mhurhangee/ep-ind-claims huggingface dataset:
A railcar comprising: a driver's cab including a first driver's cab device unit and a second driver's cab device unit, the first driver's cab device unit and the second driver's cab device unit forming at least two railcar-width-direction portions of the driver's cab, the first driver's cab device unit including: a plurality of first driver's cab devices disposed in a plurality of areas in the first driver's cab device unit, a first driver's cab device wire that connects the first driver's cab devices located in the different areas in the first driver's cab device unit to one another, and a first driver's cab floor surface plate, a first driver's cab side plate, a first driver's cab back plate, and a first driver's cab ceiling plate forming an outer body of the first driver's cab device unit; and the plurality of first driver's cab devices, the first driver's cab device wire, the first driver's cab floor surface plate, the first driver's cab side plate, the first driver's cab back plate and the first driver's cab ceiling plate are integrated to form a box shape. a driver's cab including a first driver's cab device unit and a second driver's cab device unit, the first driver's cab device unit and the second driver's cab device unit forming at least two railcar-width-direction portions of the driver's cab, the first driver's cab device unit including: a plurality of first driver's cab devices disposed in a plurality of areas in the first driver's cab device unit, a first driver's cab device wire that connects the first driver's cab devices located in the different areas in the first driver's cab device unit to one another, and a first driver's cab floor surface plate, a first driver's cab side plate, a first driver's cab back plate, and a first driver's cab ceiling plate forming an outer body of the first driver's cab device unit; and a plurality of first driver's cab devices disposed in a plurality of areas in the first driver's cab device unit, a first driver's cab device wire that connects the first driver's cab devices located in the different areas in the first driver's cab device unit to one another, and a first driver's cab floor surface plate, a first driver's cab side plate, a first driver's cab back plate, and a first driver's cab ceiling plate forming an outer body of the first driver's cab device unit; and the plurality of first driver's cab devices, the first driver's cab device wire, the first driver's cab floor surface plate, the first driver's cab side plate, the first driver's cab back plate and the first driver's cab ceiling plate are integrated to form a box shape.
A mass spectrometer comprising: a Time of Flight mass analyser comprising a source region and an ion detector; wherein, in use, ions arriving at said ion detector have a spread of ion arrival times ΔT which is related to an initial spread of positions Δx of said ions within said source region by a polynomial expression of the form ΔT = a 0 + a 1 (Δx)T' + a 2 (Δx) 2 T" + a 3 (Δx) 3 T"' +... wherein a 1 (Δx)T' is a first order spatial focusing term, a 2 (Δx) 2 T" is a second order spatial focusing term, a 3 (Δx) 3 T'" is a third order spatial focusing term and T is the mean time of flight of ions having a certain mass to charge ratio; characterised in that said Time of Flight mass analyser further comprises a fifth order spatial focusing device which is arranged and adapted to introduce a non-zero fifth order spatial focusing term so that the combined effect of said first, third and fifth order spatial focusing terms is a reduction in the spread of ion arrival times ΔT. a Time of Flight mass analyser comprising a source region and an ion detector; wherein, in use, ions arriving at said ion detector have a spread of ion arrival times ΔT which is related to an initial spread of positions Δx of said ions within said source region by a polynomial expression of the form ΔT = a 0 + a 1 (Δx)T' + a 2 (Δx) 2 T" + a 3 (Δx) 3 T"' +... wherein a 1 (Δx)T' is a first order spatial focusing term, a 2 (Δx) 2 T" is a second order spatial focusing term, a 3 (Δx) 3 T'" is a third order spatial focusing term and T is the mean time of flight of ions having a certain mass to charge ratio; characterised in that said Time of Flight mass analyser further comprises a fifth order spatial focusing device which is arranged and adapted to introduce a non-zero fifth order spatial focusing term so that the combined effect of said first, third and fifth order spatial focusing terms is a reduction in the spread of ion arrival times ΔT.
A method to localize a carrier on a laboratory transport system, the laboratory transport system comprising a carrier associated with an identity, a multi-lane transport module, and a control unit, wherein the carrier is configured to move on the multi-lane transport module, wherein the carrier comprises a signal transmitter configured to transmit a signal comprising information about the identity, wherein the multi-lane transport module comprises a transport surface comprising a first and a second transport lane (58, 60) each configured to transport the carrier, wherein the multi-lane transport module comprises a first signal receiver and a second signal receiver each configured to receive the transmitted signal, wherein the multi-lane transport module is communicatively connected to the control unit, wherein the method comprises the following steps (12, 14, 16, 18, 20): a) receiving, by the first signal receiver, a first signal strength of the transmitted signal and receiving, by the second signal receiver, a second signal strength of transmitted signal at the same time b) transmitting, by the first signal receiver, the first signal strength to the control unit and transmitting, by the second signal receiver, the second signal strength to the control unit c) calculating, by the control unit, a signal strength difference or signal strength ratio based on the first signal strength and second signal strength d) comparing, by the control unit, the calculated signal strength difference or signal strength ratio with one or more threshold values e) localizing, by the control unit, the carrier associated with the identity on one transport lane of the first and second transport lane (58, 60) based on the comparison between the calculated signal strength difference or signal strength ratio and the one or more threshold values. a) receiving, by the first signal receiver, a first signal strength of the transmitted signal and receiving, by the second signal receiver, a second signal strength of transmitted signal at the same time b) transmitting, by the first signal receiver, the first signal strength to the control unit and transmitting, by the second signal receiver, the second signal strength to the control unit c) calculating, by the control unit, a signal strength difference or signal strength ratio based on the first signal strength and second signal strength d) comparing, by the control unit, the calculated signal strength difference or signal strength ratio with one or more threshold values e) localizing, by the control unit, the carrier associated with the identity on one transport lane of the first and second transport lane (58, 60) based on the comparison between the calculated signal strength difference or signal strength ratio and the one or more threshold values.
Method for constructing a preform for pulling a microstructured optical fibre where a core element and several sub-elements are arranged along the preform, that are heated beyond the transformation point of its materials and, at least in part, so fused together that the material-free spaces (9, 10, 11) between the sub-elements and the core element and between the sub-elements and the sheath at least partially disappear, characterized in that the sub-elements in the shape of hollow cylinders of glass or solid cylinders of doped glass and the core element form a bundle whose pattern is polygonal and which is twisted at a preset angle around the bundle's longitudinal axis wherein the pattern is retained along the length of the preform.
A device for administering a surgical sealant comprising at least two components wherein a first component comprises fibrinogen and a second component comprises thrombin, wherein the device comprises: - a concentric lumen arrangement including (i) an inner cannula having a lumen with an inlet opening at a first end and a tip with an outlet opening at a second end opposite its first end, and (ii) an outer sheath having opposite first and second ends facing the respective first and second ends of the inner cannula, and surrounding the inner cannula along an axial length between the first and second ends of the inner cannula, - wherein the outer sheath at its second end is sealingly and fixedly connected to the inner cannula and defines an outer lumen around the inner cannula, - wherein the second end of the outer sheath is truncated and spaced apart from the tip end of the inner cannula, and - wherein the inner cannula is provided with one hole located 3 mm to 50 mm from the tip of the inner cannula for providing fluid communication between the outer lumen around the inner cannula and the lumen of the inner cannula - wherein the device is configured such that the first and second component flow separately through the inner and outer lumen and are mixed in the inner cannula prior to being administered. - a concentric lumen arrangement including (i) an inner cannula having a lumen with an inlet opening at a first end and a tip with an outlet opening at a second end opposite its first end, and (ii) an outer sheath having opposite first and second ends facing the respective first and second ends of the inner cannula, and surrounding the inner cannula along an axial length between the first and second ends of the inner cannula, - wherein the outer sheath at its second end is sealingly and fixedly connected to the inner cannula and defines an outer lumen around the inner cannula, - wherein the second end of the outer sheath is truncated and spaced apart from the tip end of the inner cannula, and - wherein the inner cannula is provided with one hole located 3 mm to 50 mm from the tip of the inner cannula for providing fluid communication between the outer lumen around the inner cannula and the lumen of the inner cannula - wherein the device is configured such that the first and second component flow separately through the inner and outer lumen and are mixed in the inner cannula prior to being administered.
A gas turbine engine article comprising: a substrate extending between two circumferential sides, a leading edge, a trailing edge, an inner side for resisting hot engine exhaust gases, and an outer side; and a gaspath layer bonded to the inner side of the substrate, the gaspath layer comprising a metallic alloy having a columnar microstructure; characterised in that: the substrate comprises another, different metallic alloy than the metallic alloy of the gaspath layer. a substrate extending between two circumferential sides, a leading edge, a trailing edge, an inner side for resisting hot engine exhaust gases, and an outer side; and a gaspath layer bonded to the inner side of the substrate, the gaspath layer comprising a metallic alloy having a columnar microstructure; characterised in that: the substrate comprises another, different metallic alloy than the metallic alloy of the gaspath layer.
A compound of any one of the following Formulae: and wherein, in Formula II: R 1a and R 1b are each independently selected from the group consisting of halogen and C 1-6 haloalkyl; R 2 is selected from the group consisting of CN, C 1-6 haloalkyl, C 1-6 haloalkoxy, C OR 2a and C NR 2a R 2b; R 2a and R 2b are each independently selected from the group consisting of H, C 1-6 alkyl and C 3-8 cycloalkyl, or are taken together to form a 5- or 6-membered heterocycloalkyl ring; and X is selected from the group consisting of CH and N; or a pharmaceutically acceptable salt thereof. R 1a and R 1b are each independently selected from the group consisting of halogen and C 1-6 haloalkyl; R 2 is selected from the group consisting of CN, C 1-6 haloalkyl, C 1-6 haloalkoxy, C OR 2a and C NR 2a R 2b; R 2a and R 2b are each independently selected from the group consisting of H, C 1-6 alkyl and C 3-8 cycloalkyl, or are taken together to form a 5- or 6-membered heterocycloalkyl ring; and X is selected from the group consisting of CH and N;
A method comprising the steps of: (a) automatically moving a sample comprising molecules from a first vial to a sample loop; (b) moving a volume of the sample from the sample loop to a first multi-port valve; (c) moving the volume of the sample from the first multi-port valve to a second multi-port valve fluidly coupled to and arranged downstream of the first multi-port valve; (d) when the second multi-port valve is in a first position, moving the volume of the sample from the second multi-port valve to a capture column; (e) capturing the molecules in the sample in the capture column, thereby separating the molecules in the sample from a matrix of the sample; (f) moving an elution buffer solution from a buffer source to the capture column, thereby eluting molecules captured by the capture column and moving an elution/molecule mixture comprising the elution buffer solution and the eluted molecules to a second vial arranged downstream of the capture column, the second vial comprising a flow-through vial; and (g) automatically moving the molecules in the second vial to an analytical device for analysis of the molecules. (a) automatically moving a sample comprising molecules from a first vial to a sample loop; (b) moving a volume of the sample from the sample loop to a first multi-port valve; (c) moving the volume of the sample from the first multi-port valve to a second multi-port valve fluidly coupled to and arranged downstream of the first multi-port valve; (d) when the second multi-port valve is in a first position, moving the volume of the sample from the second multi-port valve to a capture column; (e) capturing the molecules in the sample in the capture column, thereby separating the molecules in the sample from a matrix of the sample; (f) moving an elution buffer solution from a buffer source to the capture column, thereby eluting molecules captured by the capture column and moving an elution/molecule mixture comprising the elution buffer solution and the eluted molecules to a second vial arranged downstream of the capture column, the second vial comprising a flow-through vial; and (g) automatically moving the molecules in the second vial to an analytical device for analysis of the molecules.
A method for reducing artemisinin in a continuous manner comprising the following steps: 1) providing a column containing a hydride reducing agent, at least one activator and at least one solid base or providing a first column containing at least one solid base and a second column containing a hydride reducing agent and at least one activator, 2) providing a continuous flow of a solution of artemisinin in at least one aprotic solvent containing at least one C 1 -C 5 alcohol through the column containing the hydride reducing agent, the at least one activator and the at least one solid base or through the first column containing the at least one solid base and the second column containing the hydride reducing agent and the at least one activator, 3) thereby reducing artemisinin in a continuous manner to dihydroartemisinin of the following formula 1) providing a column containing a hydride reducing agent, at least one activator and at least one solid base or providing a first column containing at least one solid base and a second column containing a hydride reducing agent and at least one activator, 2) providing a continuous flow of a solution of artemisinin in at least one aprotic solvent containing at least one C 1 -C 5 alcohol through the column containing the hydride reducing agent, the at least one activator and the at least one solid base or through the first column containing the at least one solid base and the second column containing the hydride reducing agent and the at least one activator, 3) thereby reducing artemisinin in a continuous manner to dihydroartemisinin of the following formula
Crosslinked (meth)acrylate-based resin particles for cosmetics having an average particle diameter of 1.5 to 10 μm, comprising a copolymer obtained by copolymerization of monomer components comprising a monomer having a carboxyl group, at least one monomer selected from an acrylic ester and a methacrylic ester and a crosslinking monomer having 2 or more vinyl groups, wherein the surface of the resin particles is coated with a surfactant having a sulfonic acid group or a sulfonate group, wherein the surfactant is a compound represented by the following general formula: R 1 CONR 2 CH 2 CH 2 SO 3 M wherein R 1 represents C 5 to C 30 alkyl or alkenyl group which may be substituted by a hydroxyl group, carboxyl group, ester group, ether group or amide group, R 2 represents a hydrogen atom or a methyl group, and M represents a hydrogen atom or a cation, and wherein the average particle diameter is determined by measuring the weight-average particle diameter of an aqueous suspension of the particles at room temperature, 20°C, at a relative refractive index of 1.1 by using a laser-scattering particle size analyser. wherein the surface of the resin particles is coated with a surfactant having a sulfonic acid group or a sulfonate group, wherein the surfactant is a compound represented by the following general formula: R 1 CONR 2 CH 2 CH 2 SO 3 M wherein R 1 represents C 5 to C 30 alkyl or alkenyl group which may be substituted by a hydroxyl group, carboxyl group, ester group, ether group or amide group, R 2 represents a hydrogen atom or a methyl group, and M represents a hydrogen atom or a cation, and
An airfoil assembly for a gas powered turbine comprising: a plurality of floating wall sectors (110;210;310;410) arranged circumferentially about an axis defined by a flowpath; each of said floating wall sectors (110;210;310;410) comprising; a first flowpath strut component (130;230); a second flowpath strut component (140;240;340;440); a floating wall panel (120;220;320;420) connected to the first flowpath strut component (130;230) by a first clamp seal (150;250;350;450) at a first axial joint and connected to the second flowpath strut component (140; 240; 340; 440) by a second clamp seal (150;250;350;450) at a second axial joint, each clamp seal (150; 250; 350; 450) including a radially outward clamping plate (252;352;452) and a radially inward clamping plate (254;354;454) interconnected by fasteners (256;356;456); and a plurality of leading edge structures fore of the plurality of floating wall sectors (110;210;310;410), each of the leading edge structures configured to define an airfoil profile in conjunction with the first flowpath strut component (130;230) of a first floating wall sector (110;210) and the adjacent second flowpath strut component (140;240;340;440) of a second floating wall sector (110;210). a plurality of floating wall sectors (110;210;310;410) arranged circumferentially about an axis defined by a flowpath; each of said floating wall sectors (110;210;310;410) comprising; a first flowpath strut component (130;230); a second flowpath strut component (140;240;340;440); a floating wall panel (120;220;320;420) connected to the first flowpath strut component (130;230) by a first clamp seal (150;250;350;450) at a first axial joint and connected to the second flowpath strut component (140; 240; 340; 440) by a second clamp seal (150;250;350;450) at a second axial joint, each clamp seal (150; 250; 350; 450) including a radially outward clamping plate (252;352;452) and a radially inward clamping plate (254;354;454) interconnected by fasteners (256;356;456); and a plurality of leading edge structures fore of the plurality of floating wall sectors (110;210;310;410), each of the leading edge structures configured to define an airfoil profile in conjunction with the first flowpath strut component (130;230) of a first floating wall sector (110;210) and the adjacent second flowpath strut component (140;240;340;440) of a second floating wall sector (110;210).
A method of operating a harvester, wherein there is provided at least a first transverse conveyor unit, in particular a first belt swather for conveying mowed crop material in a first conveyor direction directed transversely relative to the direction of travel, and wherein there is provided at least a second transverse conveyor unit, in particular a second belt swather for conveying mowed crop material in a second conveyor direction which is directed transversely relative to the direction of travel and which is at least partially opposite to the first conveyor direction, wherein the transverse conveyor units are displaceable between a working and a transport position, wherein in a first working mode both crop material-conveying transverse conveyor units have a first conveyor speed, characterised in that there is provided a second working mode in which the second transverse conveyor unit has a second conveyor speed, wherein the second conveyor speed is less than the conveyor speed of the first transverse conveyor unit while the first transverse conveyor unit is pivoted from the working position into an intermediate position arranged between the working and the transport positions while the second transverse conveyor unit is in the working position.
An imaging lens, comprising in an ordered way from an object side: a first lens having positive (+) refractive power; a second lens having negative (-) refractive power; a third lens having negative (-) refractive power; and a fourth lens having negative (-) refractive power, wherein the imaging lens meets a conditional expression of 10 < [(v1+v4)/2-v2] < 20 and v4 < 30, where v1, v2 and v4 are Abbe's numbers of the first, second and fourth lenses, characterized in that the imaging lens meets a conditional expression of 10 < [(v1+v3)/2-v2] < 20 and v3 < 30, where v3 is Abbe's number of the third lens, the first lens takes a meniscus form convexly formed at an object side surface or takes a convex form at both sides, the second lens is concavely formed at an image side surface, and takes a meniscus form, wherein the third lens is concavely formed at an image side surface, and takes a meniscus form, and the fourth lens is convexly formed at an object side surface, and takes a meniscus form. a first lens having positive (+) refractive power; a second lens having negative (-) refractive power; a third lens having negative (-) refractive power; and a fourth lens having negative (-) refractive power, wherein the imaging lens meets a conditional expression of 10 < [(v1+v4)/2-v2] < 20 and v4 < 30, where v1, v2 and v4 are Abbe's numbers of the first, second and fourth lenses, characterized in that the imaging lens meets a conditional expression of 10 < [(v1+v3)/2-v2] < 20 and v3 < 30, where v3 is Abbe's number of the third lens, the first lens takes a meniscus form convexly formed at an object side surface or takes a convex form at both sides, the second lens is concavely formed at an image side surface, and takes a meniscus form, wherein the third lens is concavely formed at an image side surface, and takes a meniscus form, and the fourth lens is convexly formed at an object side surface, and takes a meniscus form.