mhurhangee/ep-ind-claims huggingface dataset:
A device for collecting onto a sample holder a biological tissue carried on a shaft, characterised in that, the device comprising a base, a lever and a needle bed, wherein said needle bed is attached to one of said base and said lever and is configured to support, in a pre-defined position, a shaft configured for carrying a biological tissue, whereas the other one of said base and said lever is configured to support a sample holder attachable thereto, and wherein said lever is movable between settings relative to said base so that: - in a first setting of said settings, a sample holder suitably attached to said device and said needle bed are distant from one another, and - in a second setting of said settings said sample holder and said needle bed are situated proximal to one another having a predefined arrangement relative to one another, and wherein, in said second setting, said sample holder is configured to contact a biological tissue carried on a shaft supported by said needle bed, thereby adhering to said biological tissue, and thereby detaching said biological tissue from said shaft when said lever is moved from said second setting to said first setting. the device comprising a base, a lever and a needle bed, wherein said needle bed is attached to one of said base and said lever and is configured to support, in a pre-defined position, a shaft configured for carrying a biological tissue, whereas the other one of said base and said lever is configured to support a sample holder attachable thereto, and wherein said lever is movable between settings relative to said base so that: - in a first setting of said settings, a sample holder suitably attached to said device and said needle bed are distant from one another, and - in a second setting of said settings said sample holder and said needle bed are situated proximal to one another having a predefined arrangement relative to one another, - in a first setting of said settings, a sample holder suitably attached to said device and said needle bed are distant from one another, and - in a second setting of said settings said sample holder and said needle bed are situated proximal to one another having a predefined arrangement relative to one another, and wherein, in said second setting, said sample holder is configured to contact a biological tissue carried on a shaft supported by said needle bed, thereby adhering to said biological tissue, and thereby detaching said biological tissue from said shaft when said lever is moved from said second setting to said first setting.
Domestic refrigeration appliance having a heat-insulating inner container, which is configured to delimit at least one storage space for refrigerated goods, a refrigerated goods container that is supported in the inner container and has an opening which is accessible from above, and a container lid that is supported in the inner container by a support apparatus coupled to a manual actuator, wherein the manual actuator has a slider, wherein the slider is configured to indicate a first optical display in a first slider position and to indicate a second optical display in a second slider position, in which the first optical display is concealed, characterised in that in the depth direction the slider is adjustably supported in the front panel.
A charging case (20, 32, 170) for an aerosol-generating device (10, 34, 40, 100, 150), the charging case comprising: a case connector for receiving electrical power from an external source; a plurality of case cavities (22, 176), each of the plurality of case cavities being configured to receive at least one of a plurality of power sources; a mounting section (24, 38, 18) for connecting the aerosol-generating device to the charging case; and a case control unit arranged to: charge a first one of the plurality of power sources via the case connector using electrical power from the external power source; and charge the aerosol-generating device connected to the mounting section via a second one of the plurality of power sources; wherein each one of the power sources is removable and insertable into any one of the plurality of case cavities. a case connector for receiving electrical power from an external source; a plurality of case cavities (22, 176), each of the plurality of case cavities being configured to receive at least one of a plurality of power sources; a mounting section (24, 38, 18) for connecting the aerosol-generating device to the charging case; and a case control unit arranged to: charge a first one of the plurality of power sources via the case connector using electrical power from the external power source; and charge the aerosol-generating device connected to the mounting section via a second one of the plurality of power sources; charge a first one of the plurality of power sources via the case connector using electrical power from the external power source; and charge the aerosol-generating device connected to the mounting section via a second one of the plurality of power sources; wherein each one of the power sources is removable and insertable into any one of the plurality of case cavities.
A pipe connecting mechanism for a seal device for connecting a space inside the seal device with an external pipe, said pipe connecting mechanism comprises: a communicating bore formed in a nonmetallic member constituting said seal device and communicated with said space to be connected at one of end portions thereof; characterized in that the pipe connecting mechanism further comprises: a resin connecting pipe inserted into the other end portion of said communicating bore at one of end portions thereof; a reinforcing member having a through-bore into which said connecting pipe is inserted and which is connected to the other end portion of said communicating bore at one of end portions thereof, the reinforcing member fixedly mounted to the predetermined member of said seal device; a resin connector connected with the other end portion of said connecting pipe inserted into said reinforcing member at one of end portions thereof and connected with said external pipe at the other end portion thereof; and a packing fixedly set up on one of end portions of said connecting pipe inserted into the other end portion of said communicating bore and sealing between an outer circumference surface of the one of end portions of said connecting pipe and an inner circumference surface of the other end portion of said communicating bore. a resin connecting pipe inserted into the other end portion of said communicating bore at one of end portions thereof; a reinforcing member having a through-bore into which said connecting pipe is inserted and which is connected to the other end portion of said communicating bore at one of end portions thereof, the reinforcing member fixedly mounted to the predetermined member of said seal device; a resin connector connected with the other end portion of said connecting pipe inserted into said reinforcing member at one of end portions thereof and connected with said external pipe at the other end portion thereof; and a packing fixedly set up on one of end portions of said connecting pipe inserted into the other end portion of said communicating bore and sealing between an outer circumference surface of the one of end portions of said connecting pipe and an inner circumference surface of the other end portion of said communicating bore.
An aircraft engine assembly comprising: an aircraft engine; a nacelle configured to surround the aircraft engine and having an inlet open to ambient air; an annular acoustic panel comprising an open framework, made from a first material, forming a plurality of cells, and a surface structure resulting from a surface treatment provided on the open framework to increase sound attenuation; wherein the annular acoustic panel is provided within the nacelle such that sound emitted from the aircraft engine is attenuated by the annular acoustic panel; characterised in that: the surface structure comprises at least one of a nanostructure, a particulate layer, and a cellular solid body. an aircraft engine; a nacelle configured to surround the aircraft engine and having an inlet open to ambient air; an annular acoustic panel comprising an open framework, made from a first material, forming a plurality of cells, and a surface structure resulting from a surface treatment provided on the open framework to increase sound attenuation; wherein the annular acoustic panel is provided within the nacelle such that sound emitted from the aircraft engine is attenuated by the annular acoustic panel; characterised in that: the surface structure comprises at least one of a nanostructure, a particulate layer, and a cellular solid body. the surface structure comprises at least one of a nanostructure, a particulate layer, and a cellular solid body.
Process for expression, purification and refolding of recombinant Plasmodium vivax Duffy binding protein region II (rPvRII) having multiple cysteines useful for the prophylaxis of malarial infection in mammals, the process comprising the following steps: a) culturing the host E. coli cells containing a desired recombinant gene construct comprising a codon optimized gene sequence of rPvRII, wherein rPvRII has the structure: to produce cells in high density b) inducing expression of rPvRII in E. coli as inclusion bodies, c) harvesting the cells and isolating the said inclusion bodies, d) separating rPvRII from inclusion bodies by repeated sequential washing with washing with a buffer, the buffer used being a low salt buffer consisting of 5-50 mM Tris, 2-25 mM EDTA, 50-100 mM sodium chloride, 1-6 M urea, 0.1-1% Triton X-100, pH 6.5-7.5; followed by washing with a high salt buffer containing 5-50 mM Tris, pH 6.5-7.5 and 0.5-1 M sodium chloride; and solubilizing with chaotropic agents comprising guanidine hydrochloride at 6-8 M concentration, e) purifying the protein by subjecting to metal-chelate affinity chromatography, f) re-folding of the purified rPvRII obtained in step e) by employing a buffer containing a detergent - dextrin mixture, a co-solvent and a redox pair, wherein the detergent used is Triton X-100 at a concentration of 0.1-1.0 mM, a dextrin at a concentration of 5-20 mM, L-Arginine as a co-solvent being added in a concentration of 0.4-0.8 M and a redox pair comprising L-cysteine - cystamine dihydrochloride; followed by g) further purifying the desired protein by removing impurities by subjecting to chromatography. a) culturing the host E. coli cells containing a desired recombinant gene construct comprising a codon optimized gene sequence of rPvRII, wherein rPvRII has the structure: to produce cells in high density b) inducing expression of rPvRII in E. coli as inclusion bodies, c) harvesting the cells and isolating the said inclusion bodies, d) separating rPvRII from inclusion bodies by repeated sequential washing with washing with a buffer, the buffer used being a low salt buffer consisting of 5-50 mM Tris, 2-25 mM EDTA, 50-100 mM sodium chloride, 1-6 M urea, 0.1-1% Triton X-100, pH 6.5-7.5; followed by washing with a high salt buffer containing 5-50 mM Tris, pH 6.5-7.5 and 0.5-1 M sodium chloride; and solubilizing with chaotropic agents comprising guanidine hydrochloride at 6-8 M concentration, e) purifying the protein by subjecting to metal-chelate affinity chromatography, f) re-folding of the purified rPvRII obtained in step e) by employing a buffer containing a detergent - dextrin mixture, a co-solvent and a redox pair, wherein the detergent used is Triton X-100 at a concentration of 0.1-1.0 mM, a dextrin at a concentration of 5-20 mM, L-Arginine as a co-solvent being added in a concentration of 0.4-0.8 M and a redox pair comprising L-cysteine - cystamine dihydrochloride; followed by g) further purifying the desired protein by removing impurities by subjecting to chromatography.
A compound of Formula: where: R1 = R2 = n = 1-3 wherein the R 1 substituent point of attachment is on the substituent boron atom of R 1, or a salt thereof, a solvate thereof, or a solvate of a salt thereof. R1 = R2 = n = 1-3 wherein the R 1 substituent point of attachment is on the substituent boron atom of R 1, or a salt thereof, a solvate thereof, or a solvate of a salt thereof.
Cooling layout for a turbine engine distributor blade, said blade being fitted with at least one cavity surrounded by an internal wall comprising cooling fins which are spaced apart from each other by a pitch (p) and each have a thickness (e), said blade being fitted with a jacket, and passed through by emission holes each having a diameter (d), characterised in that, when the jacket is in place in the cavity of the blade, and in respect of the critical operating point of the turbine engine, each emission hole of the jacket is opposite a place on the internal wall of the blade which is between cooling fins and when the jacket is in place in the cavity of the blade, and in respect of the critical operating point of the turbine engine, the pitch (p) and the thickness (e) of the cooling fins satisfy the relationship: p / e ≥ 3, characterized in that the jacket is not in contact with the cooling fins and is in contact with the internal wall through lobes located on the surface of the jacket.
Optoelectronic component, wherein the optoelectronic component is a laser diode, with a layer structure with an active zone for producing electromagnetic radiation, wherein the active zone is arranged in one plane, wherein the layer structure comprises an upper side and four side faces (3, 4, 5, 6), wherein the first and the third side face (3, 5) are arranged to lie opposite each other, wherein the second and the fourth side face (4, 6) are arranged to lie opposite each other, wherein a stripe-type ridge structure is disposed on the upper side of the layer structure, wherein the ridge structure extends between the first side face and the third side face, wherein the first side face represents a radiation surface for electromagnetic radiation, wherein a first recess is introduced, laterally next to the ridge structure, into the upper side of the layer structure, wherein a second recess is introduced into the first recess, and wherein the second recess extends to the second side face (4, 50, 51), wherein the second recess is introduced into a first bottom face of the first recess, wherein the second recess extends along the second side face, wherein the second recess is formed at a distance from the first side face and at a distance from the third side face, and wherein the second recess opens into the second side face, characterized in that the first recess extends over an entire length of the laser diode along the second side face from the first to the third side face (3, 5), wherein the first recess extends up to the second side face.
A method for structuring at least one surface of an OSB wood-based panel having an anti-slip surface, wherein the structuring consists of regularly arranged structural elevations on the surface of the OSB wood-based panel, comprising the steps a) providing at least one OSB wood-based panel, b) applying at least one first layer of at least one first plastic resin to the at least one surface of the wood-based panel with at least one first application tool for filling the surface of the OSB wood-based panel, c) applying at least one second layer of at least one second plastic resin to form the regularly arranged structural elevations for forming the anti-slip effect to the at least one first plastic resin layer with at least one application tool having a regularly structured surface, wherein the ratio between structural elevations and free surface of the OSB wood-based panel is between 1:3 and 1:30, and d) solidifying the first layer of the first plastic resin and the second layer having the structural elevations of the second plastic resin. a) providing at least one OSB wood-based panel, b) applying at least one first layer of at least one first plastic resin to the at least one surface of the wood-based panel with at least one first application tool for filling the surface of the OSB wood-based panel, c) applying at least one second layer of at least one second plastic resin to form the regularly arranged structural elevations for forming the anti-slip effect to the at least one first plastic resin layer with at least one application tool having a regularly structured surface, wherein the ratio between structural elevations and free surface of the OSB wood-based panel is between 1:3 and 1:30, and d) solidifying the first layer of the first plastic resin and the second layer having the structural elevations of the second plastic resin.
A storage device with multiple storage modules that are stacked against one another, wherein the storage modules are realized independently of one another and respectively have a closed storage volume, wherein the storage modules respectively have at least one storage container and at least one heat carrier channel that borders on an outer wall of the storage container, and wherein the heat carrier channels of the multiple storage modules are connected to one another by means of at least one heat carrier connecting line, characterized in that the at least one heat carrier channel is delimited by a wall surface (12, 14) of the outer wall of an associated storage container and a channel wall that is connected to the wall surface (12, 14) and formed by a sheet metal element, which is connected to the wall surface (12, 14) in a sealing manner.
An integrated air cap/nozzle (40; 140; 340; 440; 540; 640) for a liquid spray gun, wherein the integrated air cap/nozzle comprises: a cap body comprising: a nozzle body (50; 150; 350; 650) comprising a nozzle aperture, a nozzle outlet end (56; 156; 656) located within the nozzle aperture, and a liquid nozzle opening (52; 152; 352; 652) located within the nozzle outlet end (56; 156; 656) through which liquid exits during operation of the liquid spray gun; and a center air outlet (54; 154; 354; 654) located in a gap defined between the nozzle aperture and the nozzle outlet end (56; 156; 656), through which center air discharges when a liquid is sprayed through the liquid nozzle opening; wherein the liquid nozzle opening and the center air outlet are formed in a front wall (60; 160a, 160b) of the cap body. a cap body comprising: a nozzle body (50; 150; 350; 650) comprising a nozzle aperture, a nozzle outlet end (56; 156; 656) located within the nozzle aperture, and a liquid nozzle opening (52; 152; 352; 652) located within the nozzle outlet end (56; 156; 656) through which liquid exits during operation of the liquid spray gun; and a center air outlet (54; 154; 354; 654) located in a gap defined between the nozzle aperture and the nozzle outlet end (56; 156; 656), through which center air discharges when a liquid is sprayed through the liquid nozzle opening; a nozzle body (50; 150; 350; 650) comprising a nozzle aperture, a nozzle outlet end (56; 156; 656) located within the nozzle aperture, and a liquid nozzle opening (52; 152; 352; 652) located within the nozzle outlet end (56; 156; 656) through which liquid exits during operation of the liquid spray gun; and a center air outlet (54; 154; 354; 654) located in a gap defined between the nozzle aperture and the nozzle outlet end (56; 156; 656), through which center air discharges when a liquid is sprayed through the liquid nozzle opening; wherein the liquid nozzle opening and the center air outlet are formed in a front wall (60; 160a, 160b) of the cap body.
An aircraft comprising a thrust producing unit with a plurality of rotating blades that rotate at a first frequency, wherein first and second rotating blades (108a, 108b) of the plurality of rotating blades are indistinguishable from each other by the human eye at the first frequency, comprising: a light source that is installed on a fixed surface of the aircraft and pulses light towards the plurality of rotating blades at a second frequency, wherein: the second frequency is selected dependent on the first frequency such that first reflections of the light off the first rotating blade are distinguishable by the human eye from second reflections of the light off the second rotating blade; characterized in that the light source is operable in at least two different modes comprising a safety mode and a visual inspection mode; and in the visual inspection mode, the second frequency is selected dependent on the first frequency such that the first and second reflections of the light off the first and second rotating blades (108a, 108b) render the first and second rotating blades (108a, 108b) distinguishable from each other by the human eye. a light source that is installed on a fixed surface of the aircraft and pulses light towards the plurality of rotating blades at a second frequency, wherein: the second frequency is selected dependent on the first frequency such that first reflections of the light off the first rotating blade are distinguishable by the human eye from second reflections of the light off the second rotating blade; characterized in that the light source is operable in at least two different modes comprising a safety mode and a visual inspection mode; and in the visual inspection mode, the second frequency is selected dependent on the first frequency such that the first and second reflections of the light off the first and second rotating blades (108a, 108b) render the first and second rotating blades (108a, 108b) distinguishable from each other by the human eye. the second frequency is selected dependent on the first frequency such that first reflections of the light off the first rotating blade are distinguishable by the human eye from second reflections of the light off the second rotating blade; characterized in that the light source is operable in at least two different modes comprising a safety mode and a visual inspection mode; and in the visual inspection mode, the second frequency is selected dependent on the first frequency such that the first and second reflections of the light off the first and second rotating blades (108a, 108b) render the first and second rotating blades (108a, 108b) distinguishable from each other by the human eye.