Abstract: A method and a system for comminuting and cleaning waste plastic are described. For this purpose, waste plastic is comminuted and pre-washed in a wet mill and then cleaned in a washing system. The resulting wastewater is subjected to mechanical filtration and flotation and then temporarily stored as circulating water. Based on this, some of the circulating water is returned to the wet mill as first process water and some of the circulating water is returned to the washing system as second process water. In this way, the first and second portions of the circulating water may be specifically adapted to the respective water requirements of the wet mill and the washing system as well as to the required water qualities, if necessary with selective post-cleaning of the second portion of the circulating water. As a result, the fresh water requirement for the process described may be minimized.

Abstract: An apparatus (1) for the production of plastics material liquid containers (10) with a conveying device (2) which conveys the plastics material containers (10) along a pre-set conveying path (P), with a shaping device (4) which shapes plastics material pre-forms into the plastics material containers (10), with a first filling device (12) which is arranged downstream of the shaping device (4) along the conveying path and which fills the plastics material containers (10) with a liquid, and with a cooling device (8) which is arranged between the shaping device (4) and the first filling device (12) and which cools at least one area of the wall of the plastics material containers (10) by acting upon it with a flowable medium. According to the invention the cooling device has a second filling device (8) which fills a liquid into the container, which liquid is used for cooling a base area (10a) of the plastics material container (10).

Abstract: An apparatus and a method for controlling an apparatus for furnishing articles is disclosed. A conveyor unit is used to convey the articles. At least one exchangeable furnishing unit is designed to exchange identification data and/or control information during connection to the apparatus with the apparatus and/or with the conveyor unit. At least one storage area is provided, wherein the storage area stores at least two furnishing units. An automatically controlled feeding and withdrawing unit is used to operatively connect the storage area with the apparatus.

Abstract: A filter aid for a pre-coat filter, the filter agent comprising regenerated cellulose fibers, and a method for filtering or stabilizing an unfiltered product, including: provision of a pre-coat filter; pre-coating of a filter means of the pre-coat filter with regenerated cellulose fibers acting as a filter aid, in order to form a filter layer and passing of the unfiltered product through the filter layer that has been formed. Also, a filter layer including regenerated cellulose fibers for a plate press, plate-and-frame filter or plate filter for filtering a beverage.

Abstract: A frame element (10; 10?) for use in an aircraft component assembly system (46) is attachable to an aircraft structure (36) and comprises at least one fastening device for fastening at least one aircraft interior component (34) or at least one insulation pack (52) to the frame element (10; 10?). An aircraft component assembly system (46) comprises a plurality of such frame elements (10; 10?). In a method of fitting a component (34, 52) in an aircraft, a frame element (10; 10?) is provided. At least one interior component (34) or at least one insulation pack (52) is fastened to the frame element (10; 10?). Then the frame element (10; 10?) having the at least one interior component (34) or the at least one insulation pack (52) fastened thereto is attached to an aircraft structure (36).

Abstract: An apparatus (1) for the production of plastics material liquid containers (10) with a conveying device (2) which conveys the plastics material containers (10) along a pre-set conveying path (P), with a shaping device (4) which shapes plastics material pre-forms into the plastics material containers (10), with a first filling device (12) which is arranged downstream of the shaping device (4) along the conveying path and which fills the plastics material containers (10) with a liquid, and with a cooling device (8) which is arranged between the shaping device (4) and the first filling device (12) and which cools at least one area of the wall of the plastics material containers (10) by acting upon it with a flowable medium. According to the invention the cooling device (8) has a second filling device (8) which fills a liquid into the container, which liquid is used for cooling a base area (10a) of the plastics material container (10).

Abstract: A method and a device for can manufacture and canning, having cans manufactured in a manufacturing process and filled in a filling process, the manufacturing process being integral with the filling process in one plant, and the cans being transported from the manufacturing process to the filling process in a hygienic conveyor.

Abstract: An apparatus and a method for controlling an apparatus for furnishing articles is disclosed. A conveyor unit is used to convey the articles. At least one exchangeable furnishing unit is designed to exchange identification data and/or control information during connection to the apparatus with the apparatus and/or with the conveyor unit. At least one storage area is provided, wherein the storage area stores at least two furnishing units. An automatically controlled feeding and withdrawing unit is used to operatively connect the storage area with the apparatus.

Abstract: A gap covering device for covering a gap between two mutually adjacent first aircraft interior panels includes a visible portion as well as a retaining portion connected to the visible portion and extending opposite the visible portion. A receiving structure is fastened to an inner surface of the visible portion and/or of the retaining portion and has a receiving contour adapted to an edge contour of the first aircraft interior panels.

Abstract: An apparatus and a method for controlling an apparatus for furnishing articles is disclosed. A conveyor unit is used to convey the articles. At least one exchangeable furnishing unit is designed to exchange identification data and/or control information during connection to the apparatus with the apparatus and/or with the conveyor unit. At least one storage area is provided, wherein the storage area stores at least two furnishing units. An automatically controlled feeding and withdrawing unit is used to operatively connect the storage area with the apparatus.

Abstract: An aircraft component assembly system for the assembly of an interior component, a pipe or an electric line in an aircraft includes at least one arc-shaped frame element, a connection element that extends between a first and a second end of the frame element, and a fastening apparatus for fastening the interior component, the pipe or the electric line to the frame element or the connection element. The system also includes a first guide device that is provided on the frame element or the connection element and is devised to interact with a second guide device, which is complementary to the first guide device and provided on an aircraft structure, in such a way that the aircraft component assembly system is connectable to the aircraft structure in a manner displaceable relative to the aircraft structure.

Abstract: A frame element for use in an aircraft air-conditioning system is attachable to an aircraft structure and includes at least one strut which is formed to at least in sections as a hollow cylinder, wherein an air inlet connection of the at least one-section-wise hollow cylindrically formed strut of the frame element is connectable to an air outlet duct of an aircraft air-conditioning unit, and an air outlet connection of the at least one section-wise hollow cylindrically formed strut of the frame element is connectable to an air outlet opening terminating in a cabin region of an aircraft.

Abstract: A frame element (10) for use in an aircraft component installation system (46) is attachable to an aircraft structure (36) and comprises a storage bin fastening device which is designed to fasten a storage bin (26) at various positions on the frame element (10). A storage bin (26) for use in an aircraft comprises a complementary device to the storage bin fastening device of the frame element (10), in order to fasten the storage bin (26) at various positions on the frame element (10). In a method for the installation of a storage bin (26) in an aircraft a frame element (10) is provided. A storage bin (26) is fastened in a desired position on the frame element (10). The frame element (10) is attached to an aircraft structure (36).

Abstract: A frame element (10; 10?) for use in an aircraft air-conditioning system is attachable to an aircraft structure (36) and includes at least one strut (12, 14, 16, 18; 12?, 14?, 16?) which is formed at least in sections as a hollow cylinder, wherein an air inlet connection (12a, 14a; 12a?, 14a?) of the at least one section-wise hollow cylindrically formed strut (12, 14, 16, 18; 12?, 14?, 16?) of the frame element (10; 100 is connectable to an air outlet duct of an aircraft air-conditioning unit, and an air outlet connection (12b, 14b; 12b?, 14b?) of the at least one section-wise hollow cylindrically formed strut (12, 14, 16, 18; 12?, 14?, 16?) of the frame element (10; 100 is connectable to an air outlet opening terminating in a cabin region of an aircraft.

Abstract: An aircraft component assembly system (10; 10?; 10?) for the assembly of an interior component, a pipe and/or an electric line in an aircraft comprises at least one arc-shaped frame element (12; 12?; 12?), a connection element (32) that extends between a first and a second end of the frame element (12; 12?; 12?), a fastening apparatus for fastening the interior component, the pipe and/or the electric line to the frame element (12; 12?; 12?) and/or the connection element (32), and a first guide device (46) that is provided on the frame element (12; 12?; 12?) and/or the connection element (32) and is devised to interact with a second guide device (52), which is complementary to the first guide device (46) and provided on an aircraft structure (40), in such a way that the aircraft component assembly system (10; 10; 10?) is connectable to the aircraft structure (40) in a manner displaceable relative to the aircraft structure (40).

Abstract: A gap covering device (10) for covering a gap (16) between two mutually adjacent first aircraft interior components (12, 14) comprises a visible portion (18) as well as a retaining portion (20) connected to the visible portion (18) and extending opposite the visible portion (18). A receiving structure is fastened to an inner surface of the visible portion (18) and/or of the retaining portion (20) and has a receiving contour adapted to an edge contour of the first aircraft interior components (12, 14).

Abstract: An apparatus and a method for controlling an apparatus for furnishing articles is disclosed. A conveyor unit is used to convey the articles. At least one exchangeable furnishing unit is designed to exchange identification data and/or control information during connection to the apparatus with the apparatus and/or with the conveyor unit. At least one storage area is provided, wherein the storage area stores at least two furnishing units. An automatically controlled feeding and withdrawing unit is used to operatively connect the storage area with the apparatus.

Abstract: A frame element (10; 10?) for use in an aircraft component assembly system (46) is attachable to an aircraft structure (36) and comprises at least one fastening device for fastening at least one aircraft interior component (34) or at least one insulation pack (52) to the frame element (10; 10?). An aircraft component assembly system (46) comprises a plurality of such frame elements (10; 10?). In a method of fitting a component (34, 52) in an aircraft, a frame element (10; 10?) is provided. At least one interior component (34) or at least one insulation pack (52) is fastened to the frame element (10; 10?). Then the frame element (10; 10?) having the at least one interior component (34) or the at least one insulation pack (52) fastened thereto is attached to an aircraft structure (36).

Abstract: A frame element (10) for use in an aircraft component installation system (46) is attachable to an aircraft structure (36) and comprises a storage bin fastening device which is designed to fasten a storage bin (26) at various positions on the frame element (10). A storage bin (26) for use in an aircraft comprises a complementary device to the storage bin fastening device of the frame element (10), in order to fasten the storage bin (26) at various positions on the frame element (10). In a method for the installation of a storage bin (26) in an aircraft a frame element (10) is provided. A storage bin (26) is fastened in a desired position on the frame element (10). The frame element (10) is attached to an aircraft structure (36).