mhurhangee/ep-ind-claims huggingface dataset:
A method of wireless communications at a receiving node, comprising: receiving timing information corresponding to a traffic class identifier, wherein the timing information is associated with a time interval for communicating traffic data of a traffic class corresponding to the traffic class identifier; receiving the traffic data pertaining to the traffic class; determining that the traffic data was transmitted or is received outside and after a first occurrence of the time interval; buffering the traffic data in response to the traffic data being transmitted or received outside the time interval; and forwarding the traffic data in response to a next occurrence of the time interval; wherein receiving the timing information comprises receiving a time indicator included with the traffic data, wherein the time indicator identifies the next occurrence of the time interval; wherein determining that the traffic data was transmitted or is received outside the time interval is based on a value of the time indicator relative to a value of a synchronized clock that is synchronized to the time interval; and further comprising: determining the next occurrence of the time interval based on the value of the synchronized clock and the value of the time indicator. receiving timing information corresponding to a traffic class identifier, wherein the timing information is associated with a time interval for communicating traffic data of a traffic class corresponding to the traffic class identifier; receiving the traffic data pertaining to the traffic class; determining that the traffic data was transmitted or is received outside and after a first occurrence of the time interval; buffering the traffic data in response to the traffic data being transmitted or received outside the time interval; and forwarding the traffic data in response to a next occurrence of the time interval; wherein receiving the timing information comprises receiving a time indicator included with the traffic data, wherein the time indicator identifies the next occurrence of the time interval; wherein determining that the traffic data was transmitted or is received outside the time interval is based on a value of the time indicator relative to a value of a synchronized clock that is synchronized to the time interval; and further comprising: determining the next occurrence of the time interval based on the value of the synchronized clock and the value of the time indicator.
An axial fan having a drive motor and fan blades as well as a circular cylindrical fan duct and an outer diffuser adjoining the latter, wherein the fan duct and the outer diffuser are formed from one piece and from sheet metal, wherein a supporting unit for the drive motor is provided, which supporting unit at the same time cylindrically forms an inner diffuser, and wherein the inner diffuser extends in the axial direction downstream of the fan blades to the axial, downstream end of the outer diffuser, wherein the supporting unit is formed from supporting arms, a cylindrical tube as the inner diffuser, and a supporting ring, and wherein the drive motor is fastened to the supporting ring and is designed to be accommodated at least partially by the inner diffuser, wherein the supporting ring is arranged at the upstream end of the cylindrical tube, and wherein the outer diffuser is covered at its outer limit in the axial direction over the entire cross-section by a touch-guard grating, and the drive motor is connected to the downstream end of the outer diffuser via the supporting arm structure of the supporting unit.
Method for protecting a processing of sensitive data implemented by a processing device intended for processing sensitive input data in order to obtain sensitive output data, wherein data processing is divided into at least two processing functions (f, g, h, z), the method comprising: - an application of a first function (f) to the sensitive input data to obtain first intermediate data, and also comprising the three following recurring steps for each successive application of each of the following functions (g, h, z): - an application (E2, E5, E8) of the subsequent function (g, h, z) to the intermediate data (DI1, DI2, DI3) obtained earlier by applying a previous function (f, g, h), to obtain subsequent intermediate data (DI2, DI3, DI4), - simultaneously with the application of the following function, a detection (E3, E6, E9) of an attack by verifying the accuracy of the previously obtained intermediate data (DI1, DI2, DI3, and - an infection (E4, E7, E10) of the subsequently obtained intermediate data (DI2, DI3, DI4) if an attack is detected, the following intermediate data obtained by applying the subsequent last function are the sensitive output data with an accurate or infected value. - an application of a first function (f) to the sensitive input data to obtain first intermediate data, and also comprising the three following recurring steps for each successive application of each of the following functions (g, h, z): - an application (E2, E5, E8) of the subsequent function (g, h, z) to the intermediate data (DI1, DI2, DI3) obtained earlier by applying a previous function (f, g, h), to obtain subsequent intermediate data (DI2, DI3, DI4), - simultaneously with the application of the following function, a detection (E3, E6, E9) of an attack by verifying the accuracy of the previously obtained intermediate data (DI1, DI2, DI3, and - an infection (E4, E7, E10) of the subsequently obtained intermediate data (DI2, DI3, DI4) if an attack is detected, the following intermediate data obtained by applying the subsequent last function are the sensitive output data with an accurate or infected value.
An assembly for rotational equipment with an axial centerline, the assembly comprising: a carrier structure including a carrier base and a support ring, the carrier base extending axially along the centerline, and the support ring projecting radially inward from the carrier base; and a seal assembly nested radially within the carrier base and axially next to the support ring, the seal assembly including a seal base, a plurality of spring elements and a plurality of seal shoes arranged about the centerline in an annular array; the seal base circumscribing the annular array of the seal shoes; and each of the spring elements radially between and connecting a respective one of the seal shoes with the seal base; wherein the assembly further comprises: a secondary seal carrier ring nested radially within the carrier base; and at least one secondary seal device configured with the secondary seal carrier ring; wherein the secondary seal device is configured to substantially seal an annular gap between the secondary seal carrier ring and the annular array of the seal shoes; and wherein the secondary seal carrier ring is engaged axially with and between the seal base and the support ring; characterised in that the seal base is configured as an annular full hoop body and the carrier structure is monolithic. a carrier structure including a carrier base and a support ring, the carrier base extending axially along the centerline, and the support ring projecting radially inward from the carrier base; and a seal assembly nested radially within the carrier base and axially next to the support ring, the seal assembly including a seal base, a plurality of spring elements and a plurality of seal shoes arranged about the centerline in an annular array; the seal base circumscribing the annular array of the seal shoes; and each of the spring elements radially between and connecting a respective one of the seal shoes with the seal base; wherein the assembly further comprises: a secondary seal carrier ring nested radially within the carrier base; and at least one secondary seal device configured with the secondary seal carrier ring; wherein the secondary seal device is configured to substantially seal an annular gap between the secondary seal carrier ring and the annular array of the seal shoes; and wherein the secondary seal carrier ring is engaged axially with and between the seal base and the support ring; characterised in that the seal base is configured as an annular full hoop body and the carrier structure is monolithic. a secondary seal carrier ring nested radially within the carrier base; and at least one secondary seal device configured with the secondary seal carrier ring; wherein the secondary seal device is configured to substantially seal an annular gap between the secondary seal carrier ring and the annular array of the seal shoes; and wherein the secondary seal carrier ring is engaged axially with and between the seal base and the support ring; characterised in that the seal base is configured as an annular full hoop body and the carrier structure is monolithic.
A connector, comprising: a first housing defining a guide slot; a second housing configured to mate with the first housing, said second housing including a pin configured to engage the guide slot; a mate assist slider moveable from an unmated position to a mated position, said mate assist slider slideably mounted to the first housing, said mate assist slider including a gear rack; and a cam gear moveably mounted to the first housing, said cam gear engages the gear rack such that the cam gear moves in response to a movement of the mate assist slider, said cam gear defining a cam slot for receiving the pin, wherein the cam slot has an entrance having an inertial detent positioned above the guide slot, characterized in that a vibratory feedback is provided to an assembler when the pin is moved past the inertial detent enabling the mate assist slider to be moved from the unmated position to the mated position, wherein the inertial detent deflects and returns to a home position as the pin is moved past the inertial detent, wherein the inertial detent covers a portion of the guide slot and partially blocks a travel path of the pin. a first housing defining a guide slot; a second housing configured to mate with the first housing, said second housing including a pin configured to engage the guide slot; a mate assist slider moveable from an unmated position to a mated position, said mate assist slider slideably mounted to the first housing, said mate assist slider including a gear rack; and a cam gear moveably mounted to the first housing, said cam gear engages the gear rack such that the cam gear moves in response to a movement of the mate assist slider, said cam gear defining a cam slot for receiving the pin, wherein the cam slot has an entrance having an inertial detent positioned above the guide slot, characterized in that a vibratory feedback is provided to an assembler when the pin is moved past the inertial detent enabling the mate assist slider to be moved from the unmated position to the mated position, wherein the inertial detent deflects and returns to a home position as the pin is moved past the inertial detent, wherein the inertial detent covers a portion of the guide slot and partially blocks a travel path of the pin.
A method of lubricating an internal combustion engine comprising a crankcase and at least one of a gear and a wet-clutch, said method comprising supplying to said crankcase and to at least one of said gear and wet-clutch a lubricating composition comprising: (a) an oil of lubricating viscosity; and (b) a viscosity modifier with a number average molecular weight from 1000 to 75,000, wherein the viscosity modifier is a poly(meth)acrylate, wherein the viscosity modifier has a Shear Stability Index as determined by CEC L-45-A-99 of 22 or less, wherein the lubricating composition has a SAE viscosity grade from XW-Y, wherein X is from 0 to 20 and Y is from 20 to 50; and wherein the lubricating composition has a phosphorus content from a metal hydrocarbyl dithiophosphate of 0.12 wt % or less, wherein the internal combustion engine is a 4-stroke motorcycle engine. (a) an oil of lubricating viscosity; and (b) a viscosity modifier with a number average molecular weight from 1000 to 75,000, wherein the viscosity modifier is a poly(meth)acrylate, wherein the viscosity modifier has a Shear Stability Index as determined by CEC L-45-A-99 of 22 or less,
A dispensing device for dispensing bone cement from cartridges, comprising a connector for feeding a pressurised gas, a base body (1, 101, 201), in which at least one passage and/or channel (130, 135) runs, through which the pressurised gas can be guided to a first cartridge connecting piece (6, 106, 206) for connecting a cartridge, wherein the first cartridge connecting piece (6, 106, 206) comprises a first opening (25, 125) to the passage and/or to the front channel, so that a cartridge content can be expelled from the cartridge upon applying the pressurised gas to a cartridge arranged in the cartridge connecting piece (6, 106, 206), and characterised in that a second cartridge connecting piece (4, 104, 204) comprising a larger cross section and a second opening is arranged on the front edge of the first cartridge connecting piece (6, 106, 206), wherein the second cartridge connecting piece (4, 104, 204) is suitable for connecting a larger cartridge, and wherein the second opening of the second cartridge connecting piece (4, 104, 204) is so large that a cartridge can be connected to the first cartridge connecting piece (6, 106, 206) through the second opening.
A face mask comprising: at least one layer of filtration material configured to filter one or more harmful substances from the air breathed by a user; at least one layer of absorbent material configured to absorb moisture exhaled by the user, wherein: the at least one layer of absorbent material spans an entire inner surface area of the mask; the mask is configured to allow air to pass through the at least one layer of filtration material and the at least one layer of absorbent material; the at least one layer of absorbent material comprises super absorbent fibers and low melting-point fibers; the super absorbent fibers comprises sodium polyacrylate fibers; and the super absorbent fibers are configured to be combined to form a layer of the mask via through-air bonding; at least one layer of waterproof material, located between the at least one layer of filtration material and the at least one layer of absorbent material, configured to prevent moisture from the absorbent material from contacting the filtration material wherein the at least one layer of waterproof material comprises a spunbond waterproof material; and further comprising at least one layer of anti-bacterial material located adjacent to the at least one layer of absorbent material and forming the inner surface of the mask. at least one layer of filtration material configured to filter one or more harmful substances from the air breathed by a user; at least one layer of absorbent material configured to absorb moisture exhaled by the user, wherein: the at least one layer of absorbent material spans an entire inner surface area of the mask; the mask is configured to allow air to pass through the at least one layer of filtration material and the at least one layer of absorbent material; the at least one layer of absorbent material comprises super absorbent fibers and low melting-point fibers; the super absorbent fibers comprises sodium polyacrylate fibers; and the super absorbent fibers are configured to be combined to form a layer of the mask via through-air bonding; the at least one layer of absorbent material spans an entire inner surface area of the mask; the mask is configured to allow air to pass through the at least one layer of filtration material and the at least one layer of absorbent material; the at least one layer of absorbent material comprises super absorbent fibers and low melting-point fibers; the super absorbent fibers comprises sodium polyacrylate fibers; and the super absorbent fibers are configured to be combined to form a layer of the mask via through-air bonding; at least one layer of waterproof material, located between the at least one layer of filtration material and the at least one layer of absorbent material, configured to prevent moisture from the absorbent material from contacting the filtration material wherein the at least one layer of waterproof material comprises a spunbond waterproof material; and further comprising at least one layer of anti-bacterial material located adjacent to the at least one layer of absorbent material and forming the inner surface of the mask.
An energy store for storing electrical energy in the form of thermal energy, comprising: - an electric heater for converting electrical energy into thermal energy and - heat-storing elements for storing thermal energy of the electric heater, - wherein a plurality of vertical rods arranged upright are provided, characterized in that - the vertical rods are supported at their lower ends, wherein a thermal expansion upwards is rendered freely possible, - the heat-storing elements comprise a plurality of horizontal rods which extend in a horizontal direction, wherein a plurality of the horizontal rods are supported on each vertical rod, - the horizontal ends of each horizontal rod are free so that a thermal expansion in a horizontal direction is rendered freely possible. - an electric heater for converting electrical energy into thermal energy and - heat-storing elements for storing thermal energy of the electric heater, - wherein a plurality of vertical rods arranged upright are provided, characterized in that - the vertical rods are supported at their lower ends, wherein a thermal expansion upwards is rendered freely possible, - the heat-storing elements comprise a plurality of horizontal rods which extend in a horizontal direction, wherein a plurality of the horizontal rods are supported on each vertical rod, - the horizontal ends of each horizontal rod are free so that a thermal expansion in a horizontal direction is rendered freely possible.
Method for regulating a non-propulsion electrical generation turbomachine configured to supply electrically a plurality of propulsion rotors (R1-R4) of an aircraft, each propulsion rotor (R1-R4) being connected to an energy distribution module by at least one supply bus (B1-B4), the turbomachine supplying each supply bus (B1-B4) via the energy distribution module according to a supply rate (δ1- δ4), the turbomachine comprising a high-pressure shaft, having a high-pressure rotation speed N1, and a low-pressure shaft, having a low-pressure rotation speed N2, the regulation method comprising: - a step of determining the power requirement (P1-P4) of each propulsion rotor (R1-R4), - a step of determining the power requirement (PB1-PB4) of each supply bus (B1-B4) as a function of the power requirement (P1-P4) of each propulsion rotor (R1-R4), - a step of determining the elementary power requirement (PB1e-PB4e) of each supply bus (B1-B4) as a function of the supply rate (δ1- δ4) and the power requirement (PB1-PB4) of each supply bus (B1- B4), - a step of determining the overall power requirement (Pglob) from all of the elementary power requirements (PB1e-PB4e) of the supply buses (B1-B4), - a step of determining an anticipation parameter (N1ap) from the overall power requirement (Pglob), - a step of determining a high-pressure rotation speed set point (N1c) from a low-pressure rotation speed set point (N2c) and from a measurement of the low-pressure rotation speed of the turbomachine and of said anticipation parameter (N1ap) and - a step of determining a fuel flow rate set point (Qc) of the turbomachine from the high-pressure rotation speed set point (N1c) and from a measurement of the high-pressure rotation speed. - a step of determining the power requirement (P1-P4) of each propulsion rotor (R1-R4), - a step of determining the power requirement (PB1-PB4) of each supply bus (B1-B4) as a function of the power requirement (P1-P4) of each propulsion rotor (R1-R4), - a step of determining the elementary power requirement (PB1e-PB4e) of each supply bus (B1-B4) as a function of the supply rate (δ1- δ4) and the power requirement (PB1-PB4) of each supply bus (B1- B4), - a step of determining the overall power requirement (Pglob) from all of the elementary power requirements (PB1e-PB4e) of the supply buses (B1-B4), - a step of determining an anticipation parameter (N1ap) from the overall power requirement (Pglob), - a step of determining a high-pressure rotation speed set point (N1c) from a low-pressure rotation speed set point (N2c) and from a measurement of the low-pressure rotation speed of the turbomachine and of said anticipation parameter (N1ap) and - a step of determining a fuel flow rate set point (Qc) of the turbomachine from the high-pressure rotation speed set point (N1c) and from a measurement of the high-pressure rotation speed.
A method for separating of at least two transition metals from each other, the method comprising: injecting a feed solution into a chromatography column comprising a chromatographic support media, the feed solution comprising at least two transition metals; eluting the feed from the column in an elution cycle by flowing an eluent through the column, wherein a concentration of the eluent is reduced during the elution cycle prior to elution of at least one of the transition metals, and characterized in that the eluent is HCl. injecting a feed solution into a chromatography column comprising a chromatographic support media, the feed solution comprising at least two transition metals; eluting the feed from the column in an elution cycle by flowing an eluent through the column, wherein a concentration of the eluent is reduced during the elution cycle prior to elution of at least one of the transition metals, and characterized in that the eluent is HCl.
The use of at least one type of tertiary amine compound as an acid gas absorbent, said tertiary amine compound being represented by the following general formula: wherein: one of R 1, R 2 represents a substituted or non-substituted alkyl group having a carbon number from 2 to 5, the other of R 1, R 2 represents a substituted or non-substituted alkyl group having a carbon number from 1 to 5, R 1, R 2 may be either the same or different, and are coupled to form a cyclic structure; R 3 represents a methyl group or an ethyl group, and R 4 represents a hydroxyalkyl group. one of R 1, R 2 represents a substituted or non-substituted alkyl group having a carbon number from 2 to 5, the other of R 1, R 2 represents a substituted or non-substituted alkyl group having a carbon number from 1 to 5, R 1, R 2 may be either the same or different, and are coupled to form a cyclic structure; R 3 represents a methyl group or an ethyl group, and R 4 represents a hydroxyalkyl group.