mhurhangee/ep-ind-claims huggingface dataset:
A method of moulding a pad for applying stimulation to a human or animal body, comprising: forming a first portion of the pad by injecting a first material comprising a thermoplastic material into a first mould, the first mould being shaped so as to define a flange on the first portion of the pad; placing the first portion of the pad into a second mould, the second mould having a first plate and a second plate, wherein the second plate has a surface that is substantially parallel to a surface of the flange at all points at which the second plate abuts the flange when the second mould is closed; compressing the flange between the first and second plates of the second mould; and forming a second portion of the pad by injecting a second material comprising a thermoplastic material into the second mould whilst the flange is compressed between the first and second plates of the second mould. forming a first portion of the pad by injecting a first material comprising a thermoplastic material into a first mould, the first mould being shaped so as to define a flange on the first portion of the pad; placing the first portion of the pad into a second mould, the second mould having a first plate and a second plate, wherein the second plate has a surface that is substantially parallel to a surface of the flange at all points at which the second plate abuts the flange when the second mould is closed; compressing the flange between the first and second plates of the second mould; and forming a second portion of the pad by injecting a second material comprising a thermoplastic material into the second mould whilst the flange is compressed between the first and second plates of the second mould.
A laundry dryer comprising a drum wherein the laundry to be dried, an air duct wherein the processing air cycle is realized, a fan that provides the circulation of the processing air, a compressor that realizes the refrigerant cycle, an evaporator that provides the processing air in the air duct to be dehumidified, a condenser that provides the dehumidified processing air to be heated and a refrigerant pipe that provides the refrigerant pressurized by the compressor to pass through the condenser and the evaporator to be delivered to the compressor again, and wherein the refrigerant is provided to be heated before entering into the compressor, characterized in that the part of the refrigerant pipe between the evaporator and the compressor is shaped so as to touch the compressor casing before being connected to the compressor inlet, in order for the refrigerant to be heated and that an accumulator provides the liquid phase and the vapor phase of the refrigerant moving from the evaporator to the compressor, to be separated and provides the refrigerant in vapor phase to enter into the compressor, and in that the refrigerant pipe is wrapped around the compressor casing prior to the accumulator.
A method of small data communication implemented by a wireless transmit/receive unit (102, 1010), WTRU, the method comprising: receiving, via a receiver, a paging message from a wireless communication network; initiating, via a processor, a Radio Resource Control, RRC, connection request in response to the paging message; sending, via a transmitter, the RRC connection request to the wireless communication network; receiving, via the receiver, an RRC message from the communication network in response to the RRC connection request, the RRC message including appended small data, wherein the small data includes user data, wherein at least the user data is received via a control plane; and detecting, via the processor, the user data received via the control plane, characterised in that the RRC message includes an information element, IE, the IE indicating that the RRC message is a last message containing small data. receiving, via a receiver, a paging message from a wireless communication network; initiating, via a processor, a Radio Resource Control, RRC, connection request in response to the paging message; sending, via a transmitter, the RRC connection request to the wireless communication network; receiving, via the receiver, an RRC message from the communication network in response to the RRC connection request, the RRC message including appended small data, wherein the small data includes user data, wherein at least the user data is received via a control plane; and detecting, via the processor, the user data received via the control plane, characterised in that the RRC message includes an information element, IE, the IE indicating that the RRC message is a last message containing small data.
Burner for a thermal post-combustion device having a) a housing; b) a combustion nozzle arranged in the housing and having a tube through which combustion gas can flow and which has at least one discharge opening for the combustion gas; c) a turbulence apparatus, attached to an end section of the housing, through which the gas to be cleaned can flow; wherein d) the combustion nozzle comprises an outer tube and an inner tube which are delimiting a ring-shaped discharge gap with their end sections; e) combustion gas can flow through the inner space between the outer tube and the inner tube to the discharge gap; f) the flow path for the combustion gas has a constriction near the discharge gap; g) the outer tube has, in its end section delimiting the discharge gap, a portion conically tapering in flow direction of the combustion gas; h) the inner tube has, on its outer sheath surface in its end section delimiting the discharge gap, a groove which is particularly in cross section V-shaped; i) the outer tube and the inner tube are adjustable in axial direction relative to one another. a) a housing; b) a combustion nozzle arranged in the housing and having a tube through which combustion gas can flow and which has at least one discharge opening for the combustion gas; c) a turbulence apparatus, attached to an end section of the housing, through which the gas to be cleaned can flow; wherein d) the combustion nozzle comprises an outer tube and an inner tube which are delimiting a ring-shaped discharge gap with their end sections; e) combustion gas can flow through the inner space between the outer tube and the inner tube to the discharge gap; f) the flow path for the combustion gas has a constriction near the discharge gap; g) the outer tube has, in its end section delimiting the discharge gap, a portion conically tapering in flow direction of the combustion gas; h) the inner tube has, on its outer sheath surface in its end section delimiting the discharge gap, a groove which is particularly in cross section V-shaped; i) the outer tube and the inner tube are adjustable in axial direction relative to one another.
Projectile replica for insertion into a launching cup of a military launching system with an ignition interface for tapping an electrical ignition signal of the launching system and with a user interface for outputting a visual, electrical, acoustic and/or haptic user signal as a function of the ignition signal, characterized by processing electronics for processing the ignition signal tapped via the ignition interface into the modified user signal output via the user interface. with a user interface for outputting a visual, electrical, acoustic and/or haptic user signal as a function of the ignition signal, characterized by processing electronics for processing the ignition signal tapped via the ignition interface into the modified user signal output via the user interface.
A current flow control assembly, for controlling current flow in an electrical network of a plurality of interconnected electrical elements, comprising: a plurality of current flow controllers (30,32,34), each current flow controller (30,32,34) being connectable to at least one of the plurality of interconnected electrical elements, each current flow controller (30,32,34) being configured to be operable to selectively control current flow in at least one of the plurality of interconnected electrical elements within a respective current flow control range; a control unit configured to be in communication with each of the plurality of current flow controllers (30,32,34), the current flow control assembly being characterised in that the control unit is configured to: select at least one of the plurality of current flow controllers (30,32,34) with a current flow control range or a combined current flow control range that corresponds to one or more current flow control requirements of the electrical network; and operate the or each selected current flow controller (30,32,34) to control current flow in at least one of the plurality of interconnected electrical elements so as to control current flow in the electrical network in accordance with the or each current flow control requirement of the electrical network. a plurality of current flow controllers (30,32,34), each current flow controller (30,32,34) being connectable to at least one of the plurality of interconnected electrical elements, each current flow controller (30,32,34) being configured to be operable to selectively control current flow in at least one of the plurality of interconnected electrical elements within a respective current flow control range; a control unit configured to be in communication with each of the plurality of current flow controllers (30,32,34), the current flow control assembly being characterised in that the control unit is configured to: select at least one of the plurality of current flow controllers (30,32,34) with a current flow control range or a combined current flow control range that corresponds to one or more current flow control requirements of the electrical network; and operate the or each selected current flow controller (30,32,34) to control current flow in at least one of the plurality of interconnected electrical elements so as to control current flow in the electrical network in accordance with the or each current flow control requirement of the electrical network. select at least one of the plurality of current flow controllers (30,32,34) with a current flow control range or a combined current flow control range that corresponds to one or more current flow control requirements of the electrical network; and operate the or each selected current flow controller (30,32,34) to control current flow in at least one of the plurality of interconnected electrical elements so as to control current flow in the electrical network in accordance with the or each current flow control requirement of the electrical network.
An isolated monoclonal antibody comprising an antigen binding domain, said antibody capable of binding an epitope of a human RAGE molecule, said antigen binding domain comprising: a heavy chain CDR set of SEQ ID NO:10, 11, and 12 for heavy chain CDR 1, 2 and 3, respectively, and a light chain CDR set of SEQ ID NO: 14, 15 and 16 for light chain CDR1, 2 and 3 respectively. a heavy chain CDR set of SEQ ID NO:10, 11, and 12 for heavy chain CDR 1, 2 and 3, respectively, and a light chain CDR set of SEQ ID NO: 14, 15 and 16 for light chain CDR1, 2 and 3 respectively.
A control and sealing annular gasket intended, on the one hand, to carry out the sealing between a tube and a connecting part (12, 13, 13') after a crimping step between the tube and the connecting part (12, 13, 13'), the tube being intended to convey a fluid, said sealing gasket being intended, on the other hand, to arrange a sealing leakage of said fluid before the crimping step so as to control the achievement of the crimping step, said sealing gasket comprising: - a straight section called main section with circular contour, - at least one area called leakage area comprising a continuous plurality of straight sections the contour of each fits within the circular contour of the main straight section, and arranged to form a recess called leakage recess for the passage of the fluid before crimping onto a contour (2, 3) of the annular sealing gasket, said sealing gasket being characterized in that the maximum depth (d max) of the leakage recess is such that the section deviation between the main straight section with circular contour and the straight section measured at the maximum depth (d max) of a leakage area is comprised between 8 and 27% of the main straight section with circular contour, and in that the radial depth of the continuous plurality of straight sections forming the at least one recess continuously decreases from a location in which the maximum depth of the at least one recess is measured, up to at least one end location of the at least one recess in which the minimum depth of the at least recess is measured. - a straight section called main section with circular contour, - at least one area called leakage area comprising a continuous plurality of straight sections the contour of each fits within the circular contour of the main straight section, and arranged to form a recess called leakage recess for the passage of the fluid before crimping onto a contour (2, 3) of the annular sealing gasket,
A saddle type vehicle comprising, supported for rocking motion on a vehicle body frame, a power unit including an OHC type internal combustion engine and a belt-type continuously variable transmission; the OHC type internal combustion engine having a cylinder axial line (Cc) tilted forward greatly and being provided therein with a plurality of rocker arms (57, 58) arrayed and supported for rocking motion in a mutually neighboring relationship on a rocker arm shaft and operable in an interlocking relationship with engine valves (61, 62); a connection pin fitted for movement in an axial direction of the rocker arm shaft in the rocker arms (57, 58) positioned adjacent each other being provided to be movable between a connection position at which the connection pin connects the rocker arms (57, 58) positioned adjacent each other to each other for integral rocking motion and a disconnection position at which the connection pin disconnects the rocker arms (57, 58) from each other to allow independent rocking motion of each of the rocker arms (57, 58); a pressing force transmission member (74, 76) being provided which transmits pressing force of a pressing force generation source disposed outside the OHC type internal combustion engine to the connection pin to move the connection pin in the vehicle widthwise direction, wherein the OHC type internal combustion engine has side walls (100L, 100R) directed in the vehicle widthwise direction and side walls (100U, 100S) directed in a vertical direction, the side walls together assuming a rectangular tubular shape, the pressing force generation source is attached to one of the side walls (100L, 100R) directed in the vehicle widthwise direction, and the OHC type internal combustion engine is a water-cooled internal combustion engine, and a water pump is supported on one side wall on the opposite side to the side wall to which the pressing force generation source is attached, of the side walls (100L, 100R) directed in the vehicle widthwise direction, wherein the pressing force generation source is provided with a boss portion adapted to support the pressing force transmission member for sliding movement, the boss portion being formed in a projecting manner for fitting into the OHC type internal combustion engine, and the pressing force generation source is fitted in the OHC type internal combustion engine through an O-snap ring which is provided on the boss portion, and a seal member which is provided between the OHC type internal combustion engine and an end portion of the boss portion, wherein adjustment screws (57t, 58t) are screwed at action end portions (57vv, 58vv) of the rocker arms (57, 58), and an axial line (Cp) of the connection pin is disposed between head side end portions (57tt, 58tt) of the adjustment screws (57t, 58t) and an axial line (Cr) of rocker arm shaft insertion holes (57h, 58h), and upwardly of the axial line (Cr) of the rocker arm shaft insertion holes (57h, 58h).
Method for detecting icing conditions for an aircraft, characterized in that it comprises the following steps: - measurement of parameters of systems of the aircraft with the exception of ice-detecting external probes, the said systems being unsusceptible to degraded operation in the presence of ice and the said parameters being symptomatic of the presence of ice on the aircraft; - transformation of the measurements of these parameters into P -tuples of values of explanatory variables which explain the icing conditions; - classification of the measurements by at least one classifier previously trained in a supervised manner, the said classifier providing a prediction of membership in a class of icing conditions. - measurement of parameters of systems of the aircraft with the exception of ice-detecting external probes, the said systems being unsusceptible to degraded operation in the presence of ice and the said parameters being symptomatic of the presence of ice on the aircraft; - transformation of the measurements of these parameters into P -tuples of values of explanatory variables which explain the icing conditions; - classification of the measurements by at least one classifier previously trained in a supervised manner, the said classifier providing a prediction of membership in a class of icing conditions.
A stent delivery system comprising: a catheter including an elongated body having a stent attachment location, said elongated body having a proximal end and a distal end; a stent (612, 712) mounted on the elongated body at the stent attachment location, the stent being expandable from an undeployed compressed orientation to a deployed expanded orientation, the stent including proximal and distal ends, and comprising a plurality of struts, and an outer tubular member moulted on the elongated body, the outer tubular member being positionable in a transport position in which it covers the stent being mounted at the stent attachment location, the outer tubular member also being positionable in a deploy position in which the stent is exposed; characterized in that the stent also includes one or more first interlock structures (684, 784) positioned at proximal and/or distal ends of the stent, each first interlock structure (684, 784) being an opening defined within the struts of the stent (612, 712), and the elongated body includes one or more second interlock structures (682, 782), each second interlock structure (682, 782) being configured to be received in a respective first interlock structure (687, 784) when the stent is in the compressed undeployed orientation to constrain axial movement of the stent (612, 712) relative to the elongated body. a catheter including an elongated body having a stent attachment location, said elongated body having a proximal end and a distal end; a stent (612, 712) mounted on the elongated body at the stent attachment location, the stent being expandable from an undeployed compressed orientation to a deployed expanded orientation, the stent including proximal and distal ends, and comprising a plurality of struts, and an outer tubular member moulted on the elongated body, the outer tubular member being positionable in a transport position in which it covers the stent being mounted at the stent attachment location, the outer tubular member also being positionable in a deploy position in which the stent is exposed; characterized in that the stent also includes one or more first interlock structures (684, 784) positioned at proximal and/or distal ends of the stent, each first interlock structure (684, 784) being an opening defined within the struts of the stent (612, 712), and the elongated body includes one or more second interlock structures (682, 782), each second interlock structure (682, 782) being configured to be received in a respective first interlock structure (687, 784) when the stent is in the compressed undeployed orientation to constrain axial movement of the stent (612, 712) relative to the elongated body.
A pneumatic tire for heavy load comprising a carcass extending from a tread portion through a sidewall portion to a bead portion, a belt layer disposed on the radially outside of the carcass and inside the tread portion, and a belt cushion disposed between the tire-axis-direction end of the belt layer and said carcass; wherein said belt cushion comprises at least three layers including an outer layer, an interlayer, and an inner layer which are arranged in this order inwardly in the ti re-radial-direction from the tire-axis-direction end of said belt layer; said outer layer and said inner layer are made of a rubber composition B having a complex modulus E*b and a loss tangent tan δb; and said interlayer is made of a rubber composition C having a complex modulus E*c and having a loss tangent tan δc that is smaller than said loss tangent tan δb, characterized in that the complex modulus E*b of the rubber composition B and the complex modulus E*c of the rubber composition C are substantially the same, meaning that a ratio of the larger complex modulus to the smaller complex modulus is not more than 1.4.
A hygienisation unit for hygienising or pressure sterilising raw material that contains organic material and is fed to a biogas reactor, said hygienisation unit being continuously operating and said hygienisation unit including - a delimited space for a high solids content raw material, the delimited space being a pressure resistant tortuous continuous pipe, - feed equipment arranged in the vicinity of the space for feeding suppliable raw material to the space, the feed equipment including a pump for feeding raw material, a gate valve arranged between the pump and the space for preventing the return flow of raw material and a second gate valve arranged at the end of the delimited space in the direction of motion of raw material for closing the delimited space to increase pressure, - heating equipment arranged outside the pipe for heating raw material inside the pipe by the effect of heat transferred through the pipe, - measuring equipment for measuring the temperature and pressure of the raw material existing in the space, - control equipment arranged to control said feed equipment and heating equipment for adjusting the raw material dwell time and the hygienisation temperature suitable in terms of the duration of hygienisation or pressure sterilisation for hygienising raw material based on the measurement of the measuring equipment, characterised in that the pump is a piston pump arranged to supply raw material in a solids content of 15% - 35%, preferably 25% - 30%. - a delimited space for a high solids content raw material, the delimited space being a pressure resistant tortuous continuous pipe, - feed equipment arranged in the vicinity of the space for feeding suppliable raw material to the space, the feed equipment including a pump for feeding raw material, a gate valve arranged between the pump and the space for preventing the return flow of raw material and a second gate valve arranged at the end of the delimited space in the direction of motion of raw material for closing the delimited space to increase pressure, - heating equipment arranged outside the pipe for heating raw material inside the pipe by the effect of heat transferred through the pipe, - measuring equipment for measuring the temperature and pressure of the raw material existing in the space, - control equipment arranged to control said feed equipment and heating equipment for adjusting the raw material dwell time and the hygienisation temperature suitable in terms of the duration of hygienisation or pressure sterilisation for hygienising raw material based on the measurement of the measuring equipment, characterised in that the pump is a piston pump arranged to supply raw material in a solids content of 15% - 35%, preferably 25% - 30%.