mhurhangee/ep-ind-claims huggingface dataset:
An optoelectronic sensor, in particular a laser scanner, for detecting objects in a monitoring area, the sensor comprising a light transmitter for transmitting transmitted light, a movable deflection unit configured as a rotating mirror with a mirror surface, not as a polygon mirror wheel, for periodically deflecting the transmitted light, a light receiver for generating a received signal from remitted transmitted light that has been remitted from objects in the monitored area, a control and evaluation unit for detecting information about objects in the monitored area on the basis of the received signal, and a circumferential front screen having a passage area for the transmitted light and/or the remitted transmitted light, the front screen being formed with rotational symmetry at least in the passage area, characterized in that an optical element is provided that is moved along with the deflection unit and compensates a refractive influence of the front screen on transmitted light and/or remitted transmitted light passing through, wherein the mirror surface has a curvature and thus functions as the optical element moved along with the mirror, or an additional optical element is provided that is moved along with the deflection unit.
Centrifuge for automatic loading, comprising: a) a drive shaft driven to be rotatable about a rotor axis, b) a rotor which is releasably coupled to the drive shaft for conjoint rotation therewith, and has receptacles for containers for media to be centrifuged, c) a housing having lateral outer walls (14, 16, 18, 20), which delimit the centrifuge, and a cover, with at least one outer wall having a lateral opening directed to the side for loading the rotor as required, d) a safety vessel into which the drive shaft projects and which surrounds the rotor, e) a protective wall surrounding the safety vessel at least in regions, which protective wall is adapted at least to the shape of the adjacent outer wall having the lateral opening in such a way that it closes off the lateral opening, wherein the safety vessel and the protective wall firmly connect to one another to form a safety unit which is operatively connected to an adjusting mechanism that is adapted to move the safety unit in such a way as to cause the protective wall to open and close the lateral opening, thus allowing the protective wall to be moved from a closed position into an open position thereof, and vice versa, characterized in that the lateral opening extends up to the housing cover and that a cover opening is provided in the housing cover adjoining the lateral opening, thus creating a loading and unloading opening formed from the lateral opening and the cover opening, wherein the cover opening is adapted to be opened and closed via a further closing wall by means of a second adjusting mechanism. a) a drive shaft driven to be rotatable about a rotor axis, b) a rotor which is releasably coupled to the drive shaft for conjoint rotation therewith, and has receptacles for containers for media to be centrifuged, c) a housing having lateral outer walls (14, 16, 18, 20), which delimit the centrifuge, and a cover, with at least one outer wall having a lateral opening directed to the side for loading the rotor as required, d) a safety vessel into which the drive shaft projects and which surrounds the rotor, e) a protective wall surrounding the safety vessel at least in regions, which protective wall is adapted at least to the shape of the adjacent outer wall having the lateral opening in such a way that it closes off the lateral opening,
A cosmetic agent for lightening the skin and/or age spots, containing a) at least one extract from Opuntia Ficus Indica; b) at least one extract from Brassica plants; c) 2,3-dihydro-5,6-dimethoxy-3,3-dimethyl-2-(phenylmethylene)-1H-Inden-1-one (benzylidene dimethoxydimethylindanone). a) at least one extract from Opuntia Ficus Indica; b) at least one extract from Brassica plants; c) 2,3-dihydro-5,6-dimethoxy-3,3-dimethyl-2-(phenylmethylene)-1H-Inden-1-one (benzylidene dimethoxydimethylindanone).
A connection assembly for transmitting loads in a load plane between a first wing element (5, 7) and a second wing element (9, 11), wherein the connection assembly is C-shaped and comprises a first load-bearing device and a second load-bearing device, wherein each of the first and second load-bearing devices (17, 19) is L-shaped and comprises a first leg (21, 23), a second leg (25, 27) and a joint region (29, 31), wherein the first leg (21, 23) extends parallel to the load plane and away from the joint region (29, 31) towards a first end region (33, 35) and wherein the second leg (25, 27) extends parallel to the load plane and away from the joint region (29, 31) towards a second end region (37, 39), wherein the second legs (25, 27) of the first and the second load-bearing devices (17, 19) extend in parallel to one another, wherein a first coupling portion for connecting the connection assembly to the second wing element (9, 11) is formed in the joint region of the first load-bearing device, wherein a second coupling portion for connecting the connection assembly to the second wing element (9, 11) is formed in the second end region of the first load-bearing device and the joint region of the second load-bearing device, wherein a third coupling portion for connecting the connection assembly to the first wing element (5, 7) is formed in the first end region of the first load-bearing device and wherein a fourth coupling portion for connecting the connection assembly to the first wing element (5, 7) is formed in the first end region of the second load-bearing device, and wherein the second leg of the second load-bearing device is connected to the second leg of the first load-bearing device. wherein a first coupling portion for connecting the connection assembly to the second wing element (9, 11) is formed in the joint region of the first load-bearing device, wherein a second coupling portion for connecting the connection assembly to the second wing element (9, 11) is formed in the second end region of the first load-bearing device and the joint region of the second load-bearing device, wherein a third coupling portion for connecting the connection assembly to the first wing element (5, 7) is formed in the first end region of the first load-bearing device and wherein a fourth coupling portion for connecting the connection assembly to the first wing element (5, 7) is formed in the first end region of the second load-bearing device, and wherein the second leg of the second load-bearing device is connected to the second leg of the first load-bearing device.
A method of Electron Beam Physical Vapor Deposition, comprising: preheating process gasses within a deposition chamber having at least one wall (90, 92, 94) to about a deposition temperature to counteract a condensation phenomenon, the gas temperature being at least about 1300F (704 C); forming a vapor plume within the deposition chamber; forming a vortex within the deposition chamber around the vapor plume, wherein a gas pressure within said deposition chamber is about 10 Pa with an about 0.5 Pa pressure drop via the vortex; and heating refractory plates in stagnant and vortex areas of the deposition chamber to reduce heat transfer to the at least one wall (90, 92, 94). preheating process gasses within a deposition chamber having at least one wall (90, 92, 94) to about a deposition temperature to counteract a condensation phenomenon, the gas temperature being at least about 1300F (704 C); forming a vapor plume within the deposition chamber; forming a vortex within the deposition chamber around the vapor plume, wherein a gas pressure within said deposition chamber is about 10 Pa with an about 0.5 Pa pressure drop via the vortex; and heating refractory plates in stagnant and vortex areas of the deposition chamber to reduce heat transfer to the at least one wall (90, 92, 94).
A stationary member for a dynamoelectric machine comprising: a stator having an annular back iron and a plurality of teeth extending radially inward from the back iron; a plurality of windings wrapped around each of the plurality of teeth; a heat transfer feature on a radially outer side of the back iron, the heat transfer feature comprising: a base adjacent the back iron; fins (326F1, 326F2) extending radially outward from the base; and a channel formed by the fins (326F1, 326F2), the channel extending at least partially in an axial direction and partially in a circumferential direction, and the fins (326F1, 326F2) being arranged in axial stages, and each axial stage of fins (326F1, 326F2) being clocked in a circumferential direction such that fins (326F1, 326F2) in one axial stage are circumferentially offset from fins (326F1, 326F2) in an adjacent axial stage, characterized by the fins (326F1) of at least one outer axial stage being larger but farther from one another at the ends of base and the fins (326F2) of of at least one inner axial stage being smaller but closer to one another near the middle of base. a stator having an annular back iron and a plurality of teeth extending radially inward from the back iron; a plurality of windings wrapped around each of the plurality of teeth; a heat transfer feature on a radially outer side of the back iron, the heat transfer feature comprising: a base adjacent the back iron; fins (326F1, 326F2) extending radially outward from the base; and a channel formed by the fins (326F1, 326F2), the channel extending at least partially in an axial direction and partially in a circumferential direction, and the fins (326F1, 326F2) being arranged in axial stages, and each axial stage of fins (326F1, 326F2) being clocked in a circumferential direction such that fins (326F1, 326F2) in one axial stage are circumferentially offset from fins (326F1, 326F2) in an adjacent axial stage, characterized by the fins (326F1) of at least one outer axial stage being larger but farther from one another at the ends of base and the fins (326F2) of of at least one inner axial stage being smaller but closer to one another near the middle of base. a base adjacent the back iron; fins (326F1, 326F2) extending radially outward from the base; and a channel formed by the fins (326F1, 326F2), the channel extending at least partially in an axial direction and partially in a circumferential direction, and the fins (326F1, 326F2) being arranged in axial stages, and each axial stage of fins (326F1, 326F2) being clocked in a circumferential direction such that fins (326F1, 326F2) in one axial stage are circumferentially offset from fins (326F1, 326F2) in an adjacent axial stage, characterized by the fins (326F1) of at least one outer axial stage being larger but farther from one another at the ends of base and the fins (326F2) of of at least one inner axial stage being smaller but closer to one another near the middle of base.
Solid lipid particles comprising: a lipid hydrophobic matrix; and from about 5 wt.% to about 30 wt.% of curcumin, wherein said lipid hydrophobic matrix comprises: 5 wt.% to 30 wt. % lecithin; 5 wt.% to 15 wt. % glycerol dibehenate; and at least 40 wt. % mixture of monoglycerides, diglycerides, and triglycerides having a carbon number ranging from C10 to C18, and wherein said solid lipid particles have an average particle size diameter ranging from 100μm to 1500μm. 5 wt.% to 30 wt. % lecithin; 5 wt.% to 15 wt. % glycerol dibehenate; and at least 40 wt. % mixture of monoglycerides, diglycerides, and triglycerides having a carbon number ranging from C10 to C18, and wherein said solid lipid particles have an average particle size diameter ranging from 100μm to 1500μm.
A method of generating a movement profile for a layup procedure, the movement profile defining relative movement between an applicator head and a tool along a head path for laying up a course of composite material, characterized in that the method comprises: determining a bond strength profile along the head path; and determining a movement profile based on the bond strength profile, wherein the movement profile includes a variable rate of relative movement. determining a bond strength profile along the head path; and determining a movement profile based on the bond strength profile, wherein the movement profile includes a variable rate of relative movement.
A welding machine for connecting the edges of overlapping upper sheets of material with overlapped lower sheets of material, which are materially connectable together under the action of heat and the subsequent application of pressure, including a carriage, on which at least running rollers, a heating device and at least one pressure roller are arranged, wherein the heating device includes a laterally projecting contact heating element, which may be introduced between the edges of the sheets of material and the pressure roller, which may be placed on the edges of the sheets of material, is arranged downstream of the contact heating element in the working direction of movement and is driven by an electric motor with subsequent reduction gearing, wherein the carriage is of L-shaped or T-shaped construction with a longitudinal limb extending in the working direction of movement and a transverse limb extending orthogonally to the longitudinal limb, wherein the reduction gearing is an epicyclic gear train and the electric motor and the reduction gearing are combined to form a drum drive motor, characterised in that the electric motor is a brushless direct current motor, which together with the epicyclic gear train constitutes the drum drive motor, wherein the drum drive motor is at least partially integrated into the pressure roller.
Sandwich board comprising at least two outer surface layers, at least one narrow surface coating strip joined to a narrow surface of the sandwich board and at least one, preferably exactly one, core layer which consists of a lightweight construction material, preferably paper or cardboard honeycomb core or PUR foam, and at least one groove running substantially parallel to the surface layers in which at least one reinforcement element is arranged which is connected in a form-fitting or substance-bonded manner with the edge zone of the core layer, characterised in that the groove runs in an edge zone of the sandwich board in order to prevent a piercing and/or crushing of the narrow surface coating strip.
A folding device for flat material webs, in particular for continuously folding material webs based on cellulose, paper, plastic and/or wire mesh, as well as in the form of multilayer laminates comprised of the aforementioned materials, with an infeed table for continuously feeding the material web and with at least one folding bar (3, 4) with a first folding knife (5, 6) fixed thereto, which is set for specific folding heights, wherein the folding bar (3, 4) can be moved up and down in cycles, so that folds can be introduced into the material web with the folding knife acting on the material web, characterized in that at least one additional second folding knife is fixed to the folding bar (3, 4), and that turning the folding bar (3, 4) around an axis of rotation R extending parallel to the longitudinal direction of the folding bar (3, 4) makes the second folding knife available for introducing the folds into the material web instead of the first folding knife.
An acetal-containing, UV-absorbing compound of any one of formula,, or in which: R a is CH 3 or C 2 H 5; R o is H or CH 3; R 1; R 2 and R 2 ' independent of one other are H, CH 3, CCl 3, CF 3, Cl, Br, NR'R" in which R' and R" independent of each other are H or C 1 -C 4 alkyl, OH, or OCH 3; R 1 ' independent of each other are H, CH 3, CCl 3, CF 3, Cl, Br, NR'R" in which R' and R" independent of each other are H or C 1 -C 4 alkyl, OH, OCH 3, SO 3 H, or SO 3 - Na +; R 3 and R 4 independent of each other are H or a first hydrophilic group which is *-CH 2 -(OC 2 H 4) n1 -OCH 3, *-CH 2 -(OC 2 H 4) n1 -OH, provided that at least one of R 3 and R 4 is the first hydrophilic group; r1 is an integer of 3 to 6; n1 is an integer of 2 to 20 (preferably 3 to 15, more preferably 4 to 10); R 8 is CH 3, C 2 H 5, R 9 is SO 3 Na, R 9 ' is H, SO 3 Na, R 10 is methyl or ethyl; L1 is a linkage of or L2 is a linkage of *-CH 2 -*, C 2 H 4 -*, *-C 3 H 6 -*, *-C 3 H 6 -S-C 2 H 4 -*, *-C 3 H 6 -S-C 3 H 6 -*, or L3 is a linkage of *-(CH 2) r1 -* or and X1 is O or NR°; or an acetal compound selected from the group consisting of in which: R a is methyl or ethyl; R 1 and R 2 independent of each other are CH 3, CCl 3, CF 3, Cl, Br, NR'R" OH, or OCH 3; in which R' and R" independent of each other are H or C 1 -C 4 alkyl; R 8 is CH 3, C 2 H 5, R 10 is methyl or ethyl; and r1 is an integer of 3 to 6. R a is CH 3 or C 2 H 5; R o is H or CH 3; R 1; R 2 and R 2 ' independent of one other are H, CH 3, CCl 3, CF 3, Cl, Br, NR'R" in which R' and R" independent of each other are H or C 1 -C 4 alkyl, OH, or OCH 3; R 1 ' independent of each other are H, CH 3, CCl 3, CF 3, Cl, Br, NR'R" in which R' and R" independent of each other are H or C 1 -C 4 alkyl, OH, OCH 3, SO 3 H, or SO 3 - Na +; R 3 and R 4 independent of each other are H or a first hydrophilic group which is *-CH 2 -(OC 2 H 4) n1 -OCH 3, *-CH 2 -(OC 2 H 4) n1 -OH, provided that at least one of R 3 and R 4 is the first hydrophilic group; r1 is an integer of 3 to 6; n1 is an integer of 2 to 20 (preferably 3 to 15, more preferably 4 to 10); R 8 is CH 3, C 2 H 5, R 9 is SO 3 Na, R 9 ' is H, SO 3 Na, R 10 is methyl or ethyl; L1 is a linkage of or L2 is a linkage of *-CH 2 -*, C 2 H 4 -*, *-C 3 H 6 -*, *-C 3 H 6 -S-C 2 H 4 -*, *-C 3 H 6 -S-C 3 H 6 -*, or L3 is a linkage of *-(CH 2) r1 -* or and X1 is O or NR°;
A lamp having a number of plates (3, 4, 5), which plates form a lamp shade, the plates (3, 4, 5) are moveable between different positions characterized in that the plates (3, 4, 5) being placed on upper or lower arms of link mechanisms, that each arm receives at least one plate (3, 4, 5), that one end of each upper arm is connected to an upper ring, that one end of each lower arm is connected to a lower ring, and that the upper ring and lower ring are arranged moveable towards and away from each other.
A gas turbine engine comprising: a turbine section which includes a turbine rotor arranged in a plenum; a compressor section which includes a compressor rotor assembly having spaced apart inner and outer portions (70, 72) that provide an axially extending cooling channel, compressor blades extending radially outward from the outer portion which provides an inner core flow path, and a rotor spoke configured to receive a first cooling flow and fluidly connecting the outer portion to the cooling channel, the compressor rotor assembly having a coolant exit in fluid communication with the cooling channel, the compressor rotor assembly configured to communicate the first cooling flow to the turbine rotor; and a bleed source configured to provide a second cooling flow; and a combustor section which includes a tangential onboard injector in fluid communication with the bleed source, the tangential onboard injector configured to communicate the second cooling flow to the turbine rotor, wherein the turbine rotor is arranged in a plenum configured to receive the first and second cooling flows (76, 190) and wherein the plenum is arranged radially inward of a core flow path, wherein the plenum is defined by a forward wall, a shaft, an aft wall, and an inner diameter wall of the core flow path, and wherein the first and second cooling flows (76, 190) are thermally isolated from the core flow path. a turbine section which includes a turbine rotor arranged in a plenum; a compressor section which includes a compressor rotor assembly having spaced apart inner and outer portions (70, 72) that provide an axially extending cooling channel, compressor blades extending radially outward from the outer portion which provides an inner core flow path, and a rotor spoke configured to receive a first cooling flow and fluidly connecting the outer portion to the cooling channel, the compressor rotor assembly having a coolant exit in fluid communication with the cooling channel, the compressor rotor assembly configured to communicate the first cooling flow to the turbine rotor; and a bleed source configured to provide a second cooling flow; and a combustor section which includes a tangential onboard injector in fluid communication with the bleed source, the tangential onboard injector configured to communicate the second cooling flow to the turbine rotor, wherein the turbine rotor is arranged in a plenum configured to receive the first and second cooling flows (76, 190) and wherein the plenum is arranged radially inward of a core flow path, wherein the plenum is defined by a forward wall, a shaft, an aft wall, and an inner diameter wall of the core flow path, and wherein the first and second cooling flows (76, 190) are thermally isolated from the core flow path.
Method of detecting movements of a sample with respect to an objective, - wherein the sample is imaged onto an image sensor by means of the objective, - wherein images of the sample are recorded by the image sensor in that light coming from the sample is registered at image points of the image sensor, - wherein a subset of not more than 90 % of the image points of the image sensor is selected, and - wherein parts of the images that each correspond to the subset of the image point of the image sensor are compared to parts of at least one reference image that also correspond to the subset of the image points of the image sensor, characterized in - that variations of intensities of the light coming from the sample and registered at the individual image points of the image sensor during a set-up period are determined in that a temporal course of the intensity of the light registered at the respective image point of the image sensor over the set-up period is analyzed, and - that the variations are used as a criterion in selecting the subset of the image points of the image sensor. - wherein the sample is imaged onto an image sensor by means of the objective, - wherein images of the sample are recorded by the image sensor in that light coming from the sample is registered at image points of the image sensor, - wherein a subset of not more than 90 % of the image points of the image sensor is selected, and - wherein parts of the images that each correspond to the subset of the image point of the image sensor are compared to parts of at least one reference image that also correspond to the subset of the image points of the image sensor, - that variations of intensities of the light coming from the sample and registered at the individual image points of the image sensor during a set-up period are determined in that a temporal course of the intensity of the light registered at the respective image point of the image sensor over the set-up period is analyzed, and - that the variations are used as a criterion in selecting the subset of the image points of the image sensor.
A method for increasing a voltage potential available to a voltage-sensitive device sharing a battery with a high current inertial device comprising: pulsing the power to the high current inertial device within an adjustable duty cycle; storing energy between the pulses; releasing said stored energy during the pulses, when the voltage of the battery declines, to feed the voltage-sensitive device; and adjusting, by the voltage-sensitive device, the duty cycle in order to maintain an input voltage to the voltage-sensitive device at or above a threshold value needed to maintain functioning of said voltage-sensitive device. pulsing the power to the high current inertial device within an adjustable duty cycle; storing energy between the pulses; releasing said stored energy during the pulses, when the voltage of the battery declines, to feed the voltage-sensitive device; and adjusting, by the voltage-sensitive device, the duty cycle in order to maintain an input voltage to the voltage-sensitive device at or above a threshold value needed to maintain functioning of said voltage-sensitive device.