mhurhangee/ep-ind-claims huggingface dataset:
An optical element having a reflective coating, the reflective coating comprising at least - an adhesive layer, - an at least partially reflective metal layer subsequent to the adhesive layer, and - a protective layer system comprising a plurality of dielectric layers (31, 32) subsequent to the metal layer, wherein - the dielectric layers (31, 32) comprise at least one first layer and at least one second layer, and wherein the first layer and the second layer have a different resistance to at least two different contaminating substances, - the dielectric layers (31, 32) of the protective layer system hane a thickness of no greater than 30 nm, - the number of dielectric layers (31, 32) is at least five, characterized in that - the metal layer substantially comprises silver. - an adhesive layer, - an at least partially reflective metal layer subsequent to the adhesive layer, and - a protective layer system comprising a plurality of dielectric layers (31, 32) subsequent to the metal layer, - the dielectric layers (31, 32) comprise at least one first layer and at least one second layer, and wherein the first layer and the second layer have a different resistance to at least two different contaminating substances, - the dielectric layers (31, 32) of the protective layer system hane a thickness of no greater than 30 nm, - the number of dielectric layers (31, 32) is at least five, - the metal layer substantially comprises silver.
A diagnostic reagent for use in the detection of M. bovis or M. tuberculosis infection in a mammal, comprising a peptide of up to 100 amino acids in length which has a T-cell epitope from the protein having the amino acid sequence SEQ ID NO: 1, the epitope consisting of consecutive amino acids from within SEQ ID NO: 1, wherein the peptide consists of consecutive amino acids from within SEQ ID NO:1, further wherein the diagnostic reagent is a cell-mediated immunity assay diagnostic reagent.
A compound of Formula: or a pharmaceutically acceptable salt thereof, wherein: R 2 is selected from optionally substituted heteroaryl having 5 to 15 ring atoms and optionally substituted aryl having 6 to 12 ring atoms, wherein the optional substituents on R 2 groups are 1, 2 or 3 substituents independently selected from halogen, C 1 -C 4 alkyl, halo-C 1 -C 4 alkyl, C 1 -C 4 alkoxy, C 1 -C 4 thioalkoxy, hydroxyl, amino, C 1 -C 4 alkylamino, C 1 -C 4 dialkylamino, sulfhydryl, cyano, C 6 aryl and heteroaryl having 5 or 6 ring atoms; for use in treating a cancer selected from multiple myeloma, myelodysplastic syndrome, leukemia, lymphoma and a solid tumor. R 2 is selected from optionally substituted heteroaryl having 5 to 15 ring atoms and optionally substituted aryl having 6 to 12 ring atoms, wherein the optional substituents on R 2 groups are 1, 2 or 3 substituents independently selected from halogen, C 1 -C 4 alkyl, halo-C 1 -C 4 alkyl, C 1 -C 4 alkoxy, C 1 -C 4 thioalkoxy, hydroxyl, amino, C 1 -C 4 alkylamino, C 1 -C 4 dialkylamino, sulfhydryl, cyano, C 6 aryl and heteroaryl having 5 or 6 ring atoms; for use in treating a cancer selected from multiple myeloma, myelodysplastic syndrome, leukemia, lymphoma and a solid tumor.
A nozzle assembly for a gas turbine engine, comprising: a fuel distributor for issuing a spray of fuel; a fuel conduit in fluid communication with the fuel distributor having a first end and a second end, wherein at least one of the first end or second end is operatively connected to the fuel distributor; and an outer nozzle shell and an inner nozzle shell positioned radially inward of the outer nozzle shell, wherein the fuel conduit is positioned between the inner nozzle shell and the outer nozzle shell, wherein the fuel conduit is configured to allow relative movement between the first end and the second end to accommodate dimensional variations of at least one of the nozzle assembly or a combustor, characterized in that the inner nozzle shell includes a fuel feed opening to allow the fuel conduit to operatively connect to a fuel manifold, wherein a segment of the fuel conduit is allowed to slide relative to the fuel feed opening, wherein the fuel conduit wraps around a periphery of inner nozzle shell at least once, to form a coil shape, wherein the coiled fuel conduit is biased in compression between the fuel distributor and fuel manifold. a fuel distributor for issuing a spray of fuel; a fuel conduit in fluid communication with the fuel distributor having a first end and a second end, wherein at least one of the first end or second end is operatively connected to the fuel distributor; and an outer nozzle shell and an inner nozzle shell positioned radially inward of the outer nozzle shell, wherein the fuel conduit is positioned between the inner nozzle shell and the outer nozzle shell, wherein the fuel conduit is configured to allow relative movement between the first end and the second end to accommodate dimensional variations of at least one of the nozzle assembly or a combustor, characterized in that the inner nozzle shell includes a fuel feed opening to allow the fuel conduit to operatively connect to a fuel manifold, wherein a segment of the fuel conduit is allowed to slide relative to the fuel feed opening, wherein the fuel conduit wraps around a periphery of inner nozzle shell at least once, to form a coil shape, wherein the coiled fuel conduit is biased in compression between the fuel distributor and fuel manifold.
An electronic vapour provision system including: a pressure drop or air flow sensor for monitoring inhalation by a user through the electronic vapour provision system; and a control unit for detecting the start and end of inhalation based on readings from the sensor; and characterised in that the control unit is configured to: detect the start of inhalation when the sensor reading departs by more than a first threshold from a previous reading; and detect the end of inhalation when the sensor reading departs by less than a second threshold from the previous reading; wherein the first threshold is greater than the second threshold. a pressure drop or air flow sensor for monitoring inhalation by a user through the electronic vapour provision system; and a control unit for detecting the start and end of inhalation based on readings from the sensor; and characterised in that the control unit is configured to: detect the start of inhalation when the sensor reading departs by more than a first threshold from a previous reading; and detect the end of inhalation when the sensor reading departs by less than a second threshold from the previous reading; wherein the first threshold is greater than the second threshold. detect the start of inhalation when the sensor reading departs by more than a first threshold from a previous reading; and detect the end of inhalation when the sensor reading departs by less than a second threshold from the previous reading; wherein the first threshold is greater than the second threshold.
A self-replicating RNA molecule comprising a polynucleotide which comprises: a. a first nucleotide sequence encoding a first protein or fragment thereof from a herpes virus; b. a second nucleotide sequence encoding a second protein or fragment thereof from said herpes virus; c. a third nucleotide sequence encoding a third protein or fragment thereof from said herpes virus; d. a fourth nucleotide sequence encoding a fourth protein or fragment thereof from said herpes virus; and e. a fifth nucleotide sequence encoding a fifth protein or fragment thereof from said herpes virus; which first protein or fragment thereof, second protein or fragment thereof, third protein or fragment thereof, fourth protein or fragment thereof and fifth protein or fragment thereof are herpes virus proteins that form pentameric complexes with one another; and wherein the first nucleotide sequence, second nucleotide sequence, third nucleotide sequence, fourth nucleotide sequence and fifth nucleotide sequence are operably linked to one or more control elements so that when the self-replicating RNA molecule is introduced into a suitable cell, the first, second, third, fourth and fifth herpes virus proteins or fragments thereof are produced in an amount sufficient for the formation in the cell of a complex that contains the first, second, third, fourth and fifth proteins or fragments. a. a first nucleotide sequence encoding a first protein or fragment thereof from a herpes virus; b. a second nucleotide sequence encoding a second protein or fragment thereof from said herpes virus; c. a third nucleotide sequence encoding a third protein or fragment thereof from said herpes virus; d. a fourth nucleotide sequence encoding a fourth protein or fragment thereof from said herpes virus; and e. a fifth nucleotide sequence encoding a fifth protein or fragment thereof from said herpes virus;
A method for determining a crash condition of a vehicle comprising the steps of: sensing crash acceleration in a first direction substantially parallel to a front-to-rear axis of the vehicle and providing a first acceleration signal (CCU_1X) indicative thereof; sensing crash acceleration in a second direction substantially parallel to a side-to-side axis of the vehicle; sensing said crash acceleration in a second direction near opposite sides of the vehicle and providing second and third acceleration signals (RAS_1BY; RAS_2BY) indicative thereof; characterized by: determining a transverse crash value functionally related to a sum of values derived from the second and third acceleration signals (RAS_1BY; RAS_2BY); comparing the determined transverse crash value against a safing threshold; and determining a crash condition of the vehicle in response to (a) the comparison and (b) the first acceleration signal (CCU_1X). sensing crash acceleration in a first direction substantially parallel to a front-to-rear axis of the vehicle and providing a first acceleration signal (CCU_1X) indicative thereof; sensing crash acceleration in a second direction substantially parallel to a side-to-side axis of the vehicle; sensing said crash acceleration in a second direction near opposite sides of the vehicle and providing second and third acceleration signals (RAS_1BY; RAS_2BY) indicative thereof; characterized by: determining a transverse crash value functionally related to a sum of values derived from the second and third acceleration signals (RAS_1BY; RAS_2BY); comparing the determined transverse crash value against a safing threshold; and determining a crash condition of the vehicle in response to (a) the comparison and (b) the first acceleration signal (CCU_1X). determining a transverse crash value functionally related to a sum of values derived from the second and third acceleration signals (RAS_1BY; RAS_2BY); comparing the determined transverse crash value against a safing threshold; and determining a crash condition of the vehicle in response to (a) the comparison and (b) the first acceleration signal (CCU_1X). (a) the comparison and (b) the first acceleration signal (CCU_1X).
A system, comprising: an underwater assembly, comprising: a flow control device: and an actuator coupled to the flow control device, wherein the actuator is configured to actuate the flow control device; an insulated housing surrounding the flow control device and the actuator, wherein the insulated housing is configured to retain heat; and a thermal control system comprising a heat exchanger configured to control a temperature of the actuator, characterised in that the heat exchanger is coupled to the actuator. an underwater assembly, comprising: a flow control device: and an actuator coupled to the flow control device, wherein the actuator is configured to actuate the flow control device; a flow control device: and an actuator coupled to the flow control device, wherein the actuator is configured to actuate the flow control device; an insulated housing surrounding the flow control device and the actuator, wherein the insulated housing is configured to retain heat; and a thermal control system comprising a heat exchanger configured to control a temperature of the actuator, characterised in that the heat exchanger is coupled to the actuator.
Method of processing heated material, wherein the material is guided along a conveyor path and in the region of the conveyor path covered by at least one reflector element and protected against heat loss, wherein the reflector element is cooled by means of a liquid, characterised in that the reflector element comprises a reflection material with a reflectance of more than 70% and the liquid is or comprises glycol or the liquid is or comprises alcohol or the liquid is thermo-oil.
An agricultural vehicle, comprising: - a chassis; and - a header carried by said chassis, said header including: - a header frame; - a cutter (110, 910) movably coupled to said header frame; - a reel arm (123, 525, 535) pivotably coupled to said header frame; - a reel carried by said reel arm (123, 525, 535) and including a plurality of tines; and - a variable displacement fluid cylinder (200, 600) including an interior chamber (210, 610), a first piston (220, 620) linked to said reel arm (123, 525, 535) placed within said interior chamber (210, 610) characterized by a second piston (230, 630) placed within said interior chamber (210, 610), said interior chamber (210, 610) defining a shared volume (211, 611) between said first piston (220, 620) and said second piston (230, 630); and - a piston driver (300, 640) linked to said cutter (110, 910), said piston driver (300, 640) being configured to translate movement of said cutter (110, 910) relative to said header frame into displacement of said second piston (230, 630) within said interior chamber (210, 610). - a chassis; and - a header carried by said chassis, said header including: - a header frame; - a cutter (110, 910) movably coupled to said header frame; - a reel arm (123, 525, 535) pivotably coupled to said header frame; - a reel carried by said reel arm (123, 525, 535) and including a plurality of tines; and - a variable displacement fluid cylinder (200, 600) including an interior chamber (210, 610), a first piston (220, 620) linked to said reel arm (123, 525, 535) placed within said interior chamber (210, 610) characterized by a second piston (230, 630) placed within said interior chamber (210, 610), said interior chamber (210, 610) defining a shared volume (211, 611) between said first piston (220, 620) and said second piston (230, 630); and - a piston driver (300, 640) linked to said cutter (110, 910), said piston driver (300, 640) being configured to translate movement of said cutter (110, 910) relative to said header frame into displacement of said second piston (230, 630) within said interior chamber (210, 610). - a header frame; - a cutter (110, 910) movably coupled to said header frame; - a reel arm (123, 525, 535) pivotably coupled to said header frame; - a reel carried by said reel arm (123, 525, 535) and including a plurality of tines; and - a variable displacement fluid cylinder (200, 600) including an interior chamber (210, 610), a first piston (220, 620) linked to said reel arm (123, 525, 535) placed within said interior chamber (210, 610) characterized by a second piston (230, 630) placed within said interior chamber (210, 610), said interior chamber (210, 610) defining a shared volume (211, 611) between said first piston (220, 620) and said second piston (230, 630); and - a piston driver (300, 640) linked to said cutter (110, 910), said piston driver (300, 640) being configured to translate movement of said cutter (110, 910) relative to said header frame into displacement of said second piston (230, 630) within said interior chamber (210, 610).
A preparation method of a coffee additive comprising preparing a black garlic extract caramel using a black garlic extract and adding milk and then stirring and heating the mixture at 85°C to 90°C for 5 to 10 minutes.
A wholly aromatic polyester, which exhibits optical anisotropy when it is molten, which has a crystallization heat quantity of 2.3 J/g or less, and which has a melting point of 300 to 390°C both parameters measured as outlined in the description, the polymer comprising, as essential constituents, the constitutional units represented by the following formulae,,, and, containing, relative to a total of all constitutional units, the constitutional unit in an amount of 35 to 75 mol%, the constitutional unit in an amount of 2 to 8 mol%, the constitutional unit in an amount of 4.5 to 30.5 mol%, the constitutional unit in an amount of 3 to 7 mol%, the constitutional unit in an amount of 12.5 to 32.5 mol%, the total of constitutional units and being in an amount of 4 to 10 mol%; -O-Ar 4 -O- wherein Ar 1 is Ar 2 is Ar 3 is and Ar 4 is
Lock reinforcement for a motor vehicle opening, intended to be inserted between a lock and a lining of the opening, this reinforcement comprising a front plate for mounting the lock, intended to be applied internally against an edge of the lining, and a square side return intended to be applied against a side face of the lining, this reinforcement comprising at least one bracing stiffener inserted obliquely between the plate and the square return, characterised in that the stiffener is ribbed, said rib forming a Y-shape.
An assembly for an aircraft propulsion system, comprising: a variable area inlet comprising a fixed structure and a moveable structure, the variable area inlet configured to open and close an airflow inlet passage into the aircraft propulsion system; the moveable structure configured to move axially along a centerline (30, 78) between an aft position and a forward position, and the moveable structure comprising an inlet lip structure and a deflector; wherein, when the moveable structure is in the aft position, the airflow inlet passage is closed, and the deflector is at least partially recessed into the fixed structure; and wherein, when the moveable structure is in the forward position, the airflow inlet passage is opened axially between an aft end of the inlet lip structure and a forward end of the fixed structure, and a forward end of the deflector is disposed axially at the forward end of the fixed structure, characterised in that: a blind cavity projects axially partially into the variable area inlet when the moveable structure is in the forward position; and the blind cavity extends radially between the deflector and the fixed structure when the moveable structure is in the forward position. a variable area inlet comprising a fixed structure and a moveable structure, the variable area inlet configured to open and close an airflow inlet passage into the aircraft propulsion system; the moveable structure configured to move axially along a centerline (30, 78) between an aft position and a forward position, and the moveable structure comprising an inlet lip structure and a deflector; wherein, when the moveable structure is in the aft position, the airflow inlet passage is closed, and the deflector is at least partially recessed into the fixed structure; and wherein, when the moveable structure is in the forward position, the airflow inlet passage is opened axially between an aft end of the inlet lip structure and a forward end of the fixed structure, and a forward end of the deflector is disposed axially at the forward end of the fixed structure, characterised in that: a blind cavity projects axially partially into the variable area inlet when the moveable structure is in the forward position; and the blind cavity extends radially between the deflector and the fixed structure when the moveable structure is in the forward position. a blind cavity projects axially partially into the variable area inlet when the moveable structure is in the forward position; and the blind cavity extends radially between the deflector and the fixed structure when the moveable structure is in the forward position.
A vacuum cleaner comprising; - a housing comprising a motor fan unit for generating an airflow, a housing air outlet and a housing air inlet, and - a profile arrangement comprising a first profile end for attachment of a nozzle, a profile handle end for attachment of a handle and a profile extending between the first profile end and the profile handle end, and - an airflow channel extending from the first profile end to the housing air outlet via the housing air inlet, for allowing an airflow from the first profile end to the housing air outlet, characterized in that the profile arrangement comprises a first profile part and a second profile part, the second profile part is arranged to at least partly enclose the first profile part and the first profile part is slidable into the second profile part for adjustment of a length of the profile and that the housing is arranged to be moveably attached to the profile, such that the housing is moveable along at least a part of the length of the profile. - a housing comprising a motor fan unit for generating an airflow, a housing air outlet and a housing air inlet, and - a profile arrangement comprising a first profile end for attachment of a nozzle, a profile handle end for attachment of a handle and a profile extending between the first profile end and the profile handle end, and - an airflow channel extending from the first profile end to the housing air outlet via the housing air inlet, for allowing an airflow from the first profile end to the housing air outlet,
A lubricating oil composition comprising: an ether compound represented by the following general formula as the lube base oil: R 1 -O-R 2 wherein R 1 and R 2 each independently represents an alkyl group having 2 to 26 carbon atoms, and said lube base oil having a kinematic viscosity at 100°C of 3.5 mm 2 /s or lower, a mass loss due to evaporation as measured according to Noack test (250°C, 1 hour) of 30% by mass or lower a flash point measured according to JIS K2265 of 200°C or higher, and an aniline point of 60°C or higher and an organomolybdenum compound formulated therein in an amount of 100 to 2,000 ppm by mass in terms of molybdenum based on a total mass of the composition. an ether compound represented by the following general formula as the lube base oil: R 1 -O-R 2 wherein R 1 and R 2 each independently represents an alkyl group having 2 to 26 carbon atoms, and said lube base oil having a kinematic viscosity at 100°C of 3.5 mm 2 /s or lower, a mass loss due to evaporation as measured according to Noack test (250°C, 1 hour) of 30% by mass or lower a flash point measured according to JIS K2265 of 200°C or higher, and an aniline point of 60°C or higher and an organomolybdenum compound formulated therein in an amount of 100 to 2,000 ppm by mass in terms of molybdenum based on a total mass of the composition.