mhurhangee/ep-ind-claims huggingface dataset:
Method for surface treatment of laser-sintered plastic objects, which are produced from polyamide, polystyrene, or glass bead or carbon fiber filled polyamide, polyamide 11, polyamide 12, polypropylene or mixtures thereof, wherein the following steps are performed successively: a) smoothing the surfaces of the plastic objects by means of a slide finishing method; b) washing the smoothed plastic objects with clear water or by means of an ultrasonic bath with demineralized water; c) dyeing the plastic objects by means of contacting with dyes, wherein said dyes are textile dyes selected from acid dyes, metal complex dyes, dispersion dyes, direct dyes or reactive dyes; d) impregnating the surfaces of the plastic objects by means of contacting with oils, greases or combinations thereof. a) smoothing the surfaces of the plastic objects by means of a slide finishing method; b) washing the smoothed plastic objects with clear water or by means of an ultrasonic bath with demineralized water; c) dyeing the plastic objects by means of contacting with dyes, wherein said dyes are textile dyes selected from acid dyes, metal complex dyes, dispersion dyes, direct dyes or reactive dyes; d) impregnating the surfaces of the plastic objects by means of contacting with oils, greases or combinations thereof.
A liquid-repellent composition comprising the following components to and satisfying the following formula: Component: a tetrafunctional silane-based compound represented by the following general formula (a): Si(OR 1) p (X 1) 4-p (a) wherein, R 1 represents an alkyl group having 1 to 6 carbon atoms; X 1 represents a halogen atom; when plural R 1 's are present, the plural R 1 's may be the same as or different from each other; when plural X 1 's are present, the plural X 1 's may be the same as or different from each other; and p represents an integer of 0 to 4, Component: a trifunctional silane-based compound represented by the following general formula (b): R 2 Si(OR 3) q (X 2) 3-q (b) wherein, R 2 represents a n-pentadecyl group, a n-hexadecyl group, a n-heptadecyl group, a n-octadecyl group, a n-nonadecyl group, a n-eicosyl group, a n-heneicosyl group, or a n-docosyl group; R 3 represents a methyl group; X 2 represents a halogen atom; when plural X 2 's are present, the plural X 2 's may be the same as or different from each other; and q represents an integer of 0 to 3, Component: a metal catalyst, 12 ≤ x ≤ 64 wherein, x represents a ratio of a molar amount of the component to a molar amount of the component [ /] (molar ratio), and wherein the metal catalyst (Component) is a metal catalyst which does not require light irradiation for revealing a catalytic action. R 1 represents an alkyl group having 1 to 6 carbon atoms; X 1 represents a halogen atom; when plural R 1 's are present, the plural R 1 's may be the same as or different from each other; when plural X 1 's are present, the plural X 1 's may be the same as or different from each other; and p represents an integer of 0 to 4, Component: a trifunctional silane-based compound represented by the following general formula (b): R 2 Si(OR 3) q (X 2) 3-q (b) wherein, R 2 represents a n-pentadecyl group, a n-hexadecyl group, a n-heptadecyl group, a n-octadecyl group, a n-nonadecyl group, a n-eicosyl group, a n-heneicosyl group, or a n-docosyl group; R 3 represents a methyl group; X 2 represents a halogen atom; when plural X 2 's are present, the plural X 2 's may be the same as or different from each other; and q represents an integer of 0 to 3, Component: a metal catalyst, 12 ≤ x ≤ 64 wherein, x represents a ratio of a molar amount of the component to a molar amount of the component [ /] (molar ratio), and wherein the metal catalyst (Component) is a metal catalyst which does not require light irradiation for revealing a catalytic action.
A catheter stiffener adjustment system, comprising: a first member having an outer diameter and having at least three first segments (30, 32, 34, 36) with at least one joint (31, 33, 35) enabling the segments (30, 32, 34, 36) to bend relative to each other; a second member having an inner diameter defining a passageway through which the first member is movable relative to the second member, and having at least three second segments (40, 42, 44, 46) with at least one joint (41, 43, 45) enabling the segments (40, 42, 44, 46) to bend relative to each other; in a first position, the first segments (30, 32, 34, 36) and the second segments (40, 42, 44, 46) are alignable substantially in phase to generate a first flexure condition; and in a second position, the first segments (30, 32, 34, 36) and the second segments (40, 42, 44, 46) are alignable substantially out of phase to generate a second, stiffer flexure condition wherein the first member and the second member are translatable relative to each other between both the first and second positions. a first member having an outer diameter and having at least three first segments (30, 32, 34, 36) with at least one joint (31, 33, 35) enabling the segments (30, 32, 34, 36) to bend relative to each other; a second member having an inner diameter defining a passageway through which the first member is movable relative to the second member, and having at least three second segments (40, 42, 44, 46) with at least one joint (41, 43, 45) enabling the segments (40, 42, 44, 46) to bend relative to each other; in a first position, the first segments (30, 32, 34, 36) and the second segments (40, 42, 44, 46) are alignable substantially in phase to generate a first flexure condition; and in a second position, the first segments (30, 32, 34, 36) and the second segments (40, 42, 44, 46) are alignable substantially out of phase to generate a second, stiffer flexure condition wherein the first member and the second member are translatable relative to each other between both the first and second positions.
An islanding detection system for a distributed generator arranged to be connected to an electrical grid, characterized in that it comprises a first arm operable to be connected between the phase connection and the neutral connection of the electrical grid; a second arm operable to be connected between the phase connection and the neutral connection of the electrical grid, the first arm comprising a higher impedance than the second arm; and a controller arranged to connect the higher impedance arm and sense the current through it, and to connect the lower impedance arm and sense the current through it, and to disconnect the distributed generator from the electrical grid in the event that the sensed current in the lower impedance arm is similar or equal to the sensed current in the higher impedance arm.
A medical device support system, comprising: a central shaft; an extension arm having a support for a medical device and a hub at its proximal end mounted to the central shaft for pivotable movement about the central shaft; and, a brake assembly secured in the hub for rotation therewith and including first and second backing portions (620, 622) and first and second liners (624, 626) supported by the backing portions (620, 622), wherein at least the first liner is supported by the first backing portion by the first liner being snap-fitted to the first backing portion; wherein the brake assembly includes an actuator configured to flex the first and second backing portions (620, 622) to urge the first and second liners (624, 626) toward and away from each other to respectively increase and decrease a frictional braking force to the central shaft. a central shaft; an extension arm having a support for a medical device and a hub at its proximal end mounted to the central shaft for pivotable movement about the central shaft; and, a brake assembly secured in the hub for rotation therewith and including first and second backing portions (620, 622) and first and second liners (624, 626) supported by the backing portions (620, 622), wherein at least the first liner is supported by the first backing portion by the first liner being snap-fitted to the first backing portion; wherein the brake assembly includes an actuator configured to flex the first and second backing portions (620, 622) to urge the first and second liners (624, 626) toward and away from each other to respectively increase and decrease a frictional braking force to the central shaft.
Document of value (1, 8) comprising a paper substrate having a front side and a back side, wherein - the front side of the paper substrate, in a region designated as foil security element region, bears a foil security element (3, 10) having a front side and a back side, wherein the front side of the foil security element has a motif which is based on a reflective embossed structure, develops an optically variable effect when the foil security element is tilted, and is designated as embossed structural motif; - the foil security element region, when the back side of the paper substrate is viewed in reflected light, is discernible in the form of a light-dark effect, wherein the embossed structural motif is perceptible as light against a dark background, more particularly in multitonal form or in the form of a greyscale image; - the foil security element region, when the back side of the paper substrate is viewed in transmitted light, is discernible only in a unitary grey tone, so that the viewer, on changing the viewing of the back side of the paper substrate from reflected-light viewing to transmitted-light viewing, perceives a disappearance of the embossed structural motif perceptible as light against a dark background. - the front side of the paper substrate, in a region designated as foil security element region, bears a foil security element (3, 10) having a front side and a back side, wherein the front side of the foil security element has a motif which is based on a reflective embossed structure, develops an optically variable effect when the foil security element is tilted, and is designated as embossed structural motif; - the foil security element region, when the back side of the paper substrate is viewed in reflected light, is discernible in the form of a light-dark effect, wherein the embossed structural motif is perceptible as light against a dark background, more particularly in multitonal form or in the form of a greyscale image; - the foil security element region, when the back side of the paper substrate is viewed in transmitted light, is discernible only in a unitary grey tone, so that the viewer, on changing the viewing of the back side of the paper substrate from reflected-light viewing to transmitted-light viewing, perceives a disappearance of the embossed structural motif perceptible as light against a dark background.
A power generation system, comprising: at least one thermal energy accumulation vessel containing a gas; a potential energy generation system, including at least one battery vessel connected to the at least one thermal energy accumulation vessel and having a variable volume, wherein the potential energy generation system generates and stores potential energy via expansion of the volume of the at least one battery vessel when a quantity of the gas moves from the at least one thermal energy accumulation vessel to the at least one battery vessel after increasing in temperature while in the at least one thermal energy accumulation vessel; a thermal energy dissipation vessel connected to the at least one battery vessel; and an energy conversion system coupled to the potential energy generation system, wherein the energy conversion system converts potential energy stored by the potential energy generation system into electrical energy when a quantity of the gas is evacuated from the at least one battery vessel to the thermal energy dissipation vessel after expansion of the volume of the at least one battery vessel. at least one thermal energy accumulation vessel containing a gas; a potential energy generation system, including at least one battery vessel connected to the at least one thermal energy accumulation vessel and having a variable volume, wherein the potential energy generation system generates and stores potential energy via expansion of the volume of the at least one battery vessel when a quantity of the gas moves from the at least one thermal energy accumulation vessel to the at least one battery vessel after increasing in temperature while in the at least one thermal energy accumulation vessel; a thermal energy dissipation vessel connected to the at least one battery vessel; and an energy conversion system coupled to the potential energy generation system, wherein the energy conversion system converts potential energy stored by the potential energy generation system into electrical energy when a quantity of the gas is evacuated from the at least one battery vessel to the thermal energy dissipation vessel after expansion of the volume of the at least one battery vessel.
An optical device comprising a micro-optical system and a retainer, wherein the micro-optical system is attached to the retainer so as to be aligned relative to a surface thereof, characterized in that the retainer has a round, tapered recess and the micro-optical system is attached on a spherical cap and the spherical cap is attached to the retainer, wherein the spherical cap at least partially protrudes into the recess and rests directly on a partial surface of the recess along a resting line on the partial surface or an edge in the recess, wherein the spherical cap is attached to the retainer in the recess, but is not attached where it rests, wherein the spherical cap is attached by means of an adhesive at a gap formed between the recess and the spherical cap above the resting line or the edge in the recess on which the spherical cap rests.
A soil resistant security paper substrate for banknotes made from a stock comprising a suspension of paper fibres, and microfibrillated cellulose, the microfibrillated cellulose bridging pore spaces formed by and in between the paper fibres at at least a surface of the substrate to provide soil resistance, characterised in that the microfibrillated cellulose is produced from cotton pulp and in that the length of fibres in the microfibrillated cellulose lies in the range 1 to 100μm and the width of said fibres lies in the range of 2 to 50nm.
A tensioning device for an overspeed governor rope of an elevator with a spring tension mechanism for tensioning a deflection pulley for the overspeed governor rope, whereas the spring tension mechanism is composed of at least two guide columns onto each of which a respective spring element is threaded and which are secured by a main frame (3a, 3a, 3b, 3b) in such a way that their first guide column section lies entirely within the region encompassed by the main frame (3a, 3b) characterised in that, their second guide column section is situated above the main frame (3a, 3b) outside the region encompassed by it, and of a carriage (4a, 4b, 5, 6) with a deflection pulley mounted on it in rotatable fashion, which carriage is supported in sliding fashion on the guide columns by means of two yokes (5, 6); the lower yoke of the slider travels on the first guide column section and constitutes an abutment for the spring elements, which are supported at their other end against the upper horizontal section of the main frame (3a, 3b); and the upper yoke of the carriage (4a, 4b, 5, 6) travels on the second guide column section and preferably comes to a stop against an adjustable spring travel limiter.
A hybrid gas turbine engine system (201; 301) of a hybrid electric aircraft (200; 300), the hybrid gas turbine engine system comprising: a gas turbine engine; an electric motor operable to perform an electric taxiing of the hybrid electric aircraft; and a controller operable to: prevent fuel flow to the gas turbine engine during at least a portion of the electric taxiing; monitor for a powered warm-up request during the electric taxiing; initiate a powered warm-up state of the gas turbine engine based on detecting the powered warm-up request, wherein the powered warm-up state adds heat to one or more components of the gas turbine engine prior to transitioning to a takeoff power state; and transition the gas turbine engine from the powered warm-up state to the takeoff power state after reaching a target temperature of the one or more components in the powered warm-up state; characterised in that the powered warm-up state comprises enabling one or more electric heaters (262, 264), and/or the controller is configured to command a combination of vane positions and power setting of the gas turbine engine that reduces a compressor efficiency of the gas turbine engine to increase temperature at or below idle thrust in the powered warm-up state. a gas turbine engine; an electric motor operable to perform an electric taxiing of the hybrid electric aircraft; and a controller operable to: prevent fuel flow to the gas turbine engine during at least a portion of the electric taxiing; monitor for a powered warm-up request during the electric taxiing; initiate a powered warm-up state of the gas turbine engine based on detecting the powered warm-up request, wherein the powered warm-up state adds heat to one or more components of the gas turbine engine prior to transitioning to a takeoff power state; and transition the gas turbine engine from the powered warm-up state to the takeoff power state after reaching a target temperature of the one or more components in the powered warm-up state; characterised in that prevent fuel flow to the gas turbine engine during at least a portion of the electric taxiing; monitor for a powered warm-up request during the electric taxiing; initiate a powered warm-up state of the gas turbine engine based on detecting the powered warm-up request, wherein the powered warm-up state adds heat to one or more components of the gas turbine engine prior to transitioning to a takeoff power state; and transition the gas turbine engine from the powered warm-up state to the takeoff power state after reaching a target temperature of the one or more components in the powered warm-up state; characterised in that the powered warm-up state comprises enabling one or more electric heaters (262, 264), and/or the controller is configured to command a combination of vane positions and power setting of the gas turbine engine that reduces a compressor efficiency of the gas turbine engine to increase temperature at or below idle thrust in the powered warm-up state.
A wheel assembly for using in landing gear of an aircraft, comprising: a wheel structure configured to receive at least a portion of a tire; and a structure defining an alignment hole usable to align a hubcap relative to the structure and defining a pocket circumferentially aligned with the alignment hole, wherein the structure includes a hubcap attachment flange characterized in that the pocket serves to divert load, thereby reducing stresses exerted on the hubcap attachment flange at locations adjacent the alignment hole. a wheel structure configured to receive at least a portion of a tire; and a structure defining an alignment hole usable to align a hubcap relative to the structure and defining a pocket circumferentially aligned with the alignment hole, wherein the structure includes a hubcap attachment flange characterized in that the pocket serves to divert load, thereby reducing stresses exerted on the hubcap attachment flange at locations adjacent the alignment hole.
A humanized antibody or antigen binding fragment thereof, that binds IL-25, wherein the antibody or antigen binding fragment thereof comprises: a) an antibody VL domain comprising a CDR1 having the amino acid sequence SASQGISNYLN (SEQ ID NO:6), a CDR2 having the amino acid sequence YTSSLHS (SEQ ID NO:7) and a CDR3 having the amino acid sequence QQYLAFPYTF (SEQ ID NO:8); and b) an antibody VH domain comprising a CDR1 having the amino acid sequence GYTMN (SEQ ID NO:10), a CDR2 having the amino acid sequence LINPYNGGTSYNQNFKG (SEQ ID NO:11) and a CDR3 having the amino acid sequence EDYDGYLYFAMDY (SEQ ID NO:12), wherein the antibody or antigen binding fragment thereof has a binding affinity for IL-25 that is less than or equal to 53pM as determined in a Biacore assay. a) an antibody VL domain comprising a CDR1 having the amino acid sequence SASQGISNYLN (SEQ ID NO:6), a CDR2 having the amino acid sequence YTSSLHS (SEQ ID NO:7) and a CDR3 having the amino acid sequence QQYLAFPYTF (SEQ ID NO:8); and b) an antibody VH domain comprising a CDR1 having the amino acid sequence GYTMN (SEQ ID NO:10), a CDR2 having the amino acid sequence LINPYNGGTSYNQNFKG (SEQ ID NO:11) and a CDR3 having the amino acid sequence EDYDGYLYFAMDY (SEQ ID NO:12),
A method of controlling a rotating three-phase motor having three interconnected motor coils (L1, L2, L3), each corresponding to one of three phases and each supplied with current through at least one of a plurality of switching circuit components, comprising: - generating in synchronism with the rotation of the motor a variable duty cycle pulse-width modulated signal (70, 72, 74) for each of the switching circuit components; - using the generated variable duty cycle pulse-width modulated signals (70, 72, 74) to control switching circuit components to selectively place pairs of motor coils (L1, L2, L3) in current conducting states and to develop an associated varying voltage for each of the phases; - monitoring respective logical on-off states of the pulse-width modulated signals (70, 72, 74) to identify one phase that exhibits a voltage in between the voltages of the other two phases; and for the identified one phase, generating said variable duty cycle pulse-width modulated signal so that when the switching circuit components of the other two phases are concurrently switched on, the respective switching circuit component of the identified one phase is not switched on. - generating in synchronism with the rotation of the motor a variable duty cycle pulse-width modulated signal (70, 72, 74) for each of the switching circuit components; - using the generated variable duty cycle pulse-width modulated signals (70, 72, 74) to control switching circuit components to selectively place pairs of motor coils (L1, L2, L3) in current conducting states and to develop an associated varying voltage for each of the phases; - monitoring respective logical on-off states of the pulse-width modulated signals (70, 72, 74) to identify one phase that exhibits a voltage in between the voltages of the other two phases; and
A method of adaptively adjusting a receiver depending on an interferer, the method comprising configuring the receiver such that when a signal containing the interferer is received, the receiver: determines a signal metric of the signal over a predetermined time period; determines a type of interferer, including whether the interferer is continuous or discontinuous, using the signal metric; selects, dependent on the signal metric and the type of interferer, a set of parameters from a table of parameters; and adjusts, dependent on the set of parameters, characteristics of the modules in the receiver that are used to generate an off-channel flag that provides an indication to other modules within the receiver of the presence of the interferer. determines a signal metric of the signal over a predetermined time period; determines a type of interferer, including whether the interferer is continuous or discontinuous, using the signal metric; selects, dependent on the signal metric and the type of interferer, a set of parameters from a table of parameters; and adjusts, dependent on the set of parameters, characteristics of the modules in the receiver that are used to generate an off-channel flag that provides an indication to other modules within the receiver of the presence of the interferer.