mhurhangee/patent-ind-claim-en huggingface dataset:
An aerosol-generating device , comprising: a heating base , comprising a heating cavity ; and a heating member , configured to accommodate and heat an aerosol-generating substrate , wherein the heating member is disposed in the heating cavity ; wherein the heating member comprises a first sidewall , and a first airflow channel is formed between the first sidewall and the inner surface of the heating cavity characterised in that at least one protrusion is disposed on the inner surface of the first sidewall , the protrusion is configured to make a second airflow channel formed between the first sidewall and the aerosol-generating substrate , and both the first airflow channel and the second airflow channel are led from the outside of the aerosol-generating device to the bottom of the heating cavity . a heating base , comprising a heating cavity ; and a heating member , configured to accommodate and heat an aerosol-generating substrate , wherein the heating member is disposed in the heating cavity ; wherein the heating member comprises a first sidewall , and a first airflow channel is formed between the first sidewall and the inner surface of the heating cavity characterised in that at least one protrusion is disposed on the inner surface of the first sidewall , the protrusion is configured to make a second airflow channel formed between the first sidewall and the aerosol-generating substrate , and both the first airflow channel and the second airflow channel are led from the outside of the aerosol-generating device to the bottom of the heating cavity .
A method of receiving downlink data by a device in a wireless communication system, wherein plural frequency blocks are configured in a bandwidth, and downlink data reception can be scheduled per frequency block, the method comprising: receiving downlink scheduling information including 1) a frequency block indicator indicating a frequency block of the plural frequency blocks and 2) resource allocation information assigned only for the indicated frequency block among the plural frequency blocks; and receiving the downlink data via a time-frequency region indicated by the resource allocation information , within the indicated frequency block among the plural frequency blocks. receiving downlink scheduling information including 1) a frequency block indicator indicating a frequency block of the plural frequency blocks and 2) resource allocation information assigned only for the indicated frequency block among the plural frequency blocks; and receiving the downlink data via a time-frequency region indicated by the resource allocation information , within the indicated frequency block among the plural frequency blocks.
A DNA construct comprising: (A) a polynucleotide encoding a Cry1B polypeptide having insecticidal activity and comprising a sequence having at least 95% identity to any one of SEQ ID NO: 3, SEQ ID NO: 5, SEQ ID NO: 7, SEQ ID NO: 9, SEQ ID NO: 11, SEQ ID NO: 13, SEQ ID NO: 15, SEQ ID NO: 17, SEQ ID NO: 19, SEQ ID NO: 21, SEQ ID NO: 23, SEQ ID NO: 25, SEQ ID NO: 27, SEQ ID NO: 29, SEQ ID NO: 31, SEQ ID NO: 33, SEQ ID NO: 35, SEQ ID NO: 37, SEQ ID NO: 39, SEQ ID NO: 41, SEQ ID NO: 43, and SEQ ID NO: 45; and (B) one or more of: (i) a polynucleotide encoding a PtIP-50 and a PtIP-65 polypeptide having insecticidal activity; and (ii) a polynucleotide encoding a PtIP-83 polypeptide having insecticidal activity. (A) a polynucleotide encoding a Cry1B polypeptide having insecticidal activity and comprising a sequence having at least 95% identity to any one of SEQ ID NO: 3, SEQ ID NO: 5, SEQ ID NO: 7, SEQ ID NO: 9, SEQ ID NO: 11, SEQ ID NO: 13, SEQ ID NO: 15, SEQ ID NO: 17, SEQ ID NO: 19, SEQ ID NO: 21, SEQ ID NO: 23, SEQ ID NO: 25, SEQ ID NO: 27, SEQ ID NO: 29, SEQ ID NO: 31, SEQ ID NO: 33, SEQ ID NO: 35, SEQ ID NO: 37, SEQ ID NO: 39, SEQ ID NO: 41, SEQ ID NO: 43, and SEQ ID NO: 45; and (B) one or more of: (i) a polynucleotide encoding a PtIP-50 and a PtIP-65 polypeptide having insecticidal activity; and (ii) a polynucleotide encoding a PtIP-83 polypeptide having insecticidal activity. (i) a polynucleotide encoding a PtIP-50 and a PtIP-65 polypeptide having insecticidal activity; and (ii) a polynucleotide encoding a PtIP-83 polypeptide having insecticidal activity.
A composite material formulation comprising at least one liquid crystal, composed of at least one mesogen, wherein the liquid crystal is 4-pentyl-4'-cyanobiphenyl; at least one ionic liquid, composed by at least one organic salt of composition X+ and Y-, where X+ represents cation of the salt and Y- represents the anion of the salt, wherein the ionic liquid is [BMIM][CI], [BMIM][DCA] or [BMIM][FeCl 4 ]; at least one polymer, wherein the polymer is dextran or gelatin; and at least one solvent; provided that when the polymer is dextran the ionic liquid is LBMIM][Cl]. at least one liquid crystal, composed of at least one mesogen, wherein the liquid crystal is 4-pentyl-4'-cyanobiphenyl; at least one ionic liquid, composed by at least one organic salt of composition X+ and Y-, where X+ represents cation of the salt and Y- represents the anion of the salt, wherein the ionic liquid is [BMIM][CI], [BMIM][DCA] or [BMIM][FeCl 4 ]; at least one polymer, wherein the polymer is dextran or gelatin; and at least one solvent; provided that when the polymer is dextran the ionic liquid is LBMIM][Cl].
A compound of formula I wherein R 1 is a branched chain alkyl consisting of 10 to 31 carbons, R 2 is a linear alkenyl consisting of 2 to 20 carbons, R 3 is a linear or branched alkylene consisting of 1 to 6 carbons, R 4 and R 5 are the same or different, each a hydrogen or a linear or branched alkyl consisting of 1 to 6 carbons; L 1 and L 2 are the same or different, each a linear alkylene of 1 to 20 carbons or a linear alkenylene of 2 to 20 carbons, and X 1 is S; or a salt or solvate thereof. R 1 is a branched chain alkyl consisting of 10 to 31 carbons, R 2 is a linear alkenyl consisting of 2 to 20 carbons, R 3 is a linear or branched alkylene consisting of 1 to 6 carbons, R 4 and R 5 are the same or different, each a hydrogen or a linear or branched alkyl consisting of 1 to 6 carbons; L 1 and L 2 are the same or different, each a linear alkylene of 1 to 20 carbons or a linear alkenylene of 2 to 20 carbons, and X 1 is S;
A method for capturing and executing graphics processing operations, comprising: activating a memory trap function to cause a graphics processing unit , GPU, to report memory accesses in executing graphics processing operations; receiving , based on activating the memory trap function and for each of a sequence of executed graphics processing operations executed by the GPU, a sequence of multiple memory accessing commands and associated portions of memory modified based on executing the sequence of executed graphics processing operations, wherein the sequence of multiple memory accessing commands results from executing the sequence of executed graphics processing operations by the GPU; storing , in a repository , each of the sequence of multiple memory accessing commands and associated portions of memory; the method characterized by the further step of: providing , to the GPU, at least a portion of the sequence of multiple memory accessing commands and associated portions of memory to emulate re-executing of the sequence of graphics processing operations by the GPU by executing the provided portion of the sequence of memory commands. activating a memory trap function to cause a graphics processing unit , GPU, to report memory accesses in executing graphics processing operations; receiving , based on activating the memory trap function and for each of a sequence of executed graphics processing operations executed by the GPU, a sequence of multiple memory accessing commands and associated portions of memory modified based on executing the sequence of executed graphics processing operations, wherein the sequence of multiple memory accessing commands results from executing the sequence of executed graphics processing operations by the GPU; storing , in a repository , each of the sequence of multiple memory accessing commands and associated portions of memory; the method characterized by the further step of: providing , to the GPU, at least a portion of the sequence of multiple memory accessing commands and associated portions of memory to emulate re-executing of the sequence of graphics processing operations by the GPU by executing the provided portion of the sequence of memory commands.
A hydropneumatic diaphragm cylinder comprising a cylinder casing and two diaphragm pistons which are disposed in a cylinder space array and each have a diaphragm extending radially between a cylinder wall and a piston rod unit , the diaphragm pistons being disposed at an axial offset on the piston rod unit in such a manner that pressurizing one of the diaphragm pistons effects a retracting of the piston rod unit and pressurizing the other diaphragm piston effects an extracting of the piston rod unit , the cylinder space array comprising two cylinder spaces which are disposed separately in the cylinder casing and each receive a diaphragm piston , a piston-rod middle piece being formed between the diaphragm pistons and penetrating a cylinder middle wall separating the cylinder spaces , the diaphragm pistons being pressurized in two adjacent pressure chambers axially limited by the cylinder middle wall and one diaphragm piston each, the piston-rod middle piece having a smaller diameter than the piston rod part of the piston-rod unit protruding from the cylinder casing .
Catheter tubing comprising (i) an outer surface having a circumference, (ii) strips of radiopaque material that extend along the length of the catheter tubing, (iii) an antimicrobial coating applied to the outer surface in a pattern such that the pattern does not cover the entire circumference of the outer surface, wherein the pattern comprises a plurality of stripes that are formed on the outer surface by passing the catheter tubing through a die after the antimicrobial coating is applied over the entire circumference of the outer surface, and wherein the plurality of stripes of the pattern are positioned overtop and align with the strips of radiopaque material contained within the catheter tubing. (i) an outer surface having a circumference, (ii) strips of radiopaque material that extend along the length of the catheter tubing, (iii) an antimicrobial coating applied to the outer surface in a pattern such that the pattern does not cover the entire circumference of the outer surface, wherein the pattern comprises a plurality of stripes that are formed on the outer surface by passing the catheter tubing through a die after the antimicrobial coating is applied over the entire circumference of the outer surface, and wherein the plurality of stripes of the pattern are positioned overtop and align with the strips of radiopaque material contained within the catheter tubing.
A sheath for passage of an implant , comprising: at least one stiff wall portion having a stiff wall radial thickness and extending generally parallel to and partially around an elongate axis of the sheath and defining at least two edges , the two edges extending generally axially and between an inner surface and outer surface of the stiff wall portion ; and at least one elastic wall portion having an elastic wall radial thickness equal to the stiff wall radial thickness and extending generally parallel to and partially around the elongate axis , the elastic wall portion extending between the edges of the stiff wall portion so as to define an expandable tubular layer with a consistent radial thickness; wherein the expandable tubular layer has a starting profile and defines a lumen and wherein the expandable tubular layer is configured to temporarily expand at least at the elastic wall portion to allow passage of an implant through the lumen and then return to approximate the starting profile after passage of an implant through the lumen , characterized in that the sheath further comprises an intermediate tubular layer comprising a plurality of braided fibers and extending between the expandable tubular layer and an elastic outer tubular layer extending around the expandable tubular layer wherein the stiff and elastic wall portions are arc segments of the expandable tubular layer . at least one stiff wall portion having a stiff wall radial thickness and extending generally parallel to and partially around an elongate axis of the sheath and defining at least two edges , the two edges extending generally axially and between an inner surface and outer surface of the stiff wall portion ; and at least one elastic wall portion having an elastic wall radial thickness equal to the stiff wall radial thickness and extending generally parallel to and partially around the elongate axis , the elastic wall portion extending between the edges of the stiff wall portion so as to define an expandable tubular layer with a consistent radial thickness; wherein the expandable tubular layer has a starting profile and defines a lumen and wherein the expandable tubular layer is configured to temporarily expand at least at the elastic wall portion to allow passage of an implant through the lumen and then return to approximate the starting profile after passage of an implant through the lumen , characterized in that the sheath further comprises an intermediate tubular layer comprising a plurality of braided fibers and extending between the expandable tubular layer and an elastic outer tubular layer
A fuel system for a gas turbine engine comprising: a flow inlet conduit ; a primary conduit branching from the flow inlet conduit for delivering flow to a set of primary nozzles; an equalization bypass valve "EBV" that connects between the flow inlet conduit and a secondary conduit for delivering flow to a set of secondary nozzles, wherein the EBV is connected to an equalization conduit "EC" to apportion flow from the flow inlet conduit to the secondary conduit; a pressure equalization solenoid "PES" connected to the EC to selectively connect at least one of a servo supply pressure "PFA" conduit or a return pressure "PDF" conduit into fluid communication with the EC; an EBV rate limiting orifice "RLO" connected in the PDF conduit; a bypass conduit branching from the PDF conduit on a first side of the EBV rate limiting orifice and reconnecting to the PDF conduit on a second side of the EBV rate limiting orifice; and an orifice bypass valve "OBV" connected to the bypass conduit, wherein the OBV acts to selectively bypass the EBV RLO. a flow inlet conduit ; a primary conduit branching from the flow inlet conduit for delivering flow to a set of primary nozzles; an equalization bypass valve "EBV" that connects between the flow inlet conduit and a secondary conduit for delivering flow to a set of secondary nozzles, wherein the EBV is connected to an equalization conduit "EC" to apportion flow from the flow inlet conduit to the secondary conduit; a pressure equalization solenoid "PES" connected to the EC to selectively connect at least one of a servo supply pressure "PFA" conduit or a return pressure "PDF" conduit into fluid communication with the EC; an EBV rate limiting orifice "RLO" connected in the PDF conduit; a bypass conduit branching from the PDF conduit on a first side of the EBV rate limiting orifice and reconnecting to the PDF conduit on a second side of the EBV rate limiting orifice; and an orifice bypass valve "OBV" connected to the bypass conduit, wherein the OBV acts to selectively bypass the EBV RLO.
Aircraft empennage, comprising: - a vertical tail plane , - a rear fuselage section comprising a skin (1.1) and internal reinforcing members, the vertical tail plane being attached to the rear fuselage section , - a horizontal tail plane comprising two lateral torsion boxes , characterized in that the horizontal tail plane further comprises: - a framework located between the two lateral torsion boxes and in connection with them , the framework comprising a front spar , a rear spar and two ribs extending between the front spar and the rear spar , each rib adjacent to a lateral torsion box , the framework enclosing a portion of the vertical tail plane along its spanwise direction, and the aircraft empennage comprising an attachment assembly attaching the framework to the rear fuselage section , the attachment assembly crossing the skin (1.1) and extending between the internal reinforcing members of the rear fuselage section and the framework . - a vertical tail plane , - a rear fuselage section comprising a skin (1.1) and internal reinforcing members, the vertical tail plane being attached to the rear fuselage section , - a horizontal tail plane comprising two lateral torsion boxes , characterized in that the horizontal tail plane further comprises: - a framework located between the two lateral torsion boxes and in connection with them , the framework comprising a front spar , a rear spar and two ribs extending between the front spar and the rear spar , each rib adjacent to a lateral torsion box , the framework enclosing a portion of the vertical tail plane along its spanwise direction,
A slitting device for a packaging film comprising a plurality of cutting knives for severing the packaging film fed to the cutting knives in a film transport direction (F), the plurality of cutting knives including a left cutting knife , a right cutting knife and at least one intermediate cutting knife in the film transport direction (F), wherein the slitting device includes at least one feed unit assigned to the intermediate cutting knife and configured for transporting the packaging film by means of which the packaging film can be conveyed immediately at the location of a cutting operation in the film transport direction (F), wherein for conveying the packaging film at the feed unit , a non-positive coupling is produced between a first conveying element supported above the packaging film and a second conveying element supported below the packaging film , the first conveying element being a counter roller and the second conveying element being a drivable feed roller , which are supported to be rotatable with equal circumferential speeds (v) via the non-positive coupling , wherein an infeed set for the packaging film is positioned on the feed unit on the upstream side in the film transport direction (F) within a film transport plane (E) at a predetermined distance between 1 mm and 50 mm or 5% to 15% of the diameter of the intermediate cutting knife from a cutting edge of the intermediate cutting knife formed for the cutting operation. for conveying the packaging film at the feed unit , a non-positive coupling is produced between a first conveying element supported above the packaging film and a second conveying element supported below the packaging film , the first conveying element being a counter roller and the second conveying element being a drivable feed roller , which are supported to be rotatable with equal circumferential speeds (v) via the non-positive coupling , wherein an infeed set for the packaging film is positioned on the feed unit on the upstream side in the film transport direction (F) within a film transport plane (E) at a predetermined distance between 1 mm and 50 mm or 5% to 15% of the diameter of the intermediate cutting knife from a cutting edge of the intermediate cutting knife formed for the cutting operation.
Bumper device for a vehicle for supporting forces which occur during a collision of the vehicle with a barrier (B), wherein the vehicle (1; 101) has at least two bumper support members which are arranged parallel to the vehicle longitudinal direction (X) and which are connected, at the front end thereof in the direction of travel (F), to at least one bumper crossmember (20; 120) arranged transversely with respect to the vehicle longitudinal direction (X), and wherein the bumper device (2; 102) in each case has a distal force introduction structure (3; 103) which projects laterally beyond the bumper crossmember (20; 120) and which is situated at least in part in front of a wheelhouse accommodating a vehicle wheel , wherein the respective distal force introduction structure (3; 103) is mounted on the bumper crossmember (20; 120) or on the bumper support member so as to be pivotable about an axis (z) parallel to the vehicle vertical axis (Z), or is attached thereto with the ability to be bent away, and has an actuator portion (36; 136) protruding forwards in the direction of travel (F), characterized in that the respective distal force introduction structure (3; 103) is configured in such a way that, in the collision-induced pivoted or bent-away state thereof, the free end (33; 133), which is on the vehicle outer side, of the distal force introduction structure (3; 103) is displaced in the direction of the tread of the vehicle wheel and fixes the vehicle wheel in its current position.
A safety device for a ladder for protecting a user of the ladder, comprising: a guard member formed extending in one direction, the guard member being mountable on the ladder ; and a plurality of fixing members connected to the guard member , spaced apart from each other along a longitudinal direction of the guard member , and configured to fix the guard member to the ladder , wherein the guard member is configured to protrude at least partially toward a rear side of the ladder and cover a rear surface of the ladder , characterized in that the guard member includes: a connection portion to which the fixing members are connected; and a cover portion provided at at least one of both ends of the connection portion and provided with a folding line extending in the other direction perpendicular to the one direction, and the cover portion is configured to be selectively unfolded about the folding line . a guard member formed extending in one direction, the guard member being mountable on the ladder ; and a plurality of fixing members connected to the guard member , spaced apart from each other along a longitudinal direction of the guard member , and configured to fix the guard member to the ladder , wherein the guard member is configured to protrude at least partially toward a rear side of the ladder and cover a rear surface of the ladder , characterized in that the guard member includes: a connection portion to which the fixing members are connected; and a cover portion provided at at least one of both ends of the connection portion and provided with a folding line extending in the other direction perpendicular to the one direction, and the cover portion is configured to be selectively unfolded about the folding line . a connection portion to which the fixing members are connected; and a cover portion provided at at least one of both ends of the connection portion and provided with a folding line extending in the other direction perpendicular to the one direction, and the cover portion is configured to be selectively unfolded about the folding line .
A bushing for a track assembly, comprising: a tubular bushing substrate having a longitudinal length and an outer surface , characterized in that the outer surface includes at least one flat portion ; and at least one white iron member , wherein the at least one white iron member includes a flat inner surface , and wherein the flat inner surface of the at least one white iron member is fixed to the flat portion of the outer surface of the tubular bushing substrate . a tubular bushing substrate having a longitudinal length and an outer surface , characterized in that the outer surface includes at least one flat portion ; and at least one white iron member , wherein the at least one white iron member includes a flat inner surface , and wherein the flat inner surface of the at least one white iron member is fixed to the flat portion of the outer surface of the tubular bushing substrate .