mhurhangee/patent-ind-claim-en huggingface dataset:
A gimbal sensor platform positionable in a tool body having a longitudinal axis , the gimbal sensor platform comprising: an outer gimbal , the outer gimbal rotatably coupled to the tool body ; an outer angular positioning device coupled to the outer gimbal to rotate the outer gimbal relative to the tool body about an outer gimbal axis of rotation (X); an inner gimbal , the inner gimbal rotatably coupled to the outer gimbal ; an inner angular positioning device coupled to the inner gimbal to rotate the inner gimbal relative to the outer gimbal about an inner gimbal axis of rotation (Y); and a gyro coupled to the inner gimbal , characterised in that the gyro has a sensitive axis substantially orthogonal to the inner gimbal axis of rotation (Y). an outer gimbal , the outer gimbal rotatably coupled to the tool body ; an outer angular positioning device coupled to the outer gimbal to rotate the outer gimbal relative to the tool body about an outer gimbal axis of rotation (X); an inner gimbal , the inner gimbal rotatably coupled to the outer gimbal ; an inner angular positioning device coupled to the inner gimbal to rotate the inner gimbal relative to the outer gimbal about an inner gimbal axis of rotation (Y); and a gyro coupled to the inner gimbal , characterised in that the gyro has a sensitive axis substantially orthogonal to the inner gimbal axis of rotation (Y).
Fixing device of a swing arm of a tilting vehicle , having at least one first fixing means indirectly or directly fixed to a supporting structure of the tilting vehicle , having at least one second fixing means indirectly or directly fixed to a wheel suspension which is movable relative to the supporting structure and comprises a spring travel and from an extended functional position (F1), in which a distance of a wheel unit fixed to the wheel suspension from a seat unit fixed to the supporting structure is at a maximum, into a compressed functional position (F2), in which the distance between wheel unit and seat unit is reduced in relation to the extended functional position (F1), and having at least one actuator by way of which the first fixing means and/or the second fixing means are/is transferable from a release position, in which the two fixing means are arranged so as to be movable relative to one another and without contact, into a fixing position, in which the two fixing means are fixed to one another and fix the wheel suspension and the supporting structure against movement relative to one another, characterized in that the wheel suspension is fixed in a manner mounted on the supporting structure so as to be rotatable about an axis of rotation , and in that the first fixing means comprises at least two bolt-like holding elements which, in relation to the vertical axis of the tilting vehicle , are arranged above and below the axis rotation , wherein the second fixing means is formed by a surface of the wheel suspension against which the bolt-like holding elements of the first fixing means abut in the locking position.
A cooling system comprising: a main refrigerant circuit , comprising: a compressor ; a heat rejection heat exchanger ; one of an expander and an expansion device ; at least one evaporator configured to be coupled to a thermal load; and a suction accumulator ; a charge management circuit having a charge management receiver configured in parallel with the compressor and the heat rejection heat exchanger , a first receiver valve installed on a line connecting an exit of the heat rejection heat exchanger and a first port of the charge management receiver , and a second receiver valve installed on a line connecting a second port of the charge management receiver and a suction side of the compressor ; a controller configured to accumulate and discharge reserve refrigerant to and from the charge management receiver to provide flexibility in system operation as refrigerant in the main refrigerant circuit operates in sub-critical, trans-critical, and super-critical modes of operation, wherein the controller is configured to control an amount of reserve refrigerant in the charge management receiver based on a discharge pressure of the compressor by means of the first and a second receiver valves ; and a hot gas bypass line comprising a hot gas bypass valve connecting a discharge side of the compressor with the low pressure side of the compressor . a main refrigerant circuit , comprising: a compressor ; a heat rejection heat exchanger ; one of an expander and an expansion device ; at least one evaporator configured to be coupled to a thermal a compressor ; a heat rejection heat exchanger ; one of an expander and an expansion device ; at least one evaporator configured to be coupled to a thermal load; and a suction accumulator ; a charge management circuit having a charge management receiver configured in parallel with the compressor and the heat rejection heat exchanger , a first receiver valve installed on a line connecting an exit of the heat rejection heat exchanger and a first port of the charge management receiver , and a second receiver valve installed on a line connecting a second port of the charge management receiver and a suction side of the compressor ; a controller configured to accumulate and discharge reserve refrigerant to and from the charge management receiver to provide flexibility in system operation as refrigerant in the main refrigerant circuit operates in sub-critical, trans-critical, and super-critical modes of operation, wherein the controller is configured to control an amount of reserve refrigerant in the charge management receiver based on a discharge pressure of the compressor by means of the first and a second receiver valves ; and a hot gas bypass line comprising a hot gas bypass valve connecting a discharge side of the compressor with the low pressure side of the compressor .
A method for obtaining a capacitive feedback signal of a capacitive feedback micro torsion mirror, comprising: S1: using pulse signals as driving signals to drive a capacitive feedback micro torsion mirror to vibrate; ensuring free torsion of the micro torsion mirror for at least 0.5 cycles during the interval of two sets of adjacent driving pulses; S2: extracting a capacitive feedback signal of the capacitive feedback micro torsion mirror, and converting the capacitive feedback signal into a voltage signal; S3: amplifying the voltage signal obtained in S2; and S4: extracting the amplified voltage signal as a real capacitive feedback signal during the interval of two sets of adjacent driving pulses, wherein, the pulse signals have pulses at a low level and intervals at a fixed high level. S1: using pulse signals as driving signals to drive a capacitive feedback micro torsion mirror to vibrate; ensuring free torsion of the micro torsion mirror for at least 0.5 cycles during the interval of two sets of adjacent driving pulses; S2: extracting a capacitive feedback signal of the capacitive feedback micro torsion mirror, and converting the capacitive feedback signal into a voltage signal; S3: amplifying the voltage signal obtained in S2; and S4: extracting the amplified voltage signal as a real capacitive feedback signal during the interval of two sets of adjacent driving pulses, wherein, the pulse signals have pulses at a low level and intervals at a fixed high level.
Pneumatic vehicle tyre of a radial design with a footprint that is determined with a tyre mounted on a standard rim under a load of 70% of the maximum load-bearing capacity and an internal pressure of 85% of the standard pressure in accordance with E.T.R.T.O. standards and with a profiled tread with a tread shoulder outside each of the side footprint edges (k) of the footprint, wherein the tread consists of at least one rubber material and wherein the tread contains inserts which run around in the circumferential direction, reach as far as the tread periphery and are made of a rubber material that is stiffer than the other rubber material of the tread , characterized in that an insert made of the stiffer rubber material is situated outside the footprint on each side, wherein the rubber material of the inserts has a dynamic storage modulus E' mean which is 4 MPa to 8 MPa higher than that of the rubber material or the rubber materials in the rest of the tread , wherein E' mean is determined in accordance with DIN 53513 and E' is measured under 0.15% elongation and under 8% elongation, so that E' mean = [E'(0.15%) +E'(8%)]/2, and wherein the rubber material of the inserts has a Shore A hardness, determined in accordance with DIN ISO 7697-1, which is 5 Shore A to 15 Shore A, in particular 8 Shore A to 12 Shore A, higher than that of the rubber material or the rubber materials in the rest of the tread . an insert made of the stiffer rubber material is situated outside the footprint on each side, wherein the rubber material of the inserts has a dynamic storage modulus E' mean which is 4 MPa to 8 MPa higher than that of the rubber material or the rubber materials in the rest of the tread , wherein E' mean is determined in accordance with DIN 53513 and E' is measured under 0.15% elongation and under 8% elongation, so that E' mean = [E'(0.15%) +E'(8%)]/2, and wherein the rubber material of the inserts has a Shore A hardness, determined in accordance with DIN ISO 7697-1, which is 5 Shore A to 15 Shore A, in particular 8 Shore A to 12 Shore A, higher than that of the rubber material or the rubber materials in the rest of the tread .
A logging unit for logging events by causing entries to be stored in a store , wherein each of said entries comprises an n- bit timestamp field and a payload, the logging unit comprising control logic configured to: determine a timestamp for an event which is to be logged, wherein the determined timestamp comprises N bits, where N > n; determine whether one or more of the N - n most significant bits of the determined timestamp are different to a corresponding one or more of the N - n most significant bits of a timestamp for a preceding event for which a preceding event entry is stored in the store; cause a timing entry which includes a set of k bits of the determined timestamp to be stored in the store in response to determining that one or more of the N - n most significant bits of the determined timestamp are different to a corresponding one or more of the N - n most significant bits of a timestamp for a preceding event for which a preceding entry is stored in the store, said k bits being the k next least significant bits of the determined timestamp other than the n least significant bits of the determined timestamp; and cause an entry for the event to be stored in the store, wherein the n least significant bits of the determined timestamp are included in the timestamp field of the entry for the event. determine a timestamp for an event which is to be logged, wherein the determined timestamp comprises N bits, where N > n; determine whether one or more of the N - n most significant bits of the determined timestamp are different to a corresponding one or more of the N - n most significant bits of a timestamp for a preceding event for which a preceding event entry is stored in the store; cause a timing entry which includes a set of k bits of the determined timestamp to be stored in the store in response to determining that one or more of the N - n most significant bits of the determined timestamp are different to a corresponding one or more of the N - n most significant bits of a timestamp for a preceding event for which a preceding entry is stored in the store, said k bits being the k next least significant bits of the determined timestamp other than the n least significant bits of the determined timestamp; and cause an entry for the event to be stored in the store, wherein the n least significant bits of the determined timestamp are included in the timestamp field of the entry for the event.
A column for thermal treatment of fluid mixtures, having a cylindrical, vertical column body which forms a column cavity , a plurality of trays mounted with mutual vertical spacing in the column cavity , and a support construction which supports at least one of the trays in the vertical direction, where the support construction has a plurality of orifices (12; 18) which allow horizontal mass transfer through the support construction, where in a vertical section through the support construction the orifices (12; 18) take up a proportion of the sectional area of the support construction within a range from 30% to 90%, wherein the orifices are arranged in at least two horizontal rows with mutual vertical spacing, and at least two orifices (12; 18) are arranged one on top of another with vertical spacing and the support construction rests on a tray and supports a tray arranged above from beneath, where, in at least a portion of the orifices (12; 18), the lower boundary edge of the orifice (12; 18) is formed by the tray on which the support construction rests, or an element is formed, such that this portion of the orifices (12; 18) allows essentially unhindered horizontal mass transfer along the plane of this tray through the orifices (12; 18). a cylindrical, vertical column body which forms a column cavity , a plurality of trays mounted with mutual vertical spacing in the column cavity , and a support construction which supports at least one of the trays in the vertical direction, where
A sun-sky imitating lighting system for forming a room edge of a room, the lighting system comprising: an enlarged sky-perception providing unit with a light transparent panel and a mirror unit with a reflective face forming an inner edge , and a light source configured to emit a direct light beam through the light transparent panel onto the mirror unit such that the transmitted portion of the light beam is reflected completely by the reflective face , thereby creating a reflected direct light beam for imitating a sun beam, wherein the light transparent panel is configured to emit diffused light from a front face , the mirror unit comprises a reflective face positioned next to the light transparent panel to form the inner edge together with the light transparent panel , and the size of the light transparent panel is smaller than the size of the mirror unit . an enlarged sky-perception providing unit with a light transparent panel and a mirror unit with a reflective face forming an inner edge , and a light source configured to emit a direct light beam through the light transparent panel onto the mirror unit such that the transmitted portion of the light beam is reflected completely by the reflective face , thereby creating a reflected direct light beam for imitating a sun beam, wherein the light transparent panel is configured to emit diffused light from a front face , the mirror unit comprises a reflective face positioned next to the light transparent panel to form the inner edge together with the light transparent panel , and the size of the light transparent panel is smaller than the size of the mirror unit .
A negative pressure wound therapy (NPWT) dressing comprising a backing layer , wherein said backing layer comprises a thermoplastic elastomer, preferably a thermoplastic polyurethane, an adhesive skin contact layer and an absorbent structure arranged between said backing layer and said adhesive skin contact layer ; said adhesive skin contact layer being configured to detachably adhere the dressing to a dermal surface, wherein said backing layer and said adhesive skin contact layer are configured to extend beyond the periphery of the absorbent structure to form a border portion along the contour of said absorbent structure , wherein said adhesive skin contact layer comprises a plurality of apertures in the area underlying said absorbent structure , but is void of apertures in the area forming said border portion , wherein said backing layer comprises a coupling member comprising a tubing configured to connect the dressing to a negative pressure source and to a remote fluid collection means, characterized in that said backing layer has a moisture vapor transmission rate (MVTR) in the range of from 500 to 3500 g/m2/24h, preferably in the range of from 600 to 2700 g/m2/24h, as measured by NWSP070.4R0 , and in that said tubing comprises a fluid conduit configured to remove fluid from said dressing and an air conduit configured to supply air to said fluid conduit and/or said dressing .
Method for assisting in the piloting of a propeller-driven rotorcraft , said propeller-driven rotorcraft having a propulsion system connected by a mechanical system to a rotary wing and to least one propeller , said method comprising the following steps: - displaying, at the request of a computer and on a display , a minimum power marker and a maximum power marker on a first scale , said first scale being a representation of power consumed by said at least one propeller , the minimum power marker being a representation of a minimum power (PMIN) that can be consumed by said at least one propeller , the maximum power marker being a representation of a maximum power (PMAX) that can be consumed by said at least one propeller - displaying, at the request of the computer and on the display , a second scale graduated in forward speed of the propeller-driven rotorcraft , - displaying, at the request of the computer and on the display , an index comprising a power segment representing a current power (PCUR) consumed by said at least one propeller , said index comprising a speed segment indicating a current forward speed (VCUR) on said second scale , said index and said first scale being movable relative to each other, said index and said second scale being movable relative to one another - displaying, on the display and at the request of said computer, a zero-thrust marker carrying a zero forward thrust applied by said at least one propeller . - displaying, at the request of a computer and on a display , a minimum power marker and a maximum power marker on a first scale , said first scale being a representation of power consumed by said at least one propeller , the minimum power marker being a representation of a minimum power (PMIN) that can be consumed by said at least one propeller , the maximum power marker being a representation of a maximum power (PMAX) that can be consumed by said at least one propeller - displaying, at the request of the computer and on the display , a second scale graduated in forward speed of the propeller-driven rotorcraft , - displaying, at the request of the computer and on the display , an index comprising a power segment representing a current power (PCUR) consumed by said at least one propeller , said index comprising a speed segment indicating a current forward speed (VCUR) on said second scale , said index and said first scale being movable relative to each other, said index and said second scale being movable relative to one another - displaying, on the display and at the request of said computer, a zero-thrust marker carrying a zero forward thrust applied by said at least one propeller .
A method for receiving a visible light signal, comprising: controlling use of a camera as a light signal receiver to capture a group of continuous images covering an emitter, the emitter emits visible light signals, the group of continuous images includes an image of a visible light signal of the emitter and background image; obtaining a visible light signal emitted by the emitter from the group of continuous images, specifically comprises: dividing the group of continuous images into a plurality of images; comparing luminance variation with time of each region with a predetermined size of each of all images, selecting a region with continuous varying luminance, and determining that a visible light signal that comes from the emitter exists in the region; and analyzing and processing luminance changes of the region of all the images to obtain a visible light signal that comes from the emitter, outputting the image of a visible light signal of the emitter when the images captured by the camera include the visible light signal of the emitter; outputting the background images when the images captured by the camera do not include the visible light signal of the emitter; processing the visible light signal to restore original information. controlling use of a camera as a light signal receiver to capture a group of continuous images covering an emitter, the emitter emits visible light signals, the group of continuous images includes an image of a visible light signal of the emitter and background image; obtaining a visible light signal emitted by the emitter from the group of continuous images, specifically comprises: dividing the group of continuous images into a plurality of images; comparing luminance variation with time of each region with a predetermined size of each of all images, selecting a region with continuous varying luminance, and determining that a visible light signal that comes from the emitter exists in the region; and analyzing and processing luminance changes of the region of all the images to obtain a visible light signal that comes from the emitter, outputting the image of a visible light signal of the emitter when the images captured by the camera include the visible light signal of the emitter; outputting the background images when the images captured by the camera do not include the visible light signal of the emitter; processing the visible light signal to restore original information.
A method for fabricating a turbomachine component comprising a metal alloy, the method comprising: combining two or more elemental powders to form a powdered material ; forming a first metal alloy layer of the turbomachine component on a substrate , wherein forming the first metal alloy layer comprises: melting a first portion of the powdered material to a first molten material with a heat source (208; 412); mixing the first molten material with the heat source (208; 412); and cooling the first molten material to form the first metal alloy layer ; forming a second metal alloy layer of the turbomachine component on the first metal alloy layer (706; 130); and binding the first metal alloy layer with the second metal alloy layer to fabricate the turbomachine component , characterized by mixing the first molten material with the heat source (208; 412) comprises directing an energy beam of the heat source (208; 412) along the first portion of the powdered material in a substantially circular path and radially oscillating the energy beam . combining two or more elemental powders to form a powdered material ; forming a first metal alloy layer of the turbomachine component on a substrate , wherein forming the first metal alloy layer comprises: melting a first portion of the powdered material to a first molten material with a heat source (208; 412); mixing the first molten material with the heat source (208; 412); and cooling the first molten material to form the first metal alloy layer ; melting a first portion of the powdered material to a first molten material with a heat source (208; 412); mixing the first molten material with the heat source (208; 412); and cooling the first molten material to form the first metal alloy layer ; forming a second metal alloy layer of the turbomachine component on the first metal alloy layer (706; 130); and binding the first metal alloy layer with the second metal alloy layer to fabricate the turbomachine component , characterized by mixing the first molten material with the heat source (208; 412) comprises directing an energy beam of the heat source (208; 412) along the first portion of the powdered material in a substantially circular path and radially oscillating the energy beam .