position; and preventing, via the second cam, the first lock from transitioning away from the first engaged position until the second lock transitions away from the second engaged position; wherein each latch pin is oriented in a generally horizontal alignment and wherein a central axis of each latch pin is parallel to an axis of rotation of the unfixed portion (120, 122) of the wing (102, 104) with respect to the fixed portion (124, 126) of the wing (102, 104).