mhurhangee/patent-ind-claim-en huggingface dataset:
A device for tricuspid regurgitation surgery by a cerclage suture, the device comprising: a hollow coronary sinus tube formed to be inserted into coronary sinus for protecting coronary sinus tissue from the cerclage suture inserted therein; and a hollow tricuspid valve tube formed to be inserted into tricuspid valve for protecting tricuspid valve tissue and interventricular septum tissue from the cerclage suture inserted therein, wherein the coronary sinus tube and the tricuspid valve tube are laterally coupled with each other from upper portions thereof by a predetermined length, and lower portions thereof are separated from each other, and a blocking part is provided on a side of the tricuspid valve tube and is formed and arranged for blocking a space resulting from incomplete closure of the tricuspid valve of a heart, characterized in that the blocking part is in a form of a blocking membrane, wherein the blocking membrane includes: an annular support being connected to the tricuspid valve tube; and a body for blocking a blood flow caused by incomplete closure of the tricuspid valve, by being connected to a lower portion of the support, wherein the support has a stronger structure than the body such that a shape of the blocking membrane is maintained. a hollow coronary sinus tube formed to be inserted into coronary sinus for protecting coronary sinus tissue from the cerclage suture inserted therein; and a hollow tricuspid valve tube formed to be inserted into tricuspid valve for protecting tricuspid valve tissue and interventricular septum tissue from the cerclage suture inserted therein, wherein the coronary sinus tube and the tricuspid valve tube are laterally coupled with each other from upper portions thereof by a predetermined length, and lower portions thereof are separated from each other, and a blocking part is provided on a side of the tricuspid valve tube and is formed and arranged for blocking a space resulting from incomplete closure of the tricuspid valve of a heart, characterized in that the blocking part is in a form of a blocking membrane, wherein the blocking membrane includes: an annular support being connected to the tricuspid valve tube; and a body for blocking a blood flow caused by incomplete closure of the tricuspid valve, by being connected to a lower portion of the support, wherein the support has a stronger structure than the body such that a shape of the blocking membrane is maintained. an annular support being connected to the tricuspid valve tube; and a body for blocking a blood flow caused by incomplete closure of the tricuspid valve, by being connected to a lower portion of the support, wherein the support has a stronger structure than the body such that a shape of the blocking membrane is maintained.
Cable gland with at least one contact element for contacting at least one long moulded part , the contact element comprising at least a plurality of first windings and a plurality of second windings , which are geometrically different from the first windings , and a through-opening for a passage of a long moulded part , wherein a first diameter d1 of the through opening is defined by the first windings and a second diameter d2 of the through-opening is defined by the second windings and wherein the first diameter d1 and the second diameter d2 are different.
A stainless steel powder comprising in weight %: up to 0.1% of C, 0.5-3% of Si, up to 0.5% of Mn, 20-27% of Cr, 3-8% of Ni, 1-6% of Mo, up to 3% of W, up to 0.1% N, up to 4% of Cu, up to 0.04% of P, up to 0.04% of S, unavoidable impurities up to 0.8% whereof Sn may be present up to 0.2%, optionally one or more of up to 0.004% B, up to 1% Nb, up to 0.5% Hf, up to 1% Ti, up to 1% Co, rest Fe. up to 0.1% of C, 0.5-3% of Si, up to 0.5% of Mn, 20-27% of Cr, 3-8% of Ni, 1-6% of Mo, up to 3% of W, up to 0.1% N, up to 4% of Cu, up to 0.04% of P, up to 0.04% of S, unavoidable impurities up to 0.8% whereof Sn may be present up to 0.2%, optionally one or more of up to 0.004% B, up to 1% Nb, up to 0.5% Hf, up to 1% Ti, up to 1% Co, rest Fe.
Use of a coating composition comprising: a) a base composition comprising a polyetheraspartic ester having the formula (I) below wherein each R represents a linear or branched C 1 -C 10 alkyl residue, such as a linear or branched C 1 -C 6 alkyl residue, preferably a methyl, ethyl, propyl or butyl residue; and wherein X is a polyether; and b) a curing agent; and c) one or more further components selected from fillers and pigments; for coating of a wind turbine blade. a) a base composition comprising a polyetheraspartic ester having the formula (I) below wherein each R represents a linear or branched C 1 -C 10 alkyl residue, such as a linear or branched C 1 -C 6 alkyl residue, preferably a methyl, ethyl, propyl or butyl residue; and wherein X is a polyether; and wherein each R represents a linear or branched C 1 -C 10 alkyl residue, such as a linear or branched C 1 -C 6 alkyl residue, preferably a methyl, ethyl, propyl or butyl residue; and wherein X is a polyether; and b) a curing agent; and c) one or more further components selected from fillers and pigments;
Aptamer for use in therapy of a subject by treating, curing or preventing disease symptoms associated with long COVID in a patient having overcome an infection with a virus from the Coronaviridae family, wherein the aptamer comprises a nucleic acid sequence of SEQ ID No. 1 (GGT TGG TGT GGT TGG) and/or a nucleic acid sequence being at least 80% identical to SEQ ID No. 1.
A lithium ion secondary battery comprising a positive electrode having a positive electrode active material layer on a current collector, a negative electrode having a negative electrode active material layer on a current collector, and a separator disposed between the positive electrode and the negative electrode and impregnated with a non-aqueous electrolyte solution, the positive electrode active material layer comprising a positive electrode active material and a binder, the negative electrode active material layer comprising a negative electrode active material and a binder, the binder of the negative electrode active material layer comprising a copolymer of vinyl alcohol and an alkali metal neutralized product of ethylenically unsaturated carboxylic acid, and the separator comprising a polymeric base material containing an inorganic compound or comprising a polymer having a melting point or glass transition temperature of 140°C or higher. a positive electrode having a positive electrode active material layer on a current collector, a negative electrode having a negative electrode active material layer on a current collector, and a separator disposed between the positive electrode and the negative electrode and impregnated with a non-aqueous electrolyte solution, the positive electrode active material layer comprising a positive electrode active material and a binder, the negative electrode active material layer comprising a negative electrode active material and a binder, the binder of the negative electrode active material layer comprising a copolymer of vinyl alcohol and an alkali metal neutralized product of ethylenically unsaturated carboxylic acid, and the separator comprising a polymeric base material containing an inorganic compound or comprising a polymer having a melting point or glass transition temperature of 140°C or higher.
Spool for winding up a fibrous web , comprising a spool core with a coating that forms the lateral surface of the spool , wherein the outer lateral surface is formed by a plurality of separate coatings arranged axially next to one another, at least two adjacent coatings of which consist of different material, characterized in that at least one coating consists at least partially of Teflon and/or an axially central coating has a larger outer diameter than the outer coatings .
A photovoltaic power generation system comprising a first and a second inverter connected in series on the input side, wherein a center point of the series connection of the inverters is connected to an insulation monitoring device , and at least one photovoltaic string connected to the series connection of the inverters with a device for electrically separating a first part and a second part of the photovoltaic string , which are connected to a first terminal and a second terminal of the device , characterised in that the device is located between the two parts of the string, and in that the device comprises a switch and a control device adapted to open the switch when a voltage applied to at least one of the terminals is outside a predetermined value range relative to a potential applied to a reference terminal .
A separator for separating a first phase from a second phase of a fluid, more particularly serum (S) from blood clots (K) in the case of blood as the fluid, under centrifugal force in a tube-shaped container , comprising: a floating element made of an elastic material with, when viewed from above, a circumferential sealing edge for sealing contact on the inner side of the tube-like container in a sealing position ; and fastened on the underside of the floating element , at least one ballast element ; wherein the density of the ballast element is greater than the density of the floating element; wherein the density of the entire separator lies within a value range between the density of the first phase and the density of the second phase of the fluid; wherein the floating element is designed in a disk shape; and wherein the ballast element is designed in the form of a plurality of fingers which extend away from the underside of the disk-shaped floating element - distributed on its edge, characterised in that distributed on its edge and alternating with the fingers, the disk-shaped floating element comprises thickened portions as buoyancy elements ; and the buoyancy elements are arranged on the side of the disk-shaped floating element opposite the fingers. a floating element made of an elastic material with, when viewed from above, a circumferential sealing edge for sealing contact on the inner side of the tube-like container in a sealing position ; and fastened on the underside of the floating element , at least one ballast element ; wherein the density of the ballast element is greater than the density of the floating element; wherein the density of the entire separator lies within a value range between the density of the first phase and the density of the second phase of the fluid; wherein the floating element is designed in a disk shape; and wherein the ballast element is designed in the form of a plurality of fingers which extend away from the underside of the disk-shaped floating element - distributed on its edge, characterised in that distributed on its edge and alternating with the fingers, the disk-shaped floating element comprises thickened portions as buoyancy elements ; and the buoyancy elements are arranged on the side of the disk-shaped floating element opposite the fingers.
A brake disk stack (100; 200) characterised by comprising a carbon/carbon ("C/C") rotor disk (108; 208) adjacent to a ceramic matrix composite ("CMC") stator disk (106; 206), an end plate (104; 204) comprising a CMC component and a pressure plate (102; 202) comprising a CMC component.
A combined sensor/emergency light unit for a lighting system, having: - a housing , - a rechargeable store for electrical energy, - a charging circuit for charging the rechargeable store , - an emergency lighting means , and - a low voltage-voltage supply connection, wherein the combined sensor/emergency light unit can be connected by the low voltage-voltage supply connection to a bus for the light control of the lighting system and the rechargeable store can be supplied by means of the charging circuit for recharging current from the bus, and wherein the bus is a DALI bus, which maintains a voltage in a non-operating state, wherein the combined sensor/emergency light unit also has a DALI control device, which is given an increased supply current from the DALI bus, wherein the increased supply current is greater than 2 mA, and the DALI control device is a bus-capable sensor module , wherein the combined sensor/emergency light unit also has an operating circuit, which is designed to monitor the voltage at the low voltage-voltage supply connection and to assess a permanent failure of the voltage as an emergency light situation and accordingly to activate the emergency lighting means , and wherein the DALI control device, the rechargeable store , the charging circuit, the operating circuit and the emergency lighting means are arranged in the housing . - a housing , - a rechargeable store for electrical energy, - a charging circuit for charging the rechargeable store , - an emergency lighting means , and - a low voltage-voltage supply connection, wherein the combined sensor/emergency light unit can be connected by the low voltage-voltage supply connection to a bus for the light control of the lighting system and the rechargeable store can be supplied by means of the charging circuit for recharging current from the bus, and wherein the bus is a DALI bus, which maintains a voltage in a non-operating state,
Method for validation of a time synchronization of at least two controllers connected to each other via a private communication bus , wherein one of the at least two controllers is a master controller and the other one of the at least two controllers is a slave controller , the method comprising a plurality of cycles, wherein each cycle includes: - sending, from the master controller to the slave controller , a follow up message in response to a pull of a predefined pin of the master controller , - wherein the follow up message includes a global time (t' aM2 ) of the master controller when the predefined pin was pulled, - sending, from the slave controller to the master controller , a validation message in response to the received follow up message, - wherein the validation message includes a global time (t bS2 ) of the slave controller when the pull of the predefined pin is detected by the slave controller , and - validating the time synchronization by checking, at the master controller and/or the slave controller , if a difference between the global time (t' aM2 ) of the master controller when the predefined pin was pulled and the global time (t bS2 ) of the slave controller when the pull of the predefined pin is detected by the slave controller is smaller than a predefined first threshold. - sending, from the master controller to the slave controller , a follow up message in response to a pull of a predefined pin of the master controller , - wherein the follow up message includes a global time (t' aM2 ) of the master controller when the predefined pin was pulled, - sending, from the slave controller to the master controller , a validation message in response to the received follow up message, - wherein the validation message includes a global time (t bS2 ) of the slave controller when the pull of the predefined pin is detected by the slave controller , and - validating the time synchronization by checking, at the master controller and/or the slave controller , if a difference between the global time (t' aM2 ) of the master controller when the predefined pin was pulled and the global time (t bS2 ) of the slave controller when the pull of the predefined pin is detected by the slave controller is smaller than a predefined first threshold.
An opening system for a swiveling aircraft door that closes an opening in a fuselage of an aircraft in a closed position and provides access to the aircraft through the opening in the fuselage in a fully open position , the opening system comprises: a hinge bracket that is adapted for pivotally attaching the swiveling aircraft door to the fuselage of the aircraft ; a swivel mechanism that is rotatably attached to the hinge bracket and adapted for performing an opening swivel movement of the swiveling aircraft door from the closed position to the fully open position and a closing swivel movement of the swiveling aircraft door from the fully open position to the closed position ; a hold-open latch that is pivotally attached to the swivel mechanism , wherein the hold-open latch is in an unclamped state when the swiveling aircraft door is in the closed position and latches in an over-centered state when the swiveling aircraft door is in the fully open position to prevent the swiveling aircraft door from returning to the closed position ; and an actuator that is fixedly attached to the hold-open latch , wherein the actuator acts on the hold-open latch that in turn acts on the swivel mechanism , thereby performing the opening and closing swivel movements of the swiveling aircraft door ; the opening system further comprising a stop that is adapted for stopping the hold-open latch in the over-centered state ; wherein the opening system is characterized by a release system that is coupled to the stop and adapted for transitioning the hold-open latch from the over-centered state to the unclamped state . a hinge bracket that is adapted for pivotally attaching the swiveling aircraft door to the fuselage of the aircraft ; a swivel mechanism that is rotatably attached to the hinge bracket and adapted for performing an opening swivel movement of the swiveling aircraft door from the closed position to the fully open position and a closing swivel movement of the swiveling aircraft door from the fully open position to the closed position ; a hold-open latch that is pivotally attached to the swivel mechanism , wherein the hold-open latch is in an unclamped state when the swiveling aircraft door is in the closed position and latches in an over-centered state when the swiveling aircraft door is in the fully open position to prevent the swiveling aircraft door from returning to the closed position ; and an actuator that is fixedly attached to the hold-open latch , wherein the actuator acts on the hold-open latch that in turn acts on the swivel mechanism , thereby performing the opening and closing swivel movements of the swiveling aircraft door ; the opening system further comprising a stop that is adapted for stopping the hold-open latch in the over-centered state ; wherein the opening system is characterized by a release system that is coupled to the stop and adapted for transitioning the hold-open latch from the over-centered state to the unclamped state .
Method for controlling an excitation polyphase synchronous rotating electric machine of the type comprising a control step in which currents of the phases in phase windings (u, v, w; u1, v1, w1, u2, v2, w2) of a stator of said machine are driven in full-wave (FW) mode, said machine being connected to an on-board electrical network supplied with power by a battery under a predetermined nominal voltage (Ubat) for motor operation of said machine , characterized in that said control step is preceded by a step (PreMag) of premagnetizing said stator in an open circuit, in which step a peak electromotive force between phases that is substantially equal to said nominal voltage (Ubat) is created by a rotor excitation current (Ir) for a rotor of said machine , said premagnetization step comprising determining a reference value of said rotor excitation current (Ir) according to an electrical angular frequency of said machine .
A method for use in operating a radar system that is capable of performing a plurality of different types of radar missions, comprising: loading a re-configurable radar control software program into a digital processor , wherein the re-configurable radar control software program includes code for performing radar functions without regard to radar mission type, the digital processor operative to control the operation of components of the radar system ; loading a mission determination code into the digital processor ; loading a configuration information retrieval code into the digital processor ; determining, with the mission determination code , a mission type to be performed by the radar system ; retrieving, with the configuration information retrieval code , a configuration file from a configuration database that is associated with the identified mission type, the configuration database including configuration files associated with a plurality of different mission types; and using configuration information from the retrieved configuration file to configure, with the configuration information retrieval code , the re-configurable radar control software program associated with the radar system to perform a mission having the identified mission type including using the configuration information to adapt one or more common radar functions in the radar control software program for use with the identified mission type. loading a re-configurable radar control software program into a digital processor , wherein the re-configurable radar control software program includes code for performing radar functions without regard to radar mission type, the digital processor operative to control the operation of components of the radar system ; loading a mission determination code into the digital processor ; loading a configuration information retrieval code into the digital processor ; determining, with the mission determination code , a mission type to be performed by the radar system ; retrieving, with the configuration information retrieval code , a configuration file from a configuration database that is associated with the identified mission type, the configuration database including configuration files associated with a plurality of different mission types; and using configuration information from the retrieved configuration file to configure, with the configuration information retrieval code , the re-configurable radar control software program associated with the radar system to perform a mission having the identified mission type including using the configuration information to adapt one or more common radar functions in the radar control software program for use with the identified mission type.