mhurhangee/patent-ind-claim-en huggingface dataset:
A method performed by an enhanced Node B, eNB, of operating multi-band and multi-cell communication, the method comprising: transmitting a synchronization channel and a broadcasting channel for narrow-band User Equipments, UEs, through a first band narrower than a system band, the first band being located in a center band of the system band, the narrow-band UEs configured to support a bandwidth narrower than a system bandwidth of the system band of the eNB; establishing a Radio Resource Control, RRC, connection with a first narrow-band UE, which is one of said narrow-band UEs, through the first band, transmitting, to the first narrow-band UE and through the RRC connection, information on a second band and information on a position of a first subframe where a control channel is transmitted; and transmitting the control channel for scheduling a data channel for the first narrow-band UE through the second band equal to or wider than the first band, the second band not overlapping the first band within the system band, wherein the first band is equal to a band where a synchronization channel and a broadcasting channel of a host cell using the entire system band are transmitted. transmitting a synchronization channel and a broadcasting channel for narrow-band User Equipments, UEs, through a first band narrower than a system band, the first band being located in a center band of the system band, the narrow-band UEs configured to support a bandwidth narrower than a system bandwidth of the system band of the eNB; establishing a Radio Resource Control, RRC, connection with a first narrow-band UE, which is one of said narrow-band UEs, through the first band, transmitting, to the first narrow-band UE and through the RRC connection, information on a second band and information on a position of a first subframe where a control channel is transmitted; and transmitting the control channel for scheduling a data channel for the first narrow-band UE through the second band equal to or wider than the first band, the second band not overlapping the first band within the system band, wherein the first band is equal to a band where a synchronization channel and a broadcasting channel of a host cell using the entire system band are transmitted.
A process for fermenting a CO-containing substrate, the process comprising: providing the CO-containing substrate to a fermentor; fermenting the CO-containing substrate to obtain a target cell density and a target CO feed rate; and maintaining a dissolved CO concentration in the fermentation of 0.25 mM or less, wherein the dissolved CO concentration is maintained by: a) reducing the target CO feed rate to the fermentation by 25% to 35% of the target CO feed rate to provide a first reduced CO feed rate, and maintaining the first reduced CO feed rate for 1 to 10 minutes; b) increasing the first reduced CO feed rate to the fermentation to a provide a second reduced CO feed rate that is reduced by 15% to 25% of the target CO feed rate, and maintaining the second reduced feed rate for 1 to 5 minutes; c) increasing the second reduced CO feed rate to the fermentation to a provide a third reduced CO feed rate that is reduced by 5% to 15% of the target CO feed rate, and maintaining the third reduced feed rate for 1 to 5 minutes; and d) increasing the third reduced CO feed rate to the target feed rate or more, wherein the process is effective for providing a space time yield of 10 g ethanol/(L·day) or more. providing the CO-containing substrate to a fermentor; fermenting the CO-containing substrate to obtain a target cell density and a target CO feed rate; and maintaining a dissolved CO concentration in the fermentation of 0.25 mM or less, wherein the dissolved CO concentration is maintained by: a) reducing the target CO feed rate to the fermentation by 25% to 35% of the target CO feed rate to provide a first reduced CO feed rate, and maintaining the first reduced CO feed rate for 1 to 10 minutes; b) increasing the first reduced CO feed rate to the fermentation to a provide a second reduced CO feed rate that is reduced by 15% to 25% of the target CO feed rate, and maintaining the second reduced feed rate for 1 to 5 minutes; c) increasing the second reduced CO feed rate to the fermentation to a provide a third reduced CO feed rate that is reduced by 5% to 15% of the target CO feed rate, and maintaining the third reduced feed rate for 1 to 5 minutes; and d) increasing the third reduced CO feed rate to the target feed rate or more, a) reducing the target CO feed rate to the fermentation by 25% to 35% of the target CO feed rate to provide a first reduced CO feed rate, and maintaining the first reduced CO feed rate for 1 to 10 minutes; b) increasing the first reduced CO feed rate to the fermentation to a provide a second reduced CO feed rate that is reduced by 15% to 25% of the target CO feed rate, and maintaining the second reduced feed rate for 1 to 5 minutes; c) increasing the second reduced CO feed rate to the fermentation to a provide a third reduced CO feed rate that is reduced by 5% to 15% of the target CO feed rate, and maintaining the third reduced feed rate for 1 to 5 minutes; and d) increasing the third reduced CO feed rate to the target feed rate or more, wherein the process is effective for providing a space time yield of 10 g ethanol/(L·day) or more.
Photobioreactor (PBR) module (D) for insulating and/or regulating the temperature of a building, said module (D) comprising an algal and/or microorganism culture container (W) in an aqueous medium, at least two parallel or substantially parallel walls defining at least one interior space said at least one interior space comprising said algal and/or microorganism culture container (W) in an aqueous medium, one of these walls being able to serve as a facade wall or to be affixed to a facade wall of the building, said at least two walls being multi-layer walls, characterized in that said at least two multi-layer walls defining one or more air space (L 2 , L 1 ).
Vacuum induction casting device for casting metal and metal alloys under vacuum and/or protective gas atmosphere, comprising at least one storage chamber and a forehearth which communicates with the storage chamber and which has at least one stopper casting device , wherein the vacuum induction casting device can be gas-tightly and detachably coupled to a continuous casting plant or a powder atomising plant as downstream unit and the vacuum induction casting device is constructed for the purpose of transferring the melt under vacuum and/or protective gas atmosphere to the downstream unit, wherein the storage chamber together with the forehearth is mounted to be rotatable about a tilt axis in such a way that melt is displaceable from the forehearth into the storage chamber and back and the stopper casting device comprises means for gas-tight closure of at least one casting nozzle within the forehearth , characteried in that the stopper casting device comprises as means for gas-tight closure of the at least one casting nozzle at least one refractory hood which within the forehearth forms a gas-tight enclosure of an inlet of the casting nozzle .
An espagnolette handle for a truck door comprising: - a base intended to be secured to said door , said base defining a base plane; - a rotating arm mounted movably on said base intended to be rigidly secured to an espagnolette bar to rotate said espagnolette bar between a closed position where said rotating arm is folded against said base and an open position where said rotating arm is spaced from said base ; - a hook mounted movable in rotation on said base to switch between a retaining position in which said hook retains said rotating arm in the closed position and a release position of said rotating arm ; and - a mechanism for locking and unlocking the handle in the closed position comprising a motor , a rotary cam and a system for transmitting the movement of said motor to said cam , said transmission system being adapted to drive said cam in rotation about a cam axis (A6) perpendicular to said base plane between a locked position in which said cam prohibits the switching of said hook toward said release position and an unlocked position in which said cam allows the switching of said hook to said release position, characterized in that: - said motor is a rotary motor about a motor axis (A5); - said transmission system is formed by a worm coupled to a shaft of said motor and by teeth present on a cylindrical outer surface of said cam and meshing with said worm . - a base intended to be secured to said door , said base defining a base plane; - a rotating arm mounted movably on said base intended to be rigidly secured to an espagnolette bar to rotate said espagnolette bar between a closed position where said rotating arm is folded against said base and an open position where said rotating arm is spaced from said base ; - a hook mounted movable in rotation on said base to switch between a retaining position in which said hook retains said rotating arm in the closed position and a release position of said rotating arm ; and - a mechanism for locking and unlocking the handle in the closed position comprising a motor , a rotary cam and a system for transmitting the movement of said motor to said cam , said transmission system being adapted to drive said cam in rotation about a cam axis (A6) perpendicular to said base plane between a locked position in which said cam prohibits the switching of said hook toward said release position and an unlocked position in which said cam allows the switching of said hook to said release position, - said motor is a rotary motor about a motor axis (A5); - said transmission system is formed by a worm coupled to a shaft of said motor and by teeth present on a cylindrical outer surface of said cam and meshing with said worm .
A method for decoding a video sequence in H.265 or Versatile Video Coding, VVC, comprising: decoding a fixed length binary coded network abstraction layer unit, NALU, class type included in an NALU header, wherein the NALU class type indicates a class of segment types, including random access segment types, leading picture segment types, switching picture segment types, parameter set types and bitstream markers; decoding an NALU type in the NALU header; and reconstructing a picture, wherein a type of the picture is identified by a combination of the NALU class type and the NALU type, wherein the type of the picture includes a leading picture, a switching picture and a random access picture. decoding a fixed length binary coded network abstraction layer unit, NALU, class type included in an NALU header, wherein the NALU class type indicates a class of segment types, including random access segment types, leading picture segment types, switching picture segment types, parameter set types and bitstream markers; decoding an NALU type in the NALU header; and reconstructing a picture, wherein a type of the picture is identified by a combination of the NALU class type and the NALU type, wherein the type of the picture includes a leading picture, a switching picture and a random access picture.
A foundry mold including at least: a first molding cavity extending, along a horizontal axis (X), from a first end to a second end , a first pair of feeder arms comprising: a first feeder arm , oriented in a substantially vertical direction and connected to the first end of the first molding cavity , and a second feeder arm , substantially parallel to the first feeder arm and connected to the second end of the first molding cavity , the foundry mold being characterized in that any transverse section (Sb) of the first and second feeder arms of the first pair of feeder arms, perpendicular to a vertical axis (Z), has a greater area than any transverse section (Sc) of the first molding cavity perpendicular to the horizontal axis (X). a first molding cavity extending, along a horizontal axis (X), from a first end to a second end , a first pair of feeder arms comprising: a first feeder arm , oriented in a substantially vertical direction and connected to the first end of the first molding cavity , and a second feeder arm , substantially parallel to the first feeder arm and connected to the second end of the first molding cavity , the foundry mold being characterized in that any transverse section (Sb) of the first and second feeder arms of the first pair of feeder arms, perpendicular to a vertical axis (Z), has a greater area than any transverse section (Sc) of the first molding cavity perpendicular to the horizontal axis (X). a first feeder arm , oriented in a substantially vertical direction and connected to the first end of the first molding cavity , and a second feeder arm , substantially parallel to the first feeder arm and connected to the second end of the first molding cavity , the foundry mold being characterized in that any transverse section (Sb) of the first and second feeder arms of the first pair of feeder arms, perpendicular to a vertical axis (Z), has a greater area than any transverse section (Sc) of the first molding cavity perpendicular to the horizontal axis (X).
Device and anti-shock bearing with - at least two attachment sections and - at least one spring section arranged between two attachment sections , wherein - the spring section is formed by two partial spring sections arranged in series and curved in opposite directions, wherein - the attachment sections are aligned parallel to one another, - the partial spring sections comprise different radii (R1, R2), characterized in that - the radius (R1, R2) of one of the partial spring sections is larger by a factor of 1.1 to 3.0 than the radius (R1, R2) of the respective other partial spring section , and - the partial spring sections are each formed by a circular arc section with an angle (B1, B2) of greater than 100 degrees and less than 170 degrees. - at least two attachment sections and - at least one spring section arranged between two attachment sections , wherein - the spring section is formed by two partial spring sections arranged in series and curved in opposite directions, wherein - the attachment sections are aligned parallel to one another, - the partial spring sections comprise different radii (R1, R2), - the radius (R1, R2) of one of the partial spring sections is larger by a factor of 1.1 to 3.0 than the radius (R1, R2) of the respective other partial spring section , and - the partial spring sections are each formed by a circular arc section with an angle (B1, B2) of greater than 100 degrees and less than 170 degrees.
A continuous casting method for producing a slab by supplying molten steel to a mold, the method comprising: forming a Ni coating layer made of a nickel oxide in a surface portion of the slab by supplying a mold flux onto a top face of the molten steel, wherein the mold flux contains SiO 2 , CaO, MgO, Al 2 O 3 , Na 2 O, F, and nickel (Ni) oxide, wherein the nickel (Ni) oxide has a content in a range from 10 wt% exclusive to 40 wt% with respect to a total weight of the mold flux, wherein the molten steel contains copper, wherein a Ni concentration in the surface portion is at least 1.5 times greater than a Cu concentration in the surface portion. forming a Ni coating layer made of a nickel oxide in a surface portion of the slab by supplying a mold flux onto a top face of the molten steel, wherein the mold flux contains SiO 2 , CaO, MgO, Al 2 O 3 , Na 2 O, F, and nickel (Ni) oxide, wherein the nickel (Ni) oxide has a content in a range from 10 wt% exclusive to 40 wt% with respect to a total weight of the mold flux, wherein the molten steel contains copper, wherein a Ni concentration in the surface portion is at least 1.5 times greater than a Cu concentration in the surface portion.
A computer-implemented method for localizing data from at least one of two or more data sets, the method comprising: receiving first drive data from a given road segment as a first data set and one of second drive data or map data from the given road segment as a second data set, wherein each of the first and the second drive data (i) is derived from data collected from one or more sensors onboard a vehicle driving along the given road segment and (ii) identifies the location of each of a plurality of features on or along the given road segment; creating a first synthetic image from the first data set and a second synthetic image from the second data set, wherein creating the first and second synthetic images comprises rasterizing representations of one or more of the plurality of features from the first and second data sets, respectively; the method characterized by : determining a transformation between the first and second synthetic images based upon a phase correlation between the first and second synthetic images, wherein the transformation provides for improved localization of the data from at least one of the first or second data sets; generating a report that defines the transformation; and correcting a positional difference between the first and the second data sets based upon the transformation. receiving first drive data from a given road segment as a first data set and one of second drive data or map data from the given road segment as a second data set, wherein each of the first and the second drive data (i) is derived from data collected from one or more sensors onboard a vehicle driving along the given road segment and (ii) identifies the location of each of a plurality of features on or along the given road segment; creating a first synthetic image from the first data set and a second synthetic image from the second data set, wherein creating the first and second synthetic images comprises rasterizing representations of one or more of the plurality of features from the first and second data sets, respectively; the method characterized by : determining a transformation between the first and second synthetic images based upon a phase correlation between the first and second synthetic images, wherein the transformation provides for improved localization of the data from at least one of the first or second data sets; generating a report that defines the transformation; and correcting a positional difference between the first and the second data sets based upon the transformation.
A flight path holding pattern system that is configured to generate an efficient holding pattern for an aircraft , the flight path holding pattern system comprising: a tracking sub-system adapted to track a current position of the aircraft and other aircraft proximate to a destination airport and comprising a communication device adapted to wirelessly communicate with the aircraft ; a holding pattern determination unit that is configured to determine that the aircraft is diverted into a holding pattern by comparing the current position of the aircraft with a flight plan of the aircraft , to automatically generate the holding pattern for the aircraft and to output the holding pattern to the aircraft , wherein the holding pattern determination unit is configured to automatically generate the holding pattern for the aircraft upon determining that the aircraft is to be diverted into a holding pattern based on current air traffic transmitted by the tracking-subsystem , historical holding patterns in relation to the destination airport , current weather conditions in relation to the destination airport , and fuel consumption data representative of actual fuel consumed by the aircraft , fuel efficiency performance of the aircraft and estimated fuel consumption based on previous performance of the aircraft or one or more other aircraft. a tracking sub-system adapted to track a current position of the aircraft and other aircraft proximate to a destination airport and comprising a communication device adapted to wirelessly communicate with the aircraft ; a holding pattern determination unit that is configured to determine that the aircraft is diverted into a holding pattern by comparing the current position of the aircraft with a flight plan of the aircraft , to automatically generate the holding pattern for the aircraft and to output the holding pattern to the aircraft , wherein the holding pattern determination unit is configured to automatically generate the holding pattern for the aircraft upon determining that the aircraft is to be diverted into a holding pattern based on current air traffic transmitted by the tracking-subsystem , historical holding patterns in relation to the destination airport , current weather conditions in relation to the destination airport , and fuel consumption data representative of actual fuel consumed by the aircraft , fuel efficiency performance of the aircraft and estimated fuel consumption based on previous performance of the aircraft or one or more other aircraft.
An anionic surfactant of general formula (I), in which R represents a linear or branched alkyl, alkenyl, alkylaryl or alkenylaryl group having 5 to 25 C atoms and X + represents a charge-balancing cation.
A spark plug comprising: a cylindrical metal shell ; and a cylindrical insulator disposed in an inner circumference of the metal shell , having an axial hole extending in an axial line (CL1) direction, and having a tip located more to a tip side of the spark plug than a tip of the metal shell , wherein a distance (L) along the axial line (CL1) from the tip of the metal shell to the tip of the insulator is 0.5 mm or more, and wherein V ≤ 3.9 mm 3 is satisfied, wherein V is a volume of the insulator within a range (RA) of 0.5 mm from the tip of the insulator to a rear end side in the axial line (CL1) direction characterized in that C >= 1.07 mm, wherein C is a thickness of the insulator in a cross section that passes a tip of an inner circumference surface of the metal shell and that is orthogonal to the axial line (CL1). a cylindrical metal shell ; and a cylindrical insulator disposed in an inner circumference of the metal shell , having an axial hole extending in an axial line (CL1) direction, and having a tip located more to a tip side of the spark plug than a tip of the metal shell , wherein a distance (L) along the axial line (CL1) from the tip of the metal shell to the tip of the insulator is 0.5 mm or more, and wherein V ≤ 3.9 mm 3 is satisfied, wherein V is a volume of the insulator within a range (RA) of 0.5 mm from the tip of the insulator to a rear end side in the axial line (CL1) direction characterized in that C >= 1.07 mm, wherein C is a thickness of the insulator in a cross section that passes a tip of an inner circumference surface of the metal shell and that is orthogonal to the axial line (CL1).