mhurhangee/ep-ind-claims huggingface dataset:
A stent comprising: a dilating portion in which a diameter increases from a front end to a rear end of the dilating portion; an indwelled portion which is disposed behind the dilating portion; and a through hole which passes through the dilating portion and the indwelled portion in a longitudinal direction of the stent; wherein the dilating portion penetrates biological tissues along with dilating a perforation previously formed in the biological tissues by pushing the dilating portion into the perforation; the indwelled portion is indwelled within the perforation dilated by the dilating portion after the dilating portion penetrates through the biological tissues, and the stent comprises a mounting section for detachably attaching the stent to a distal end of a sheath, wherein the mounting section is configured to radially engage with the sheath, characterized in that the distal end of the sheath is received in the through hole of the stent, and the mounting section includes projections which are configured to engage with small holes or indentations formed on an outer peripheral surface of the distal end of the sheath, or the mounting section includes small holes or indentations which are configured to engage with protrusions formed on the outer peripheral surface of the distal end of the sheath, or the mounting section includes small bellows-shaped projections which are configured to engage with a bellows portion formed on the outer peripheral surface of the distal end of the sheath. a dilating portion in which a diameter increases from a front end to a rear end of the dilating portion; an indwelled portion which is disposed behind the dilating portion; and a through hole which passes through the dilating portion and the indwelled portion in a longitudinal direction of the stent; wherein the dilating portion penetrates biological tissues along with dilating a perforation previously formed in the biological tissues by pushing the dilating portion into the perforation; the indwelled portion is indwelled within the perforation dilated by the dilating portion after the dilating portion penetrates through the biological tissues, and the stent comprises a mounting section for detachably attaching the stent to a distal end of a sheath, wherein the mounting section is configured to radially engage with the sheath, characterized in that the distal end of the sheath is received in the through hole of the stent, and the mounting section includes projections which are configured to engage with small holes or indentations formed on an outer peripheral surface of the distal end of the sheath, or the mounting section includes small holes or indentations which are configured to engage with protrusions formed on the outer peripheral surface of the distal end of the sheath, or the mounting section includes small bellows-shaped projections which are configured to engage with a bellows portion formed on the outer peripheral surface of the distal end of the sheath.
A method for delay scheduling, the method comprising: determining a first subframe on which to transmit a first downlink control information, DCI, message; characterized in that the method further comprises: if a first information is for a machine type communications, MTC, type user equipment, transmitting, by a communications controller to the MTC type user equipment and in accordance with a delay, a second subframe conveying the first information after transmitting the first subframe, the first information being scheduled to be transmitted on the second subframe in accordance with scheduling information indicated in the first DCI message (step 166). determining a first subframe on which to transmit a first downlink control information, DCI, message; characterized in that the method further comprises: if a first information is for a machine type communications, MTC, type user equipment, transmitting, by a communications controller to the MTC type user equipment and in accordance with a delay, a second subframe conveying the first information after transmitting the first subframe, the first information being scheduled to be transmitted on the second subframe in accordance with scheduling information indicated in the first DCI message (step 166).
A method for producing a rotor of a charging apparatus, particularly an exhaust gas turbocharger, with at least one compressor wheel and a turbine wheel, wherein another bearing section with a radial bearing surface (5, 5') for mounting the rotor in a bearing housing is provided in each case at the longitudinal end, characterised - in that at least the radial bearing surfaces (5, 5') are assembled with radial oversizing, - in that the compressor wheel and the turbine wheel and the bearing sections are assembled to form the rotor, - in that at least the radial bearing surfaces (5, 5') of the fully assembled rotor are subsequently machined, particularly turned or ground until the radial bearing surfaces (5, 5') are rotationally symmetrical. - in that at least the radial bearing surfaces (5, 5') are assembled with radial oversizing, - in that the compressor wheel and the turbine wheel and the bearing sections are assembled to form the rotor, - in that at least the radial bearing surfaces (5, 5') of the fully assembled rotor are subsequently machined, particularly turned or ground until the radial bearing surfaces (5, 5') are rotationally symmetrical.
An auger feeder for drying and loading a filler insulation material, in particular vacuum insulation material, into a vacuum insulated structure, the auger feeder comprising: a hopper having an inner hopper wall and an outer hopper wall wherein the inner hopper wall includes an air permeable surface; a space positioned between the inner and outer hopper walls (18, 22); a heater coupled to an outside edge of the inner hopper wall or an outside edge of the outer hopper wall; a feed screw positioned along an inside edge of the inner hopper wall and an aperture exit positioned at the bottom of the inner and outer hopper walls (18, 22), characterised in that: the auger feeder further comprises an evacuator coupled to a vacuum port positioned in the outer hopper wall and the air permeable surface comprises additionally a permeable membrane, the inner hopper wall comprising plurality of holes having a diameter less than 300 μm. a hopper having an inner hopper wall and an outer hopper wall wherein the inner hopper wall includes an air permeable surface; a space positioned between the inner and outer hopper walls (18, 22); a heater coupled to an outside edge of the inner hopper wall or an outside edge of the outer hopper wall; a feed screw positioned along an inside edge of the inner hopper wall and an aperture exit positioned at the bottom of the inner and outer hopper walls (18, 22), characterised in that: the auger feeder further comprises an evacuator coupled to a vacuum port positioned in the outer hopper wall and the air permeable surface comprises additionally a permeable membrane, the inner hopper wall comprising plurality of holes having a diameter less than 300 μm. the auger feeder further comprises an evacuator coupled to a vacuum port positioned in the outer hopper wall and the air permeable surface comprises additionally a permeable membrane, the inner hopper wall comprising plurality of holes having a diameter less than 300 μm.
A gas turbine engine, comprising: a compressor; a combustor in fluid communication with the compressor; a turbine in fluid communication with the combustor; a diffuser case disposed around the combustor; and a cooling system comprising: a heat exchanger; a first conduit fluidly coupled to an inlet of the heat exchanger; a second conduit fluidly coupled to an outlet of the heat exchanger; an annular passage fluidly coupled to the second conduit; a tangential onboard injector (TOBI) fluidly coupled to the annular passage, wherein the first conduit is fluidly coupled to the diffuser case and is configured to extract air from the diffuser case; a distal surface of the annular passage at least partially defines a boundary of the diffuser case; mixing openings defined by the distal surface of the annular passage; characterised in that the distal surface meets a plurality of jumper tubes configured to deliver cooled air into the annular passage; and in that the mixing openings are more concentrated near the jumper tubes and less concentrated further from the jumper tubes. a compressor; a combustor in fluid communication with the compressor; a turbine in fluid communication with the combustor; a diffuser case disposed around the combustor; and a cooling system comprising: a heat exchanger; a first conduit fluidly coupled to an inlet of the heat exchanger; a second conduit fluidly coupled to an outlet of the heat exchanger; an annular passage fluidly coupled to the second conduit; a tangential onboard injector (TOBI) fluidly coupled to the annular passage, wherein the first conduit is fluidly coupled to the diffuser case and is configured to extract air from the diffuser case; a heat exchanger; a first conduit fluidly coupled to an inlet of the heat exchanger; a second conduit fluidly coupled to an outlet of the heat exchanger; an annular passage fluidly coupled to the second conduit; a tangential onboard injector (TOBI) fluidly coupled to the annular passage, wherein the first conduit is fluidly coupled to the diffuser case and is configured to extract air from the diffuser case; a distal surface of the annular passage at least partially defines a boundary of the diffuser case; mixing openings defined by the distal surface of the annular passage; characterised in that the distal surface meets a plurality of jumper tubes configured to deliver cooled air into the annular passage; and in that the mixing openings are more concentrated near the jumper tubes and less concentrated further from the jumper tubes.
A metal diaphragm damper (1, 31), comprising: a diaphragm (2,3, 32) including a deformable portion disposed in a center thereof and an outer circumferential fixation portion formed by an outer circumferential rim of the diaphragm (2,3, 32), the metal diaphragm damper (1, 31) being filled with gas inside and formed in a disk shape, wherein the deformable portion includes a third curved portion located at a radially outward side and formed to be bulged out, a first curved portion located radially inward of the third curved portion and formed to be bulged out, and a second curved portion located between the first curved portion and the third curved portion, and the second curved portion includes at least a curved wall part formed to be dented in, characterized in that the curved wall part of the second curved portion is formed so as to have a curvature radius smaller than a curvature radius of a curved wall part forming the third curved portion. a diaphragm (2,3, 32) including a deformable portion disposed in a center thereof and an outer circumferential fixation portion formed by an outer circumferential rim of the diaphragm (2,3, 32), the metal diaphragm damper (1, 31) being filled with gas inside and formed in a disk shape, wherein the deformable portion includes a third curved portion located at a radially outward side and formed to be bulged out, a first curved portion located radially inward of the third curved portion and formed to be bulged out, and a second curved portion located between the first curved portion and the third curved portion, and the second curved portion includes at least a curved wall part formed to be dented in, characterized in that the curved wall part of the second curved portion is formed so as to have a curvature radius smaller than a curvature radius of a curved wall part forming the third curved portion.
A computer-implemented method for automatically applying firewall policies within data center applications, at least a portion of the method being performed by a computing device comprising at least one processor, the method comprising: identifying a data center application whose functionality is provided by a set of systems (208,... 208(n)); organizing automatically by the computing device, the set of systems into one or more application model groups that each comprise a group of systems with a same security context by, for each system (208,... 208(n)) in the set of systems: identifying (304(a)) an attribute (212,... 212(n)) of the system that is indicative of a security context under which the system should operate, wherein the attribute comprises a type of data stored by the system and the security context comprises a classification of at least one security need of the system; and assigning (304(b)) the system to an application model group for which the security context will be provided; and for each application model group in the one or more application model groups, protecting the application model group by: selecting (306(a)) a firewall configuration that, when applied, will provide the security context for the application model group; and using (306(b)) the selected firewall configuration to protect the application model group. identifying a data center application whose functionality is provided by a set of systems (208,... 208(n)); organizing automatically by the computing device, the set of systems into one or more application model groups that each comprise a group of systems with a same security context by, for each system (208,... 208(n)) in the set of systems: identifying (304(a)) an attribute (212,... 212(n)) of the system that is indicative of a security context under which the system should operate, wherein the attribute comprises a type of data stored by the system and the security context comprises a classification of at least one security need of the system; and assigning (304(b)) the system to an application model group for which the security context will be provided; and identifying (304(a)) an attribute (212,... 212(n)) of the system that is indicative of a security context under which the system should operate, wherein the attribute comprises a type of data stored by the system and the security context comprises a classification of at least one security need of the system; and assigning (304(b)) the system to an application model group for which the security context will be provided; and for each application model group in the one or more application model groups, protecting the application model group by: selecting (306(a)) a firewall configuration that, when applied, will provide the security context for the application model group; and using (306(b)) the selected firewall configuration to protect the application model group. selecting (306(a)) a firewall configuration that, when applied, will provide the security context for the application model group; and using (306(b)) the selected firewall configuration to protect the application model group.
An electrode wound element for a non-aqueous electrolyte rechargeable battery, comprising a belt-shaped positive electrode; a belt-shaped negative electrode; a belt-shaped porous layer between the belt-shaped positive electrode and the belt-shaped negative electrode; and an adhesive layer formed on a surface of the belt-shaped porous layer, wherein the adhesive layer comprises heat resistance filler particles, a fluorine resin-containing particulate (20b-1) and a binder (20b-2) for the adhesive layer supporting the fluorine resin-containing particulate (20b-1) and having a total volume which is less than that of the fluorine resin-containing particulate (20b-1), wherein a content of the heat resistance filler particles is less then or equal to 80 wt% based on the total weight of the adhesive layer and wherein the binder (20b-2) for the adhesive layer comprises (i) an ionic non-water-soluble binder selected from the group consisting of a carboxylic acid-modified acrylic acid ester, a polyolefin ionomer, and a carboxylic acid-modified styrene-butadiene copolymer, and (ii) a non-ionic water-soluble binder selected from the group consisting of poly-N-vinyl acetamide, polyvinyl alcohol, polyvinylpyrrolidone, and polyoxyethylene, provided that when the binder for the adhesive layer comprises an ionic water-soluble binder, a content of the ionic water-soluble binder is 2 wt% or less based on a weight of the fluorine resin-containing particulate (20b-1). (i) an ionic non-water-soluble binder selected from the group consisting of a carboxylic acid-modified acrylic acid ester, a polyolefin ionomer, and a carboxylic acid-modified styrene-butadiene copolymer, and (ii) a non-ionic water-soluble binder selected from the group consisting of poly-N-vinyl acetamide, polyvinyl alcohol, polyvinylpyrrolidone, and polyoxyethylene,
An aircraft assembly having an aircraft and multi-position landing gear, the landing gear comprising: a first landing skid disposed on a bottom side of said aircraft; a second landing skid disposed on one of a top side or said bottom side of said aircraft; and skid actuator mechanisms operably coupled to said first landing skid and said second landing skid to rotate said first landing skid and said second landing skid relative to said aircraft, wherein said first landing skid is spaced away from said second landing skid along a longitudinal axis of said aircraft, and wherein said first landing skid and said second landing skid are rotatable relative to said aircraft for reorienting the aircraft. a first landing skid disposed on a bottom side of said aircraft; a second landing skid disposed on one of a top side or said bottom side of said aircraft; and skid actuator mechanisms operably coupled to said first landing skid and said second landing skid to rotate said first landing skid and said second landing skid relative to said aircraft, wherein said first landing skid is spaced away from said second landing skid along a longitudinal axis of said aircraft, and wherein said first landing skid and said second landing skid are rotatable relative to said aircraft for reorienting the aircraft.
Method for treating at least one surface of a solid elastomer part with helium ions characterised in that He + and He 2+ multi-energy ions are implanted simultaneously, where the ratio RHe, where RHe = He + /He 2+ with He + and He 2+ expressed as an atomic percentage is less than or equal to 100, for example less than 20, and where the extraction voltage of the source for implanting He + and He 2+ multi-energy ions is between 10 and 400 kV, where the He + and He 2+ multi-energy ion dose is between 5.10 14 and 10 18 ions/cm 2 and where the He + and He 2+ multi-energy ions are obtained simultaneously by extracting with a single extraction voltage single- and multi-charged ions in the plasma chamber of an electron cyclotron resonance source (ECR source).
Refrigeration appliance with a carcass and a door fastened to the carcass such that it can pivot about an axis up to a maximum opening angle, which enclose an interior, with at least two carriers for goods to be refrigerated (11, 12) which are accommodated one above the other in the interior, of which the lower (11, 12) is guided on rails and can be slid outwards from a rear end stop when the door is open, wherein one of the rails is arranged on a side wall of the carcass, to which the door is fastened, wherein at least one door rack (15, 16) is attached to an inner side of the door, and wherein the lower carrier for goods to be refrigerated (11, 12), when it is situated at the rear end stop, is largely covered by the upper carrier for goods to be refrigerated, characterised in that, when it is situated at a front end stop when the door is opened by at least 90°, it completely emerges below the upper carrier for goods to be refrigerated, that the front end stop is defined by a contact between the lower carrier for goods to be refrigerated (11, 12) and the door rack (15, 16), or that it has a front end stop, which stops the lower carrier for goods to be refrigerated (11, 12) before contact with the door rack (15, 16) when the door is opened by at least 90°, and that the door rack (15, 16) has a depth which amounts to 0.4 to 0.6 times the depth of the carrier for goods to be refrigerated (11, 12), and that the door rack (15, 16) has a depth of at least 13 cm.
A method for optically measuring a sample, comprising: directing probe light to a sample under measurement using a fibre waveguide; directing a first portion of the probe light to propagate away from the sample to the waveguide without reaching the sample; directing a second portion of the probe light to the sample to cause reflection at the sample; wherein the first and second probe light portions are mutually orthogonal polarization modes directing reflected light from the sample to the waveguide to overlap with the first portion at a location where the first portion is generated and to co-propagate with the first portion along a common optical path beginning at the location; separating light from the common optical path into a first light portion and a second light portion; subsequently varying a relative phase delay between the first light portion and the second light portion by varying the relative optical path lengths of the first and second light portions; subsequent to varying the relative phase delay, combining the first light portion and the second light portion to produce combined light; and detecting and processing the combined light to obtain measurements of the sample at different depths corresponding to different relative phase delays caused by varying the relative phase delay. directing probe light to a sample under measurement using a fibre waveguide; directing a first portion of the probe light to propagate away from the sample to the waveguide without reaching the sample; directing a second portion of the probe light to the sample to cause reflection at the sample; wherein the first and second probe light portions are mutually orthogonal polarization modes directing reflected light from the sample to the waveguide to overlap with the first portion at a location where the first portion is generated and to co-propagate with the first portion along a common optical path beginning at the location; separating light from the common optical path into a first light portion and a second light portion; subsequently varying a relative phase delay between the first light portion and the second light portion by varying the relative optical path lengths of the first and second light portions; subsequent to varying the relative phase delay, combining the first light portion and the second light portion to produce combined light; and detecting and processing the combined light to obtain measurements of the sample at different depths corresponding to different relative phase delays caused by varying the relative phase delay.
Synthetic silicate granules comprising: 52.5-59.8 wt% of SiO 2, 33.5-41.1 wt% of Al 2 O 3, and 0.3-3.1 wt% of Na 2 O, based on the weight of the synthetic silicate granules. 52.5-59.8 wt% of SiO 2, 33.5-41.1 wt% of Al 2 O 3, and 0.3-3.1 wt% of Na 2 O,
A method, comprising: receiving, at a service manager located in a remote network, router configuration information of a home router located in a home network separate from the remote network, the router configuration information including at least one slice setting for a service deployment at the home router; wherein the router configuration is received after a successful three-way identification, authentication and authorization between the service manager, a service user entity located at the home network, and a router manager, wherein the service user entity controls the home router in the home network, wherein the service manager is associated with a tenant service provider deploying the service, wherein the router manager manages the home router and provides the router configuration information, wherein the service user entity has a pre-existing security association with the router manager; and configuring, by the service manager, the slice setting on the home router for the service from the remote network.