mhurhangee/patent-ind-claim-en huggingface dataset:
A factor VIII molecule with a domain structure A1-a1-A2-a2-B-a3-A3-C1-C2, in which A1, A2, B, A3, C1 and C2 represent domains and a1, a2 and a3 acidic regions linking said domains, said factor VIII molecule having a reduced capacity to activate NKT cells and is obtainable by: a. identification of at least one NKT cell epitope wherein said epitope motif is [FWTHY]-X 2 X 3 -[ILMV]-X 5 X 6 -[FWTHY]; b. modification of said epitope(s) by replacing the F, W, T, H or Y amino acid in positions P1 and P7 with a non-hydrophobic amino acid residue, wherein at least one of the said NKT cell epitopes is located within the amino acid sequence of SEQ ID NO:1. a. identification of at least one NKT cell epitope wherein said epitope motif is [FWTHY]-X 2 X 3 -[ILMV]-X 5 X 6 -[FWTHY]; b. modification of said epitope(s) by replacing the F, W, T, H or Y amino acid in positions P1 and P7 with a non-hydrophobic amino acid residue, wherein at least one of the said NKT cell epitopes is located within the amino acid sequence of SEQ ID NO:1.
A cartridge assembly for an aerosol delivery system , the cartridge assembly comprising: an active part of the cartridge assembly including a capillary tube , the capillary tube configured to receive a liquid formulation; a susceptor configured to be heated by induction, the susceptor configured to partially surround and heat the capillary tube ; and a pair of displaceable covers , which surround at least the capillary tube and the susceptor . an active part of the cartridge assembly including a capillary tube , the capillary tube configured to receive a liquid formulation; a susceptor configured to be heated by induction, the susceptor configured to partially surround and heat the capillary tube ; and a pair of displaceable covers , which surround at least the capillary tube and the susceptor .
Hand-held power tool device having a drive unit (12a; 12b; 12c) which has at least one drive shaft (14a; 14b; 14c), and having at least one rotary impact mechanism (16a; 16b; 16c) which has at least one intermediate shaft (18a; 18b; 18c), oriented at least substantially in a manner aligned with the drive shaft (14a; 14b; 14c), and an impact mechanism cover (44a; 44b; 44c) arranged between the drive unit (12a; 12b; 12c) and a planetary transmission (50a; 50b; 50c), and having at least one bearing (20a; 20b; 20c) for supporting the drive shaft (14a; 14b; 14c), wherein the bearing is arranged at least partially in a plane (22a; 22b; 22c) intersecting the intermediate shaft (18a; 18b; 18c), said plane (22a; 22b; 22c) extending at least substantially perpendicularly to the intermediate shaft (18a; 18b; 18c), and an intermediate shaft bearing (48a; 48b; 48c), in the form of a radial bearing, which is intended to support the intermediate shaft (18a; 18b; 18c) in a rotatable manner in the impact mechanism cover (44a; 44b; 44c), characterized in that the intermediate shaft (18a; 18b; 18c) has at least one sealing element receptacle (30a; 30b; 30c), wherein the intermediate shaft (18a; 18b; 18c) has at least one sealing element (32a; 32b; 32c) arranged in the sealing element receptacle (30a; 30b; 30c).
A cleaning system comprising a spraying device and a foamable liquid cleaning composition, said spraying device comprising a container holding the foamable liquid cleaning composition, a spray head, and a liquid supply arrangement for transferring the foamable liquid detergent composition from the container to the spray head, said foamable liquid cleaning composition comprising: a) 1 to 20 wt.% of alkoxylated C 8-18 alkyl ether sulfate surfactant having 1 to 30 moles of alkylene oxide; b) 0.1 to 3 wt.% of amphoteric surfactant; c) 2 to 12 wt.% of hydrogen peroxide; d) at least 65 wt.% water; said cleaning composition having a viscosity of less than 100 mPa.s at 25°C and 20 s -1 , and forming a foam with a density of less than 0.4 g/ml when ejected from the spray device through the spray head wherein the cleaning composition contains the alkoxylated C 8-18 alkyl ether sulfate surfactant and the amphoteric surfactant in a weight ratio of .1:1 to 200:1; and wherein the pH of the composition is in the range of 2.5 to 4. a) 1 to 20 wt.% of alkoxylated C 8-18 alkyl ether sulfate surfactant having 1 to 30 moles of alkylene oxide; b) 0.1 to 3 wt.% of amphoteric surfactant; c) 2 to 12 wt.% of hydrogen peroxide; d) at least 65 wt.% water;
Cable core , suitable as a bead core of a pneumatic vehicle tyre, the cable core having a core filament , which is sheathed by at least three plies (3 1 , 3 2 , 3 3 ) comprising filaments , the filaments of each of these at least three plies (3 1 , 3 2 , 3 3 ) having a specific number of turns about the ply lying respectively thereunder or the core filament lying thereunder, the filaments of the first and second plies (3 1 , 3 2 ) having the same number of turns and that the filaments of the third and possibly further ply/plies (3 3 ) have an equal or lower number of turns, the ply (3 1 ) that lies directly on the core filament being referred to as the first ply and the further plies, following in the outward direction, being consecutively numbered in series, characterized in that the cable core has the construction 1×5.0+(10+16+22)×2.0, the filaments of the first ply and those of the second ply (3 1 , 3 2 ) having an equal number of turns of nine each, and the filaments of the third ply (3 3 ) having a number of turns of eight.
A dyeing machine, which includes a storage trough connected with the exit of a conveyance tube , characterized in that : the mentioned storage trough is tiled down to the floor and includes three sections (5; 6; 7), a first section having a smooth surface which is a curved impermeable plate and is of low friction relative to the friction of a relatively high friction second section; the following second section is a sieve which is liquid permeable and a final third section is a row of low friction polytetrafluoroethylene coated plates, wherein, in use, a fabric travels along said conveyance tube to the first section and enters the storage trough , and a dyeing solution ejecting from a nozzle propels the fabric to the first section of the storage trough .
Multilayer security element comprising: - a support , - an optically variable structure borne by the support, so as to be reflective in a first observation direction and transparent in a second observation direction, - a pixelated image , superposed on the optically variable structure, giving the impression of relief when observed in transmitted light in the second observation direction, this impression of relief decreasing when observed in reflected light in the first observation direction, the pixelated image producing a visual depth effect when observed in transmitted light, a visual depth effect being a visual effect by way of which various elements defining a flat image appear to be further away from or closer to an observer owing to a perspective effect, the pixelated image comprising a set of points that appear to be further away or closer when observed in transmitted light, the points being of varied shapes and/or sizes. - a support , - an optically variable structure borne by the support, so as to be reflective in a first observation direction and transparent in a second observation direction, - a pixelated image , superposed on the optically variable structure, giving the impression of relief when observed in transmitted light in the second observation direction, this impression of relief decreasing when observed in reflected light in the first observation direction, the pixelated image producing a visual depth effect when observed in transmitted light, a visual depth effect being a visual effect by way of which various elements defining a flat image appear to be further away from or closer to an observer owing to a perspective effect, the pixelated image comprising a set of points that appear to be further away or closer when observed in transmitted light, the points being of varied shapes and/or sizes.
A coupling for joining pipe elements, said coupling comprising: a plurality of segments attached to one another end to end surrounding a central space for receiving said pipe elements, each of said segments comprising: first and second channels positioned on opposite sides of said segments, each of said channels extending between said ends of said segments and having a first floor and a second floor facing said central space, said first floor having a greater radius of curvature than said second floor; first and second retainers positioned respectively in said first and second channels , each of said retainers comprising a band having oppositely disposed ends, a plurality of teeth being positioned along one edge of said band and projecting toward said central space , at least one tab being positioned along an opposite edge of said band, said band overlying said first floor, said at least one tab overlying said second floor when said retainers are positioned within said channels. first and second channels positioned on opposite sides of said segments, each of said channels extending between said ends of said segments and having a first floor and a second floor facing said central space, said first floor having a greater radius of curvature than said second floor; first and second retainers positioned respectively in said first and second channels , each of said retainers comprising a band having oppositely disposed ends, a plurality of teeth being positioned along one edge of said band and projecting toward said central space , at least one tab being positioned along an opposite edge of said band, said band overlying said first floor, said at least one tab overlying said second floor when said retainers are positioned within said channels.
An assembly comprising a liquid carrying line (44; 144; 162) of a gas turbine engine and a hydraulic snubber insert (42; 142) for the liquid carrying line (44; 144; 162), the insert (42; 142) comprising an elongated stem (46; 146) and at least one segment (48; 148) extending transversally from the stem (46; 146), each segment (48; 148) having a size and shape mating a cross-sectional size and shape of the liquid carrying line (44; 144; 162), and having at least one aperture (50; 150), the insert (42; 142) being configured for the at least one segment (48; 148) to be pushable snugly inside and along the liquid carrying line (44; 144; 162) and pullable out from the liquid carrying line (44; 144; 162) via the stem (46; 146), wherein the stem (46; 146) is flexible, characterised in that : the liquid carrying line (44; 144; 162) is curvilinear; and in that the at least one segment (48; 148) includes a plurality of segments (48; 148) interspaced from one another along a length of the stem (46; 146), and at least one of : a number of the plurality of segments (48; 148); a number of said at least one aperture (50; 150) per segment (48; 148) a configuration of said at least one aperture (50; 150) per segment (48; 148); a shape of the apertures (50; 150); and a configuration of the at least one aperture (50; 150) in each segment (48; 148) relative to the at least one aperture (50; 150) of the other segments (48; 148), are configured to provide a substantial attenuation of repetitive pressure transients of a pump in liquids in the form of pressure ripples during operation of the gas turbine engine while preserving response time of slower pressure variations across the hydraulic snubber insert (42; 142) via the apertures (50; 150). the liquid carrying line (44; 144; 162) is curvilinear; and in that the at least one segment (48; 148) includes a plurality of segments (48; 148) interspaced from one another along a length of the stem (46; 146), and at least one of : a number of the plurality of segments (48; 148); a number of said at least one aperture (50; 150) per segment (48; 148) a configuration of said at least one aperture (50; 150) per segment (48; 148); a shape of the apertures (50; 150); and a configuration of the at least one aperture (50; 150) in each segment (48; 148) relative to the at least one aperture (50; 150) of the other segments (48; 148), a number of the plurality of segments (48; 148); a number of said at least one aperture (50; 150) per segment (48; 148) a configuration of said at least one aperture (50; 150) per segment (48; 148); a shape of the apertures (50; 150); and a configuration of the at least one aperture (50; 150) in each segment (48; 148) relative to the at least one aperture (50; 150) of the other segments (48; 148), are configured to provide a substantial attenuation of repetitive pressure transients of a pump in liquids in the form of pressure ripples during operation of the gas turbine engine while preserving response time of slower pressure variations across the hydraulic snubber insert (42; 142) via the apertures (50; 150).
A nonwoven fabric to be used for a liquid permeable sheet of an absorbent article , which includes a thickness direction (T), a plane direction (P), a first surface , and a second surface , the nonwoven fabric comprising: thermoplastic resin fibers ; cellulose based fibers a portion of which configuring a plurality of fiber masses ; and a plurality of gap portions , wherein a gap portion is adjacent to a first region in the thickness direction, the first region facing the first surface in each of the plurality of fiber masses ; and each of the plurality of fiber masses is not joined to the thermoplastic resin fibers . thermoplastic resin fibers ; cellulose based fibers a portion of which configuring a plurality of fiber masses ; and a plurality of gap portions , wherein a gap portion is adjacent to a first region in the thickness direction, the first region facing the first surface in each of the plurality of fiber masses ; and each of the plurality of fiber masses is not joined to the thermoplastic resin fibers .
Support frame configured to bear a heat exchanger comprising a flange for passage of coolant fluid, the frame comprising a side wall in which a slot is produced for the flange to pass through, the side wall comprises at least one rim placed near an end of the slot and characterized in that the rim being arranged at least partially through the slot so as to define an insertion path for the flange which is inclined relative to the normal to the side wall, said rim also being configured to form a pivot point for the flange.
A secondary radar comprising an antenna having a radiating pattern forming a sum channel, called SUM, a radiating pattern forming a difference channel called DIFF and a pattern forming a control channel called CONT, means for generating at least interrogation messages on the SUM channel and ISLS signals on the CONT channel, means for transmitting these messages via the SUM channel and via the CONT channel respectively, means for receiving and processing signals received via the SUM, DIFF and CONT channels, configured for detecting the replies of targets on the signals received via the SUM and/or DIFF channels and carrying out deviation measurement processing and RSLS processing on these replies, characterized in that the transmission means are configured so that, for each target independently, the width of the beam for transmitting interrogations and receiving mode S selective replies is controlled dynamically on the basis of the movement window of said target and the position of the axis of said antenna in said window, in order to provide the detection of said target while reducing the number of selective interrogations by a selective sub-interrogation of said target and while ensuring its precise positioning in azimuth: - by pre-locating said target at the edge of the main reception lobe of said antenna by deviation measurement between the signals received on the DIFF and SUM channels; - by selectively re-interrogating said pre-located target in mode S by calculation of the roll-call period nearest to the centre of said main lobe to ensure precision in azimuth. - by pre-locating said target at the edge of the main reception lobe of said antenna by deviation measurement between the signals received on the DIFF and SUM channels; - by selectively re-interrogating said pre-located target in mode S by calculation of the roll-call period nearest to the centre of said main lobe to ensure precision in azimuth.
A multirotor aircraft with an airframe that extends in a longitudinal direction , and with at least one thrust producing unit for producing thrust in a predetermined thrust direction , wherein the at least one thrust producing unit comprises a shrouding that is associated with at least one rotor assembly comprising at least one electrical engine , wherein the shrouding defines a cylindrical air duct that is axially delimited by an air inlet region and an air outlet region , wherein a carrier beam is at least mounted at a leading edge region of the cylindrical air duct to the shrouding such that the carrier beam is arranged inside of the cylindrical air duct and oriented at least essentially in parallel to the longitudinal direction , wherein the at least one electrical engine is mounted to the carrier beam , characterised in that the shrouding comprises a forward beam and an aft beam which both connect the carrier beam to the airframe , the forward beam and the aft beam being arranged outside of the cylindrical air duct , wherein the forward beam comprises a forward flange and the aft beam comprises an aft flange , the forward flange and the aft flange being rigidly attached to the airframe .
A method for receiving a signal by a user equipment in a wireless communication system, the method comprising: receiving a higher layer signal indicating a subframe in which a detection of downlink control information is performed; receiving (S902) the downlink control information comprising scheduling information through a physical downlink control channel within the indicated subframe, wherein the downlink control information further includes information indicating whether the downlink control information is targeted to K subframes, K being greater than 1, or targeted to one subframe, wherein the scheduling information is not applied to at least a subframe configured for a multicast-broadcast single-frequency network, MBSFN and a subframe configured to transmit system information; and when the downlink control information is targeted to the K subframes, receiving (S904) a data signal using the scheduling information in M subframes other than the at least one subframe from among the K subframes. receiving a higher layer signal indicating a subframe in which a detection of downlink control information is performed; receiving (S902) the downlink control information comprising scheduling information through a physical downlink control channel within the indicated subframe, wherein the downlink control information further includes information indicating whether the downlink control information is targeted to K subframes, K being greater than 1, or targeted to one subframe, wherein the scheduling information is not applied to at least a subframe configured for a multicast-broadcast single-frequency network, MBSFN and a subframe configured to transmit system information; and when the downlink control information is targeted to the K subframes, receiving (S904) a data signal using the scheduling information in M subframes other than the at least one subframe from among the K subframes.
An aircraft comprising: - a flight deck door , wherein the flight deck door , when in a closed position , separates a flight deck area of the aircraft from a cabin area of the aircraft ; - a privacy door disposed within the cabin area of the aircraft and aft of the flight deck door such that the privacy door , when in a closed position , separates the cabin area into an intermediate cabin area between the privacy door and the flight deck door and a main cabin area aft of the privacy door , wherein the privacy door further comprises a decompression latch ; - a door frame comprising a first post and a second post , wherein the privacy door is rotatably coupled to the first post via a set of hinges such that the privacy door is rotatable into the intermediate cabin area to an open position ; and a latch recess positioned within the second post , wherein the latch recess is arranged to engage the decompression latch of the privacy door when the privacy door is in the closed position , and wherein the decompression latch is configured to disengage from the latch recess in response to a decompression of the aircraft detected forward of the privacy door , wherein the privacy door comprises a slam latch positioned to engage a slot in the first post of the door frame when the privacy door is in the open position and when the slam latch is in a first position , wherein the slam latch is coupled to a lever positioned on a forward side of the privacy door , and wherein the lever is operable to move the slam latch away from the first post to a second position so as to disengage the slam latch from the slot , wherein the privacy door further comprises a slam latch spring positioned to bias the slam latch toward the first post , wherein the first post comprises a cylindrical striker , wherein the cylindrical striker comprises the slot . - a flight deck door , wherein the flight deck door , when in a closed position , separates a flight deck area of the aircraft from a cabin area of the aircraft ; - a privacy door disposed within the cabin area of the aircraft and aft of the flight deck door such that the privacy door , when in a closed position , separates the cabin area into an intermediate cabin area between the privacy door and the flight deck door and a main cabin area aft of the privacy door , wherein the privacy door further comprises a decompression latch ; - a door frame comprising a first post and a second post , wherein the privacy door is rotatably coupled to the first post via a set of hinges such that the privacy door is rotatable into the intermediate cabin area to an open position ; and
Domestic appliance having a carcass and a sliding element which can be extended therefrom by means of a drive assembly arranged in or on the carcass, wherein a liftable storage container can be moved out of the carcass by means of the sliding element , wherein a push-chain assembly is provided which has at least one push chain which is driven by the drive assembly , characterized in that the at least one push chain is fixed to the storage container by a free end and extends between the drive assembly and the storage container through a return guide which is arranged on the sliding element , wherein the return guide converts a horizontal movement of the push chain into a vertical movement.
A cold runner block in a vertically operating injection molding machine for processing elastomer materials with an upper fixed molding platen and a molding platen arranged thereunder which is movable relative to the fixed molding platen, between which a molding tool having a plurality of mold cavities is arranged and wherein the cold runner block is arranged between the fixed molding platen and the molding tool, the cold runner block containing a distribution plate having the cold runners and containing a nozzle plate with nozzles each assigned to one of the plurality of mold cavities, characterized in that the distribution plate formed from a plurality of distribution strips (10-40) is arranged on a retaining plate , which can be fastened to the fixed, feed-side molding platen, in such a way that each distribution strip (10-40) is connected by means of two bolts to the retaining plate in that the head of each bolt facing away from the distribution strip (10-40) forms a retaining element which is T-shaped in section, the retaining element being displaceably guided in the direction transverse to the distribution strip's longitudinal axis in guide rails which are formed in the retaining plate and are designed in section to complement the bolt head .