mhurhangee/ep-ind-claims huggingface dataset:
A method of forming a flexible annular seal for a moveable thrust assembly of a rocket motor assembly comprising: selecting a first silicone material; selecting a second silicone material; combining the first silicone material and the second silicone material with at least one curing/crosslinking agent to form a polysiloxane composition including the first silicone material, the second silicone material, and the at least one curing/crosslinking agent, the at least one curing/crosslinking agent being selected from dicumyl peroxide and bis (2,4-dischlorobenzoyl)-peroxide; forming a preliminary structure having an annular shape from the polysiloxane composition; and curing the preliminary structure to form a cured structure comprising a cured polysiloxane composition, wherein the curing comprises subjecting the preliminary structure to a temperature within a range of from about 50°C to 300°C for a period of time within a range of from 5 minutes to 10 hours; the method characterized by; forming the polysiloxane composition to be homogeneous, including a uniform dispersion of the first silicone material, the second silicone material, and the at least one curing/crosslinking agent; and forming the cured structure, the cured polysiloxane composition comprising crosslinked polysiloxane chains of the first silicone material and the second silicone material. selecting a first silicone material; selecting a second silicone material; combining the first silicone material and the second silicone material with at least one curing/crosslinking agent to form a polysiloxane composition including the first silicone material, the second silicone material, and the at least one curing/crosslinking agent, the at least one curing/crosslinking agent being selected from dicumyl peroxide and bis (2,4-dischlorobenzoyl)-peroxide; forming a preliminary structure having an annular shape from the polysiloxane composition; and curing the preliminary structure to form a cured structure comprising a cured polysiloxane composition, wherein the curing comprises subjecting the preliminary structure to a temperature within a range of from about 50°C to 300°C for a period of time within a range of from 5 minutes to 10 hours; the method characterized by; forming the polysiloxane composition to be homogeneous, including a uniform dispersion of the first silicone material, the second silicone material, and the at least one curing/crosslinking agent; and forming the cured structure, the cured polysiloxane composition comprising crosslinked polysiloxane chains of the first silicone material and the second silicone material.
A carbon steel container containing a volume of monochlorosilane, characterized in that the container has an internal surface modification capable of containing monochlorosilane in a stable condition wherein the internal surface consists of carbon steel that has been mechanically polished using an abrasive slurry wherein the mechanical polishing provides a 1 micron R a surface finish.
A method for determining tire/runway interface friction properties along a portion of a runway comprising: measuring, by a brake control unit, a first axle reference speed for a braked wheel of an aircraft and a wheel acceleration; establishing, by the brake control unit, a wheel reference speed for the braked wheel of the aircraft; determining, by the brake control unit, a slip ratio of the braked wheel from the first axle reference speed and the wheel reference speed; estimating, by the brake control unit, a weight of the aircraft associated with the braked wheel to provide a tire normal force estimation; mapping, by the brake control unit, position data to the first axle reference speed, the wheel reference speed, wheel acceleration and tire normal force estimation; and estimating, by the brake control unit, coefficients of friction associated with locations along the portion of the runway from the tire normal force estimation and wheel acceleration; characterised in that a lower bound of wheel slip values is calculated in response to a braking stop comprising no anti-skid system event. measuring, by a brake control unit, a first axle reference speed for a braked wheel of an aircraft and a wheel acceleration; establishing, by the brake control unit, a wheel reference speed for the braked wheel of the aircraft; determining, by the brake control unit, a slip ratio of the braked wheel from the first axle reference speed and the wheel reference speed; estimating, by the brake control unit, a weight of the aircraft associated with the braked wheel to provide a tire normal force estimation; mapping, by the brake control unit, position data to the first axle reference speed, the wheel reference speed, wheel acceleration and tire normal force estimation; and estimating, by the brake control unit, coefficients of friction associated with locations along the portion of the runway from the tire normal force estimation and wheel acceleration; characterised in that a lower bound of wheel slip values is calculated in response to a braking stop comprising no anti-skid system event.
Battery, in particular a lithium-ion battery, comprising a battery can comprising a cylindrical can body,an electrode assembly accommodated in the cylindrical can body and formed by winding an anode and a cathode that are isolated by a separator, wherein the can body has a first end forming a base, and a peripheral side wall extending from the base in a longitudinal direction to a second end of the can body comprising an opening, wherein the second end is closed by a cap assembly inserted into the can body opening to the can body, wherein the cap assembly has been attached to the can body by crimping an annular shoulder surrounding the opening inwardly such that the annular shoulder is in engagement with an upper section of the cap assembly, characterized in that the side wall of the can body ends in an end edge at the second end and the end edge of the peripheral side wall is folded in an inwardly extending loop into the annular shoulder; and that inner opposing side wall surfaces of the inner annular shoulder abut each other and the end edge contacts the inner side wall of the can body, that the annular shoulder has been crimped inwardly such that the end edge of the side wall is bent away from the longitudinal axis of the can body and faces the inner side wall of the can body and the end face of the side wall at the second end forms an outer flat annular surface when viewed in the longitudinal direction of the can body; and that a section of the side wall has been crimped inwardly and forms an annular projection that engages a lower section of the cap assembly. wherein the can body has a first end forming a base, and a peripheral side wall extending from the base in a longitudinal direction to a second end of the can body comprising an opening, wherein the second end is closed by a cap assembly inserted into the can body opening to the can body, wherein the cap assembly has been attached to the can body by crimping an annular shoulder surrounding the opening inwardly such that the annular shoulder is in engagement with an upper section of the cap assembly, that the side wall of the can body ends in an end edge at the second end and the end edge of the peripheral side wall is folded in an inwardly extending loop into the annular shoulder; and that inner opposing side wall surfaces of the inner annular shoulder abut each other and the end edge contacts the inner side wall of the can body, that the annular shoulder has been crimped inwardly such that the end edge of the side wall is bent away from the longitudinal axis of the can body and faces the inner side wall of the can body and the end face of the side wall at the second end forms an outer flat annular surface when viewed in the longitudinal direction of the can body; and that a section of the side wall has been crimped inwardly and forms an annular projection that engages a lower section of the cap assembly.
A method of providing limited slip performance in a limited slip differential comprising the step of introducing a lubricating composition comprising a major amount of an oil of lubricating viscosity, and an oil soluble compound of formula R'N((CH 2) 2 CONHR") 2, wherein R' is H or a C 8-28 hydrocarbyl group, and wherein R" is H or a C 8-28 hydrocarbyl group, with the proviso that at least one of R' or R" is a hydrocarbyl group; and operating the limited slip differential.
Stator of a dynamo-electric rotary machine, which forms a hollow-cylindrical body, wherein correspondingly shaped metal sheets are layered in the axial direction and embody said cylindrical hollow body with a stator bore, wherein the cylindrical hollow body has teeth and axially running grooves in the axial direction, wherein the parallel-edged or trapezoidal teeth are surrounded by a coil body in each case, wherein at least one electrical cable is wrapped around the coil body, and forms a coil which is part of a winding system of the stator, wherein an insulating body having an H-shaped cross-section is located between adjacent coil sections in a groove, wherein the insulating body has side parts, characterised in that the side parts are configured to be rigid at least on the side of the groove opening, in order to fix the coil body to the tooth, by the side parts of the insulating body abutting, engaging or latching into recesses of the teeth, at least in sections, wherein the recesses of the teeth are in the region of the groove opening.
A computer-implemented method for performing frequency selective scheduling between a user equipment and a base station, the method comprising: a) selecting (104, 124), by the user equipment, a sub-band within a predetermined system bandwidth based on observed radio conditions; b) communicating (106, 126) the selected sub-band from the user equipment to the base station; c) receiving (114, 134), by the user equipment, a resource block on the selected sub-band, wherein a discrete number of transmit time intervals separate communicating the selected sub-band and receiving the resource block; and d) using the resource block for communication between the base station and the user equipment. a) selecting (104, 124), by the user equipment, a sub-band within a predetermined system bandwidth based on observed radio conditions; b) communicating (106, 126) the selected sub-band from the user equipment to the base station; c) receiving (114, 134), by the user equipment, a resource block on the selected sub-band, wherein a discrete number of transmit time intervals separate communicating the selected sub-band and receiving the resource block; and d) using the resource block for communication between the base station and the user equipment.
High temperature thermal energy exchange system, with - at least one heat exchange chamber with chamber boundaries which surround at least one heat exchange chamber interior of the heat exchange chamber, wherein - the chamber boundaries comprise at least one inlet opening for guiding in an inflow of at least one heat transfer fluid into the heat exchange chamber interior and at least one outlet opening for guiding out an outflow of the heat transfer fluid out of the heat exchange chamber interior; and - at least one heat storage material is arranged in the heat exchange chamber interior such that a heat exchange flow of the heat transfer fluid through the heat exchange chamber interior causes a heat exchange between the heat storage material and the heat transfer fluid, wherein - the heat transfer fluid comprises a gas at ambient gas pressure and - the gas at the ambient gas pressure is air, characterized in that the chamber boundary with one of the openings (1111, 1112) comprises a transition area with a tapering profile such that an opening diameter of the opening (1111, 1112) aligns to a first tapering profile diameter of the tapering profile and a chamber diameter of the heat exchange chamber aligns to a second tapering profile diameter of the tapering profile. - at least one heat exchange chamber with chamber boundaries which surround at least one heat exchange chamber interior of the heat exchange chamber, wherein - the chamber boundaries comprise at least one inlet opening for guiding in an inflow of at least one heat transfer fluid into the heat exchange chamber interior and at least one outlet opening for guiding out an outflow of the heat transfer fluid out of the heat exchange chamber interior; and - at least one heat storage material is arranged in the heat exchange chamber interior such that a heat exchange flow of the heat transfer fluid through the heat exchange chamber interior causes a heat exchange between the heat storage material and the heat transfer fluid, wherein - the heat transfer fluid comprises a gas at ambient gas pressure and - the gas at the ambient gas pressure is air, characterized in that the chamber boundary with one of the openings (1111, 1112) comprises a transition area with a tapering profile such that an opening diameter of the opening (1111, 1112) aligns to a first tapering profile diameter of the tapering profile and a chamber diameter of the heat exchange chamber aligns to a second tapering profile diameter of the tapering profile.
A method of establishing an ad hoc cellular network having an ad hoc cellular base station or integrating an ad hoc cellular base station into a fixed cellular network comprising the steps of: a. establishing a wireless backhaul connection for an ad hoc cellular base station characterized by the steps of: i. receiving a data packet from an ad hoc cellular base station; ii. extracting a tunnel overhead packet from the data packet so as to create a modified data packet; iii. storing the tunnel overhead packet in a memory; iv. forwarding the modified data packet to a second ad hoc cellular base station using an IP routing protocol; v. receiving an acknowledgement from the second ad hoc cellular base station indicating that an establishment of a bearer is complete; and vi. anchoring an IP session to shield an external network from a backhaul IP change. a. establishing a wireless backhaul connection for an ad hoc cellular base station characterized by the steps of: i. receiving a data packet from an ad hoc cellular base station; ii. extracting a tunnel overhead packet from the data packet so as to create a modified data packet; iii. storing the tunnel overhead packet in a memory; iv. forwarding the modified data packet to a second ad hoc cellular base station using an IP routing protocol; v. receiving an acknowledgement from the second ad hoc cellular base station indicating that an establishment of a bearer is complete; and vi. anchoring an IP session to shield an external network from a backhaul IP change. i. receiving a data packet from an ad hoc cellular base station; ii. extracting a tunnel overhead packet from the data packet so as to create a modified data packet; iii. storing the tunnel overhead packet in a memory; iv. forwarding the modified data packet to a second ad hoc cellular base station using an IP routing protocol; v. receiving an acknowledgement from the second ad hoc cellular base station indicating that an establishment of a bearer is complete; and vi. anchoring an IP session to shield an external network from a backhaul IP change.
A positive active material for a lithium secondary battery comprising a lithium transition metal composite oxide, wherein the lithium transition metal composite oxide has an α-NaFeO 2 type crystal structure, and is represented by formula Li w Ni x Co y Mn z O 1+w with w > 1, x + y + z = 1 0.315 < x < 0.35, 0 ≤ y ≤ 0.02, 0.655 < z < 0.675, and and 0.475 < w − 2 x − y / w < 0.510. has an α-NaFeO 2 type crystal structure, and is represented by formula Li w Ni x Co y Mn z O 1+w with w > 1, x + y + z = 1 0.315 < x < 0.35, 0 ≤ y ≤ 0.02, 0.655 < z < 0.675, and and 0.475 < w − 2 x − y / w < 0.510.
Pharmaceutical composition containing a double strand RNA mimic of miR-27a-5p, for use thereof for preventing or reducing intestinal lesions in a subject suffering from an infection with Clostridium Difficile.
A pharmaceutical composition which comprises (a) -8-(3,4-dimethoxystyryl)-1,3-diethyl-7-methyl-3,7-dihydro-1H-purine-2,6-dione represented by the formula: or a pharmaceutically acceptable salt thereof, and (b) an antidepressant drug selected from the group consisting of venlafaxine, paroxetine and fluoxetine and pharmaceutically acceptable salts thereof and hydrates thereof. (a) -8-(3,4-dimethoxystyryl)-1,3-diethyl-7-methyl-3,7-dihydro-1H-purine-2,6-dione represented by the formula: or a pharmaceutically acceptable salt thereof, and (b) an antidepressant drug selected from the group consisting of venlafaxine, paroxetine and fluoxetine and pharmaceutically acceptable salts thereof and hydrates thereof.
A tinting machine comprising a plurality of colorant reservoirs containing colorant, one or more cleaning fluid supply conduits, one or more dispenser heads for dispensing colorant into a paint container, the one or more dispenser heads comprising: - a fluid outlet for dispensing the colorant into the paint container; and - an internal chamber having an inner surface and having a downstream end opening in the fluid outlet, wherein each colorant reservoir is fluidly connected to the internal chamber of at least one of the one or more dispenser heads via a colorant supply conduit opening in the internal chamber at a colorant inlet, characterized in that the one or more cleaning fluid supply conduits are opening in the one or more dispenser heads at a cleaning fluid inlet in the internal chamber, wherein the one or more dispenser heads further comprise a piston having an outer side surface, which piston is longitudinally and movably arranged in the internal chamber such that an annular space is defined by the outer side surface of the piston and the inner surface of the internal chamber, the piston comprising a circumventional protrusion defining a constriction in the annular space, and wherein the piston is movable through the internal chamber between a first position wherein the protrusion is upstream of the colorant inlet, and a second position wherein the protrusion is downstream of the colorant inlet. - a fluid outlet for dispensing the colorant into the paint container; and - an internal chamber having an inner surface and having a downstream end opening in the fluid outlet,
A sheet feeder, comprising: a sheet placing portion on which a sheet is to be placed; a feeding member configured to pick up a sheet from the sheet placing portion; a supporting body configured to support the feeding member and capable of changing a posture between a sheet feeding posture for bringing the feeding member into contact with the upper surface of a sheet placed on the sheet placing portion and a retracting posture for retracting the feeding member upward relative to the sheet feeding posture; a driver configured to output a drive force for changing the posture of the supporting body to the retracting posture against a gravitational force; an electromagnetic clutch capable of changing a state between an engaged state in which a drive force output from the driver is transmitted to the supporting body and a disengaged state in which the drive force is not transmitted to the supporting body; characterized by a retraction controller configured to perform a retraction holding process for switching the supporting body to the retracting posture; wherein the retraction holding process is a process for stopping the output of a drive force by the driver after the electromagnetic clutch is set in the engaged state and the supporting body is set to the retracting posture by the drive force from the driver and setting the electromagnetic clutch in the disengaged state when an engagement keeping time set in advance elapses after the output of the drive force is stopped. a sheet placing portion on which a sheet is to be placed; a feeding member configured to pick up a sheet from the sheet placing portion; a supporting body configured to support the feeding member and capable of changing a posture between a sheet feeding posture for bringing the feeding member into contact with the upper surface of a sheet placed on the sheet placing portion and a retracting posture for retracting the feeding member upward relative to the sheet feeding posture; a driver configured to output a drive force for changing the posture of the supporting body to the retracting posture against a gravitational force; an electromagnetic clutch capable of changing a state between an engaged state in which a drive force output from the driver is transmitted to the supporting body and a disengaged state in which the drive force is not transmitted to the supporting body; characterized by a retraction controller configured to perform a retraction holding process for switching the supporting body to the retracting posture;
A guiding apparatus, comprising: a first member (20, 20', 20a) having sliding grooves formed on both side surfaces and formed along a longitudinal direction; and a plurality of second members (30, 30', 30b) which are slidably assembled along the sliding grooves so as to hold the first member (20, 20', 20a) in between, wherein the first member (20, 20', 20a) is formed with a first mounting hole on a bottom surface of the sliding groove, and each of the second members (30, 30', 30b) is formed with a second mounting hole on a surface opposed to the bottom surface, and wherein a stopper member (50, 50', 60, 51, 51', 70) is mounted to each of the first mounting hole and the second mounting hole via a mounting bolt, each of the stopper member having an insertion part (52, 52', 52a) which is to be inserted into each of the first mounting hole and the second mounting hole and is formed to be shorter in a length in an axial direction than a depth of each of the first mounting hole and the second mounting hole, and a protruding part (53, 53', 53a) protruding from each of the bottom surface and a surface opposed to the bottom surface, respectively, and the stopper members (50, 50', 60, 51, 51', 70) prevent the second members (30, 30', 30b) from falling off. a first member (20, 20', 20a) having sliding grooves formed on both side surfaces and formed along a longitudinal direction; and a plurality of second members (30, 30', 30b) which are slidably assembled along the sliding grooves so as to hold the first member (20, 20', 20a) in between, wherein the first member (20, 20', 20a) is formed with a first mounting hole on a bottom surface of the sliding groove, and each of the second members (30, 30', 30b) is formed with a second mounting hole on a surface opposed to the bottom surface, and wherein a stopper member (50, 50', 60, 51, 51', 70) is mounted to each of the first mounting hole and the second mounting hole via a mounting bolt, each of the stopper member having an insertion part (52, 52', 52a) which is to be inserted into each of the first mounting hole and the second mounting hole and is formed to be shorter in a length in an axial direction than a depth of each of the first mounting hole and the second mounting hole, and a protruding part (53, 53', 53a) protruding from each of the bottom surface and a surface opposed to the bottom surface, respectively, and the stopper members (50, 50', 60, 51, 51', 70) prevent the second members (30, 30', 30b) from falling off.
An assembly for an aircraft, comprising: an aircraft control surface; and a hydraulic actuator including a housing and a piston within the housing, the housing formed integral with the aircraft control surface, characterised in that: the aircraft control surface comprises an internal stiffener extending along a camber line of the aircraft control surface and a portion of the housing is formed by the internal stiffener, and the internal stiffener extends longitudinally from a base of the aircraft control surface to a tip of the aircraft control surface. an aircraft control surface; and a hydraulic actuator including a housing and a piston within the housing, the housing formed integral with the aircraft control surface,