mhurhangee/patent-ind-claim-en huggingface dataset:
Pressure controlled multistage cooling plant having at least a high stage comprising at least a set of first compressors , a set of first condensers , at least a first receiver means and a first duct of an intermediate heat exchanger means mutually connected to form the high stage refrigeration circuit; said plant being further provided with at least a low stage comprising at least a set of second compressors , a second duct of the intermediate heat exchanger means , at least a second receiver means , a set of low stage user apparatus mutually connected to form the low stage refrigeration circuit, a control means for controlling various elements of the plant, feeding means to feed the intermediate heat exchanger means with a cooling fluid; said plant comprises pressure sensor means assigned to detect the pressure of the fluid of the low stage and connected to the control means configured to activate the feeding means when said pressure of the fluid of the idle low stage reaches or exceeds a predetermined threshold value; said feeding means are activated and connected to a duct of the intermediate heat exchanger means to feed in said duct a cooling fluid for cooling the fluid of the low stage in a condition of activation of said feeding means ; said duct of the intermediate heat exchanger means that can be connected to the feeding means consists of the first duct of the intermediate heat exchanger means and the cooling fluid feed by the feeding means consists of the fluid of the high stage ; said plant is characterized in that the feeding means comprising at least a safety compressor , at least one safety condenser , a first cut-off valve and a first expansion means ; the inlet of the safety compressor is connected to a first inlet of the first duct of the intermediate heat exchanger means and the outlet of said safety compressor is connected to an inlet of the at least one safety condenser whose outlet is connected to the inlet of the first receiver means whose outlet is connectable, by means of the first cut-off valve and of the first expansion means operated by the control means, to the second inlet of the first duct , where said first duct , safety compressor , safety condenser , first receiver means , first cut-off valve and first expansion means , in the condition of activation operated by the control means, carry out the circuit of the feeding means for cooling the fluid of the low stage .
A roof window arrangement comprising a roof window with a stationary frame and a sash carrying a pane , in which the sash includes at least a top member defining a width of the sash, two mutually parallel side members defining a length of the sash, and a bottom member parallel to the top member , and is connected to the stationary frame by means of a set of hinges and configured to assume at least an open position and a closed position by rotation about a hinge axis substantially parallel to the top member of the sash , a manual operating assembly configured to assist in operation of the sash between the open and the closed positions, said manual operating assembly including a handle portion located at the top member of the sash and having a longitudinal extension substantially in parallel with the top member of the sash , and an electrical operating assembly configured to assist in operation of the sash between the open and the closed position, characterised in that the manual operating assembly is provided with an integrated control unit configured to cooperate with the electrical operating assembly . a roof window with a stationary frame and a sash carrying a pane , in which the sash includes at least a top member defining a width of the sash, two mutually parallel side members defining a length of the sash, and a bottom member parallel to the top member , and is connected to the stationary frame by means of a set of hinges and configured to assume at least an open position and a closed position by rotation about a hinge axis substantially parallel to the top member of the sash , a manual operating assembly configured to assist in operation of the sash between the open and the closed positions, said manual operating assembly including a handle portion located at the top member of the sash and having a longitudinal extension substantially in parallel with the top member of the sash , and an electrical operating assembly configured to assist in operation of the sash between the open and the closed position, characterised in that the manual operating assembly is provided with an integrated control unit configured to cooperate with the electrical operating assembly .
A buoy device for a marine hose (H) or the like; wherein the buoy device is configured to at least partly enclose said hose (H); wherein the buoy device comprises a shell unit and a bladder unit which is arranged within the shell unit and which is inflatable and/or deflatable by means of a fluid in order to adjust the buoyancy of the buoy device during use; characterised in that the bladder unit comprises a first bladder element and a second bladder element ; and wherein the first bladder element is arranged within a first shell element and the second bladder element is arranged within a second shell element .
A service data transmission method, comprising: determining, by a first device, a switching request, wherein the switching request comprises first slot configuration information and second slot configuration information, the switching request is used to request to switch a slot configuration of a flexible Ethernet connection instance from a configuration indicated by the first slot configuration information to a configuration indicated by the second slot configuration information, and a slot division quantity indicated by the first slot configuration information is different from a slot division quantity indicated by the second slot configuration information; and sending, by the first device, the switching request to a second device, wherein the first device is connected to the second device by using a flexible Ethernet group comprising at least one flexible Ethernet connection instance; the method is further characterized by that the first slot configuration information comprises a first slot division quantity indication and a client signal identifier of each of Q slots obtained through division based on the first slot division quantity indication; the second slot configuration information comprises a second slot division quantity indication and a client signal identifier of each of P slots obtained through division based on the second slot division quantity indication; and Q and P are integers greater than 0. determining, by a first device, a switching request, wherein the switching request comprises first slot configuration information and second slot configuration information, the switching request is used to request to switch a slot configuration of a flexible Ethernet connection instance from a configuration indicated by the first slot configuration information to a configuration indicated by the second slot configuration information, and a slot division quantity indicated by the first slot configuration information is different from a slot division quantity indicated by the second slot configuration information; and sending, by the first device, the switching request to a second device, wherein the first device is connected to the second device by using a flexible Ethernet group comprising at least one flexible Ethernet connection instance; the method is further characterized by that the first slot configuration information comprises a first slot division quantity indication and a client signal identifier of each of Q slots obtained through division based on the first slot division quantity indication; the second slot configuration information comprises a second slot division quantity indication and a client signal identifier of each of P slots obtained through division based on the second slot division quantity indication; and Q and P are integers greater than 0.
An aerosol-generating device comprising: an elongate housing having a first end , a second end , and a longitudinal axis extending between the first end and the second end; a cavity configured for insertion of an aerosol-generating article into the cavity along a first direction, wherein the first direction is substantially perpendicular to the longitudinal axis of the elongate housing; a first aperture positioned at a first end of the cavity and extending through a portion of the elongate housing, wherein the aerosol-generating device is configured for insertion of an aerosol-generating article into the cavity through the first aperture; a second aperture positioned at a second end of the cavity and extending through a portion of the elongate housing, wherein the aerosol-generating device is configured for removal of an aerosol-generating article from the cavity through at least one of the first aperture and the second aperture; an electrical power supply positioned within the housing; at least one electrical heater ; and a controller positioned within the housing and configured to control a supply of electrical power from the electrical power supply to the at least one electrical heater when an aerosol-generating article is received within the cavity. an elongate housing having a first end , a second end , and a longitudinal axis extending between the first end and the second end; a cavity configured for insertion of an aerosol-generating article into the cavity along a first direction, wherein the first direction is substantially perpendicular to the longitudinal axis of the elongate housing; a first aperture positioned at a first end of the cavity and extending through a portion of the elongate housing, wherein the aerosol-generating device is configured for insertion of an aerosol-generating article into the cavity through the first aperture; a second aperture positioned at a second end of the cavity and extending through a portion of the elongate housing, wherein the aerosol-generating device is configured for removal of an aerosol-generating article from the cavity through at least one of the first aperture and the second aperture; an electrical power supply positioned within the housing; at least one electrical heater ; and a controller positioned within the housing and configured to control a supply of electrical power from the electrical power supply to the at least one electrical heater when an aerosol-generating article is received within the cavity.
An image forming apparatus , comprising: a fixing device comprising a plurality of heating elements arranged in a main scanning direction of the image forming apparatus , a band-shaped thin film configured to slide on an outer surface of each of the heating elements while being in contact with the heating elements , and a rotatable member configured to press against a surface of the thin film to cause the thin film to rotate; an image reading unit of the fixing device; and a control unit configured to control: the fixing device to heat the plurality of heating elements when an inspection sheet is passed through the fixing device , the inspection sheet having plural images formed by using a developer that becomes decolored when subject to heating, each of the images having an image density that differs in a sub-scanning direction of the image forming apparatus ; and the image reading unit to read an image of the plural images of the heated inspection sheet characterized in that the control unit determines an operative state of each of the plurality of heating elements based on the read image of the plural images. a fixing device comprising a plurality of heating elements arranged in a main scanning direction of the image forming apparatus , a band-shaped thin film configured to slide on an outer surface of each of the heating elements while being in contact with the heating elements , and a rotatable member configured to press against a surface of the thin film to cause the thin film to rotate; an image reading unit of the fixing device; and a control unit configured to control: the fixing device to heat the plurality of heating elements when an inspection sheet is passed through the fixing device , the inspection sheet having plural images formed by using a developer that becomes decolored when subject to heating, each of the images having an image density that differs in a sub-scanning direction of the image forming apparatus ; and the image reading unit to read an image of the plural images of the heated inspection sheet characterized in that the control unit determines an operative state of each of the plurality of heating elements based on the read image of the plural images. the fixing device to heat the plurality of heating elements when an inspection sheet is passed through the fixing device , the inspection sheet having plural images formed by using a developer that becomes decolored when subject to heating, each of the images having an image density that differs in a sub-scanning direction of the image forming apparatus ; and the image reading unit to read an image of the plural images of the heated inspection sheet characterized in that the control unit determines an operative state of each of the plurality of heating elements based on the read image of the plural images.
A peptide able to bind multiple sclerosis auto-antibodies consisting of an amino acid sequence having at least 90 % identity with DDSKVFKEGS (SEQ ID No. 157).
A closure system for a receptacle, comprising: - a neck element intended to be fastened on the receptacle, the neck element comprising a neck portion provided with a retaining collar which is flexible, - a closure cap intended to be screwed on the neck portion , the closure cap including a closure wall and a fastening skirt , and - a tamper-proof ring connected to the fastening skirt by a plurality of frangible elements , the tamper-proof ring comprising at least one flexible retaining element the neck portion and the tamper-proof ring being configured such that, when the closure cap is fastened on the neck portion and at least until a breakage of the frangible elements , the retaining collar defines an annular hooking housing , and the at least one flexible retaining element is configured to be at least partially received and be hooked into the annular hooking housing , characterized in that the retaining collar is configured to extend at least partially between the fastening skirt and the tamper-proof ring during the first screwing back of the closure cap on the neck portion after breakage of the frangible elements . - a neck element intended to be fastened on the receptacle, the neck element comprising a neck portion provided with a retaining collar which is flexible, - a closure cap intended to be screwed on the neck portion , the closure cap including a closure wall and a fastening skirt , and - a tamper-proof ring connected to the fastening skirt by a plurality of frangible elements , the tamper-proof ring comprising at least one flexible retaining element
A drone comprising: a lift mechanism configured to lift and propel the drone; an error detection circuit configured to: detect an error in operation of the drone, the error indicating a failure of the drone, and upon detecting the error, send a trigger event; a parachute securely attached to the drone and configured to slow a decent of the drone when deployed; a parachute deployment mechanism configured to release the parachute in response to the trigger event, or in response to another trigger event generated in response to a command from a base unit operated by a remote user ; and a cut-off circuit configured to disable the lift mechanism in response to the trigger event, the cut-off circuit comprising one or more multiplexers configured to block a throttle signal from a flight controller to the lift mechanism and substitute the throttle signal with a zero-throttle signal. a lift mechanism configured to lift and propel the drone; an error detection circuit configured to: detect an error in operation of the drone, the error indicating a failure of the drone, and upon detecting the error, send a trigger event; detect an error in operation of the drone, the error indicating a failure of the drone, and upon detecting the error, send a trigger event; a parachute securely attached to the drone and configured to slow a decent of the drone when deployed; a parachute deployment mechanism configured to release the parachute in response to the trigger event, or in response to another trigger event generated in response to a command from a base unit operated by a remote user ; and a cut-off circuit configured to disable the lift mechanism in response to the trigger event, the cut-off circuit comprising one or more multiplexers configured to block a throttle signal from a flight controller to the lift mechanism and substitute the throttle signal with a zero-throttle signal.
A heart valve prosthesis comprising: a tubular stent having a compressed configuration for delivery within a vasculature and a deployed configuration for deployment within a native heart valve; a prosthetic valve component disposed within and secured to the stent; and at least two positioning elements coupled to an outflow end of the stent and configured to position and anchor the prosthesis within the native heart valve, each positioning element including an outer generally U-shaped or V-shaped support arm and an inner generally V-shaped or U-shaped support arm configured to both extend downstream from the outflow end of the stent when the stent is in the compressed configuration, wherein during deployment of the prosthesis each support arm is configured to bend radially outward and then towards an outer surface of the stent such that it translates more than ninety degrees from the compressed configuration to extend upstream from the outflow end of the stent when the stent is in the deployed configuration, characterised in that each outer support arm is connected to each inner support arm by two curved legs , wherein first ends of the legs extend from a peak of the inner support arm and the curved legs flare away from each other such that second ends of the legs extend from opposing sides of a peak of the outer support arm. a tubular stent having a compressed configuration for delivery within a vasculature and a deployed configuration for deployment within a native heart valve; a prosthetic valve component disposed within and secured to the stent; and at least two positioning elements coupled to an outflow end of the stent and configured to position and anchor the prosthesis within the native heart valve, each positioning element including an outer generally U-shaped or V-shaped support arm and an inner generally V-shaped or U-shaped support arm configured to both extend downstream from the outflow end of the stent when the stent is in the compressed configuration, wherein during deployment of the prosthesis each support arm is configured to bend radially outward and then towards an outer surface of the stent such that it translates more than ninety degrees from the compressed configuration to extend upstream from the outflow end of the stent when the stent is in the deployed configuration, characterised in that each outer support arm is connected to each inner support arm by two curved legs , wherein first ends of the legs extend from a peak of the inner support arm and the curved legs flare away from each other such that second ends of the legs extend from opposing sides of a peak of the outer support arm.
A method of making a landing gear assembly, comprising: forging a mounting interface portion comprising a base, and first and second ends that each extend upwardly from the base, wherein the first and second ends comprise first and second holes, respectively, that are aligned with one another and that accommodate coupling to an airframe to allow the landing gear assembly to be moved between a stowed position and a deployed position, wherein an open space extends between the first and second holes; joining each of a first curved sheet metal element and a second curved sheet metal element to the mounting interface portion to define an upper section of a thin-skin support member , wherein the first and second holes of the mounting interface portion are disposed beyond an upper end of the upper section of the thin-skin support member ; forging a mid-body support having a cylinder extending from the mid-body support ; joining a third curved sheet metal element and a fourth curved sheet metal element to each other as well as to the mid-body support , thereby defining a lower section of the thin-skin support member ; and joining the upper section of the thin-skin support member to the lower section of the thin-skin support member ; wherein the landing gear assembly comprises a strut assembly retained by the cylinder and coupled to an axle by an upper torsion link and a lower torsion link , the mid-body support including an interface proximate an opening end of the cylinder and configured for joining to the upper torsion link . forging a mounting interface portion comprising a base, and first and second ends that each extend upwardly from the base, wherein the first and second ends comprise first and second holes, respectively, that are aligned with one another and that accommodate coupling to an airframe to allow the landing gear assembly to be moved between a stowed position and a deployed position, wherein an open space extends between the first and second holes; joining each of a first curved sheet metal element and a second curved sheet metal element to the mounting interface portion to define an upper section of a thin-skin support member , wherein the first and second holes of the mounting interface portion are disposed beyond an upper end of the upper section of the thin-skin support member ; forging a mid-body support having a cylinder extending from the mid-body support ; joining a third curved sheet metal element and a fourth curved sheet metal element to each other as well as to the mid-body support , thereby defining a lower section of the thin-skin support member ; and joining the upper section of the thin-skin support member to the lower section of the thin-skin support member ; wherein the landing gear assembly comprises a strut assembly retained by the cylinder and coupled to an axle by an upper torsion link and a lower torsion link , the mid-body support including an interface proximate an opening end of the cylinder and configured for joining to the upper torsion link .
Burnishing tool with a burnishing element provided for machining on a workpiece and with a retaining plate for the burnishing element , wherein the contour on the operative end face of the burnishing element , viewed towards the burnishing line on the workpiece , is identical to its contour to be burnished and is at least partially convex in the direction transverse to the burnishing line , characterised in that the burnishing element is received in a groove in a receiving part which is received as an insert in the retaining plate .