mhurhangee/patent-ind-claim-en huggingface dataset:
A method for establishing a secure link over a wireless area network, WLAN, the method executed at a user equipment, UE, the method comprising: - sending a transport layer security, TLS, type Ethernet frame carrying a TLS client Hello message over a link layer connection for establishment of a secure TLS tunnel over Ethernet, ETLS, between the UE and a receiver of the TLS type Ethernet frame through an Access Point, AP, wherein the receiver is a wireless access gateway, WAG; - upon obtaining from the receiver a TLS server Hello message encapsulated in the TLS type Ethernet frame, establishing the secure ETLS between the UE and the receiver in accordance with TLS handshake messages encapsulated in the TLS type Ethernet frame; and - tunneling selected data traffic and signaling over the secure ETLS, wherein the selected data traffic is encrypted and encapsulated in a data TLS type Ethernet frame. - sending a transport layer security, TLS, type Ethernet frame carrying a TLS client Hello message over a link layer connection for establishment of a secure TLS tunnel over Ethernet, ETLS, between the UE and a receiver of the TLS type Ethernet frame through an Access Point, AP, wherein the receiver is a wireless access gateway, WAG; - upon obtaining from the receiver a TLS server Hello message encapsulated in the TLS type Ethernet frame, establishing the secure ETLS between the UE and the receiver in accordance with TLS handshake messages encapsulated in the TLS type Ethernet frame; and - tunneling selected data traffic and signaling over the secure ETLS, wherein the selected data traffic is encrypted and encapsulated in a data TLS type Ethernet frame.
A ball end mill comprising a ball end cutting edge on a distal end in an axis line (o) direction, a rotation locus of the ball end cutting edge around the axis line (o) being formed in an approximately hemispherical shape, wherein the ball end cutting edge includes a plurality of large diameter edges , and each large diameter edge is formed in an arc shape having a curvature radius larger than a ball radius (R1) of the ball end cutting edge , wherein the ball radius (R1) is a length of a line segment perpendicularly extending from the axis line to an outer peripheral end (E1; E2) of the ball end cutting edge (110;120), and an intersection point between the line segment and the axis line becomes the center (C) of the first ball end cutting edge and the second ball end cutting edge , a plurality of the large diameter edges are formed in a region 80% or more to 120% or less of the ball radius (R1) from the center (C) of the ball end cutting edge from a distal end to an outer peripheral end of the ball end cutting edge , the plurality of large diameter edges each have an identical cutting width in a predetermined region from the distal end to the outer peripheral end side of the ball end cutting edge , the plurality of large diameter edges each have the identical curvature radius, and when an imaginary circle having the ball radius (R1) is drawn with the center of the ball end cutting edge as a center, the imaginary circle internally contacts respective rotation loci of the plurality of large diameter edges . a ball end cutting edge on a distal end in an axis line (o) direction, a rotation locus of the ball end cutting edge around the axis line (o) being formed in an approximately hemispherical shape, wherein the ball end cutting edge includes a plurality of large diameter edges , and each large diameter edge is formed in an arc shape having a curvature radius larger than a ball radius (R1) of the ball end cutting edge , wherein the ball radius (R1) is a length of a line segment perpendicularly extending from the axis line to an outer peripheral end (E1; E2) of the ball end cutting edge (110;120), and an intersection point between the line segment and the axis line becomes the center (C) of the first ball end cutting edge and the second ball end cutting edge , a plurality of the large diameter edges are formed in a region 80% or more to 120% or less of the ball radius (R1) from the center (C) of the ball end cutting edge from a distal end to an outer peripheral end of the ball end cutting edge , the plurality of large diameter edges each have an identical cutting width in a predetermined region from the distal end to the outer peripheral end side of the ball end cutting edge , the plurality of large diameter edges each have the identical curvature radius, and when an imaginary circle having the ball radius (R1) is drawn with the center of the ball end cutting edge as a center, the imaginary circle internally contacts respective rotation loci of the plurality of large diameter edges .
A fluid pump device changeable in diameter, in particular for medical application, with a pump housing which is changeable in diameter, with a rotor which is changeable in diameter and having at least one delivery element for the fluid, as well as with at least one actuation means which may be moved in a longitudinal direction and at whose distal end the fluid pump and at whose proximal end an actuation device is arranged, wherein the pump housing and the rotor are displaceable relative to one another by way of actuating the actuation means , wherein a bearing arrangement is arranged at the distal end of the actuation means behind the rotor seen from the actuation device, characterized in that the bearing arrangement is movable into the inside of the pump housing , and that struts are provided, which elastically brace between a hub of the bearing arrangement and the pump housing, when the bearing arrangement is moved into the inside of the pump housing .
A steering module for a motor vehicle , the steering module comprising an optical signaling unit , which optically indicates an operating state of the motor vehicle , wherein the optical signaling unit comprises at least one light source and a light guide , by which the light emitted by the light source with a main radiation direction is capable of being deflected in an exit direction which is different from the main radiation direction and the light exits in this exit direction from an emission surface from the light guide , characterized in that the light guide is shaped in such a way that light rays of the coupled-in light are reflected therein at least twice so that the exit direction is opposite to the main radiation direction .
A method for configuring the functions of a server using a firmware image , the method comprising: storing a plurality of desired parameters and corresponding server identifications in a straps structure in the firmware image by a basic input output system; reading a board identification including a server product type from a memory on a baseboard by the basic input output system or a Unified Extensible Firmware Interface; comparing the server product type with the server identifications in the straps structure by the basic input output system or the Unified Extensible Firmware Interface; reprogramming a plurality of parameters with the plurality of desired parameters by the basic input output system or the Unified Extensible Firmware Interface; loading the corresponding desired parameters to a baseboard component on the baseboard to perform a server function by the basic input output system or the Unified Extensible Firmware Interface; and sending a system error log by the basic input output system or the Unified Extensible Firmware Interface if none of the server identifications match the server product type. storing a plurality of desired parameters and corresponding server identifications in a straps structure in the firmware image by a basic input output system; reading a board identification including a server product type from a memory on a baseboard by the basic input output system or a Unified Extensible Firmware Interface; comparing the server product type with the server identifications in the straps structure by the basic input output system or the Unified Extensible Firmware Interface; reprogramming a plurality of parameters with the plurality of desired parameters by the basic input output system or the Unified Extensible Firmware Interface; loading the corresponding desired parameters to a baseboard component on the baseboard to perform a server function by the basic input output system or the Unified Extensible Firmware Interface; and sending a system error log by the basic input output system or the Unified Extensible Firmware Interface if none of the server identifications match the server product type.
A method for wireless communications by a wireless device , comprising: generating a query message indicating a requested data rate for streaming services, wherein the requested data rate is indicated via a bit rate field and one or more additional bits, wherein the requested data rate is indicated via a media access control, MAC, control element, CE, that includes the bit rate field and the one or more additional bits, and wherein a value of the bit rate field corresponds to a bit rate value in a bit rate table, and the one or more additional bits indicate that a multiplier is to be applied to the requested bit rate value corresponding to the value of the bit rate field; and sending the query message to a base station. generating a query message indicating a requested data rate for streaming services, wherein the requested data rate is indicated via a bit rate field and one or more additional bits, wherein the requested data rate is indicated via a media access control, MAC, control element, CE, that includes the bit rate field and the one or more additional bits, and wherein a value of the bit rate field corresponds to a bit rate value in a bit rate table, and the one or more additional bits indicate that a multiplier is to be applied to the requested bit rate value corresponding to the value of the bit rate field; and a value of the bit rate field corresponds to a bit rate value in a bit rate table, and the one or more additional bits indicate that a multiplier is to be applied to the requested bit rate value corresponding to the value of the bit rate field; and sending the query message to a base station.
A gas turbine engine comprising: a compressor portion ; a combustor fluidly connected to the compressor portion; a turbine section fluidly connected to the combustor , wherein the turbine section includes at least a first turbine portion and a second turbine portion connected to the first turbine portion via a transition duct , fluid in the second turbine portion having a lower pressure than fluid in the first turbine portion ; a fan drive gear system connecting the second turbine portion to a fan; wherein the first turbine portion (110; 210) drives a first shaft (130; 230) and the second turbine portion (120; 220) drives a second shaft (140; 240), and wherein the first shaft (130; 230) is supported relative to the second shaft (140; 240) via a piggyback intershaft bearing arrangement in which a bearing is supported radially between two revolving races relative to an axis of the engine; the gas turbine engine characterized in that the transition duct lacks flow correcting vanes, the first turbine portion and the second turbine portion are counter rotating turbine portions, and in that the second turbine portion includes exactly three turbine stages. a compressor portion ; a combustor fluidly connected to the compressor portion; a turbine section fluidly connected to the combustor , wherein the turbine section includes at least a first turbine portion and a second turbine portion connected to the first turbine portion via a transition duct , fluid in the second turbine portion having a lower pressure than fluid in the first turbine portion ; a fan drive gear system connecting the second turbine portion to a fan; wherein the first turbine portion (110; 210) drives a first shaft (130; 230) and the second turbine portion (120; 220) drives a second shaft (140; 240), and wherein the first shaft (130; 230) is supported relative to the second shaft (140; 240) via a piggyback intershaft bearing arrangement in which a bearing is supported radially between two revolving races relative to an axis of the engine; the gas turbine engine characterized in that the transition duct lacks flow correcting vanes, the first turbine portion and the second turbine portion are counter rotating turbine portions, and in that the second turbine portion includes exactly three turbine stages.
A display apparatus comprising: a substrate having adjacent first and second areas for displaying an image, the first area comprising a transmission area (TA) and a pixel area (PA); a first inorganic insulating layer (IL1) over the transmission area (TA) and the pixel area (PA); a second inorganic insulating layer (IL2) over the first inorganic insulating layer (IL1) to correspond to the pixel area (PA), and defining a transmission hole (HT) corresponding to the transmission area (TA); a first organic insulating layer over the second inorganic insulating layer (IL2); a second organic insulating layer over the first organic insulating layer ; a first inorganic encapsulation layer arranged in the transmission area (TA); and a pixel electrode over the second organic insulating layer , wherein the transmission hole (HT) is defined by an inner sloped surface of the second inorganic insulating layer (IL2) that is clad with at least one of the first organic insulating layer and the second organic insulating layer , and wherein at least one of the first organic insulating layer and the second organic insulating layer comprises a sloped surface (117-S;118-S), where the slope of the sloped surface of the first or second organic insulating layer with respect to the upper surface of the first inorganic insulating layer is more gentle than the slope of the inner sloped surface of the second inorganic insulating layer (IL2) with respect to the upper surface of the first inorganic insulating layer. a substrate having adjacent first and second areas for displaying an image, the first area comprising a transmission area (TA) and a pixel area (PA); a first inorganic insulating layer (IL1) over the transmission area (TA) and the pixel area (PA); a second inorganic insulating layer (IL2) over the first inorganic insulating layer (IL1) to correspond to the pixel area (PA), and defining a transmission hole (HT) corresponding to the transmission area (TA); a first organic insulating layer over the second inorganic insulating layer (IL2); a second organic insulating layer over the first organic insulating layer ; a first inorganic encapsulation layer arranged in the transmission area (TA); and a pixel electrode over the second organic insulating layer , wherein the transmission hole (HT) is defined by an inner sloped surface of the second inorganic insulating layer (IL2) that is clad with at least one of the first organic insulating layer and the second organic insulating layer , and wherein at least one of the first organic insulating layer and the second organic insulating layer comprises a sloped surface (117-S;118-S), where the slope of the sloped surface of the first or second organic insulating layer with respect to the upper surface of the first inorganic insulating layer is more gentle than the slope of the inner sloped surface of the second inorganic insulating layer (IL2) with respect to the upper surface of the first inorganic insulating layer.
A folding machine for folding sheet shaped material, the folding machine comprising: a first beam arranged to support sheet shaped material during a folding operation; a second beam arranged to clamp the sheet shaped material against the first beam during the folding operation; a folding beam arranged to rotate around an axis of rotation (R) during the folding operation so as to fold the sheet shaped material against the first beam or the second beam ; a first eccentric coupled to the folding beam and arranged to change a location of the axis of rotation (R) of the folding beam ; characterised in that it further comprises a second eccentric coupled to the folding beam , wherein the second eccentric is arranged to change a location of the folding beam in relation to the first beam so as to adapt to a thickness of the sheet shaped material during the folding operation. a first beam arranged to support sheet shaped material during a folding operation; a second beam arranged to clamp the sheet shaped material against the first beam during the folding operation; a folding beam arranged to rotate around an axis of rotation (R) during the folding operation so as to fold the sheet shaped material against the first beam or the second beam ; a first eccentric coupled to the folding beam and arranged to change a location of the axis of rotation (R) of the folding beam ; characterised in that it further comprises a second eccentric coupled to the folding beam , wherein the second eccentric is arranged to change a location of the folding beam in relation to the first beam so as to adapt to a thickness of the sheet shaped material during the folding operation.
A spatial structure comprising at least: - one node with a plurality of sockets , wherein each socket has coupling means , - one bar which is to be inserted at either of the two ends thereof into the sockets of the nodes and wherein said ends each comprise at least one retaining element , - one perforated screw whose inner surface allows the insertion of the end of the bar and whose outer surface has coupling means formed by a male threaded portion complementary to a similar female thread that forms the coupling means of the sockets , and - a portion of flexible washer suitable for insertion into the socket of the node and being closed by means of compression as a result of the thrust of the perforated screw in order to adopt the shape of a substantially closed washer which cooperates with the retaining element of the end of the bar , such that said bar is locked inside the perforated screw , thus preventing disassembly of the assembly but not the rotation of the bar within the socket ; where in order to close the portion of flexible washer by compression as a result of a thrust by means of a perforated screw , the perforated screw has an inclined plane with an angle α intended for coupling at an inclined plane with the same angle α as the portion of flexible washer , characterized in that the portion of flexible washer comprises: - a thin strip that corresponds to the outer diameter thereof, and - on the inner diameter of said strip , a plurality of teeth greater in thickness than the strip , which project inwards and wherein said teeth alternate with empty areas where only the strip is found, forming a portion of ring gear. and in that - the retaining element of the bar for retaining the portion of flexible washer is formed by a perimeter step. - one node with a plurality of sockets , wherein each socket has coupling means , - one bar which is to be inserted at either of the two ends thereof into the sockets of the nodes and wherein said ends each comprise at least one retaining element , - one perforated screw whose inner surface allows the insertion of the end of the bar and whose outer surface has coupling means formed by a male threaded portion complementary to a similar female thread that forms the coupling means of the sockets , and - a portion of flexible washer suitable for insertion into the socket of the node and being closed by means of compression as a result of the thrust of the perforated screw in order to adopt the shape of a substantially closed washer which cooperates with the retaining element of the end of the bar , such that said bar is locked inside the perforated screw , thus preventing disassembly of the assembly but not the rotation of the bar within the socket ; - a thin strip that corresponds to the outer diameter thereof, and - on the inner diameter of said strip , a plurality of teeth greater in thickness than the strip , which project inwards and wherein said teeth alternate with empty areas where only the strip is found, forming a portion of ring gear. - the retaining element of the bar for retaining the portion of flexible washer is formed by a perimeter step.
Method for operating a medium voltage circuit breaker or recloser, comprising at least one electric pole, each comprising a movable contact and a fixed contact, adapted to be in closed or open position after the switching operations of said switching device, and an electromagnetic actuator, wherein the travel curve of the movable contact is monitored wherein the travel curve is derived by the evaluation of the magnitude of the back electromagnetic force related to the speed of the motion and integrating the speed over discrete time steps, wherein the actuator is driven with a controlled current, in such, that a controller and a voltage source with puls width modulation (PWM) is used, detecting a deviation of the actual travel curve compared to an original curve.
Method for improving the aerodynamic performance of a blade , said blade extending along a longitudinal spanwise direction (X) from a first end to a second end and along a transversal direction (Y) from a leading edge to a trailing edge , said blade comprising successive transversal areas, each transversal area being defined by an aerodynamic profile , each aerodynamic profile being defined by two half profiles including an upper surface half profile and a lower surface half profile , said two half profiles each comprising a leading edge section , an intermediate section and a trailing edge section , said first end being intended to be connected to a hub of a rotor , said second end being intended to be free, characterised in that said method comprises the following steps: - definition of a line segment connecting said leading edge and said trailing edge of said aerodynamic profile , - movement of said leading edge of said aerodynamic profiles situated on an extremal spanwise zone of said blade comprising said second end , said movement being made from said upper surface half profile to said lower surface half profile over a first distance d1 perpendicularly to said line segment , - modification of said leading edge sections of said two half profiles connecting said leading edge to said intermediate sections of said two half profiles on said extremal zone , and - manufacture of said blade according to said modified aerodynamic profiles . - definition of a line segment connecting said leading edge and said trailing edge of said aerodynamic profile , - movement of said leading edge of said aerodynamic profiles situated on an extremal spanwise zone of said blade comprising said second end , said movement being made from said upper surface half profile to said lower surface half profile over a first distance d1 perpendicularly to said line segment , - modification of said leading edge sections of said two half profiles connecting said leading edge to said intermediate sections of said two half profiles on said extremal zone , and - manufacture of said blade according to said modified aerodynamic profiles .
An in vitro method for predicting the response to continuous positive airway pressure (CPAP) in a subject with obstructive sleep apnea (OSA) and resistant hypertension, the method comprising determining in an isolated sample of the subject the level of expression of a cardiovascular system functionally related and cardiovascular disease related microRNA, said microRNA selected from the group comprising miR.100.5p or miR.378a.3p, or any combinations thereof, wherein the response is defined in terms of BP (blood pressure), and wherein the response to continuous positive airway pressure is a decrease of mean blood pressure (MBP) of at least 4.5 mm Hg in relation to initial mean blood pressure before treatment.