mhurhangee/patent-ind-claim-en huggingface dataset:
A plastering strip for placement at a building transition between a first building component designed as window or door frame and a second building component, in particular a thermal insulation and/or a plaster layer, comprising: a base body (6, 12, 14; 28, 40) of plastics material; and a foam adhesive tape that is adhesive on both sides and on one side thereof is adhesively bonded to the base body (6, 12, 14; 28, 40) and on another side thereof is provided with an adhesive layer and is intended to be adhesively bonded to the first component of the building; characterised in that the double-sided foam adhesive tape has a base material whose behavior in the event of fire is in fire protection class B1 "not easily flammable" according to DIN standard 4102-1: 1998-05 or in fire protection class B2 "normal flammability" according to DIN standard 4102-1: 1998-05; wherein the double-sided foam adhesive tape comprises a closed-cell foam and a flame retardant. a base body (6, 12, 14; 28, 40) of plastics material; and a foam adhesive tape that is adhesive on both sides and on one side thereof is adhesively bonded to the base body (6, 12, 14; 28, 40) and on another side thereof is provided with an adhesive layer and is intended to be adhesively bonded to the first component of the building; characterised in that the double-sided foam adhesive tape has a base material whose behavior in the event of fire is in fire protection class B1 "not easily flammable" according to DIN standard 4102-1: 1998-05 or in fire protection class B2 "normal flammability" according to DIN standard 4102-1: 1998-05; wherein the double-sided foam adhesive tape comprises a closed-cell foam and a flame retardant.
A fuel tank communication system, comprising a first chimney configured to be secured to a first fuel bladder; a second chimney configured to be secured to a second fuel bladder; each chimney comprising a central opening ; a main body configured to be received by the central openings of each of the first and second chimneys ; a securement feature for maintaining cooperation between the first chimney and the main body ; and first and second locking systems for maintaining cooperation between the second chimney and the main body , wherein the main body comprises a rear shoulder , characterized in that the first and the second locking systems comprise independent locking systems with the first locking system comprising a notched ring and a spring and the second locking system comprising a lock ring . a first chimney configured to be secured to a first fuel bladder; a second chimney configured to be secured to a second fuel bladder; each chimney comprising a central opening ; a main body configured to be received by the central openings of each of the first and second chimneys ; a securement feature for maintaining cooperation between the first chimney and the main body ; and first and second locking systems for maintaining cooperation between the second chimney and the main body , wherein the main body comprises a rear shoulder , characterized in that the first and the second locking systems comprise independent locking systems with the first locking system comprising a notched ring and a spring and the second locking system comprising a lock ring .
A medical implant, comprising: - an expandable structure which is designed to be expanded from a crimped state into an expanded state, wherein the structure forms a tubular scaffolding in the expanded state, and wherein the structure comprises a plurality of first struts arranged along a periphery of the structure in said expanded state, characterized in that, the first struts each comprise a recess (O) within the respective strut, the recess forming a well-defined channel at the outer surface of the structure , wherein the medical implant further comprises a sealing member arranged in said recesses (O), wherein said sealing member is formed annularly in said expanded state, and wherein the sealing member comprises a plurality of filling portions , wherein each filling portion is arranged in one of said recesses (O). - an expandable structure which is designed to be expanded from a crimped state into an expanded state, wherein the structure forms a tubular scaffolding in the expanded state, and wherein the structure comprises a plurality of first struts arranged along a periphery of the structure in said expanded state,
A wind turbine comprising an intake assembly and an output assembly arranged adjacent one another on a common axis, said assemblies being rotatable relative to one another to work a generator that generates electrical energy; each assembly comprising an annular ring of aerofoil blades , wherein each of the intake assembly blades has a first pitch and each of the output assembly blades has a second pitch that is oriented contrary to first pitch; the intake assembly comprising a centrally located dome-shaped hub and a peripherally mounted convergent nozzle , said hub and nozzle being configured to direct air moving through the wind turbine towards the aerofoil blades of the intake and output assemblies; wherein the aerofoil blades of at least one of the intake and output assemblies have an overlapping arrangement such that, when viewed from along the common axis of rotation, it is not possible to see through the wind turbine; and characterised in that the peripherally mounted convergent nozzle of the intake assembly is formed from a flexible material supported by a structural framework mounted on the intake assembly, wherein the nozzle is configured to fail in high wind conditions , which in turn reduces the wind resistance provided by the wind turbine . each assembly comprising an annular ring of aerofoil blades , wherein each of the intake assembly blades has a first pitch and each of the output assembly blades has a second pitch that is oriented contrary to first pitch; the intake assembly comprising a centrally located dome-shaped hub and a peripherally mounted convergent nozzle , said hub and nozzle being configured to direct air moving through the wind turbine towards the aerofoil blades of the intake and output assemblies; wherein the aerofoil blades of at least one of the intake and output assemblies have an overlapping arrangement such that, when viewed from along the common axis of rotation, it is not possible to see through the wind turbine; and characterised in that the peripherally mounted convergent nozzle of the intake assembly is formed from a flexible material supported by a structural framework mounted on the intake assembly, wherein the nozzle is configured to fail in high wind conditions , which in turn reduces the wind resistance provided by the wind turbine .
A control system with aircraft harnessing for an aircraft, the control system comprising: a single effector Line-Replaceable Unit LRU, comprising a first connection port , a second connection port , a third connection port , and characterised by comprising a first interconnect wire disposed internal to the effector LRU and internally connecting only the first connection port with only the second connection port , a second interconnect wire disposed internal to the effector LRU and internally connecting only the first connection port with only the third connection port , and a third interconnect wire disposed internal to the effector LRU and internally connecting only the second connection port with only the third connection port ; a first control LRU connected using a first harnessing to the effector LRU ; a second control LRU connected using a second harnessing to the effector LRU ; and a third control LRU connected using a third harnessing to the effector LRU , wherein the first control LRU and the second control LRU are configured to communicate using the first harnessing and the second harnessing and using only the first interconnect wire internal to the effector LRU , the first control LRU and the third control LRU are configured to communicate using the first harnessing and the third harnessing and using only the second interconnect wire internal to the effector LRU , and the second control LRU and the third control LRU are configured to communicate using the second harnessing and the third harnessing and using only the third interconnect wire internal to the effector LRU ,. a single effector Line-Replaceable Unit LRU, comprising a first connection port , a second connection port , a third connection port , and characterised by comprising a first interconnect wire disposed internal to the effector LRU and internally connecting only the first connection port with only the second connection port , a second interconnect wire disposed internal to the effector LRU and internally connecting only the first connection port with only the third connection port , and a third interconnect wire disposed internal to the effector LRU and internally connecting only the second connection port with only the third connection port ; a first control LRU connected using a first harnessing to the effector LRU ; a second control LRU connected using a second harnessing to the effector LRU ; and a third control LRU connected using a third harnessing to the effector LRU , wherein the first control LRU and the second control LRU are configured to communicate using the first harnessing and the second harnessing and using only the first interconnect wire internal to the effector LRU , the first control LRU and the third control LRU are configured to communicate using the first harnessing and the third harnessing and using only the second interconnect wire internal to the effector LRU , and the second control LRU and the third control LRU are configured to communicate using the second harnessing and the third harnessing and using only the third interconnect wire internal to the effector LRU ,.
A propulsion system for a helicopter comprising a main engine , a main rotor , a main gearbox including an output connected mechanically to the main rotor and a first input , and the main engine comprising an output shaft driven by a power turbine of the main engine , the propulsion system further comprising an assistance device comprising a first electric machine configured to operate as an electric generator to extract some energy produced by the main engine , and a second electric machine mechanically coupled to a second input of the main gearbox , the second electric machine being supplied with electrical power by the first electric machine and configured to operate as an electric motor to provide additional mechanical power to the main gearbox when required, characterized in that the main engine comprises a reduction gearbox mechanically coupled between the main engine and the first input of the main gearbox , and in that the output shaft is mechanically connected to the reduction gearbox , and in that the first electric machine is mechanically coupled to the reduction gearbox and comprises a rotor and a stator , the rotor being formed by an electromagnetic portion of the output shaft of the main engine and the stator being mounted around said electromagnetic portion of the output shaft of the main engine .
Switching device , in particular DC switching device, with at least one electrical input and at least one electrical output , and with at least one first switching contact and a movable switching bridge , wherein the switching device further comprises an arc extinguishing arrangement with at least one arc extinguishing chamber , wherein a U-shaped yoke is arranged in regions externally around at least one arc extinguishing chamber , characterised in that at least one first leg of the U-shaped yoke has a predeterminable plurality of apertures which are provided or arranged to allow a view of the interior of the arc extinguishing arrangement .
A method of performing a handover of a mobile network device from a first gateway device to a second gateway device , in an industrial facility comprising two or more production cells, wherein the mobile network device moves in between and within the two or more production cells for transporting material and work in process items between the two or more production cells, the method comprising: a. determining the second gateway device from a plurality of gateway devices based on a movement information associated the mobile network device , wherein the movement information is indicative of a potential movement of the mobile network device ; and b. reserving one or more radio resources at the second gateway device in relation to the mobile network device and releasing one or more radio resources at the first gateway device in relation to the mobile network device ; wherein the movement information associated with the mobile network device is estimated based on process data associated with the mobile network device , wherein the process data is obtained from one of a process controller associated with a first process, a manufacturing execution system associated with a first process and a mobile network device controller associated with the mobile network device , the process data indicative of a first production cell , wherein the mobile network device visits the first production cell for transfer of manufacturing material and wherein the first production cell is within a radio coverage of the second gateway device , and transmitting a route control message to the mobile network device based on an unavailability of the one or more resources at the second gateway device , wherein the mobile network device is configured to adjust one of the route associated with the mobile network device and the velocity associated with the mobile network device . a. determining the second gateway device from a plurality of gateway devices based on a movement information associated the mobile network device , wherein the movement information is indicative of a potential movement of the mobile network device ; and b. reserving one or more radio resources at the second gateway device in relation to the mobile network device and releasing one or more radio resources at the first gateway device in relation to the mobile network device ;
A method for wireless communication by a User Equipment, UE, (102; 206) comprising: receiving a system information block 1, SIB1, and a physical control format indicator channel, PCFICH, wherein the SIB1 indicates a first number of symbols and the PCFICH indicates a second number of symbols; monitoring a first set of resources for a first control channel in a first subframe in a first bandwidth region, wherein the first set of resources occupies the first number of symbols of the first subframe; and in response to detecting the first control channel, monitoring a second set of resources in a second subframe and in a second bandwidth region for control information and data, the second bandwidth region larger than the first bandwidth region, wherein the monitoring the second set of resources for the control information comprises monitoring the second set of resources for a second control channel for receiving the control information scheduling resources for receiving the data and the second set of resources occupies the second number of symbols at the start of the second subframe. receiving a system information block 1, SIB1, and a physical control format indicator channel, PCFICH, wherein the SIB1 indicates a first number of symbols and the PCFICH indicates a second number of symbols; monitoring a first set of resources for a first control channel in a first subframe in a first bandwidth region, wherein the first set of resources occupies the first number of symbols of the first subframe; and in response to detecting the first control channel, monitoring a second set of resources in a second subframe and in a second bandwidth region for control information and data, the second bandwidth region larger than the first bandwidth region, wherein the monitoring the second set of resources for the control information comprises monitoring the second set of resources for a second control channel for receiving the control information scheduling resources for receiving the data and the second set of resources occupies the second number of symbols at the start of the second subframe.
An image processing apparatus comprising at least one processor that functions as: a first calculation unit configured to calculate a first color difference value (Cr1, Cb1) between a pixel value of a first color and a pixel value of a second color of pixels in first image data (G,B,R) obtained according to an optical image formed on an image pickup device via an image pickup optical member ; a restoration processing unit configured to perform restoration processing on the first image data (G,B,R), using a restoration filter operating based on an optical transfer function of the image pickup optical member , to thereby generate second image data (G,B,R); a second calculation unit configured to calculate a second color difference value (Cr2, Cb2) between a pixel value of the first color and a pixel value of the second color of pixels in the second image data; and a correction unit configured to correct pixel values of the second image data according to a result of comparison between an amount of change in the second color difference value with respect to the first color difference value, and a threshold value (Th1r, Th1b), wherein, in a case where the result of comparison is larger than the threshold value (Th1r, Th1b), said correction unit is configured to correct the pixel values of the second image data such that the result of comparison will not be larger than the threshold value, characterized in that said correction unit is configured to set the threshold value based on a gain applied when generating the first image data (G, B, R). a first calculation unit configured to calculate a first color difference value (Cr1, Cb1) between a pixel value of a first color and a pixel value of a second color of pixels in first image data (G,B,R) obtained according to an optical image formed on an image pickup device via an image pickup optical member ; a restoration processing unit configured to perform restoration processing on the first image data (G,B,R), using a restoration filter operating based on an optical transfer function of the image pickup optical member , to thereby generate second image data (G,B,R); a second calculation unit configured to calculate a second color difference value (Cr2, Cb2) between a pixel value of the first color and a pixel value of the second color of pixels in the second image data; and a correction unit configured to correct pixel values of the second image data according to a result of comparison between an amount of change in the second color difference value with respect to the first color difference value, and a threshold value (Th1r, Th1b), wherein, in a case where the result of comparison is larger than the threshold value (Th1r, Th1b), said correction unit is configured to correct the pixel values of the second image data such that the result of comparison will not be larger than the threshold value, characterized in that said correction unit is configured to set the threshold value based on a gain applied when generating the first image data (G, B, R).
Holding apparatus which is configured and adapted for holding a gutted poultry body or a part thereof, in particular a breast cap, during processing in an apparatus for processing gutted poultry bodies or parts thereof, the holding apparatus comprising a support body which is configured and adapted for supporting the poultry body or the part thereof, a fastening body which is configured and adapted for holding the support body on the one hand and for fastening the holding apparatus to a circulatingly driven transport unit of the apparatus for processing gutted poultry bodies or parts thereof on the other hand, and a clamping device which is configured and adapted for securing the poultry body or the part thereof to the support body during processing, wherein the clamping device comprises a hook which is configured and adapted for penetrating into soft parts of the poultry body or the part thereof and a clamping lever , comprising clamping jaws , which is configured and adapted for clamping parts of the poultry body or the part thereof against the lower side of the hook directed towards the support body , wherein the hook is arranged such that its lower side is spaced apart from the support body in order to form a free space for receiving the parts of the poultry body or a part thereof to be clamped, and the clamping lever is designed so as to be movable, counter to a spring force, out of a standby position into a clamping position, and back again, characterised in that in addition to clamping jaws , the clamping lever comprises a centring shoulder which projects into the free space between the lower side of the hook and the support body when the clamping lever is in the standby position.
An attachment mechanism to attach a component to a particular location on a tube in a blood sampling-blood pressure monitoring system by a user, the attachment mechanism comprising: a piercing feature, wherein the piercing feature pierces the tube to attach the component to the particular location on the tube of the blood sampling-blood pressure monitoring system selected by the user.
An shroud assembly to seal with a turbine blade stage of a gas turbine, the assembly comprising: an outer shroud configured to circumferentially surround the turbine blade stage wherein the outer shroud is configured to be coupled to a casing that at least partially encloses the gas turbine; and an inner shroud configured to circumferentially surround the turbine blade stage to seal with the turbine blade stage and comprising an attachment element configured to be inserted into the outer shroud to couple the inner shroud to the outer shroud , characterized in that the attachment element comprises at least one flange extending from an upper face of the inner shroud; the outer shroud comprises an opening configured to receive each attachment flange, and a hole ; the flange comprising a hole , wherein the hole of the flange and the hole of the outer flange are configured to be aligned with each other when a flange is received in the respective opening of the outer shroud, so that a pin may be received jointly through the hole of the flange and the hole of the outer shroud. an outer shroud configured to circumferentially surround the turbine blade stage wherein the outer shroud is configured to be coupled to a casing that at least partially encloses the gas turbine; and an inner shroud configured to circumferentially surround the turbine blade stage to seal with the turbine blade stage and comprising an attachment element configured to be inserted into the outer shroud to couple the inner shroud to the outer shroud , characterized in that the attachment element comprises at least one flange extending from an upper face of the inner shroud; the outer shroud comprises an opening configured to receive each attachment flange, and a hole ; the flange comprising a hole , wherein the hole of the flange and the hole of the outer flange are configured to be aligned with each other when a flange is received in the respective opening of the outer shroud, so that a pin may be received jointly through the hole of the flange and the hole of the outer shroud.