mhurhangee/patent-ind-claim-en huggingface dataset:
Modified bacteria suitable for human or non-human animal consumption that express heterologous secreted antigen A (SagA), wherein the modified bacteria are not E. coli ; wherein the heterologous SagA is Enterococcus faecium SagA; and wherein the heterologous SagA comprises a sequence that has at least 90% identity to the sequence of SEQ ID NO: 1 and that retains amino acid 389 through amino acid 530 of SEQ ID NO:1.
A process for making cyclopentadiene (CPD) and/or dicyclopentadiene (DCPD), the process comprising: (I) feeding a C5 feedstock comprising at least one acyclic C5 hydrocarbon and a light hydrocarbon co-feedstock comprising at least one C1 to C4 hydrocarbon into a first reactor; (II) contacting the at least one acyclic C5 hydrocarbon with a catalyst under conversion conditions to obtain a first reactor hydrocarbon effluent from an outlet on the first reactor comprising: C5 components including CPD and acyclic diolefins; light components including hydrogen and C1-C4 hydrocarbons; one-ring aromatics; and multiple-ring aromatics; wherein sufficient light hydrocarbon co-feedstock is provided in step (I) such that: the total absolute pressure of the first reactor hydrocarbon effluent at the outlet is P(fre); the total partial pressure of C5 hydrocarbons in the first reactor hydrocarbon effluent at the outlet is P(C5); the partial pressure of hydrogen in the first reactor hydrocarbon effluent at the outlet is P(H2); where [P(C5) + P(H2)] ÷ P(fre) ≤ 0.90; and P(fre) is greater than 100 kilopascal absolute; and wherein dicyclopentadiene is obtainable from cyclopentadiene via Diels-Alder condensation. (I) feeding a C5 feedstock comprising at least one acyclic C5 hydrocarbon and a light hydrocarbon co-feedstock comprising at least one C1 to C4 hydrocarbon into a first reactor; (II) contacting the at least one acyclic C5 hydrocarbon with a catalyst under conversion conditions to obtain a first reactor hydrocarbon effluent from an outlet on the first reactor comprising: C5 components including CPD and acyclic diolefins; light components including hydrogen and C1-C4 hydrocarbons; one-ring aromatics; and multiple-ring aromatics; wherein sufficient light hydrocarbon co-feedstock is provided in step (I) such that: the total absolute pressure of the first reactor hydrocarbon effluent at the outlet is P(fre); the total partial pressure of C5 hydrocarbons in the first reactor hydrocarbon effluent at the outlet is P(C5); the partial pressure of hydrogen in the first reactor hydrocarbon effluent at the outlet is P(H2); where [P(C5) + P(H2)] ÷ P(fre) ≤ 0.90; and P(fre) is greater than 100 kilopascal absolute; and wherein dicyclopentadiene is obtainable from cyclopentadiene via Diels-Alder condensation.
A system for supplying air for a commercial vehicle with an air compressor , characterized by: - a flow rate sensor configured to provide a sensor signal indicative of a flow rate of air supplied by the compressor ; and - an air processing unit configured to process compressed air provided by the air compressor wherein the flow rate sensor is configured to sense the flow rate based on at least one of the following principles: a hot film measurement principle, a hot wire measurement principle, a floating body measurement principle, a Coriolis measurement principle, a rotary measurement principle, a reciprocating measurement principle, a vortex measurement principle, an ultrasonic measurement principle, a laser Doppler measurement principle. - a flow rate sensor configured to provide a sensor signal indicative of a flow rate of air supplied by the compressor ; and - an air processing unit configured to process compressed air provided by the air compressor
A gas turbine engine comprising: a plurality of compressor rotors ; a plurality of turbine rotors ; a tie shaft , the compressor and turbine rotors being constrained to rotate with the tie shaft in a normal operating condition; an upstream hub located upstream of the compressor rotors , the upstream hub in threaded engagement with the tie shaft , threads of the upstream hub handed in a first manner when viewed from an upstream location; and a downstream abutment member located downstream of the turbine rotors , the downstream abutment member in threaded engagement with the tie shaft , threads of the downstream abutment member handed in the first manner when viewed from a downstream location, wherein the tie shaft includes a first set of threads corresponding to the threads of the upstream hub and a second set of threads corresponding to the threads of the downstream abutment member , the threads of the upstream hub , the threads of the downstream abutment member , and the first and second sets of threads each including load flanks and clearance flanks , and, when in an initial assembled condition, the load flanks of the upstream hub contact the load flanks of the first set of threads , and the load flanks of the downstream abutment member contact the load flanks of the second set of threads ; characterised in that : when in an attempted unwinding condition, the load flanks of the upstream hub contact the load flanks of the first set of threads , and the clearance flanks of the downstream abutment member contact the clearance flanks of the second set of threads . a plurality of compressor rotors ; a plurality of turbine rotors ; a tie shaft , the compressor and turbine rotors being constrained to rotate with the tie shaft in a normal operating condition; an upstream hub located upstream of the compressor rotors , the upstream hub in threaded engagement with the tie shaft , threads of the upstream hub handed in a first manner when viewed from an upstream location; and a downstream abutment member located downstream of the turbine rotors , the downstream abutment member in threaded engagement with the tie shaft , threads of the downstream abutment member handed in the first manner when viewed from a downstream location, wherein the tie shaft includes a first set of threads corresponding to the threads of the upstream hub and a second set of threads corresponding to the threads of the downstream abutment member , the threads of the upstream hub , the threads of the downstream abutment member , and the first and second sets of threads each including load flanks and clearance flanks , and, when in an initial assembled condition, the load flanks of the upstream hub contact the load flanks of the first set of threads , and the load flanks of the downstream abutment member contact the load flanks of the second set of threads ;
A stapling assembly, comprising: a first jaw; a second jaw movable relative to said first jaw; a staple cartridge comprising a plurality of staples, wherein each said staple is comprised of a wire defined by a staple diameter, and wherein each said staple comprises staple legs; and an anvil configured to deform said staples, said anvil comprising: a tissue-engaging surface ; and a pair of forming pockets defined in said tissue-engaging surface, wherein said pair of forming pockets is configured to deform the staple legs of a said staple, characterised in that said pair of forming pockets comprises: a proximal forming pocket comprising a forming surface , wherein said forming surface comprises an entry zone comprising a first radius of curvature and an exit zone comprising a second radius of curvature , wherein said first radius of curvature and said second radius of curvature comprise a ratio of 1.5:1 to 3:1, and wherein said first radius of curvature is between 8 times and 10 times larger than said staple diameter, and wherein said second radius of curvature is between 4 and 6 times larger than said staple diameter; and a distal forming pocket . a first jaw; a second jaw movable relative to said first jaw; a staple cartridge comprising a plurality of staples, wherein each said staple is comprised of a wire defined by a staple diameter, and wherein each said staple comprises staple legs; and an anvil configured to deform said staples, said anvil comprising: a tissue-engaging surface ; and a pair of forming pockets defined in said tissue-engaging surface, wherein said pair of forming pockets is configured to deform the staple legs of a said staple, a tissue-engaging surface ; and a pair of forming pockets defined in said tissue-engaging surface, wherein said pair of forming pockets is configured to deform the staple legs of a said staple, characterised in that said pair of forming pockets comprises: a proximal forming pocket comprising a forming surface , wherein said forming surface comprises an entry zone comprising a first radius of curvature and an exit zone comprising a second radius of curvature , wherein said first radius of curvature and said second radius of curvature comprise a ratio of 1.5:1 to 3:1, and wherein said first radius of curvature is between 8 times and 10 times larger than said staple diameter, and wherein said second radius of curvature is between 4 and 6 times larger than said staple diameter; and a distal forming pocket . a proximal forming pocket comprising a forming surface , wherein said forming surface comprises an entry zone comprising a first radius of curvature and an exit zone comprising a second radius of curvature , wherein said first radius of curvature and said second radius of curvature comprise a ratio of 1.5:1 to 3:1, and wherein said first radius of curvature is between 8 times and 10 times larger than said staple diameter, and wherein said second radius of curvature is between 4 and 6 times larger than said staple diameter; and a distal forming pocket .
A secondary battery comprising: an electrode assembly comprising a plurality of electrode plates each comprising a pair of non-coating portion tabs at a side and a plurality of separators each located between the electrode plates ; characterized in that the non-coating tabs of each pair are bent in opposite directions and a current collector plate is welded to the non-coating tabs , wherein the non-coating portion tabs comprise a first tab and a second tab , and at least one of the first tab and the second tab is in a welded state with the current collector plate . an electrode assembly comprising a plurality of electrode plates each comprising a pair of non-coating portion tabs at a side and a plurality of separators each located between the electrode plates ; characterized in that the non-coating tabs of each pair are bent in opposite directions and a current collector plate is welded to the non-coating tabs , wherein the non-coating portion tabs comprise a first tab and a second tab , and at least one of the first tab and the second tab is in a welded state with the current collector plate .
An ultrasonic surgical instrument comprising: an ultrasonic transducer ; an acoustic horn acoustically coupled to the ultrasonic transducer ; an ultrasonic transmission waveguide acoustically coupled to the acoustic horn , the ultrasonic transmission waveguide having a central waveguide axis ; and an ultrasonic surgical blade acoustically coupled to the ultrasonic transmission waveguide through a compound curvature component ; wherein the compound curvature component transversely off-sets the ultrasonic surgical blade from the central waveguide axis , and wherein the ultrasonic surgical instrument further comprises a shaft assembly comprising an outer sheath around at least a portion of the ultrasonic transmission waveguide , wherein the ultrasonic surgical blade is transversely off-set past an outer surface of the outer sheath, and wherein the outer sheath comprises a closed and/or sealed slot extending longitudinally along at least a portion of the outer sheath length. an ultrasonic transducer ; an acoustic horn acoustically coupled to the ultrasonic transducer ; an ultrasonic transmission waveguide acoustically coupled to the acoustic horn , the ultrasonic transmission waveguide having a central waveguide axis ; and an ultrasonic surgical blade acoustically coupled to the ultrasonic transmission waveguide through a compound curvature component ; wherein the compound curvature component transversely off-sets the ultrasonic surgical blade from the central waveguide axis , and wherein the ultrasonic surgical instrument further comprises a shaft assembly comprising an outer sheath around at least a portion of the ultrasonic transmission waveguide , wherein the ultrasonic surgical blade is transversely off-set past an outer surface of the outer sheath, and wherein the outer sheath comprises a closed and/or sealed slot extending longitudinally along at least a portion of the outer sheath length.
Spark plug, in particular a prechamber spark plug, having a housing , an ignition electrode , an earth electrode and a supply line , wherein the supply line serves to act on the ignition electrode with electrical voltage and wherein the supply line has a front region which faces the ignition electrode and a rear region which faces an ignition coil, wherein the rear region is produced by means of an ignition cable , characterised in that exclusively the ignition cable has a sufficiently high electrical resistance to act as a resistance type suppressor.
- A projectile including at least one pair of airfoil sections that are deployable from housings that are located inside the body and are emerging toward the outside of the projectile , the projectile including a casing of revolution surrounding at least part of the body of the projectile and the outer surface of which is in profile continuity with the body of the projectile, the casing being able to pivot, owing to a motor means, around the body along the longitudinal axis (X) thereof and including an opening for each airfoil section , the projectile being characterised in that each opening includes two zones (Z1,Z2), namely a first zone (Z1) being intended to be positioned, by pivoting of the casing , so as to face a housing in order to allow the section to pass so as to allow it to be deployed, and a second zone (Z2) forming a lateral recess relative to the first zone (Z1), the recess being oriented along a direction substantially perpendicular to the longitudinal direction of the first zone (Z1), the second zone (Z2) having a width (L) allowing passage of a foot of the airfoil section once deployed, the casing covering the housing by continuation of its pivoting so as to prevent folding of the airfoil section .
Functional preparation comprising (percentage by weight on the total weight of the preparation): inulin 99.9975-99.998245% vitamin B12 0.001685-0.002445% selenium 0.000055-0.00007% wherein inulin has a degree of polymerization of 20.
A rechargeable socket , which is configured for charging a rechargeable battery of a wireless hair dryer ; wherein the wireless hair dryer comprises a handle , the rechargeable socket comprises a pedestal and a rechargeable assembly arranged in the pedestal, a top of the pedestal is recessed to form a plug-in part , the rechargeable assembly comprises a circuit board and a rechargeable terminal electrically coupled to the circuit board, the rechargeable terminal passes through the plug-in part and extends to an inner cavity of the plug-in part; an end of the handle arranges a rechargeable connector , the end of the handle is insertable into the inner cavity of the plug-in part to allow the rechargeable terminal to be in contact with the rechargeable connector, and in process of the handle rotatable relative to the plug-in part, the rechargeable terminal is suitable to be kept in contact with the rechargeable connector; wherein the plug-in part comprises a plug-in duct coupled to a top of the rechargeable socket and a connecting plate arranged at a bottom of the plug-in duct, a plug-in space is formed by the plug-in duct and the connecting plate, the handle is receivable in the plug-in space, characterized in that the connecting plate defines a diversion hole , and the diversion hole is in liquid communication with an outside of the rechargeable socket.
A hybrid propulsion unit for an aircraft with multi-rotor rotary wing, comprising: - an internal combustion engine , - an electric generator coupled to the internal combustion engine such that in operation the internal combustion engine drives the electric generator, - a rectifier connected to the electric generator and configured to convert an alternative current delivered by the electric generator into a direct current, the hybrid propulsion unit further comprising: - means for converting direct current into alternative current, - an electrical network connecting the rectifier to the conversion means , the electrical network comprising a high voltage direct current bus, - electric motors connected to the conversion means so that in operation the conversion means supply the electric motors with alternative current, - propellers coupled to the electric motors so that in operation the electric motors drive the propellers, and - means connected to the electrical network , said storage means comprising at least one primary storage element and at least one secondary storage element , and in that said at least one primary storage element is connected in series with the electrical network , and said at least one secondary storage element is connected in parallel with the electrical network . - an internal combustion engine , - an electric generator coupled to the internal combustion engine such that in operation the internal combustion engine drives the electric generator, - a rectifier connected to the electric generator and configured to convert an alternative current delivered by the electric generator into a direct current, - means for converting direct current into alternative current, - an electrical network connecting the rectifier to the conversion means , the electrical network comprising a high voltage direct current bus, - electric motors connected to the conversion means so that in operation the conversion means supply the electric motors with alternative current, - propellers coupled to the electric motors so that in operation the electric motors drive the propellers, and - means connected to the electrical network , said storage means comprising at least one primary storage element and at least one secondary storage element , and in that said at least one primary storage element is connected in series with the electrical network , and said at least one secondary storage element is connected in parallel with the electrical network .
Method for detecting defects in a gas safety valve of heating devices in the case of a faulty ignition, characterised by the steps - measuring the mass flow or volume flow of the combustion air supplied to a heating device by means of a sensor - forming the gradient of the measurement signal of the sensor - assigning the course of the gradient to stored error images - recognising the error using the assigned gradient - outputting an error signal. - measuring the mass flow or volume flow of the combustion air supplied to a heating device by means of a sensor - forming the gradient of the measurement signal of the sensor - assigning the course of the gradient to stored error images - recognising the error using the assigned gradient - outputting an error signal.
Gap bridging for a rail vehicle for bridging the gap between a platform and a floor of the rail vehicle, comprising a step plate mounted in a moveable manner and a cover plate that is arranged above the step plate and at least partially covers the step plate , characterised in that a wiper manufactured from spring steel is provided, which is fastened to a lower side of the cover plate and which is pressed onto the step plate by means of spring force in any position of the step plate .
A method of coding implemented by an encoding/decoding device for marking the unavailability of a candidate coding block for intra prediction mode estimation of a current coding block, the intra prediction mode of the candidate coding block being a Most Probable Mode, MPM, candidate. the method comprising: obtaining a parent block of the current coding block, denoted as parentCurr, and a parent block of a candidate coding block, denoted as parentCand, wherein the current coding block is obtained by splitting of the parentCurr, the candidate coding block is obtained by splitting of the parentCand; and marking the candidate coding block unavailable such that the current coding block cannot use the intra prediction mode of the candidate coding block, when the following conditions are fulfilled: a) parentCand and parentCurr are the same block, b) a function of number of quadtree, ternary tree and binary tree splitting operations that are performed to obtain parentCand block is greater than a threshold minus 1, and c) a split mode of the parent block of the current coding block is a ternary tree split.
Support rail fastening device for fastening a support rail which is populated with construction elements to a wall , having a fastening device which has at least two fastening elements for receiving the support rail ; a rail assembly which is connected to the two fastening elements ; and at least one clamp which is disposed on the rail assembly , characterized in that the rail assembly has at least two holding rails , wherein each fastening element is assigned one of the at least two holding rails , and wherein the rail assembly has a busbar which is connected to the at least two holding rails , wherein the at least one clamp is fastened to the busbar . a rail assembly which is connected to the two fastening elements ; and at least one clamp which is disposed on the rail assembly , characterized in that the rail assembly has at least two holding rails , wherein each fastening element is assigned one of the at least two holding rails , and wherein the rail assembly has a busbar which is connected to the at least two holding rails , wherein the at least one clamp is fastened to the busbar .
An attachment device for a heating apparatus comprising: a housing , the housing having a through bore , the through bore being configured to allow a fluid conduit to pass through the housing , and a heat source member receiving section , the heat source member receiving section being configured to receive at least a portion of a heat source member therein; and a thermal connection member , the thermal connection member being arranged such that, in use, the thermal connection member is engagable with both the fluid conduit passing through the housing and at least a portion of the heat source member located within the housing , wherein the housing is formed from at least two pieces ; characterised in that the housing includes a locking member that locks each piece of the housing together; and wherein the locking member is operable to bias the thermal connection member into engagement with the fluid conduit and/or the heat source member . a housing , the housing having a through bore , the through bore being configured to allow a fluid conduit to pass through the housing , and a heat source member receiving section , the heat source member receiving section being configured to receive at least a portion of a heat source member therein; and a thermal connection member , the thermal connection member being arranged such that, in use, the thermal connection member is engagable with both the fluid conduit passing through the housing and at least a portion of the heat source member located within the housing , wherein the housing is formed from at least two pieces ; characterised in that the housing includes a locking member that locks each piece of the housing together; and