mhurhangee/ep-ind-claims huggingface dataset:
Home automation system comprising a central control unit for sending, to one or more devices (2a, 2b, 2c) to which it is connected, home automation instructions corresponding to actions to be executed, and a portable unit including means for establishing a communication link with the central control unit, characterised in that the portable unit includes a contactless communication module and in that the portable unit is configured, in a home automation phase of use, for reading, via the contactless communication module, a home automation instruction written in a radiolabel located in the vicinity of the portable unit, which corresponds to an action to be executed by a device, and for reporting to the central control unit, via the communication link with said central control unit, the instruction read on the radiolabel so that the action can be executed by the device after the sending of the instruction to the device from the central control unit.
A method for calibrating a first pressure sensor or force sensor which measures a first pressure of a liquid present inside a tube, being a dialyzer tube in an extracorporeal circuit, in the form of a force signal, wherein the first pressure or force sensor abuts directly on the tube and is integrated into or inserted into a first clamping device, characterized by the following steps: a) regression analysis and prediction of at least one tube-parameter-independent correction function for finding a correction signal for correcting the drift signal caused by clamping of the tube into the first clamping device using a corresponding force or pressure reference signal measured by a first force or pressure reference sensor (PHOP) at a constant internal tube pressure and a constant internal tube temperature; b) first calibrating of the pressure or force signal, measured by the first pressure or force sensor and corrected using the correction signal, with the force or pressure reference signal measured by the first force or pressure reference sensor (PHOP) before active use of the tube where the tube is connected to a patient; and c) second calibrating of the pressure or force signal, measured by the first pressure or force sensor and corrected using the correction function, with the force or pressure reference signal measured by a second force or pressure reference sensor during active use of the tube. a) regression analysis and prediction of at least one tube-parameter-independent correction function for finding a correction signal for correcting the drift signal caused by clamping of the tube into the first clamping device using a corresponding force or pressure reference signal measured by a first force or pressure reference sensor (PHOP) at a constant internal tube pressure and a constant internal tube temperature; b) first calibrating of the pressure or force signal, measured by the first pressure or force sensor and corrected using the correction signal, with the force or pressure reference signal measured by the first force or pressure reference sensor (PHOP) before active use of the tube where the tube is connected to a patient; and c) second calibrating of the pressure or force signal, measured by the first pressure or force sensor and corrected using the correction function, with the force or pressure reference signal measured by a second force or pressure reference sensor during active use of the tube.
A method of controlling the level of corrosivity of an aqueous solution recovered during a process for producing a blanket of mineral fibers, comprising in particular the fiberizing and the coating of said fibers with a binder comprising a polyacid typically of the acrylic type, said aqueous solution being at least partly recycled into a zone in which said binder is prepared and/or a scrubbing zone of the production plant, the method being characterized in that the pH of the solution in the recycling circuit is maintained between minimum and maximum values by injecting into said circuit an agent for modifying said pH, such as a base, the flow rate of the pH-modifying agent being adjusted directly according to the flow rate of acid binder injected during the fiberizing process, without the use of control devices that continuously control the probes measuring the pH or the level of corrosion of the pipes of the circuit.
A beverage can end suitable for carbonated beverages at pressures of greater than 60 psi (413.685 kPa), the end comprising a peripheral curl capable of forming a double seam with a beverage can flange; a wall extending inwardly from the curl; a circular center panel located radially inwardly from the wall; a rivet that is offset from a center of the center panel; a main centerline defined by a center of the rivet and a point P on the periphery of the center panel that is closest to a rivet center, and a normal centerline that lies on the rivet center and is perpendicular to the main center line; the main centerline and normal centerline defining first and second small sectors and first and second large sectors on the center panel such that the first small sector is adjacent to the first large sector; a stay-on tab coupled to the center panel by the rivet; a score formed in the center panel and having a first end and a second end, the first score end being located in either the second small sector or the second large sector, the second score end being located in either the second large sector or the first large sector, characterized by the score forming a tear panel being openable to form an opening of at least 0.35 square inches (225.806 mm 2) and no more than 50 percent of the center panel area; the score defining a first lobe having an end located in the first small sector and a second lobe having an end located in the second large sector; the score defining a first hinge (H1,H1') associated with opening of the first lobe upon a first actuation of the tab and a second hinge associated with opening of the second lobe upon a second actuation of the tab.
A method of determining a flight plan for an aircraft, the method comprising, in sequence: a) initializing a plurality of legs comprising the flight plan; b) initializing performance predictions for the aircraft flying the flight plan; c) initializing pseudo constraints to null values, wherein pseudo constraints comprise internally computed values for use in lateral and vertical trajectory construction associated with the plurality of legs; d) generating a flyable lateral path for the aircraft; e) generating a vertical path for the aircraft; f) determining lateral path excursions for each of the plurality of legs based on the flyable lateral path and the vertical path, wherein an excursion comprises a deviation from a published procedure; g) for each lateral path excursion, determining whether the lateral path excursion qualifies for a pseudo constraint and incrementing a count when the lateral path excursion qualifies for a pseudo-constraint; h) stopping if the count is not greater than zero, or determining a pseudo constraint for a respective lateral path excursion if the count is greater than zero; i) applying the pseudo constraint to an associated leg; j) returning to step c if there is a pseudo constraint restart event; k) returning to step b if aircraft performance prediction initialization data is changed; and l) returning to step a if the flight plan legs are changed, or returning to step d if the leg is not changed. a) initializing a plurality of legs comprising the flight plan; b) initializing performance predictions for the aircraft flying the flight plan; c) initializing pseudo constraints to null values, wherein pseudo constraints comprise internally computed values for use in lateral and vertical trajectory construction associated with the plurality of legs; d) generating a flyable lateral path for the aircraft; e) generating a vertical path for the aircraft; f) determining lateral path excursions for each of the plurality of legs based on the flyable lateral path and the vertical path, wherein an excursion comprises a deviation from a published procedure; g) for each lateral path excursion, determining whether the lateral path excursion qualifies for a pseudo constraint and incrementing a count when the lateral path excursion qualifies for a pseudo-constraint; h) stopping if the count is not greater than zero, or determining a pseudo constraint for a respective lateral path excursion if the count is greater than zero; i) applying the pseudo constraint to an associated leg; j) returning to step c if there is a pseudo constraint restart event; k) returning to step b if aircraft performance prediction initialization data is changed; and l) returning to step a if the flight plan legs are changed, or returning to step d if the leg is not changed.
A system for fusing composite structures, the system comprising: a composite part comprising - a substructure (68, 70, 70a) comprising a flange and a raised segment (77, 77a), the flange comprising a faying surface; a skin comprising a first side and a second side opposite the first side, the second side of the skin comprising: another faying surface contacting the faying surface of the flange, and an exposed portion not contacted by the substructure; an insulation layer (86, 86a) covering the flange opposite the faying surface of the flange and covering the exposed portion of the skin; a tool comprising - a shaping surface in a shape of an outer mold line and receiving the first side of the skin; a heating element supplying heat to the shaping surface; and a vacuum bag covering the composite part such that the composite part is at least partially enclosed by the combination of the vacuum bag and the shaping surface of the tool, the vacuum bag comprising - a first side adjacent the composite part and a second side opposite the first side; the system further comprising a coolant fluid in contact with the second side of the vacuum bag, the coolant fluid being at a lower temperature than the composite part. a composite part comprising - a substructure (68, 70, 70a) comprising a flange and a raised segment (77, 77a), the flange comprising a faying surface; a skin comprising a first side and a second side opposite the first side, the second side of the skin comprising: another faying surface contacting the faying surface of the flange, and an exposed portion not contacted by the substructure; a substructure (68, 70, 70a) comprising a flange and a raised segment (77, 77a), the flange comprising a faying surface; a skin comprising a first side and a second side opposite the first side, the second side of the skin comprising: another faying surface contacting the faying surface of the flange, and an exposed portion not contacted by the substructure; an insulation layer (86, 86a) covering the flange opposite the faying surface of the flange and covering the exposed portion of the skin; a tool comprising - a shaping surface in a shape of an outer mold line and receiving the first side of the skin; a heating element supplying heat to the shaping surface; and a shaping surface in a shape of an outer mold line and receiving the first side of the skin; a heating element supplying heat to the shaping surface; and a vacuum bag covering the composite part such that the composite part is at least partially enclosed by the combination of the vacuum bag and the shaping surface of the tool, the vacuum bag comprising - a first side adjacent the composite part and a second side opposite the first side; the system further comprising a coolant fluid in contact with the second side of the vacuum bag, the coolant fluid being at a lower temperature than the composite part.
A linear compressor comprising: a cylinder part including a cylinder bore, a piston (3, 4) disposed in said cylinder bore and slidable therein, a main spring connecting directly or indirectly said cylinder part to said piston (3,4), a connecting rod connecting between said main spring and said piston (3, 4), with a connection (35, 37) between the connecting rod and the piston (3, 4) and a connection between the connecting rod and the main spring, characterised in that the connection (35, 37) between said piston (3,4) and connecting rod is a compliant connection. a cylinder part including a cylinder bore, a piston (3, 4) disposed in said cylinder bore and slidable therein, a main spring connecting directly or indirectly said cylinder part to said piston (3,4), a connecting rod connecting between said main spring and said piston (3, 4), with a connection (35, 37) between the connecting rod and the piston (3, 4) and a connection between the connecting rod and the main spring, characterised in that the connection (35, 37) between said piston (3,4) and connecting rod is a compliant connection.
A method for designing an airfoil, the method comprising the steps of: considering a baseline airfoil (204, 300) having a first camber distribution and a first aerodynamic efficiency; reducing the first camber distribution to result in a reduced camber airfoil with a second camber distribution and a second aerodynamic efficiency, wherein the second aerodynamic efficiency is approximately equal to the first aerodynamic efficiency, such that a difference between the second aerodynamic efficiency and the first aerodynamic efficiency is less than 5%, or demonstrates a relative improvement; and producing the airfoil with the second camber distribution, wherein the reducing step includes reducing the first camber distribution in one or more areas within a first range between approximately 25% to approximately 75% along a radial height and within a second range between approximately 25% to approximately 75% along a chord length, wherein the reducing step further includes maintaining the first camber distribution outside of the first range and the second range. considering a baseline airfoil (204, 300) having a first camber distribution and a first aerodynamic efficiency; reducing the first camber distribution to result in a reduced camber airfoil with a second camber distribution and a second aerodynamic efficiency, wherein the second aerodynamic efficiency is approximately equal to the first aerodynamic efficiency, such that a difference between the second aerodynamic efficiency and the first aerodynamic efficiency is less than 5%, or demonstrates a relative improvement; and producing the airfoil with the second camber distribution, wherein the reducing step includes reducing the first camber distribution in one or more areas within a first range between approximately 25% to approximately 75% along a radial height and within a second range between approximately 25% to approximately 75% along a chord length, wherein the reducing step further includes maintaining the first camber distribution outside of the first range and the second range.
A rotor for an electric machine, wherein the rotor comprises a plurality of stack elements (100, 100', 100", 100"') and each of the stack elements comprises material of first magnetic conductance; each of the stack elements (100, 100', 100", 100"') comprises a plurality of sectorial sections (102, 102', 102", 102"') distributed round a rotational axis of the rotor; each of the sectorial sections (102, 102', 102", 102'") comprises one or more flux barriers (106, 108, 110, 112), characterized in that at least one of said one or more flux barriers (106, 108, 110, 112) is configured to have an electrically conductive material of a third magnetic conductance at least approximately in only one sectorial half (102A, 102B) and a difference associated with filling of the electrically conductive material in different sectorial halves (102A, 102B) of a common sectorial section (102, 102', 102", 102'"), a numeric value of the first magnetic conductance being larger than that of the third magnetic conductance.
Folding-table arrangement having a first folding-table leaf and a second folding-table leaf and having a crossmember for fastening the first folding-table leaf and the second folding-table leaf, which can be displaced between a swung-up position and a swung-down position by means of a folding-action mechanism, wherein, in the swung-up position, the first folding-table leaf and the second folding-table leaf can be arrested vertically, and wherein the first folding-table leaf and the second folding-table leaf each have a first end and a second end, and the folding-action mechanism is located at the second end, characterized in that at the first end, which is directed away from the crossmember, the first folding-table leaf and the second folding-table leaf have a person-supporting element, wherein the person-supporting element is formed in a semicircle around the first end of the first folding-table leaf and of the second folding-table leaf.
Pneumatic tyre with a decorative sidewall pattern comprising a multiplicity of ridges (5, 5', 5", 5"') running next to one another, which form a background pattern (6, 6', 6", 6"'), wherein portions (5a, 5'a, 5"a, 5"'a) of ridges (5, 5', 5", 5"') diverted at angles of equal magnitude out of the background pattern (6, 6', 6", 6"') form at least a locally delimited surface pattern (7a, 8a, 9a, 9c, 11a, 11b), wherein, as a result of further diversion, occurring at angles of equal magnitude, the diverted portions (5a, 5'a, 5''a, 5"'a) go over into at least one further surface pattern (7b, 7c, 8b, 8c, 9b, 9d, 11c, 11d), wherein the ridges in all of the surface patterns (7a, 7b, 7c, 8a, 8b, 8c, 9a, 9b, 9c, 9d, 11a, 11b, 11c, 11d) are portions (5a, 5b, 5c, 5'a, 5'b, 5'c, 5"a to 5"d, 5"'a to 5"'d) that are in the course of ridges (5, 5', 5", 5"') from the background pattern (6, 6', 6", 6"'), characterized in that the background pattern (6, 6', 6", 6"') is diverted from its basic alignment in such a way that the surface patterns (7a, 7b, 7c, 8a, 8b, 8c, 9a, 9b, 9c, 9d, 11a, 11b, 11c, 11d) formed simulate three-dimensional shapes or bodies that interrupt the background pattern (6, 6', 6", 6"').
Method for distinguishing between blinking events and instrument glances with the aid of an apparatus and using an extent to which the eye is open, wherein an instrument glance corresponds to a lowered gaze, wherein the extent to which the eye is open represents a currently detected distance between the eyelids of an eye, wherein the method includes the following steps: ascertaining a blinking event using at least one blinking limit value, wherein the blinking event is ascertained if a value for the extent of opening, mapping a value of the extent to which the eye is open, is less than the blinking limit value; and wherein in the ascertainment step a mid blinking event is ascertained if the value for the extent of opening is less than a mid blinking limit value and a low blinking event is ascertained if the value for the extent of opening is less than a low blinking limit value, wherein, further, a low blinking event is ascertained if a value for the extent of opening following the ascertainment of the mid blinking event is less than the low blinking limit value, and determining an instrument glance using a maximum blinking duration, wherein the instrument glance is determined in the determination step if the mid blinking event is ascertained for a period longer than the maximum blinking duration and wherein no instrument glance is determined if the low blinking event is ascertained for a period longer than the maximum blinking duration, more particularly wherein the steps (502, 504) of the method are carried out again if the value for the extent of opening is greater than an open limit value following the determination of the instrument glance. ascertaining a blinking event using at least one blinking limit value, wherein the blinking event is ascertained if a value for the extent of opening, mapping a value of the extent to which the eye is open, is less than the blinking limit value; and wherein in the ascertainment step a mid blinking event is ascertained if the value for the extent of opening is less than a mid blinking limit value and a low blinking event is ascertained if the value for the extent of opening is less than a low blinking limit value, wherein, further, a low blinking event is ascertained if a value for the extent of opening following the ascertainment of the mid blinking event is less than the low blinking limit value, and determining an instrument glance using a maximum blinking duration, wherein the instrument glance is determined in the determination step if the mid blinking event is ascertained for a period longer than the maximum blinking duration and wherein no instrument glance is determined if the low blinking event is ascertained for a period longer than the maximum blinking duration, more particularly wherein the steps (502, 504) of the method are carried out again if the value for the extent of opening is greater than an open limit value following the determination of the instrument glance.
Anti-friction bearing for rotatably mounting a journal, having - a sleeve, - rolling bodies which roll in the sleeve, - a sealing ring, and - a cup spring, on which the rolling bodies run axially and which is supported axially on the sealing ring, characterized in that the sealing ring has a seat face for a torque-proof arrangement of the sealing ring on the journal, and the axial spacing between the cup spring and the rolling bodies decreases radially to the outside at least in regions. - a sleeve, - rolling bodies which roll in the sleeve, - a sealing ring, and - a cup spring, on which the rolling bodies run axially and which is supported axially on the sealing ring,
A system comprising: a chair for supporting a patient; and a location pad, comprising: multiple field-generators, which are configured to generate respective magnetic fields in a region-of-interest of a patient body, for measuring a position of a medical instrument in the region-of-interest; a frame, which is configured to fix the multiple field-generators at respective positions surrounding the region-of-interest; a mounting fixture, wherein the mounting fixture is configured to mount to the chair and to position the frame above the chair such that, during a procedure, the region-of-interest is interposed between the location pad and the chair; and characterised by: one or more illumination elements, which are mounted in the frame and are configured to illuminate the patient body. a chair for supporting a patient; and a location pad, comprising: multiple field-generators, which are configured to generate respective magnetic fields in a region-of-interest of a patient body, for measuring a position of a medical instrument in the region-of-interest; a frame, which is configured to fix the multiple field-generators at respective positions surrounding the region-of-interest; a mounting fixture, wherein the mounting fixture is configured to mount to the chair and to position the frame above the chair such that, during a procedure, the region-of-interest is interposed between the location pad and the chair; and characterised by: multiple field-generators, which are configured to generate respective magnetic fields in a region-of-interest of a patient body, for measuring a position of a medical instrument in the region-of-interest; a frame, which is configured to fix the multiple field-generators at respective positions surrounding the region-of-interest; a mounting fixture, wherein the mounting fixture is configured to mount to the chair and to position the frame above the chair such that, during a procedure, the region-of-interest is interposed between the location pad and the chair; and characterised by: one or more illumination elements, which are mounted in the frame and are configured to illuminate the patient body.