mhurhangee/ep-ind-claims huggingface dataset:
Method for evaluating an asymmetric residual stress for a material by an indentation test comprising: applying the residual stresses σ x res and σ y res with uniaxial and symmetrical biaxial tensions on the material and then performing an instrumented indentation test indenting an Knoop indenter on the material; comparing a slope of indentation load-depth curve when the long diagonal direction of the Knoop indenter is perpendicular to the direction of the largest residual stress with that in stress-free state, and then a slope of indentation load-depth curve when the long diagonal direction of the Knoop indenter is parallel to the direction of the largest residual stress with that in stress-free state, so as to evaluate the asymmetric residual stress for the material; determining the ratio of the conversion factor (α ⊥, α //) which associates the residual stress with the induced indentation load difference from the residual stress according to the uniaxial residual stress and the longer diagonal direction of the asymmetric indenter and which is defined by ΔL 1 = α ⊥ σ res x + α / / σ res y ΔL 2 = α / / σ res x + α ⊥ σ res y whereby ΔL 1 is the difference of loads between the indented state where the long diagonal of the Knoop indenter is perpendicular to the x-axis and stress-free state at the same indentation depth, and ΔL 2 is the difference of loads between the indented state where the long diagonal of the Knoop indenter is parallel to the x-axis and stress-free state at the same indentation depth; and using the conversion factor ratio and the ratio of the induced indentation load differences (Δ L 1 and Δ L 2) when the long diagonal direction of the Knoop indenter in the biaxial residual stress state is perpendicular or parallel to the direction of the largest residual stress, then to determine the stress directionality (p).
A solvate of ivacaftor selected from crystalline ivacaftor.n-butanol solvate characterized by X-ray Diffraction spectrum having peak reflections at about 3.4 and 14.2 ±0.2 degrees 2 theta or crystalline ivacaftor.methanol solvate characterized by X-ray Diffraction spectrum having peak reflections at about 7.28, 13.84, 14.03, 19.78, 20.27 and 20.92 ±0.2 degrees 2 theta.
A system for securing a first composite panel to a second composite panel, the system comprising: a latch assembly having one or more latches (124, 126), wherein the latch assembly is configured to be secured to one of the first composite panel or the second composite panel; one or more strikes configured to retain at least a portion of the one or more latches (124, 126), wherein the one or more strikes are configured to be secured to the other of the first composite panel or the second composite panel, wherein the latch assembly comprises: a first latch; a second latch; and a lock disposed between the first latch and the second latch. a latch assembly having one or more latches (124, 126), wherein the latch assembly is configured to be secured to one of the first composite panel or the second composite panel; one or more strikes configured to retain at least a portion of the one or more latches (124, 126), wherein the one or more strikes are configured to be secured to the other of the first composite panel or the second composite panel, wherein the latch assembly comprises: a first latch; a second latch; and a lock disposed between the first latch and the second latch. a first latch; a second latch; and a lock disposed between the first latch and the second latch.
A precipitation hardening type martensitic stainless steel consisting of: Cr (chromium): 9 to 10%; Mo (molybdenum): 1 to 2%; Ni (nickel): 8.5 to 11.5%; Ti (titanium): no less than 0.6 and no greater than 1.4%; C (carbon): 0.0005 to 0.05%; Al (aluminum): 0.0005 to 0.25%; Cu (copper): 0.005 to 0.75%; Nb (niobium): 0.0005 to 0.3%; Si (silicon): 0.005 to 0.75%; Mn (manganese): 0.005 to 1%; and N (nitrogen): 0.0001 to 0.03% by mass, and the balance of Fe (iron) and unavoidable impurities.
Coupling for a shaft-end, substantially having a square cross-section, which at a distance (a) from its outer end is provided with a region, hereinafter indicated as transverse groove, having a circular or non-circular cross-section which is not greater - over any angle - than the smallest cross-section of the square shaft-end, characterised in that, the coupling comprises a front plate, a locking plate and a rear plate, wherein the front plate and the locking plate both are provided with a continuous square opening (9 and 10 respectively), through which the square shaft-end is inserted, and wherein the rear plate is provided with a non-continuous square opening, in which the square shaft-end can be inserted, wherein the front plate and the rear plate are fixedly interconnected in a position, in which the orientation of the square openings correspond to each other, wherein the locking plate is bearing-mounted rotatably between the front plate and the rear plate in such a way that it can be rotated back and forth between an unlocked position, in which the orientations of the square openings in the front plate and in the rear plate and the orientation of the square opening in the locking plate coincide with one another, and a locked position, in which the openings do not coincide, the coupling being arranged and sized such that in the unlocked position the square shaft-end can be inserted through the continuous square openings in the front plate and locking plate into the non-continuous square opening in the rear plate, after which the locking plate is rotated relative to the front plate and rear plate over a certain interlocking angle, by which the shaft-end is coupled with the assembly, which comprises the mutually interconnected front plate and rear plate and the interposed locking plate, so that the shaft-end can not be pulled out without reversely rotating the locking plate into its unlocked position.
A fluid dispenser device comprising a body, a reservoir, a dispenser head incorporating a dispenser orifice, and a dispenser member, such as a pump or a valve, that is mounted on said reservoir by means of a fastener ring, said dispenser member comprising a dispenser-member body and a movable member that moves axially in said dispenser-member body while said dispenser member is being actuated, said device further comprising a lateral actuator system that is secured to said body, said system including an actuator element that is movable, substantially transversally to the direction of movement of said movable member, between a rest position in which said dispenser member is not actuated, and an actuated position in which said dispenser member is actuated, said body including at least one guide surface for guiding said actuator element, said at least one guide surface being stationary relative to said dispenser head and substantially parallel to the movement axis of the movable member in the dispenser-member body while said dispenser member is being actuated, said actuator element including at least one end edge that is preferably rounded and that co-operates with said at least one guide surface, said fluid dispenser device being characterized in that said at least one guide surface includes resistance means that modify the co-operation between said actuator element and said guide surface, in order to be passed over, said resistance means require the user to act on said lateral actuator system with an actuation force that is different.
A method for controlling operation of an internal combustion engine in which the engine is temporarily stopped according to a request for a stop to the engine having an exhaust gas recirculation system incorporated therein, and the engine is started again according to a request for a start to the engine, wherein the exhaust gas recirculation system includes: an EGR passage for recirculating a part of exhaust gas discharged from the engine to an air intake passage as EGR gas, one end of the EGR passage being communicated with the air intake passage and the other end thereof being communicated with an exhaust passage; an EGR control valve arranged on one end side of the EGR passage for controlling a flow rate of the EGR gas flowing through the EGR passage; and an on-off valve arranged on the other end side of the EGR passage for opening and closing the EGR passage, the method comprising the steps of: determining whether or not the engine is in a pressure-accumulable operational state in which the EGR gas can be pressure-accumulated in the EGR passage between the EGR valve and the on-off valve; bringing the EGR valve into a full closed state when it is determined that the engine is in the pressure-accumulable operational state; comparing a pressure of exhaust gas interposed in the exhaust passage to be led to the EGR passage, and a pressure of the EGR gas interposed in the EGR passage between the EGR valve and the on-off valve after bringing the EGR valve into the full closed state; and bringing the on-off valve into the full closed state when the pressure of the exhaust gas interposed in the exhaust passage to be led to the EGR passage becomes lower than the pressure of the EGR gas interposed in the EGR passage between the EGR valve and the on-off valve. determining whether or not the engine is in a pressure-accumulable operational state in which the EGR gas can be pressure-accumulated in the EGR passage between the EGR valve and the on-off valve; bringing the EGR valve into a full closed state when it is determined that the engine is in the pressure-accumulable operational state; comparing a pressure of exhaust gas interposed in the exhaust passage to be led to the EGR passage, and a pressure of the EGR gas interposed in the EGR passage between the EGR valve and the on-off valve after bringing the EGR valve into the full closed state; and bringing the on-off valve into the full closed state when the pressure of the exhaust gas interposed in the exhaust passage to be led to the EGR passage becomes lower than the pressure of the EGR gas interposed in the EGR passage between the EGR valve and the on-off valve.
Fuselage nose cap for a missile, having an outer surface, a cap wall forming the outer surface, and a force element, wherein the cap wall has a predetermined breaking geometry and the force element is prepared for destructive fragmentation of the cap wall in accordance with the predetermined breaking geometry, characterized in that the force element is enclosed by a number of press-off shells which are arranged on the inner surface of the cap wall, wherein in each case a press-off shell (20a, 20b) is arranged on in each case a subregion, which is delimited at least partially by the predetermined breaking geometry, of the inner surface (18a, 18b) of the cap wall and is prepared for separating the respective subregion (18a, 18b) from the other subregion (18a, 18b).
Method for machining the interior of a brake caliper of a disc brake, on which are formed: - a first caliper portion on the one side of the brake disc of the disc brake, - a second caliper portion on the other side of the brake disc, and - a bridge portion connecting the caliper portions (11, 12) and providing a free space for at least a part of the brake disc, wherein at least one of the caliper portions is provided with a cavity for receiving a brake application device, which cavity comprises a mounting opening towards the free space and extends in the opposite direction as far as a caliper rear wall, on the inner side of which at least one support surface is formed for the forces acting during the brake application, wherein the machining of the support surface is carried out from the free space and through the mounting opening, and for this purpose, a tool is brought into the cavity from outside the brake caliper, characterized in that the tool is guided into the cavity through an opening other than the mounting opening. - a first caliper portion on the one side of the brake disc of the disc brake, - a second caliper portion on the other side of the brake disc, and - a bridge portion connecting the caliper portions (11, 12) and providing a free space for at least a part of the brake disc,
Coriolis flow sensor (1, 101, 201, 301, 401), comprising a housing (5, 105, 205, 305) and at least a Coriolis-tube (2, 102, 202, 302) with at least two ends being fixed in a tube fixation means, wherein the flow sensor (1, 101, 201, 301, 401) comprises excitation means for causing the tube (2, 102, 202, 302) to oscillate, as well as detection means (11a-c, 111, 111a-c, 211a-c, 311a-c) for detecting at least a measure of displacements of parts of the tube (2, 102, 202, 302) during operation, characterized in that it comprises - a reference mass (15, 125, 225, 325), comprising the detection means (11a-c, 111, 111a-c, 211a-c, 311a-c) for the Coriolis tube; - further excitation means (31, 32, 131, 331) arranged for causing the reference mass (15, 125, 225, 325) to oscillate with respect to the housing (5, 105, 205, 305), wherein the further excitation means (31, 32, 131, 331) are provided between the housing (5, 105, 205, 305) or a part rigidly connected to the housing (5, 105, 205, 305), on the one hand, and to the reference mass (15, 125, 225, 325) on the other hand; - further detection means (13, 14, 16, 113, 114, 116, 313, 314, 316) arranged for detecting at least a measure of displacements of the reference mass (15, 125, 225, 325) and/or the housing (5, 105, 205, 305) during operation; as well as - control means for controlling the excitation means and/or the further excitation means (31, 32, 131, 331) based on movements measured by the detection means (11a-c, 111, 111a-c, 211a-c, 311a-c) and/or further detection means (13, 14, 16). - a reference mass (15, 125, 225, 325), comprising the detection means (11a-c, 111, 111a-c, 211a-c, 311a-c) for the Coriolis tube; - further excitation means (31, 32, 131, 331) arranged for causing the reference mass (15, 125, 225, 325) to oscillate with respect to the housing (5, 105, 205, 305), wherein the further excitation means (31, 32, 131, 331) are provided between the housing (5, 105, 205, 305) or a part rigidly connected to the housing (5, 105, 205, 305), on the one hand, and to the reference mass (15, 125, 225, 325) on the other hand; - further detection means (13, 14, 16, 113, 114, 116, 313, 314, 316) arranged for detecting at least a measure of displacements of the reference mass (15, 125, 225, 325) and/or the housing (5, 105, 205, 305) during operation; as well as - control means for controlling the excitation means and/or the further excitation means (31, 32, 131, 331) based on movements measured by the detection means (11a-c, 111, 111a-c, 211a-c, 311a-c) and/or further detection means (13, 14, 16).
A measuring device comprising a heat exchanger which has a pressure tube arrangement spaced apart by bars and having a combustion side and an isolation side and is embodied with at least one heat flow sensor, wherein - the heat flow sensor is arranged at the combustion side in such a way that at least two temperatures T 1 and T 2 and the temperature difference thereof can be determined there, and - at least one temperature sensor for measuring a temperature T 3 is additionally arranged on the isolation side and at a distance from the heat flow sensor, characterized in that the at least one temperature sensor is arranged on a bar of the pressure tube arrangement. - the heat flow sensor is arranged at the combustion side in such a way that at least two temperatures T 1 and T 2 and the temperature difference thereof can be determined there, and - at least one temperature sensor for measuring a temperature T 3 is additionally arranged on the isolation side and at a distance from the heat flow sensor, characterized in that the at least one temperature sensor is arranged on a bar of the pressure tube arrangement.
Cleaning device, particularly a washing machine or dishwasher, for cleaning a product to be cleaned by means of process water in a washing process, with a vat for receiving the product to be cleaned, a waste water container for temporarily storing waste water from the vat, a heat pump (7 - 10) for extracting heat from the waste water container and for adding it to the process water in the vat, a temperature sensor (20, 21) for measuring a temperature and a controller for controlling the cleaning device, the controller being adapted to control the heat pump (7 - 10) in such a way that heat is extracted from the waste water container by the heat pump (7 - 10) until a part of the process water freezes inside the waste water container, wherein a maximum operating time of the heat pump depends on the temperature measured by the temperature sensor (20, 21), characterized in that the controller is adapted to determine an ambient temperature with the temperature sensor (20, 21), to determine a maximum operating time of the heat pump based on the ambient temperature and to limit the operating time of the heat pump during the washing process to the maximum operating time, wherein no temperature sensor is arranged at or inside the waste water container.
Method for regulating an installation for producing containers, the installation comprising a unit for heating preforms and a unit for forming by blow moulding or stretch blow moulding, each container being produced from a preform made of plastics material, this method comprising the steps of: a) identifying a preform model; b) identifying a container model to be produced from the preform model; c) on the basis of these identifications, selecting from a database a production recipe associated with the preform model and the container model and comprising control setpoints for the installation; d) setting the installation into operation as per the production recipe so as to produce a hollow body (3'; 2) from a preform according to the model; this method being characterized in that it comprises the steps of: e) measuring one or more actual properties of the hollow body (3'; 2) produced using the production recipe; f) comparing each actual property with a corresponding predetermined theoretical property; g) if at least one actual property is deemed to be non-compliant: h) adjusting the recipe; i) repeating steps d) to f) following the adjusted recipe; j) as soon as each actual property is deemed to be compliant, saving the adjusted production recipe in the database. a) identifying a preform model; b) identifying a container model to be produced from the preform model; c) on the basis of these identifications, selecting from a database a production recipe associated with the preform model and the container model and comprising control setpoints for the installation; d) setting the installation into operation as per the production recipe so as to produce a hollow body (3'; 2) from a preform according to the model; e) measuring one or more actual properties of the hollow body (3'; 2) produced using the production recipe; f) comparing each actual property with a corresponding predetermined theoretical property; g) if at least one actual property is deemed to be non-compliant: h) adjusting the recipe; i) repeating steps d) to f) following the adjusted recipe; h) adjusting the recipe; i) repeating steps d) to f) following the adjusted recipe; j) as soon as each actual property is deemed to be compliant, saving the adjusted production recipe in the database.
Floor covering consisting of at least three layers which are connected together by means of a thermoplastic process, wherein one of the layers consists of thermoplastically deformable starting materials and the connection of the at least three layers is produced under the influence of pressure and temperature between two encircling belts arranged at a spacing from one another and forming a gap, characterised in that sections of the surface of the floor covering consist of a natural material, wherein these sections are respectively arranged at a spacing from one another or respectively arranged to lie against one another and wherein this natural material consists of stone material or wood material in the form of stone-surfaced sheeting or wood veneer and is the layer of the floor covering visible after laying and that arranged under the layer of stone material or wood material is an intermediate layer consisting substantially of a resilient material which consists of thermoplastically bound resilient additives.
A predistortion circuit for countering interference affecting a digital signal during transmission over a transmission link between a mapper at a transmitter side and a demapper at a receiver side, wherein the predistortion circuit is arranged for receiving a digital symbol selected from a predefined constellation used for mapping a bit stream, and comprises at least one correction stage arranged for - determining the output value of a transmission link model receiving an input symbol, which is the selected digital symbol for the first correction stage and the output of a previous correction stage for any following correction stage, - determining a correction term as a function of said output value and a target constellation symbol, the predistortion circuit further comprising an adder after each correction stage arranged for adding said correction term to said input symbol received by that correction stage and for outputting to a following correction stage or to an output of the predistortion circuit in case the correction stage is the last one, the result of said adding as an updated version of said digital symbol, and wherein said target constellation symbol is the symbol of a target constellation corresponding to said digital symbol, said target constellation being derived from said predefined constellation and said transmission link model and having the position of the target constellation points determined by calculating a mass point for groups of output values of said transmission link model, each output value of a same group corresponding to a same digital symbol of said predefined constellation. - determining the output value of a transmission link model receiving an input symbol, which is the selected digital symbol for the first correction stage and the output of a previous correction stage for any following correction stage, - determining a correction term as a function of said output value and a target constellation symbol,
A humanised isolated antibody or antigen binding fragment thereof, wherein the antibody or fragment thereof comprises a heavy chain variable region and a light chain variable region, wherein the VH comprises SEQ ID NO: 20 and the VL comprises SEQ ID NO: 29 and wherein the antibody binds brain microvascular endothelial cells.
Method, comprising: multiplexing an in-band pilot and an out-band pilot for providing a pilot transmission in a multiple antenna closed loop transmission, and transmitting the in-band pilot and the out-band pilot in an uplink sub-frame, wherein said in-band pilot is a beam-specific pilot and said out-band pilot is an antenna-specific pilot, wherein for beam-specific pilots, pilots are transmitted using the same beam as data transmission, and for antenna-specific pilots, orthogonal pilots are transmitted from multiple antennas. multiplexing an in-band pilot and an out-band pilot for providing a pilot transmission in a multiple antenna closed loop transmission, and transmitting the in-band pilot and the out-band pilot in an uplink sub-frame, wherein said in-band pilot is a beam-specific pilot and said out-band pilot is an antenna-specific pilot, wherein for beam-specific pilots, pilots are transmitted using the same beam as data transmission, and for antenna-specific pilots, orthogonal pilots are transmitted from multiple antennas.
A heat dissipating substrate which is a composite substrate consisting of three layers, namely a first, surface layer composed of single crystal silicon, a second, handle substrate layer composed of aluminum nitride or silicon carbide and a third, intermediate layer between the surface layer and the second layer and composed of silicon carbide or diamond wherein the intermediate layer has higher thermal conductivity than the second layer.