mhurhangee/ep-ind-claims huggingface dataset:
Apparatus for monitoring and detecting failures in the actuation of a control system, the apparatus comprising: a nominal model of the control system defined in terms of the state variables of the control system; a model of an asymmetric actuation monitoring envelope that dynamically bounds a range that measured state variables of the system are allowed to take during operation of the system defined as a function of the nominal system state model; means for monitoring a signal corresponding to a state variable of the system during operation thereof; and, means for detecting a failure in the actuation of the control system when the monitored signal exceeds the bounds of the monitoring envelope, wherein the actuation monitoring envelope comprises: a first subsystem defining an upper bound of the monitoring envelope; and, a second subsystem defining a lower bound of the monitoring envelope, wherein the monitoring envelope accounts for the dynamics and non-linearities of each element of the control system and the respective variations therein during system operation, and means for selecting between respective fast and slow system dynamics models of the subsystems with respective switches thereof so as to define the maximum permissible monitoring envelope upper and lower bounds as a function of variations in the respective system dynamics and non-linearity models of each subsystem during system operation. a nominal model of the control system defined in terms of the state variables of the control system; a model of an asymmetric actuation monitoring envelope that dynamically bounds a range that measured state variables of the system are allowed to take during operation of the system defined as a function of the nominal system state model; means for monitoring a signal corresponding to a state variable of the system during operation thereof; and, means for detecting a failure in the actuation of the control system when the monitored signal exceeds the bounds of the monitoring envelope, wherein the actuation monitoring envelope comprises: a first subsystem defining an upper bound of the monitoring envelope; and, a second subsystem defining a lower bound of the monitoring envelope, a first subsystem defining an upper bound of the monitoring envelope; and, a second subsystem defining a lower bound of the monitoring envelope, wherein the monitoring envelope accounts for the dynamics and non-linearities of each element of the control system and the respective variations therein during system operation, and means for selecting between respective fast and slow system dynamics models of the subsystems with respective switches thereof so as to define the maximum permissible monitoring envelope upper and lower bounds as a function of variations in the respective system dynamics and non-linearity models of each subsystem during system operation.
A two-package dental adhesive composition including a first agent and a second agent, which are divided from each other, the two-package dental adhesive composition comprising at least five components including: an acidic group-containing polymerizable monomer; a sulfur atom-containing polymerizable monomer; a silane coupling agent; a tetraarylborate compound; and water, wherein the first agent contains only the acidic group-containing polymerizable monomer and the sulfur atom-containing polymerizable monomer out of the five components, wherein the second agent contains only the silane coupling agent, the borate compound, and the water out of the five components, wherein the acidic group of the acidic group-containing polymerizable monomer is selected from the group consisting of a phosphinico group {=P(=O)OH}, a phosphono group {-P(=O) 2}, a dihydrogen phosphate monoester group {-O-P(=O) 2} and a hydrogen phosphate diester group {(-O-) 2 P(=O)OH}, and wherein the sulfur atom-containing polymerizable monomer does not contain a sulfur atom-containing acidic group. an acidic group-containing polymerizable monomer; a sulfur atom-containing polymerizable monomer; a silane coupling agent; a tetraarylborate compound; and water,
A method for creating, by a terminal, an access control object instance for use in a wireless communication system, the method comprising: receiving from a server, an operation for adding an account of a specific server; adding the account of the specific server; and creating an access control object instance for an object instance having no access control object instance from among object instances stored in the terminal if the account of the specific server is added when the terminal has only one existing server account, wherein the server corresponding to the existing server account is set to be an access control owner of the created access control object instance. receiving from a server, an operation for adding an account of a specific server; adding the account of the specific server; and creating an access control object instance for an object instance having no access control object instance from among object instances stored in the terminal if the account of the specific server is added when the terminal has only one existing server account, wherein the server corresponding to the existing server account is set to be an access control owner of the created access control object instance.
A turbine blade assembly comprising: a turbine blade comprising a turbine blade cavity; a blade platform supporting the turbine blade and comprising an upper surface adjacent the turbine blade and a lower surface opposite the upper surface; a blade root positioned on the lower surface of the blade platform, the blade root defining a blade root cavity; and a first rib the first rib extending from the blade root to the lower surface, tapering as it extends away from the blade root, the first rib defining a rib cavity fluidly coupled to the blade root cavity and the turbine blade cavity, the first rib and the blade platform further defining a first port extending from the rib cavity, through the blade platform to the upper surface, wherein the blade platform has a trailing edge and the first port extends from the rib cavity toward the trailing edge. a turbine blade comprising a turbine blade cavity; a blade platform supporting the turbine blade and comprising an upper surface adjacent the turbine blade and a lower surface opposite the upper surface; a blade root positioned on the lower surface of the blade platform, the blade root defining a blade root cavity; and a first rib the first rib extending from the blade root to the lower surface, tapering as it extends away from the blade root, the first rib defining a rib cavity fluidly coupled to the blade root cavity and the turbine blade cavity, the first rib and the blade platform further defining a first port extending from the rib cavity, through the blade platform to the upper surface, wherein the blade platform has a trailing edge and the first port extends from the rib cavity toward the trailing edge.
Magnet-based angular displacement measuring system for measuring a rotational movement of a driveshaft, comprising a drive shaft, an exciter unit rotationally coupled to the free end of the drive shaft, and a stationary sensor unit which functionally cooperates with the exciter unit for measuring the rotational movement of the drive shaft, characterized in that the drive shaft, at the free end thereof, has a coaxial recess such that a hollow shaft section is formed, wherein the exciter unit is fixed on the drive shaft by means of a fastening means extending through the recess, wherein a radial air gap is formed in the region of the hollow shaft section between the drive shaft and a fastening means.
A Tumor Micro-Environment responsive expression vector comprising: a nucleic acid sequence encoding a chimeric antigen receptor operably linked to a synthetic promoter, said promoter comprising two or more different TME dependent promoter response elements, wherein said at least two PRE's are an interferon-gamma-(IFN-γ) PRE and an NEκB PRE, and wherein the IFN-γ promoter response element comprises the nucleic acid sequence set forth in SEQ ID NO: 1, and wherein the NEκB PRE comprises the nucleic acid sequence set forth in SEQ ID NO: 2 ("K"); wherein the TME responsive expression vector is so constructed that a) the presence of IFN-γ and TNFα in the TME, when binding to interferon-gamma-(IFN-γ) PRE and NEκB PRE, induces a higher expression level of CAR than when only IFN-γ or TNFα are present in the TME, and b) minimal or low expression of CAR occurs in the absence of IFN-γ and TNFα, so that the CAR is upregulated and directing activities against the tumor while sparing normal tissue. a nucleic acid sequence encoding a chimeric antigen receptor operably linked to a synthetic promoter, said promoter comprising two or more different TME dependent promoter response elements, wherein said at least two PRE's are an interferon-gamma-(IFN-γ) PRE and an NEκB PRE, and wherein the IFN-γ promoter response element comprises the nucleic acid sequence set forth in SEQ ID NO: 1, and wherein the NEκB PRE comprises the nucleic acid sequence set forth in SEQ ID NO: 2 ("K"); wherein the TME responsive expression vector is so constructed that a) the presence of IFN-γ and TNFα in the TME, when binding to interferon-gamma-(IFN-γ) PRE and NEκB PRE, induces a higher expression level of CAR than when only IFN-γ or TNFα are present in the TME, and b) minimal or low expression of CAR occurs in the absence of IFN-γ and TNFα, a) the presence of IFN-γ and TNFα in the TME, when binding to interferon-gamma-(IFN-γ) PRE and NEκB PRE, induces a higher expression level of CAR than when only IFN-γ or TNFα are present in the TME, and b) minimal or low expression of CAR occurs in the absence of IFN-γ and TNFα,
Apparatus for regulating the temperature of at least one electric battery set of a motor vehicle, the battery set comprising at least one electric storage battery, the apparatus comprising a closed circuit which, in service, is in a heat transfer relationship with said battery set in such a way as to enable the temperature of the battery set to be regulated, the circuit comprising, in series, successively: - a vaporising means comprising a biphasic mixture of a regulating gas with a liquid absorbent, - a condenser for condensing the regulating gas escaping from the vaporising means into its state as a regulating liquid, - means for lowering the pressure of the regulating liquid, - a evaporator for evaporating the regulating liquid and causing it to return to its state as a regulating gas, - an absorber for absorbing the regulating gas and re-forming the biphasic mixture, - means for pumping the biphasic mixture from the absorber towards the vaporising means, the circuit also comprising a duct which permits the biphasic mixture to flow from the vaporising means towards the absorber and which extends in parallel with the pumping means and, characterised in that it comprises a first connecting member which is adapted to, in service, put the condenser or the evaporator into a heat transfer relationship with the battery set such that the apparatus is capable of both cooling and heating the battery set. - a vaporising means comprising a biphasic mixture of a regulating gas with a liquid absorbent, - a condenser for condensing the regulating gas escaping from the vaporising means into its state as a regulating liquid, - means for lowering the pressure of the regulating liquid, - a evaporator for evaporating the regulating liquid and causing it to return to its state as a regulating gas, - an absorber for absorbing the regulating gas and re-forming the biphasic mixture, - means for pumping the biphasic mixture from the absorber towards the vaporising means,
Method for determining the rebound of a movable component on a limit stop of a handling unit, wherein the handling unit comprises a damping element for damping the movement of the component before reaching the limit stop as well as a limit stop switch with a magnetic sensor, wherein the limit stop switch generates a limit stop signal (A1=1) when the component is detected at the limit stop by the sensor, wherein the limit stop switch generates a rebound signal (A2=1), if the sensor after a first impact of the component on the limit stop detects a reverse movement (a) of the component due to a rebound of the component and after that a second impact of the component on the limit stop.
Carrier for supplying organic kitchen waste to a shredding device of a waste disposal device for organic kitchen waste, characterised by a shaft, a rotation axis which extends coaxially relative to the shaft and at least one pre-shredding blade which is provided on the shaft and which is arranged perpendicularly to the rotation axis thereof for shredding organic kitchen waste, and which is constructed as a triangular blade having flanks which are inclined in the direction towards the shredding device, wherein the carrier can be connected to the shredding device in a rotationally secure manner, wherein the at least one pre-shredding blade is arranged on the shaft in such a manner that in the connected state of the carrier to the shredding device it is arranged spaced apart from the shredding device.
A throttle device for varying the pressure of a fluid in a plurality of parallel outlets, wherein said throttle device comprises: a header comprising an inlet and a plurality of outlets for the fluid, a control element that is mounted so as to be at least partially displaceable in an internal chamber of said header and comprises a plurality of orifices (21, 22), wherein said orifices (21, 22) in said control element and said outlets on said header are configured and positioned such that the cross-section of a plurality of fluid communication routes between said internal chamber of said header and a plurality of outlets on said header can be varied by means of a relative movement of said control element in relation to said header, characterized in that said control element is a sleeve, wherein said orifices (21, 22) are disposed in said sleeve such that they correspond to said outlets of said header, wherein between said sleeve and said header seals are provided such that in a region between an outside surface of said sleeve and an inside surface of said internal chamber of said header no fluid communication exists between said orifices (21, 22) in said sleeve. a header comprising an inlet and a plurality of outlets for the fluid, a control element that is mounted so as to be at least partially displaceable in an internal chamber of said header and comprises a plurality of orifices (21, 22), wherein said orifices (21, 22) in said control element and said outlets on said header are configured and positioned such that the cross-section of a plurality of fluid communication routes between said internal chamber of said header and a plurality of outlets on said header can be varied by means of a relative movement of said control element in relation to said header, characterized in that said control element is a sleeve, wherein said orifices (21, 22) are disposed in said sleeve such that they correspond to said outlets of said header, wherein between said sleeve and said header seals are provided such that in a region between an outside surface of said sleeve and an inside surface of said internal chamber of said header no fluid communication exists between said orifices (21, 22) in said sleeve.
Optical sensor for detecting objects in a detection region, having at least one sensor component, which has a lens, in a housing and having at least one evaluation unit for generating an object detection signal as a function of sensor signals from said at least one sensor component, a plurality of display elements which surround the lens being provided in a wall of the housing, which complement each other to form a symbol display unit, characterised in that the display elements are provided to surround two lenses, wherein these display elements form a seven-segment display, or in that the symbol display unit forms a bar graph display, wherein the symbol display unit can be switched between a bar graph display and a symbol display.
An actuator for a landing gear of an aircraft, wherein the actuator can be connected to the landing gear of the aircraft in such a way that the landing gear of the aircraft is retractable and/or extendable by means of the actuator, wherein the actuator has at least one drive unit by means of which at least one movable part of the actuator can be moved into different positions and that said drive unit is formed by at least one electric motor or comprises at least one electric motor, characterised in that two locking members (100, 110) are provided, which fix the movable part of the actuator in both of its extreme positions in such a way that the landing gear that can be connected to the movable part of the actuator is also locked thereby.
A kit comprising: at least partially double-stranded adapters with a single nucleotide T overhang at a 3' end (T-tailed adapters); and at least partially double-stranded adapters with a single nucleotide C overhang at a 3' end (C-tailed adapters). at least partially double-stranded adapters with a single nucleotide T overhang at a 3' end (T-tailed adapters); and at least partially double-stranded adapters with a single nucleotide C overhang at a 3' end (C-tailed adapters).
A method for controlling power flow within a wind park system for power transmission to a main power grid, the wind park system comprising two or more parallel-connected island wind park grids (120, 130,140, 150), each island wind park grid (120, 130,140, 150) comprising a wind park (11, 21, 31, 41) with at least one wind turbine, the wind park (11, 21, 31, 41) being connected to an AC bus (13, 23, 33, 43), in turn connected to a voltage source converter (10, 20, 30, 40) arranged to feed power to the main power grid by means of a direct current transmission line (15, 25, 35, 45), the method comprising the steps of: - controlling a first voltage source converter as a swing bus in frequency control, the frequency control comprising controlling frequency to a steady state reference operating point for operating points within a power dead band and by means of frequency droop control when exceeding an end point of the power dead band, and - controlling at least a second voltage source converter (20, 30, 40) in power control, the power control comprising controlling power flow to a steady state reference operating point for operating points within a frequency dead band and by means of power droop control when exceeding an end point of the frequency dead band. - controlling a first voltage source converter as a swing bus in frequency control, the frequency control comprising controlling frequency to a steady state reference operating point for operating points within a power dead band and by means of frequency droop control when exceeding an end point of the power dead band, and - controlling at least a second voltage source converter (20, 30, 40) in power control, the power control comprising controlling power flow to a steady state reference operating point for operating points within a frequency dead band and by means of power droop control when exceeding an end point of the frequency dead band.
A method for generating a weather band selection, the method comprising: responsive to receiving a weather band selection request for a flight plan, identifying weather information for the flight plan; selecting one or more weather bands for the flight plan based on the weather information to form a weather band selection; and outputting the weather band selection. responsive to receiving a weather band selection request for a flight plan, identifying weather information for the flight plan; selecting one or more weather bands for the flight plan based on the weather information to form a weather band selection; and outputting the weather band selection.
A wastegate assembly for a turbocharger comprising: a housing enclosing an actuator operatively connected to a wastegate valve, the housing terminating at an end in a crush seal; and a mounting member connectable to a mounting plate of the turbocharger with the wastegate valve received in an opening of the mounting plate to place the crush seal in sealing engagement against a surface of the turbocharger that defines a wastegate opening in the turbocharger; wherein the crush seal is permanently and fixedly deformed by the sealing engagement and corrects for tolerance variations between at least the mounting member and the mounting plate of the turbocharger. a housing enclosing an actuator operatively connected to a wastegate valve, the housing terminating at an end in a crush seal; and a mounting member connectable to a mounting plate of the turbocharger with the wastegate valve received in an opening of the mounting plate to place the crush seal in sealing engagement against a surface of the turbocharger that defines a wastegate opening in the turbocharger; wherein the crush seal is permanently and fixedly deformed by the sealing engagement and corrects for tolerance variations between at least the mounting member and the mounting plate of the turbocharger.
A formed body that is obtainable by injection-forming a resin composition constituted by a thermoplastic resin and a barrier resin, the formed body having a layer of said resin composition, wherein: the layer of said resin composition forms, in a matrix of the thermoplastic resin, a layer structure in which the barrier resin is dispersed in the form of a lamellar dispersion phase stretching in one direction; the ratio (a) / (b) of an aspect ratio (a) of the dispersion phase of the barrier resin in a surface layer portion of the layer and an aspect ratio (b) of the dispersion phase of the barrier resin in the central portion in the direction of thickness of the layer, is not more than 2.0, wherein said central portion in the direction of thickness of the layer stands for a range of 40 to 60% of the whole thickness of the layer that is regarded to be 100%, and said surface layer portion stands for the portions excluding the central portion; and the melt flow rate (MFRm) of said thermoplastic resin is 0.1 to 29 g/10 min., the melt flow rate (MFRb) of said barrier resin is 3 to 100 g/10 min, and the ratio (MFRb/MFRm) of the melt flow rate (MFRb) of said barrier resin and the melt flow rate (MFRm) of said thermoplastic resin is 11 to 200, wherein melt flow is measured under the conditions of a temperature of 230°C and a load of 2160 g in compliance with JIS K7210. the layer of said resin composition forms, in a matrix of the thermoplastic resin, a layer structure in which the barrier resin is dispersed in the form of a lamellar dispersion phase stretching in one direction; the ratio (a) / (b) of an aspect ratio (a) of the dispersion phase of the barrier resin in a surface layer portion of the layer and an aspect ratio (b) of the dispersion phase of the barrier resin in the central portion in the direction of thickness of the layer, is not more than 2.0, wherein said central portion in the direction of thickness of the layer stands for a range of 40 to 60% of the whole thickness of the layer that is regarded to be 100%, and said surface layer portion stands for the portions excluding the central portion; and the melt flow rate (MFRm) of said thermoplastic resin is 0.1 to 29 g/10 min., the melt flow rate (MFRb) of said barrier resin is 3 to 100 g/10 min, and the ratio (MFRb/MFRm) of the melt flow rate (MFRb) of said barrier resin and the melt flow rate (MFRm) of said thermoplastic resin is 11 to 200, wherein melt flow is measured under the conditions of a temperature of 230°C and a load of 2160 g in compliance with JIS K7210.