mhurhangee/ep-ind-claims huggingface dataset:
A method for wireless communication, carried out by a user equipment, UE,, comprising identifying a slot format for normal cyclic prefix, NCP, transmissions between the UE and a base station, the slot format indicating a first transmission direction for each NCP symbol (310, 405, 705) of a set of NCP symbols within a slot; determining, according to the identified slot format for NCP transmissions and based at least in part on a transmission direction of at least one NCP symbol (310, 405, 705) that fully or partially overlaps in a time domain with a corresponding extended cyclic prefix, ECP, symbol (410, 710), a second transmission direction of the corresponding ECP symbol (410, 710), wherein a starting and ending time of each NCP symbol (310, 405, 705) is mapped to each ECP symbol of a set of ECP symbols (410, 710) in the time domain, wherein the determining comprises: identifying a subset of the NCP symbols that overlap in the time domain with a first ECP symbol of the set of ECP symbols; and determining that the first ECP symbol has a flexible transmission direction when at least one of the NCP symbols of the subset of the NCP symbols has a flexible transmission direction; and communicating with the base station based at least in part on the determining. identifying a slot format for normal cyclic prefix, NCP, transmissions between the UE and a base station, the slot format indicating a first transmission direction for each NCP symbol (310, 405, 705) of a set of NCP symbols within a slot; determining, according to the identified slot format for NCP transmissions and based at least in part on a transmission direction of at least one NCP symbol (310, 405, 705) that fully or partially overlaps in a time domain with a corresponding extended cyclic prefix, ECP, symbol (410, 710), a second transmission direction of the corresponding ECP symbol (410, 710), wherein a starting and ending time of each NCP symbol (310, 405, 705) is mapped to each ECP symbol of a set of ECP symbols (410, 710) in the time domain, wherein the determining comprises: identifying a subset of the NCP symbols that overlap in the time domain with a first ECP symbol of the set of ECP symbols; and determining that the first ECP symbol has a flexible transmission direction when at least one of the NCP symbols of the subset of the NCP symbols has a flexible transmission direction; and identifying a subset of the NCP symbols that overlap in the time domain with a first ECP symbol of the set of ECP symbols; and determining that the first ECP symbol has a flexible transmission direction when at least one of the NCP symbols of the subset of the NCP symbols has a flexible transmission direction; and communicating with the base station based at least in part on the determining.
A method for manufacturing an instructional booklet mounted to a substrate comprising the steps of: providing a multi-up book having two or more booklets (12, 120a) and a waste zone that share a common spine; adhering the multi-up book to an overlaminate that is larger than the booklets; progressively slitting the overlaminate and multi-up book into two or more overlaminate strips having booklets secured thereto; and applying the overlaminate strips to a substrate, wherein the booklets are retained between the overlaminate strips and the substrate. providing a multi-up book having two or more booklets (12, 120a) and a waste zone that share a common spine; adhering the multi-up book to an overlaminate that is larger than the booklets; progressively slitting the overlaminate and multi-up book into two or more overlaminate strips having booklets secured thereto; and applying the overlaminate strips to a substrate, wherein the booklets are retained between the overlaminate strips and the substrate.
A method for allocating a dynamic frame structure of a Time Division Duplexing, TDD, LTE system, characterized in that, the method comprises: Sending (Step 101), by an Evolved NodeB, eNB, to a User Equipment, UE, a Radio Resource Control, RRC, information of entering a state of dynamically allocating the frame structure, and sending (Step 102) configuration information of the frame structure in a Physical Downlink Control Channel, PDCCH; and (Step 103) after the UE receives the RRC information, detecting, by the UE, the configuration information of the frame structure in the PDCCH, and configuring the frame structure to be adopted in the next configuration period according to the detected configuration information. Sending (Step 101), by an Evolved NodeB, eNB, to a User Equipment, UE, a Radio Resource Control, RRC, information of entering a state of dynamically allocating the frame structure, and sending (Step 102) configuration information of the frame structure in a Physical Downlink Control Channel, PDCCH; and (Step 103) after the UE receives the RRC information, detecting, by the UE, the configuration information of the frame structure in the PDCCH, and configuring the frame structure to be adopted in the next configuration period according to the detected configuration information.
A hybrid propulsion system, the system comprising: a gas turbine engine; a generator powered by the gas turbine engine; an electric propulsion machine comprising an electric motor configured to provide propulsion for the aircraft by being mechanically coupled to a propulsor via a driveshaft, the electric propulsion machine configured to also be electrically powered by the generator; an electric starter; and an energy storage system comprising: a main battery; a propulsion power bus configured to convey electricity, which is supplied by the main battery, to the electric propulsion machine; a non-critical bus configured to convey electricity to the hotel load on the aircraft, wherein the hotel load does not provides safety functionality and is not required for continued safe operation of the aircraft; a critical bus configured to convey electricity, which is supplied by the main battery, to a critical load on the aircraft, wherein the critical load provides safety functionality or is required for continued safe operation of the aircraft; and an engine starter bus configured to convey electricity, which is supplied by the main battery, to the electric starter for the gas turbine engine. a gas turbine engine; a generator powered by the gas turbine engine; an electric propulsion machine comprising an electric motor configured to provide propulsion for the aircraft by being mechanically coupled to a propulsor via a driveshaft, the electric propulsion machine configured to also be electrically powered by the generator; an electric starter; and an energy storage system comprising: a main battery; a propulsion power bus configured to convey electricity, which is supplied by the main battery, to the electric propulsion machine; a non-critical bus configured to convey electricity to the hotel load on the aircraft, wherein the hotel load does not provides safety functionality and is not required for continued safe operation of the aircraft; a critical bus configured to convey electricity, which is supplied by the main battery, to a critical load on the aircraft, wherein the critical load provides safety functionality or is required for continued safe operation of the aircraft; and an engine starter bus configured to convey electricity, which is supplied by the main battery, to the electric starter for the gas turbine engine. a main battery; a propulsion power bus configured to convey electricity, which is supplied by the main battery, to the electric propulsion machine; a non-critical bus configured to convey electricity to the hotel load on the aircraft, wherein the hotel load does not provides safety functionality and is not required for continued safe operation of the aircraft; a critical bus configured to convey electricity, which is supplied by the main battery, to a critical load on the aircraft, wherein the critical load provides safety functionality or is required for continued safe operation of the aircraft; and an engine starter bus configured to convey electricity, which is supplied by the main battery, to the electric starter for the gas turbine engine.
A detergent composition, comprising: a) from 2 to 95 wt.%, preferably from 2 to 50 wt.%, more preferably from 2 to 40 wt.%, most preferably from 2.5 wt.% to 40 wt.% of an organic acid derivative of mono- and di- glycerides of the form:- wherein one or two, of R 1, R 2 and R 3 are independently selected from an acyl group of the formula R 4 CO-; where R 4 is a linear or branched, saturated or mon-unsaturated C 9 to C 21 alkyl chain; wherein one or two, of R 1, R 2 and R 3 is selected from an organic acid of generic formulation (HOOC) n XCO-; wherein X is saturated or monounsaturated organic group containing 1 to 6 carbon atoms and n = 1 to 3; wherein one or none of R 1, R 2 and R 3 is selected from H; and, b) from 0.0005 to 0.5 wt.%, preferably from 0.005 to 0.2 wt.% of a lipid esterase enzyme. a) from 2 to 95 wt.%, preferably from 2 to 50 wt.%, more preferably from 2 to 40 wt.%, most preferably from 2.5 wt.% to 40 wt.% of an organic acid derivative of mono- and di- glycerides of the form:- wherein one or two, of R 1, R 2 and R 3 are independently selected from an acyl group of the formula R 4 CO-; where R 4 is a linear or branched, saturated or mon-unsaturated C 9 to C 21 alkyl chain; wherein one or two, of R 1, R 2 and R 3 is selected from an organic acid of generic formulation (HOOC) n XCO-; wherein X is saturated or monounsaturated organic group containing 1 to 6 carbon atoms and n = 1 to 3; wherein one or none of R 1, R 2 and R 3 is selected from H; and, wherein one or two, of R 1, R 2 and R 3 is selected from an organic acid of generic formulation (HOOC) n XCO-; wherein X is saturated or monounsaturated organic group containing 1 to 6 carbon atoms and n = 1 to 3; wherein one or none of R 1, R 2 and R 3 is selected from H; and, b) from 0.0005 to 0.5 wt.%, preferably from 0.005 to 0.2 wt.% of a lipid esterase enzyme.
A headwear for use in the alleviation of tension-type headaches, migraine and other types of cephalalgia, said headwear comprising: - a textile; - a system of compartments formed in or on said textile, each compartment containing a material suitable for being heated in a microwave oven to a temperature of within the range of 40-60 degrees Celsius; and - a fastening means adapted for approximating the textile to the curvature of a user's head; wherein said system of compartments is configured to target specific muscles and/or nerves on the user's head with heat, wherein said system of compartments comprises a pair of compartments of a second type positioned on said headwear to target the occipitalis muscles and the occipital nerve with heat; characterized in that said system of compartments is configured to target specific muscles and/or nerves on the user's head with heat within the range of 40-60 degrees Celsius; said system of compartments further comprising a pair of compartments of a first type positioned on said headwear to target the masseter muscles and the trigeminus nerve; and wherein the textile is selected from cotton, wool, linen, hemp, and mixtures thereof. - a textile; - a system of compartments formed in or on said textile, each compartment containing a material suitable for being heated in a microwave oven to a temperature of within the range of 40-60 degrees Celsius; and - a fastening means adapted for approximating the textile to the curvature of a user's head; wherein said system of compartments is configured to target specific muscles and/or nerves on the user's head with heat, wherein said system of compartments comprises a pair of compartments of a second type positioned on said headwear to target the occipitalis muscles and the occipital nerve with heat; characterized in that said system of compartments is configured to target specific muscles and/or nerves on the user's head with heat within the range of 40-60 degrees Celsius; said system of compartments further comprising a pair of compartments of a first type positioned on said headwear to target the masseter muscles and the trigeminus nerve; and wherein the textile is selected from cotton, wool, linen, hemp, and mixtures thereof.
A method for the production of open structure foam moulded parts based on polymer foam granules, wherein the method comprises the following steps: i) the provision of polymer foam granules chosen from the group consisting of E-PLA, PLA-starch mixture, PLA-PBAT mixture, PLA with PHA, EPS, EPS/PPO, EPP, EPE, E-PET and starch foam, or one or more combinations thereof, ii) mixing the polymer foam granules with a glue composition, iii) flowing a heat transfer medium through the mixture obtained in step ii) to obtain said open structure foamed moulded parts, wherein in said open structure foamed moulded parts said polymer foam granules are adhered to each other via said glue composition, wherein step ii) further comprises adding the mixture of glue composition and polymer foam granules to two pressure bodies and subsequently exerting pressure via the said pressure bodies, wherein said pressure bodies comprise two parallel arranged transport bands between which the mixture of glue composition and polymer foam granules is located, wherein said transport bands are located one above the other so that said mixture of glue composition and polymer foam granules is poured on the lower band and compression is exerted by the position of said transport bands, wherein said compression is in the range of 10 - 50%. i) the provision of polymer foam granules chosen from the group consisting of E-PLA, PLA-starch mixture, PLA-PBAT mixture, PLA with PHA, EPS, EPS/PPO, EPP, EPE, E-PET and starch foam, or one or more combinations thereof, ii) mixing the polymer foam granules with a glue composition, iii) flowing a heat transfer medium through the mixture obtained in step ii) to obtain said open structure foamed moulded parts, wherein in said open structure foamed moulded parts said polymer foam granules are adhered to each other via said glue composition, wherein step ii) further comprises adding the mixture of glue composition and polymer foam granules to two pressure bodies and subsequently exerting pressure via the said pressure bodies, wherein said pressure bodies comprise two parallel arranged transport bands between which the mixture of glue composition and polymer foam granules is located, wherein said transport bands are located one above the other so that said mixture of glue composition and polymer foam granules is poured on the lower band and compression is exerted by the position of said transport bands, wherein said compression is in the range of 10 - 50%.
An indoor unit of an air conditioner, the indoor unit having in a casing an indoor heat exchanger, an indoor fan for drawing air from a room, and an air filter located on an intake side of the indoor fan, the indoor unit comprising: dust removal means for removing dust captured by the air filter; a storage portion for storing the dust removed by the dust removal means; a dust collecting box which communicates with the storage portion; dust transfer means for transferring, together with air, the dust stored in the storage portion to the dust collecting box by utilizing an effect of blown air or an effect of suction; characterized in that the air conditioner indoor unit furthermore comprises: a full condition detection means for detecting a dust full condition of the dust collecting box, based on an amount of transmission of light through the storage portion. dust removal means for removing dust captured by the air filter; a storage portion for storing the dust removed by the dust removal means; a dust collecting box which communicates with the storage portion; dust transfer means for transferring, together with air, the dust stored in the storage portion to the dust collecting box by utilizing an effect of blown air or an effect of suction; characterized in that the air conditioner indoor unit furthermore comprises: a full condition detection means for detecting a dust full condition of the dust collecting box, based on an amount of transmission of light through the storage portion.
A housing, comprising: a frame formed from a first material; a skin formed from the first material separately from the frame and bonded to the frame; wherein the first material is a composite of at least fiber and a matrix suspending the fiber; the skin is formed from multiple layers (600,605... 630) of the first material; an outer edge of each of the multiple layers (600,605... 630) form at least one stair-step pattern; the frame defines a tapered segment; the multiple layers (600,605... 630) are adjacent the tapered segment; the stair-step pattern is formed in a section of the skin adjacent to the tapered segment of the frame; and a portion of the skin covers at least a wall of the frame. a frame formed from a first material; a skin formed from the first material separately from the frame and bonded to the frame; wherein the first material is a composite of at least fiber and a matrix suspending the fiber; the skin is formed from multiple layers (600,605... 630) of the first material; an outer edge of each of the multiple layers (600,605... 630) form at least one stair-step pattern; the frame defines a tapered segment; the multiple layers (600,605... 630) are adjacent the tapered segment; the stair-step pattern is formed in a section of the skin adjacent to the tapered segment of the frame; and a portion of the skin covers at least a wall of the frame.
A refractory mounting unit for ceiling mounted or wall mounted electric devices, comprising a refractory housing having at least one wall and an inner and an outer side; the at least one wall comprising one section, in which internal contacts are directed to an inner side of the housing, external contacts are directed to an outer side of the housing and a line-through is integrated as part of the at least one wall for electrically interconnecting the internal contacts and external contacts, a plug having a side being form-closed to the one section of the at least one wall at the outer side of the housing, the side comprising contacts for contacting the external contacts of the housing, and a clamp for clamping the plug against the one section of the at least one wall.
Parking lock unit for a drive assembly, in particular with an electric motor, comprising: a parking lock housing, a parking ratchet wheel connected in a rotationally fixed manner to a part of the drive assembly, that is rotatably supported about an axis of rotation by at least one bearing (24, 24', 24", 25, 25', 25"), and comprising a connecting portion and an engagement portion which are connected to one another via a web portion, wherein the parking ratchet wheel is formed such that the engagement portion is axially offset with respect to the connecting portion, a locking element which is supported in the parking lock housing and can lock and release a rotational movement of the parking ratchet wheel about a longitudinal axis of the parking ratchet wheel, and a controllable locking actuator which can reversibly transfer the locking element into a position locking the parking ratchet wheel and a position releasing the parking ratchet wheel, characterized in that a central plane of the engagement portion of the parking ratchet wheel has a first distance to a central plane of the connecting portion of the parking ratchet wheel which is greater than a smallest axial thickness of the web portion. a parking lock housing, a parking ratchet wheel connected in a rotationally fixed manner to a part of the drive assembly, that is rotatably supported about an axis of rotation by at least one bearing (24, 24', 24", 25, 25', 25"), and comprising a connecting portion and an engagement portion which are connected to one another via a web portion, wherein the parking ratchet wheel is formed such that the engagement portion is axially offset with respect to the connecting portion, a locking element which is supported in the parking lock housing and can lock and release a rotational movement of the parking ratchet wheel about a longitudinal axis of the parking ratchet wheel, and a controllable locking actuator which can reversibly transfer the locking element into a position locking the parking ratchet wheel and a position releasing the parking ratchet wheel, characterized in that a central plane of the engagement portion of the parking ratchet wheel has a first distance to a central plane of the connecting portion of the parking ratchet wheel which is greater than a smallest axial thickness of the web portion.
Method for operating an internal combustion engine using natural gas, in which liquefied natural gas is stored in a fuel tank and is sucked up out of a liquid phase region of the fuel tank by means of a pre-supply pump via an intake line and supplied to a high-pressure pump, characterized in that, in order to regulate the pre-supply pressure on the delivery side of the pre-supply pump, gaseous natural gas from a gas phase region of the fuel tank is added to the liquefied natural gas sucked up on the intake side of the pre-supply pump, the pre-supply pump being designed as a side-channel pump.
A device for monitoring the progress of at least one aircraft, referred to as a detected aircraft, in an airspace, comprising: - a module for receiving a sequence of airspace images; - a generation module comprising a plurality of filters including kinematic models, and configured to generate a set of states (X, P) relating to kinematic parameters of the detected aircraft as a function of said sequence of images and as a function of a transition matrix capable of modifying probabilities defining, for a given iteration of the tracking device, the filter(s) from among the plurality of filters generating, during this given iteration, the said set of states (X, P); - a transmission module configured to transmit trajectory data for the detected aircraft as a function of the set of states (X, P); characterised in that the method comprises: - an intermediate settings module comprising a first artificial neural network, an input variable of said first artificial neural network derived from the set of states (X, P), an output variable of said first artificial neural network being a settings data item, - a settings module comprising a second artificial neural network, an input variable of the second artificial neural network being said settings data, an output variable of said second artificial neural network being said transition matrix - a module for receiving a sequence of airspace images; - a generation module comprising a plurality of filters including kinematic models, and configured to generate a set of states (X, P) relating to kinematic parameters of the detected aircraft as a function of said sequence of images and as a function of a transition matrix capable of modifying probabilities defining, for a given iteration of the tracking device, the filter(s) from among the plurality of filters generating, during this given iteration, the said set of states (X, P); - a transmission module configured to transmit trajectory data for the detected aircraft as a function of the set of states (X, P); - an intermediate settings module comprising a first artificial neural network, an input variable of said first artificial neural network derived from the set of states (X, P), an output variable of said first artificial neural network being a settings data item, - a settings module comprising a second artificial neural network, an input variable of the second artificial neural network being said settings data, an output variable of said second artificial neural network being said transition matrix