mhurhangee/patent-ind-claim-en huggingface dataset:
A shaving cartridge comprising: a housing having a top surface , a bottom surface , a front edge , a rear edge , and a pair of side edges extending between the front edge and the rear edge , the housing having a main blade disposed between the front edge and the rear edge , the main blade having a main cutting edge extending toward the top surface , the main blade being movable in the housing toward the bottom surface 18 during shaving, wherein the shaving cartridge comprises a masking foil comprising a front portion located forward of the main cutting edge and a back portion located rearward the main cutting edge , the masking foil further comprising at least one ribbon which partially covers the main cutting edge , wherein the at least one ribbon comprises a front bent portion connected to the front portion and a back bent portion connected to the back portion of the masking foil , the front and the back bent portion being directed toward the bottom surface , and wherein the masking foil is inserted in the housing of the cartridge . a housing having a top surface , a bottom surface , a front edge , a rear edge , and a pair of side edges extending between the front edge and the rear edge , the housing having a main blade disposed between the front edge and the rear edge , the main blade having a main cutting edge extending toward the top surface , the main blade being movable in the housing toward the bottom surface 18 during shaving, wherein the shaving cartridge comprises a masking foil comprising a front portion located forward of the main cutting edge and a back portion located rearward the main cutting edge , the masking foil further comprising at least one ribbon which partially covers the main cutting edge , wherein the at least one ribbon comprises a front bent portion connected to the front portion and a back bent portion connected to the back portion of the masking foil , the front and the back bent portion being directed toward the bottom surface , and wherein the masking foil is inserted in the housing of the cartridge .
A prosthetic liner defining a proximal end and a distal end , the prosthetic liner having a liner body defined between the proximal end and the distal end, and the liner body having a tubular shape, the liner comprising: a lattice structure defined as a plurality of layers monolithically formed as an inseparable and continuous structure; wherein the lattice structure includes a first layer of first filaments discretely formed from a first elastomeric material, and overlapping a second layer of second filaments discretely formed from a second elastomeric material, the first and second filaments of the first and second layers , respectively, overlapping and forming a first set of interstices located therebetween in a predetermined pattern, wherein the first filaments are spaced apart from each other, and extend in a first direction oriented differently from a second direction in which the second filaments extend; wherein the first and second filaments extend continuously about the tubular shape of the liner body, and the first and second layers are relatively concentric to one another, characterized in that the first and second layers of the first and second filaments are permanently and chemically bonded to one another, the first and second layers are blended at least in part with one another in a blended region. a lattice structure defined as a plurality of layers monolithically formed as an inseparable and continuous structure; wherein the lattice structure includes a first layer of first filaments discretely formed from a first elastomeric material, and overlapping a second layer of second filaments discretely formed from a second elastomeric material, the first and second filaments of the first and second layers , respectively, overlapping and forming a first set of interstices located therebetween in a predetermined pattern, wherein the first filaments are spaced apart from each other, and extend in a first direction oriented differently from a second direction in which the second filaments extend; wherein the first and second filaments extend continuously about the tubular shape of the liner body, and the first and second layers are relatively concentric to one another, characterized in that the first and second layers of the first and second filaments are permanently and chemically bonded to one another, the first and second layers are blended at least in part with one another in a blended region.
A torque transmitting apparatus for a drive assembly for transmitting a torque from a first shaft to a second shaft, with a first coupling device that is used for transmitting torques and compensating a shaft offset, with a second coupling device that is used for transmitting torques and limiting torques, wherein the first coupling device and the second coupling device are connected in series, wherein the second coupling device has an inner part in the form of a hollow component and an outer part in the form of a hollow component, the inner part has on its radially outer side a first friction surface and the outer part has on its radially inner side a second friction surface , which adjoins the first friction surface radially outward and interacts therewith, the inner part has a pressure chamber that can be filled with a pressure medium and makes it possible to adjust a torque, which is the maximum torque transmittable by the friction surfaces, in order to provide the torque limiting, wherein the inner part has a pressure connection for the pressure chamber and the pressure in the pressure chamber can be adjusted and varied during the operation by means of the pressure connection . with a first coupling device that is used for transmitting torques and compensating a shaft offset, with a second coupling device that is used for transmitting torques and limiting torques, wherein the first coupling device and the second coupling device are connected in series, wherein the second coupling device has an inner part in the form of a hollow component and an outer part in the form of a hollow component, the inner part has on its radially outer side a first friction surface and the outer part has on its radially inner side a second friction surface , which adjoins the first friction surface radially outward and interacts therewith, the inner part has a pressure chamber that can be filled with a pressure medium and makes it possible to adjust a torque, which is the maximum torque transmittable by the friction surfaces, in order to provide the torque limiting, wherein the inner part has a pressure connection for the pressure chamber and the pressure in the pressure chamber can be adjusted and varied during the operation by means of the pressure connection .
A glucagon derivative comprising an amino acid sequence represented by SEQ ID NO: 20.
A combustion engine comprising a turbo unit having a compressor and a turbine including a turbine inlet and turbine outlet for the throughflow of exhaust gases to and from the turbine , an EGR system arranged between an intake system and the exhaust gas system of the combustion engine , wherein the EGR system is connected to the intake system downstream of the compressor and connected to the exhaust gas system upstream of the turbine , a first exhaust gas pipe , which is connected to the turbine inlet , a second exhaust gas pipe , which is connected to the turbine outlet , a waste gate duct , which is connected to the first and second exhaust gas pipes , and a flow-limiting unit arranged in the second exhaust gas pipe , which flow-limiting unit has a cross-sectional area (Ar) smaller than the second exhaust gas pipe's cross-sectional area (Ae), wherein the waste gate duct has a cross-sectional area (Aw) which is smaller than the second exhaust gas pipe's cross-sectional area (Ae) and in that a waste gate valve arranged in the waste gate duct is adapted to fine adjustment of the exhaust gas flow through the waste gate duct , and wherein the waste gate duct's cross-sectional area (Aw) is the same size as or smaller than the flow-limiting unit's cross-sectional area (Ar), and wherein the waste gate duct flows into the second exhaust gas pipe upstream of the flow-limiting unit , and wherein the flow-limiting unit is a passive unit without moving components and wherein the combustion engine is an Otto engine. an EGR system arranged between an intake system and the exhaust gas system of the combustion engine , wherein the EGR system is connected to the intake system downstream of the compressor and connected to the exhaust gas system upstream of the turbine , a first exhaust gas pipe , which is connected to the turbine inlet , a second exhaust gas pipe , which is connected to the turbine outlet , a waste gate duct , which is connected to the first and second exhaust gas pipes , and a flow-limiting unit arranged in the second exhaust gas pipe , which flow-limiting unit has a cross-sectional area (Ar) smaller than the second exhaust gas pipe's cross-sectional area (Ae), wherein the waste gate duct has a cross-sectional area (Aw) which is smaller than the second exhaust gas pipe's cross-sectional area (Ae) and in that a waste gate valve arranged in the waste gate duct is adapted to fine adjustment of the exhaust gas flow through the waste gate duct , and wherein the waste gate duct's cross-sectional area (Aw) is the same size as or smaller than the flow-limiting unit's cross-sectional area (Ar), and wherein the waste gate duct flows into the second exhaust gas pipe upstream of the flow-limiting unit , and wherein the flow-limiting unit is a passive unit without moving components and wherein the combustion engine is an Otto engine.
A muographic observation instrument for the use in a muographic observation system for imaging an internal structure of a gigantic object, said instrument comprising an arrangement of muon-detecting gaseous detectors (40a-40f) arranged to be parallel to a flat surface with certain distance between them; characterized in that said instrument further comprising detachable detector sockets (34a-34f) mounting the gaseous detectors (40a-40f); radiation shields (50a-50e, 51a-51e) composed of lead plates arranged in stainless steel cases; detachable shield sockets (35a-35e) mounting the radiation shields (50a-50e, 51a-51e), said shield sockets (35a-35e) are arranged between the detector sockets (34a-34f); said detector sockets (34a-34f) are attached to wires (36a-36f). an arrangement of muon-detecting gaseous detectors (40a-40f) arranged to be parallel to a flat surface with certain distance between them; characterized in that said instrument further comprising detachable detector sockets (34a-34f) mounting the gaseous detectors (40a-40f); radiation shields (50a-50e, 51a-51e) composed of lead plates arranged in stainless steel cases; detachable shield sockets (35a-35e) mounting the radiation shields (50a-50e, 51a-51e), said shield sockets (35a-35e) are arranged between the detector sockets (34a-34f); said detector sockets (34a-34f) are attached to wires (36a-36f).
An activated EU-2 zeolite, comprising: pores having a diameter of 30 to 40 Å while maintaining a crystal structure of the EU-2 zeolite; and pores having a diameter of 40 to 200 Å, wherein a volume of the pores having a diameter of 30 to 40 Å is 0.01 to 0.06 cc/g, and a volume of the pores having a diameter of 40 to 200 Å is 0.07 to 0.4 cc/g, wherein a total specific surface area of the activated EU-2 zeolite is 240 to 330 m 2 /g, and wherein the specific surface area, pore size and pore volume of zeolite are measured using a BET meter ASAP 2020 manufactured by Micromeritics Corporation.
Structural element comprising at least two fibre cast nub mats , wherein the fibre cast nub mats have several elevations (4, 4', 4"; 5, 5', 5"), wherein the elevations (4, 4', 4"; 5, 5', 5") are arranged in a checkerboard pattern in horizontal rows and vertical rows, wherein grooves (6, 6', 6"; 7, 7', 7", 8, 8', 8", 8′′′; 9, 9', 9") are formed between the projections (4, 4', 4"; 5, 5', 5"), wherein the first fibre casting nub mat is applied to the second fibre casting nub mat in such a way that the upper sides of the elevations (4, 4', 4") of the first fibre casting nub mat and the upper sides of the elevations (5, 5', 5") of the second fibre casting nub mat face one another and are brought into alignment, wherein the first fibre cast nubbed mat and the second fibre cast nubbed mat are joined together, characterised in that reed-like grasses are introduced into the channels (6, 6', 6"; 7, 7', 7", 8, 8', 8", 8′′′; 9, 9', 9"). at least two fibre cast nub mats , wherein the fibre cast nub mats have several elevations (4, 4', 4"; 5, 5', 5"), wherein the elevations (4, 4', 4"; 5, 5', 5") are arranged in a checkerboard pattern in horizontal rows and vertical rows, wherein grooves (6, 6', 6"; 7, 7', 7", 8, 8', 8", 8′′′; 9, 9', 9") are formed between the projections (4, 4', 4"; 5, 5', 5"), wherein the first fibre casting nub mat is applied to the second fibre casting nub mat in such a way that the upper sides of the elevations (4, 4', 4") of the first fibre casting nub mat and the upper sides of the elevations (5, 5', 5") of the second fibre casting nub mat face one another and are brought into alignment, wherein the first fibre cast nubbed mat and the second fibre cast nubbed mat are joined together, characterised in that reed-like grasses are introduced into the channels (6, 6', 6"; 7, 7', 7", 8, 8', 8", 8′′′; 9, 9', 9").
Use of a modified effect pigment in a radiation-curable coating composition, wherein the modified effect pigment has no organic oligomers or polymers and wherein the modified effect pigment is an effect pigment which is coated with a layer of a metal oxide, comprising silicon dioxide, aluminium oxide, or mixtures thereof, characterized in that at least one organic compound, which has one or more functional groups with a carbon-carbon multiple bond, is bound to the layer.
A coating system for a component of a gas turbine engine, the coating system comprising a bond coat layer and a thermal barrier coating layer above the bond coat layer , wherein the bond coat layer has a roughness Ra of its surface facing the thermal barrier coating layer in a range 12.8-19.0 micrometers, and the thermal barrier coating layer has a thickness in the range 200-700 micrometers and a porosity in the range 15.0-23.0 vol %, with ends of ranges included in the ranges, characterised in that the bond coat layer has a thickness in the range 180-300 micrometers.
A composition comprising: a poly(ester-carbonate-siloxane) copolymer; 1 to 5 wt% based on a total weight of the composition of a nanosilica having a D 50 particle size by volume of 5 to 50 nanometers measured as defined in the description ; wherein the nanosilica has a hydrophobic coating; 1 to 10 wt% based on a total weight of the composition of a plurality of polysiloxane particles having a D 50 particle size by volume of 0.1 to 10 micrometers measured as defined in the description; and 0.005 to 5 wt% based on a total weight of the composition of a fluoropolymer. a poly(ester-carbonate-siloxane) copolymer; 1 to 5 wt% based on a total weight of the composition of a nanosilica having a D 50 particle size by volume of 5 to 50 nanometers measured as defined in the description ; wherein the nanosilica has a hydrophobic coating; 1 to 10 wt% based on a total weight of the composition of a plurality of polysiloxane particles having a D 50 particle size by volume of 0.1 to 10 micrometers measured as defined in the description; and 0.005 to 5 wt% based on a total weight of the composition of a fluoropolymer.
A water-soluble film having a thickness of from 0.05 mm to 0.3 mm, comprising at least one biologically active substance and/or at least one therapeutically active substance and, as a film-forming agent, an alginate salt of monovalent cation or a mixture of alginate salts of monovalent cation, the film-forming agent having a mean guluronate (G) content of from 50 to 85% by weight, a mean mannuronate (M) content of from 15 to 50% by weight, a mean molecular weight of from 30,000 g/mol to 90,000 g/mol and being such that a 10% aqueous solution thereof at a temperature of 20°C has a viscosity of 100-1000 mPas, as measured at a shear rate of 20 rpm by use of a Brookfield viscometer with a spindle No. 2, said film being obtainable by preparing a solution of said film forming agent, which solution also contains the at least one biologically active substance and/or at least one therapeutically active substance, distributing the solution onto a solid surface, and permitting the solution to dry on said surface.
A fluid handling structure for use in an immersion lithographic apparatus, wherein the fluid handling structure is configured to provide an immersion fluid to a space between a final element of a projection system (PS) and an opposing surface (W, WT) that is moveable relative to the final element of the projection system, the fluid handling structure comprising: a fluid extraction conduit configured to conduct a used fluid away from the space, wherein the fluid extraction conduit comprises a recovery port configured to receive the used fluid into the conduit and a plurality of flow breakers that each extend across at least a portion of the conduit; the flow breakers are positioned downstream of the recovery port; the flow breakers are arranged so that a common plane cuts through at least a portion of two or more of the flow breakers; and the common plane is aligned so as to be perpendicular to the average direction of flow, in use, in the conduit at the position of the common plane, characterized in that the fluid extraction conduit further comprises a peripheral wall configured to contain the fluid peripherally within the conduit, and in that at least one of the two or more flow breakers having a portion in the common plane is a discrete element with the only connection between the flow breaker and any other of the two or more flow breakers having a portion in the common plane being made via the peripheral wall a fluid extraction conduit configured to conduct a used fluid away from the space, wherein the fluid extraction conduit comprises a recovery port configured to receive the used fluid into the conduit and a plurality of flow breakers that each extend across at least a portion of the conduit; the flow breakers are positioned downstream of the recovery port; the flow breakers are arranged so that a common plane cuts through at least a portion of two or more of the flow breakers; and the common plane is aligned so as to be perpendicular to the average direction of flow, in use, in the conduit at the position of the common plane, characterized in that the fluid extraction conduit further comprises a peripheral wall configured to contain the fluid peripherally within the conduit, and in that at least one of the two or more flow breakers having a portion in the common plane is a discrete element with the only connection between the flow breaker and any other of the two or more flow breakers having a portion in the common plane being made via the peripheral wall
An ambient image projection device, comprising: a light source assembly ; and a first projection mechanism and a second projection mechanism provided side by side; wherein, the second projection mechanism comprises an interference lens and a second optical module ; light emitted from the light source assembly is guided by the second optical module to pass through the interference lens and forms an interference pattern to be projected in space; characterized in that the first projection mechanism comprises a display and a first optical module ; a content played on the display is guided by the first optical module to form a dynamic image to be projected in space; wherein the interference pattern and the dynamic image overlap at least partially with each other in the space; the second optical module comprises a reflector provided between the light source assembly and the interference lens for directing light emitted from the light source assembly to the interference lens , wherein reflective surfaces on an inner wall of the reflector consists of a plurality of planes capable of reflecting light, such that light incident on the reflective surfaces is reflected out from the plurality of planes to create numerous interlaced rays. a light source assembly ; and a first projection mechanism and a second projection mechanism provided side by side; wherein, the second projection mechanism comprises an interference lens and a second optical module ; light emitted from the light source assembly is guided by the second optical module to pass through the interference lens and forms an interference pattern to be projected in space; characterized in that the first projection mechanism comprises a display and a first optical module ; a content played on the display is guided by the first optical module to form a dynamic image to be projected in space; wherein the interference pattern and the dynamic image overlap at least partially with each other in the space; the second optical module comprises a reflector provided between the light source assembly and the interference lens for directing light emitted from the light source assembly to the interference lens , wherein reflective surfaces on an inner wall of the reflector consists of a plurality of planes capable of reflecting light, such that light incident on the reflective surfaces is reflected out from the plurality of planes to create numerous interlaced rays.
A lens unit comprising: a first lens (L1); and a second lens (L2); the first lens (L1) and the second lens (L2) being arranged in order of the first lens and the second lens from a display surface side (ID) on which an image is displayed to an observation surface side (SP); the first lens being a Fresnel lens having a first lens surface (L1b) having a Fresnel structure on the second lens side, and having a positive refractive power; the second lens being a Fresnel lens having a second lens surface (L2a) having a Fresnel structure on the first lens side, and having a positive refractive power, wherein a third lens surface (L3a) facing the display surface side (ID) is formed more to the display surface side than the first lens surface (L1b), and the third lens surface (L3a) has a surface that refracts light in a direction of going away from an optical axis at least in a peripheral region separated from the optical axis, wherein a lens (L3) in which the third lens surface (L3a) is formed includes a center intersecting the optical axis, the outside region (R2), and an intermediate region as a region (R4) between the center and the outside region (R2), and a following condition is satisfied: Condition: T3 > T1 > T2 where T1 is a thickness in the center, T2 is a thickness in the intermediate region, and T3 is a thickness in the peripheral region. a first lens (L1); and a second lens (L2); the first lens (L1) and the second lens (L2) being arranged in order of the first lens and the second lens from a display surface side (ID) on which an image is displayed to an observation surface side (SP); the first lens being a Fresnel lens having a first lens surface (L1b) having a Fresnel structure on the second lens side, and having a positive refractive power; the second lens being a Fresnel lens having a second lens surface (L2a) having a Fresnel structure on the first lens side, and having a positive refractive power, wherein a third lens surface (L3a) facing the display surface side (ID) is formed more to the display surface side than the first lens surface (L1b), and the third lens surface (L3a) has a surface that refracts light in a direction of going away from an optical axis at least in a peripheral region separated from the optical axis, wherein a lens (L3) in which the third lens surface (L3a) is formed includes a center intersecting the optical axis, the outside region (R2), and an intermediate region as a region (R4) between the center and the outside region (R2), and a following condition is satisfied: Condition: T3 > T1 > T2 where T1 is a thickness in the center, T2 is a thickness in the intermediate region, and T3 is a thickness in the peripheral region.