mhurhangee/patent-ind-claim-en huggingface dataset:
Apparatus for internal cleaning of a pipeline , the apparatus comprising: - an interchangeable rotary cleaning head ; - a motor device coupled to the rotary cleaning head to selectively control the rotation thereof, the motor device comprising a casing , a gearmotor accommodated within the casing and a transmission shaft , defining an axis of rotation A, projecting from the casing ; - a movement device configured to move the apparatus within the pipeline , the movement device being connected to the motor device ; - a remote system for controlling the apparatus connected to the motor device and to the movement device by means apt to transfer electrical signals and power; the motor device being interposed between the rotary cleaning head and the movement device ; wherein the motor device comprises: - one or more metal heat-dissipator elements placed in contact with the housing of the gearmotor the casing of the motor device being filled with a diathermic and dielectric fluid; - a pressure compensator exposed both to the pressure of the diathermic and dielectric fluid and to the pressure of the fluid external to the casing ; the pressure compensator being configured to balance the pressure of the diathermic and dielectric fluid, the volume of which is influenced by the variations in temperature induced by the metal heat-dissipator elements relative to the external pressure. - an interchangeable rotary cleaning head ; - a motor device coupled to the rotary cleaning head to selectively control the rotation thereof, the motor device comprising a casing , a gearmotor accommodated within the casing and a transmission shaft , defining an axis of rotation A, projecting from the casing ; - a movement device configured to move the apparatus within the pipeline , the movement device being connected to the motor device ; - a remote system for controlling the apparatus connected to the motor device and to the movement device by means apt to transfer electrical signals and power; - one or more metal heat-dissipator elements placed in contact with the housing of the gearmotor the casing of the motor device being filled with a diathermic and dielectric fluid; - a pressure compensator exposed both to the pressure of the diathermic and dielectric fluid and to the pressure of the fluid external to the casing ;
Method for detecting a position of a mobile, in particular autonomous, robot vehicle along a boundary conductor surrounding a defined area , having at least the method steps of - transmitting a first runtime signal S1 in the form of a current signal supplied to the boundary conductor , with an electromagnetic alternating field being generated, - detecting an arrival of the first runtime signal S1 at the robot vehicle , in particular as a result of a detection of an electromagnetic field change, caused by the runtime signal S1, that stems from the generated electromagnetic alternating field , - transmitting a second runtime signal S2, - detecting an arrival of the second runtime signal S2 at the robot vehicle , characterized by the method steps of - determining a time delay between the arrival of the first runtime signal S1 and the arrival of the second runtime signal S2, - determining the position of the robot vehicle along the boundary conductor on the basis of the determined time delay. - transmitting a first runtime signal S1 in the form of a current signal supplied to the boundary conductor , with an electromagnetic alternating field being generated, - detecting an arrival of the first runtime signal S1 at the robot vehicle , in particular as a result of a detection of an electromagnetic field change, caused by the runtime signal S1, that stems from the generated electromagnetic alternating field , - transmitting a second runtime signal S2, - detecting an arrival of the second runtime signal S2 at the robot vehicle , characterized by the method steps of - determining a time delay between the arrival of the first runtime signal S1 and the arrival of the second runtime signal S2, - determining the position of the robot vehicle along the boundary conductor on the basis of the determined time delay.
A water-based ink composition for ink jet recording, which has a pH of 7.0 or more and 10.0 or less, comprising: a coloring material; a first resin; a surface tension adjusting agent; and water, wherein the first resin contains a first vinyl monomer having a phenol skeleton as a constituent unit; the surface tension adjusting agent is at least one selected from the group consisting of a nonionic surfactant having an HLB of 8 or less and a water-soluble organic solvent having a water-octanol partition coefficient (log P value) of 0.5 or more; the first resin further contains a second aromatic vinyl monomer other than the vinyl monomer having the phenol skeleton as a constituent unit; and the first resin further contains a third water-soluble vinyl monomer as a constituent unit. a coloring material; a first resin; a surface tension adjusting agent; and water, wherein the first resin contains a first vinyl monomer having a phenol skeleton as a constituent unit; the surface tension adjusting agent is at least one selected from the group consisting of a nonionic surfactant having an HLB of 8 or less and a water-soluble organic solvent having a water-octanol partition coefficient (log P value) of 0.5 or more; the first resin further contains a second aromatic vinyl monomer other than the vinyl monomer having the phenol skeleton as a constituent unit; and the first resin further contains a third water-soluble vinyl monomer as a constituent unit.
A modular element for a thermally insulated construction such as a freezer construction or a heated construction, said modular element being a thermally insulated structural element comprising - an inner cladding , - an outer cladding and - an insulating layer located between the inner cladding and the outer cladding , wherein the insulating layer of the modular element is placed adjacent to the inner cladding of the modular element prior to assembly of said modular element in a modular construction characterized in that the inner cladding of said modular element is made of metal and that the inner cladding of said modular element has a joining edge part along at least a substantial part of a periphery of the modular element, said joining edge part being formed to project away from a basis plane of the inner cladding, by means of which the inner cladding of the modular element is joinable to an inner cladding of said modular construction by welding and wherein the inner cladding of said modular element, when formed as a wall element , has a lower part that is offset in an inwards direction and where furthermore a rear component is placed at the rear side of the inner cladding, said rear component having a protective part for providing a distance (d1) between the insulating layer and the inner cladding at least at a lower edge of the inner cladding, to maintain the insulating layer intact. - an inner cladding , - an outer cladding and - an insulating layer located between the inner cladding and the outer cladding ,
A method for strengthening a thin walled pipe comprising the steps of: extruding a base portion of a cylindrical pipe wall and co-extruding continuous axially extending rib-like bulge members upon the base portion, the rib-like bulge members being circumferentially spaced apart, characterised by attaching drip emitters to an inner side of the pipe wall, wherein at least some of the bulge members are extruded generally along lateral sides of the drip emitters, possibly along inner and/or outer sides of the pipe wall. extruding a base portion of a cylindrical pipe wall and co-extruding continuous axially extending rib-like bulge members upon the base portion, the rib-like bulge members being circumferentially spaced apart, characterised by attaching drip emitters to an inner side of the pipe wall, wherein at least some of the bulge members are extruded generally along lateral sides of the drip emitters, possibly along inner and/or outer sides of the pipe wall.
Jet engine having a chamber , which is delimited in a radial direction (R) by a fixed housing with a fixed wall region , of a planetary gear box device , or a bearing chamber , in which a rotatable device (29; 70) which can be impinged on with hydraulic fluid is arranged, wherein hydraulic fluid and air introduced into the chamber through the housing can be discharged from the chamber , wherein the housing is, in a region (57A; 57A, 57B) through which air and hydraulic fluid can be discharged from the chamber , formed with a separating device (63; 63A) for separating oil from an air-oil mixture, in the region of which separating device air and hydraulic fluid can be separated from one another, wherein the separating device (63; 63A) is formed with a grille structure and/or a cellular structure, through which the air-oil mixture flows for the separation of oil from the air-oil mixture, and, on a side facing towards an interior space of the chamber , said separating device is fixedly connected to the wall region .
A battery module comprising: a cartridge assembly comprising a plurality of cartridges, each cartridge accommodating a battery cell ; a casing comprising an opening formed therein and accommodating the cartridge assembly through the opening and surrounding the cartridge assembly ; a cover coupled to the opening of the casing ; and a heat management member , wherein the cover comprises a pressurizing portion pressurizing the battery cell when the battery cell swells, wherein the heat management member contacts the pressurizing portion and radiates heat of the battery cell or transfers heat to the battery cell , characterized in that the battery module further comprises a cooling unit or a heating unit , wherein the heat management member comprises: a first member which contacts the pressurizing portion and is spaced apart from the cooling unit or the heating unit , and a second member which extends inclinedly from the first member and is disposed alongside the pressurizing portion to contact the cooling unit or the heating unit . a cartridge assembly comprising a plurality of cartridges, each cartridge accommodating a battery cell ; a casing comprising an opening formed therein and accommodating the cartridge assembly through the opening and surrounding the cartridge assembly ; a cover coupled to the opening of the casing ; and a heat management member , wherein the cover comprises a pressurizing portion pressurizing the battery cell when the battery cell swells, wherein the heat management member contacts the pressurizing portion and radiates heat of the battery cell or transfers heat to the battery cell , characterized in that the battery module further comprises a cooling unit or a heating unit , wherein the heat management member comprises: a first member which contacts the pressurizing portion and is spaced apart from the cooling unit or the heating unit , and a second member which extends inclinedly from the first member and is disposed alongside the pressurizing portion to contact the cooling unit or the heating unit . a first member which contacts the pressurizing portion and is spaced apart from the cooling unit or the heating unit , and a second member which extends inclinedly from the first member and is disposed alongside the pressurizing portion to contact the cooling unit or the heating unit .
An aircraft defining a longitudinal direction and comprising: a fuselage extending between a forward end and an aft end along the longitudinal direction of the aircraft ; and an aft engine mounted to the aft end of the fuselage and defining a centerline , the aft engine further comprising a nacelle extending around the fuselage at the aft end of the fuselage , characterized in that : the nacelle comprising a forward transition duct at a forward end of the nacelle , the forward transition duct defining a centerline , the centerline of the forward transition duct angled downward relative to the centerline of the aft engine; wherein the nacelle defines an inlet having a top half positioned above the centerline of the aft engine and a bottom half positioned below the centerline of the aft engine, wherein the top half of the inlet defines a top half inlet area, wherein the bottom half of the inlet defines a bottom half inlet area, and wherein the bottom half inlet area is greater than the top half inlet area. a fuselage extending between a forward end and an aft end along the longitudinal direction of the aircraft ; and an aft engine mounted to the aft end of the fuselage and defining a centerline , the aft engine further comprising a nacelle extending around the fuselage at the aft end of the fuselage , the nacelle comprising a forward transition duct at a forward end of the nacelle , the forward transition duct defining a centerline , the centerline of the forward transition duct angled downward relative to the centerline of the aft engine; wherein the nacelle defines an inlet having a top half positioned above the centerline of the aft engine and a bottom half positioned below the centerline of the aft engine, wherein the top half of the inlet defines a top half inlet area, wherein the bottom half of the inlet defines a bottom half inlet area, and wherein the bottom half inlet area is greater than the top half inlet area.
A communication method for a transceiver device, comprising: receiving (S430) a physical downlink control channel, PDCCH, indicating a slot format indicating a sequence of symbol types in compliance with which the transmission is to be performed on a plurality of symbols included in a slot on the frequency range, the symbol types including at least one of an uplink symbol type, a downlink symbol type, and a flexible symbol type; determining (S440), based on the received PDCCH, the frequency range and the slot format; and performing (S470) the transmission on the determined frequency range in compliance with the determined slot format, characterized in that the PDCCH indicates a frequency range which is included in a carrier and applicable for transmission to be performed between the transceiver device and a scheduling device, the PDCCH includes a first field indicating the frequency range and a second field indicating the slot format, the first field is a bitmap including a plurality of bits respectively corresponding to a plurality of ranges included in the carrier and including said frequency range, and the bitmap indicates whether or not a range from among the plurality of ranges is applicable for the transmission. receiving (S430) a physical downlink control channel, PDCCH, indicating a slot format indicating a sequence of symbol types in compliance with which the transmission is to be performed on a plurality of symbols included in a slot on the frequency range, the symbol types including at least one of an uplink symbol type, a downlink symbol type, and a flexible symbol type; determining (S440), based on the received PDCCH, the frequency range and the slot format; and performing (S470) the transmission on the determined frequency range in compliance with the determined slot format, characterized in that the PDCCH indicates a frequency range which is included in a carrier and applicable for transmission to be performed between the transceiver device and a scheduling device, the PDCCH includes a first field indicating the frequency range and a second field indicating the slot format, the first field is a bitmap including a plurality of bits respectively corresponding to a plurality of ranges included in the carrier and including said frequency range, and the bitmap indicates whether or not a range from among the plurality of ranges is applicable for the transmission.
A cosmetic cream for application to the skin, containing: - 30 % by weight to 50 % by weight of avocado oil, - 30 % by weight to 55 % by weight of water, - 5 % by weight to 25 % by weight of one or more emulsifying agents, - 0.1 % by weight to 1.5 % by weight of tocopherol, - 0.1 % by weight to 2.0 % by weight of at least one preservative, - 0.5 % by weight to 1.2 % by weight of folic acid (vitamin B 9 ), - 0.5 % by weight to 1.2 % by weight of carnitine, - one or more further active ingredients selected from the group comprising cyanocobalamin (vitamin B 12 ), ubiquinone (coenzyme Q 10 ), allantoin, astaxanthin, curcuma, nigella sativa (black cumin) and cannabidiol (CBD) in a total quantity of 0.5 % by weight to 3 % by weight, wherein for at least two active ingredients selected from the cited group, it contains each of these active ingredients in a quantity of at least 0.1 % by weight and in a quantity of at most 1.0 % by weight, preferably at most 0.5 % by weight. - 30 % by weight to 50 % by weight of avocado oil, - 30 % by weight to 55 % by weight of water, - 5 % by weight to 25 % by weight of one or more emulsifying agents, - 0.1 % by weight to 1.5 % by weight of tocopherol, - 0.1 % by weight to 2.0 % by weight of at least one preservative, - 0.5 % by weight to 1.2 % by weight of folic acid (vitamin B 9 ), - 0.5 % by weight to 1.2 % by weight of carnitine, - one or more further active ingredients selected from the group comprising cyanocobalamin (vitamin B 12 ), ubiquinone (coenzyme Q 10 ), allantoin, astaxanthin, curcuma, nigella sativa (black cumin) and cannabidiol (CBD) in a total quantity of 0.5 % by weight to 3 % by weight, wherein for at least two active ingredients selected from the cited group, it contains each of these active ingredients in a quantity of at least 0.1 % by weight and in a quantity of at most 1.0 % by weight, preferably at most 0.5 % by weight.
An air-ground communication control method for a hierarchical network, the hierarchical network comprises a ground network and at least one aerial network, and the method comprises: obtaining (S110), by a ground device, a beam coverage radius for a high-altitude device, wherein the beam coverage radius is calculated by the high-altitude device according to a current moving speed of the high-altitude device relative to the ground or a flight track radius of the high-altitude device, the flight track radius of the high-altitude device is calculated according to location information of the high-altitude device with reference to a central location, the ground device is located in the ground network, the high-altitude device is located in the aerial network, and a beam of the high-altitude device covers the ground device; determining (S120), by the ground device, a direction of a beam from the ground device to the high-altitude device according to location information of the ground device; determining (S130), by the ground device, a width of the beam from the ground device to the high-altitude device according to the beam coverage radius; and controlling (S140), by the ground device, the beam from the ground device to the high-altitude device according to the beam direction and the beam width. obtaining (S110), by a ground device, a beam coverage radius for a high-altitude device, wherein the beam coverage radius is calculated by the high-altitude device according to a current moving speed of the high-altitude device relative to the ground or a flight track radius of the high-altitude device, the flight track radius of the high-altitude device is calculated according to location information of the high-altitude device with reference to a central location, the ground device is located in the ground network, the high-altitude device is located in the aerial network, and a beam of the high-altitude device covers the ground device; determining (S120), by the ground device, a direction of a beam from the ground device to the high-altitude device according to location information of the ground device; determining (S130), by the ground device, a width of the beam from the ground device to the high-altitude device according to the beam coverage radius; and controlling (S140), by the ground device, the beam from the ground device to the high-altitude device according to the beam direction and the beam width.
A thermally conductive grease comprising: (A) from 2 vol% to 35 vol% of a combination of polyorganosiloxanes comprising a first polyorganosiloxane of formula (I) R 1 R 2 2 Si-(OSiR 2 2 ) a -R 3 -Si(OR 4 ) 3 where each R 1 is independently an alkyl group or an alkenyl group, each R 2 is independently an alkyl group, each R 3 is selected from an oxygen atom and a divalent hydrocarbon group, each R 4 is independently an alkyl group of 1 to 6 carbon atoms, and subscript a has an average value ranging from 5 to 200; a second polyorganosiloxane of formula (II) R 5 3 Si-(OSiR 5 R 6 ) b (OSiR 5 2 ) c -R 7 -SiR 5 3 where each R 5 is an alkyl group, each R 6 is an aryl group, each R 7 is selected from an oxygen atom and a divalent hydrocarbon group, subscript b has an average value of at least 1, and subscript c an average value of at least 1 and with the provisos that subscript b and subscript c have average values such that a sum of (b + c) is sufficient to provide the second polyorganosiloxane with a viscosity, determined in accordance with the method outlined in the description, ranging from 5 to 30,000 cSt, and the second polyorganosiloxane is compatible with the first polyorganosiloxane; and (B) from 65 vol% to 98 vol% of a thermally conductive filler. (A) from 2 vol% to 35 vol% of a combination of polyorganosiloxanes comprising a first polyorganosiloxane of formula (I) R 1 R 2 2 Si-(OSiR 2 2 ) a -R 3 -Si(OR 4 ) 3 where each R 1 is independently an alkyl group or an alkenyl group, each R 2 is independently an alkyl group, each R 3 is selected from an oxygen atom and a divalent hydrocarbon group, each R 4 is independently an alkyl group of 1 to 6 carbon atoms, and subscript a has an average value ranging from 5 to 200; a second polyorganosiloxane of formula (II) R 5 3 Si-(OSiR 5 R 6 ) b (OSiR 5 2 ) c -R 7 -SiR 5 3 where each R 5 is an alkyl group, each R 6 is an aryl group, each R 7 is selected from an oxygen atom and a divalent hydrocarbon group, subscript b has an average value of at least 1, and subscript c an average value of at least 1 and with the provisos that subscript b and subscript c have average values such that a sum of (b + c) is sufficient to provide the second polyorganosiloxane with a viscosity, determined in accordance with the method outlined in the description, ranging from 5 to 30,000 cSt, and the second polyorganosiloxane is compatible with the first polyorganosiloxane; and (B) from 65 vol% to 98 vol% of a thermally conductive filler.