mhurhangee/ep-ind-claims huggingface dataset:
A dual lock cylinder arrangement comprising; - a housing having a front end and a rear end, said housing being provided with a first cylinder bore (3, 103, 203) and a second cylinder bore (5, 105, 205) each of which cylinder bore exhibits a forwardly open mouth; - a single carrier (20, 120, 220) arranged to engage a follower of a lock mechanism and extending out from the rear end of the housing and being rotatable about a rotational axis which is parallel with the first (3, 103, 203) and second (5, 105, 205)) cylinder bores; - a transmission arrangement (10, 110, 210) received in the housing and arranged to selectively connect a first plug (4a, 104a, 204a) of a first lock cylinder (4, 104, 204) received in the first cylinder bore (3, 103, 203) or a second plug (6a, 206a, 206a) of a second lock cylinder (6, 106, 206) received in the second cylinder bore (5, 105, 205) with the carrier (20, 120, 220) wherein the transmission arrangement (10, 110, 210) comprises a first rotatable drive (11, 111, 211) connectable with the first plug (4a, 104a, 204a), a second rotatable drive (12, 112, 212) connectable with the second plug (6a, 106a, 206a) and connected to the first rotatable drive (11, 111, 211), a third rotatable drive (13, 113, 213) connected to the carrier (20, 120, 220) and a fourth rotatable drive (14, 114, 214) which is connected to the third rotatable drive (13, 113, 213) and selectively connectable with the second rotatable drive (12, 112, 212).. - a housing having a front end and a rear end, said housing being provided with a first cylinder bore (3, 103, 203) and a second cylinder bore (5, 105, 205) each of which cylinder bore exhibits a forwardly open mouth; - a single carrier (20, 120, 220) arranged to engage a follower of a lock mechanism and extending out from the rear end of the housing and being rotatable about a rotational axis which is parallel with the first (3, 103, 203) and second (5, 105, 205)) cylinder bores; - a transmission arrangement (10, 110, 210) received in the housing and arranged to selectively connect a first plug (4a, 104a, 204a) of a first lock cylinder (4, 104, 204) received in the first cylinder bore (3, 103, 203) or a second plug (6a, 206a, 206a) of a second lock cylinder (6, 106, 206) received in the second cylinder bore (5, 105, 205) with the carrier (20, 120, 220)
A collapsible container, comprising a base, four hinged lateral walls configured for collapsing separately on the base; attachment means between adjoining lateral walls in the assembled position, the attachment means comprising retention elements arranged on each lateral wall of a first pair of opposite lateral walls; and a flexible internal structure for separating and protecting products to be transported in the container, the flexible internal structure being fixed on bars; the collapsible container characterized in that: - the attachment means further comprise flaps arranged on opposite edges of each lateral wall of a second pair of opposite lateral walls adjoining said first pair of lateral walls, each flap being bent inwards, - each retention element comprises an extension that together with the lateral wall to which it is fixed forms a groove for inserting and retaining the respective flap of the adjoining lateral wall for which, during the unfolding procedure, the flap surpasses the retaining element and then is allowed to recede slightly until it is inserted into the groove, - each retention element is spaced a distance from an edge of the lateral wall in which it is arranged, a distance that is a function of the width of the flap to enable the insertion thereof into the retention element, during the assembly of the container, - and each of the lateral walls of the second pair of opposite lateral walls comprises a bar which extends between the flaps of the same lateral wall. - the attachment means further comprise flaps arranged on opposite edges of each lateral wall of a second pair of opposite lateral walls adjoining said first pair of lateral walls, each flap being bent inwards, - each retention element comprises an extension that together with the lateral wall to which it is fixed forms a groove for inserting and retaining the respective flap of the adjoining lateral wall for which, during the unfolding procedure, the flap surpasses the retaining element and then is allowed to recede slightly until it is inserted into the groove, - each retention element is spaced a distance from an edge of the lateral wall in which it is arranged, a distance that is a function of the width of the flap to enable the insertion thereof into the retention element, during the assembly of the container, - and each of the lateral walls of the second pair of opposite lateral walls comprises a bar which extends between the flaps of the same lateral wall.
A method for preparing a polymer, comprising polycondensation of a polyether macromonomer A, a monomer B and an aldehyde C, wherein - the polyether macromonomer A has a structural formula (Ia), (Ib), (Ic), or (Id): in which Z is NR 3, O or O(CH 2) f O, L = O(CH 2) f or (CH 2) f, f is an integer from 1 to 10, Q is C2 to C24 alkylene, R 2 is H or C1 to C10 alkyl, R 3 is a C1 to C10 alkyl, m = 8 to 112, n = 8 to 112; - the monomer B has a structural formula (IIa) or (IIb): in which G is N(CH 2 -PO 3 H 2) 2 or C (PO 3 H 2) 2, wherein R 1 is H, a C1 to C10 alkyl or SO 3 H, K is a C1 to C10 alkylene, X = NR 8 or O, Y is OH or OR 7, R 7 is a C1 to C10 alkyl, and R 8 is a C1 to C10 alkyl, - the aldehyde C has a structural formula: R 5 CHO in which R 5 is H, COOH, or a C1 to C10 alkyl; and the molar ratio of the polyether macromonomer A and the monomer B is 1: (0.5 to 12). - the polyether macromonomer A has a structural formula (Ia), (Ib), (Ic), or (Id): in which Z is NR 3, O or O(CH 2) f O, L = O(CH 2) f or (CH 2) f, f is an integer from 1 to 10, Q is C2 to C24 alkylene, R 2 is H or C1 to C10 alkyl, R 3 is a C1 to C10 alkyl, m = 8 to 112, n = 8 to 112; - the monomer B has a structural formula (IIa) or (IIb): in which G is N(CH 2 -PO 3 H 2) 2 or C (PO 3 H 2) 2, wherein R 1 is H, a C1 to C10 alkyl or SO 3 H, K is a C1 to C10 alkylene, X = NR 8 or O, Y is OH or OR 7, R 7 is a C1 to C10 alkyl, and R 8 is a C1 to C10 alkyl, - the aldehyde C has a structural formula: R 5 CHO in which R 5 is H, COOH, or a C1 to C10 alkyl; and the molar ratio of the polyether macromonomer A and the monomer B is 1: (0.5 to 12). in which R 5 is H, COOH, or a C1 to C10 alkyl; and the molar ratio of the polyether macromonomer A and the monomer B is 1: (0.5 to 12).
An actuator comprising: a drum defining a longitudinal axis and having axially opposed first and second end portions that are rotatable relative to one another about the longitudinal axis; and a shape memory element wrapped around the drum and extending from the first end portion of the drum to the second end portion of the drum to actuate relative rotation of the first and second end portions of the drum about the longitudinal axis by activation of the shape memory element; characterised in that the first and second end portions of the drum are connected to one another by an annular flexible drum portion with slots defined therethrough, wherein the slots are aligned in a generally axial direction, and are oblique relative to the axial direction when the actuator is in a relaxed state so as to counteract axial shortening of the drum during actuation. a drum defining a longitudinal axis and having axially opposed first and second end portions that are rotatable relative to one another about the longitudinal axis; and a shape memory element wrapped around the drum and extending from the first end portion of the drum to the second end portion of the drum to actuate relative rotation of the first and second end portions of the drum about the longitudinal axis by activation of the shape memory element; characterised in that the first and second end portions of the drum are connected to one another by an annular flexible drum portion with slots defined therethrough, wherein the slots are aligned in a generally axial direction, and are oblique relative to the axial direction when the actuator is in a relaxed state so as to counteract axial shortening of the drum during actuation.
A half thrust bearing for receiving an axial force (f) of a crankshaft of an internal combustion engine, the half thrust bearing having a semi-annular shape and comprising a sliding surface for receiving the axial force (f), and a rear surface on an opposite side of the sliding surface, and the half thrust bearing defining a reference plane on a rear surface side that is perpendicular to an axial direction, wherein the sliding surface includes a flat surface portion extending in parallel with the reference plane from a radially inner end of the half thrust bearing to a radially outer end thereof, and two inclined flat surface portions formed on both sides in a circumferential direction of the flat surface portion, an axial distance (thickness T) between the reference plane and the sliding surface is maximum in the flat surface portion, at any radial positions, the axial distance in each inclined flat surface portion is maximum at a circumferential end of the inclined flat surface portion on a circumferentially central portion side of the half thrust bearing and is reduced toward a circumferential end portion of the half thrust bearing, and the flat surface portion has a circumferential length extending over a circumferential angle of 5° or more and 35° or less, at any radial positions of the half thrust bearing, characterized in that each inclined flat surface portion is arranged to form one constant thickness portion which extends linearly from the radially inner end to the radially outer end of the half thrust bearing as a straight line at a position between circumferential angles of 35° and 55° from the circumferential end portion toward the circumferentially central portion side of the half thrust bearing, the axial distance being constant in the constant thickness portion, and at any circumferential positions, the axial distance in each inclined flat surface portion is maximum at the radially inner end and is reduced toward the radially outer end in a region of the inclined flat surface portion on a circumferential end portion side of the constant thickness portion, and is minimum at the radially inner end and is increased toward the radially outer end in a region of the inclined flat surface portion on the circumferentially central portion side of the constant thickness portion.
A method for performing a nucleic acid high speed melting analysis, the method comprising: providing a microfluidic device having one or more nucleic acid samples therein, wherein each of the one or more nucleic acids is less than 100bp long; providing an imaging system in communication with the one or more nucleic acid samples; providing a thermal system in thermal communication with the one or more nucleic acid samples; increasing a temperature of the one or more nucleic acid samples to achieve nucleic acid dissociation, wherein the temperature is increased by the thermal system at a ramp rate selected from a range of 1 °C/s to 50 °C/s; acquiring images of the one or more nucleic acid samples during nucleic acid dissociation to generate a melting profile for each nucleic acid sample; sequentially obtaining melting curves for the one or more nucleic acid samples at a plurality of ramp rates between 0.13 °C/s and 32 °C/s to determine an optimal ramp rate corresponding to a highest genotype discrimination, the genotype discrimination being calculated for a plurality of ramp rates between 0.13 °C/s and 32 °C/s; and genotyping the nucleic acids based on the melting profiles. providing a microfluidic device having one or more nucleic acid samples therein, wherein each of the one or more nucleic acids is less than 100bp long; providing an imaging system in communication with the one or more nucleic acid samples; providing a thermal system in thermal communication with the one or more nucleic acid samples; increasing a temperature of the one or more nucleic acid samples to achieve nucleic acid dissociation, wherein the temperature is increased by the thermal system at a ramp rate selected from a range of 1 °C/s to 50 °C/s; acquiring images of the one or more nucleic acid samples during nucleic acid dissociation to generate a melting profile for each nucleic acid sample; sequentially obtaining melting curves for the one or more nucleic acid samples at a plurality of ramp rates between 0.13 °C/s and 32 °C/s to determine an optimal ramp rate corresponding to a highest genotype discrimination, the genotype discrimination being calculated for a plurality of ramp rates between 0.13 °C/s and 32 °C/s; and genotyping the nucleic acids based on the melting profiles.
A gel to remove a graffiti on a surface of a solid substrate, consisting of a colloidal solution comprising, preferably consisting of: - 0.1 to 30 mass %, preferably 0.1 to 25 mass %, more preferably 5 to 25 mass %, further preferably 8 to 20 mass %, for exemple 10 mass % relative to the total mass of the gel of at least one inorganic viscosifying agent; - 70 to 99.9 mass %, preferably 75 to 99.9 mass %, more preferably 75 to 95 mass %, for example 90 mass %, of a mixture of ethyl acetate and diethyl malonate or of a mixture of ethyl acetate and methyl acetoacetate; - optionally, 0.1 to 2 mass % relative to the total mass of the gel of at least one surfactant; - and optionally, 0.01 to 10 mass % relative to the mass of the gel of at least one dye and/or pigment. - 0.1 to 30 mass %, preferably 0.1 to 25 mass %, more preferably 5 to 25 mass %, further preferably 8 to 20 mass %, for exemple 10 mass % relative to the total mass of the gel of at least one inorganic viscosifying agent; - 70 to 99.9 mass %, preferably 75 to 99.9 mass %, more preferably 75 to 95 mass %, for example 90 mass %, of a mixture of ethyl acetate and diethyl malonate or of a mixture of ethyl acetate and methyl acetoacetate; - optionally, 0.1 to 2 mass % relative to the total mass of the gel of at least one surfactant; - and optionally, 0.01 to 10 mass % relative to the mass of the gel of at least one dye and/or pigment.
A turbomachine combustion assembly, comprising a turbomachine combustion chamber, and an injector for starting the turbomachine combustion chamber, disposed on a wall of the combustion chamber and opening thereinto through an orifice of the wall, the starting injector including: - a fuel injection circuit, - a fuel ignition circuit, comprising a fuel injector supplied by the fuel injection circuit, and a plug for igniting the injected fuel, - a partitioned enclosure comprising a first compartment in which the ignition of the fuel by the plug is carried out, and a second compartment separated from the first one by a thermally conductive partition, the assembly being characterized in that the first compartment communicates with the second compartment so that all the ignited fuel is discharged from the injector through the opening of the second compartment, and - a main circuit for starting the combustion, including at least one fuel injector supplied by said fuel injection circuit and opening into the second compartment of the enclosure by being disposed so as to inject the fuel against said wall. - a fuel injection circuit, - a fuel ignition circuit, comprising a fuel injector supplied by the fuel injection circuit, and a plug for igniting the injected fuel, - a partitioned enclosure comprising a first compartment in which the ignition of the fuel by the plug is carried out, and a second compartment separated from the first one by a thermally conductive partition, - a main circuit for starting the combustion, including at least one fuel injector supplied by said fuel injection circuit and opening into the second compartment of the enclosure by being disposed so as to inject the fuel against said wall.
A method of operating a detection system, comprising: switching the system from a normal mode for sensing smoke to a high sensitivity mode for sensing airborne particles, such that in the high sensitivity mode the detection system is configured to discriminate between particles of diameters less than 2.5 micrometers and 10 micrometers; emitting light at a first wavelength from a first light source of the detection system into a monitored space and detecting an amount of light backscatter at the first wavelength at one or more light sensing devices (18, 20) of the detection system, wherein the first wavelength is characteristic of infrared light; emitting light at a second wavelength from a second light source of the detection system into the monitored space and detecting an amount of light backscatter at the second wavelength at the one or more light sensing devices of the detection system, wherein the second wavelength is characteristic of visible blue light; and determining a particulate particle size via a ratio of the amount of light backscatter at the first wavelength to the amount of light backscatter at the second wavelength. switching the system from a normal mode for sensing smoke to a high sensitivity mode for sensing airborne particles, such that in the high sensitivity mode the detection system is configured to discriminate between particles of diameters less than 2.5 micrometers and 10 micrometers; emitting light at a first wavelength from a first light source of the detection system into a monitored space and detecting an amount of light backscatter at the first wavelength at one or more light sensing devices (18, 20) of the detection system, wherein the first wavelength is characteristic of infrared light; emitting light at a second wavelength from a second light source of the detection system into the monitored space and detecting an amount of light backscatter at the second wavelength at the one or more light sensing devices of the detection system, wherein the second wavelength is characteristic of visible blue light; and determining a particulate particle size via a ratio of the amount of light backscatter at the first wavelength to the amount of light backscatter at the second wavelength.
Process for preparing a stable dairy-based sauce comprising fat and/or oil and a dairy component and wherein the sauce contains less than 2% of reducing sugars, which process involves the subsequent steps of: (a) preparing a mixture containing all ingredients, (b) packing, further comprising a sterilisation step after step (b), and wherein the mixture, prior to packing is not subjected to temperatures above 50°C (preferably not above 40°C). (a) preparing a mixture containing all ingredients, (b) packing,
Tyre inflation valve (1, 100, 200) including a tubular body (4, 204) defining a passage (7, 70, 71) and having an inside end (46, 246) and an outside end (43, 243), a valve mechanism (44, 244) positioned in the passage, the valve mechanism including a valve shutter and a seat arranged so as to engage in an airtight manner with one another, the seat is arranged on the tubular body in the passage, characterised in that the seat is located in an area of limited solicitation (42, 45, 46, 242, 246) of the tubular body and in that the seat is located at the inside end of the tubular body, so as to be positioned inside the tyre when assembling the inflation valve.
A waterproof stage light with efficient heat dissipation, comprising: a light source component; a heat dissipating system; and a waterproof main housing, at the rear end of which an opening is arranged, wherein the heat dissipating system is in seal connection with the opening, characterized in that one end of the heat dissipating system is positioned inside the main housing and the other end thereof is positioned outside the main housing, and the light source component is positioned on the end of the heat dissipating system that is positioned inside the main housing, the heat dissipating system contains a heat absorbing component; a heat transfer substrate covering the opening at the rear end of the main housing and in seal connection with the main housing; and a heat dissipating component; wherein the heat absorbing component and the heat dissipating component are respectively provided on both sides of the heat transfer substrate, and the heat absorbing component is located inside the main housing and the heat dissipating component is located outside the main housing. a light source component; a heat dissipating system; and a waterproof main housing, at the rear end of which an opening is arranged, wherein the heat dissipating system is in seal connection with the opening, characterized in that one end of the heat dissipating system is positioned inside the main housing and the other end thereof is positioned outside the main housing, and the light source component is positioned on the end of the heat dissipating system that is positioned inside the main housing, the heat dissipating system contains a heat absorbing component; a heat transfer substrate covering the opening at the rear end of the main housing and in seal connection with the main housing; and a heat dissipating component; wherein the heat absorbing component and the heat dissipating component are respectively provided on both sides of the heat transfer substrate, and the heat absorbing component is located inside the main housing and the heat dissipating component is located outside the main housing.
Magnus rotor (1, 100) which has a cylindrical rotation member (2, 102) for converting wind power into a feed force using the Magnus effect, comprising: - a rotation axis about which the rotation member (2, 102) rotates, - a carrier on which the rotation member (2, 102) is supported, characterised in that - the rotation member has means for reinforcing the rotation member (2, 102), - the rotation member (2, 102) has, in at least two planes which are spaced apart from each other in an axial direction perpendicular relative to the rotation axis of the rotation member (2, 102), receiving members to which balancing weights are fitted. - a rotation axis about which the rotation member (2, 102) rotates, - a carrier on which the rotation member (2, 102) is supported, characterised in that - the rotation member has means for reinforcing the rotation member (2, 102), - the rotation member (2, 102) has, in at least two planes which are spaced apart from each other in an axial direction perpendicular relative to the rotation axis of the rotation member (2, 102), receiving members to which balancing weights are fitted.
A method to perform a timing acquisition process between a transmitter and a receiver in a wireless communication system, comprising: selecting, at the transmitter, a system frequency resolution, f r; generating, at the transmitter, a set of frequency tones which are relatively prime integers with respect to the frequency resolution f r and within an operating frequency range, R, of the wireless communication system; selecting, at the transmitter, a first subset of frequency tones from the set of frequency tones; transmitting, at the transmitter, the subset of frequency tones; receiving, at the receiver, at least two signals comprising the first subset of frequency tones; computing, at the receiver, a phase difference between the two signals; and using the computed phase difference to synchronise the transmitter and the receiver. selecting, at the transmitter, a system frequency resolution, f r; generating, at the transmitter, a set of frequency tones which are relatively prime integers with respect to the frequency resolution f r and within an operating frequency range, R, of the wireless communication system; selecting, at the transmitter, a first subset of frequency tones from the set of frequency tones; transmitting, at the transmitter, the subset of frequency tones; receiving, at the receiver, at least two signals comprising the first subset of frequency tones; computing, at the receiver, a phase difference between the two signals; and using the computed phase difference to synchronise the transmitter and the receiver.