[특허]Device for receiving liquids in aircraft and/or releasing liquids therefrom

von Mohos, Zoltan

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Device for receiving liquids in aircraft and/or releasing liquids therefrom

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64D-001/16 B64D-001/22
미국특허분류(USC)	137/899.2; 137/266; 137/576; 169/053; 244/136
출원번호	US-0308869 (2011-12-01)
등록번호	US-8978703 (2015-03-17)
우선권정보	DE-10 2004 041 774 (2004-08-28)
발명자 / 주소	von Mohos, Zoltan
출원인 / 주소	von Mohos, Zoltan
대리인 / 주소	Gifford, Krass, Sprinkle, Anderson & Citkowski, P.C.
인용정보	피인용 횟수 : 0 인용 특허 : 8

초록
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The invention relates to a device for receiving liquids in an aircraft and/or releasing liquids therefrom, especially during the flight, said device being arranged especially in an airplane. The aim of the invention is to provide a device which can receive large quantities of liquids in a rapid, reliable and flexible manner. To this end, the device can include a tank module with at least one tank container that is connected to a collector using a connecting shaft and a bulkhead module that can be connected to the tank module by the collecting tank. A closing element in the open position releases liquid from the tank module. In addition, a refueling module which is connected to the tank module by a supply line and a tube arranged on a winding device, and a receiving element attached to the tube, can provide refueling of the device.

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1. A modular aircraft liquid transferring system for receiving liquids in an aircraft and/or releasing liquids therefrom, said modular aircraft liquid transferring system comprising: at least two tank modules releasably attached to each other to form an array of tank modules, each tank module having at least one storage tank container, at least one collecting tank connectable to and in fluid communication with said at least one tank container via at least one connecting shaft, wherein said at least one collecting tank of each tank module has a first end, a second end and a rectangular cross-sectional shape that is generally as wide as said at least one storage tank container and extends between said first end and said second end, said first end adapted to engage with said second end of said at least one collecting tank of another tank module, and said first end and said second end of said at least one collecting tank of another tank module are releasably attached to each other, said collecting tank is arranged under said tank containers and said tank containers of said at least two tank modules are interconnected via said at least one collecting tank of each tank module;a bulkhead module connectable to one of said at least two tank modules via said collecting tank of said tank module connectable to said bulkhead module, said bulkhead module having a closing element by means of which, in the open position, liquids are released from said tank module; anda filling module connectable to said at least two tank modules via at least one feeding line, and a hose pipe which is arranged on a coiling device having a receiving element defining at least one aperture for receiving and releasing liquids from the aircraft. 2. The modular aircraft liquid transferring system according to claim 1, wherein said receiving element is at least double-walled. 3. The modular aircraft liquid transferring system according to claim 2, wherein said aperture is defined in an exterior wall of said receiving element and is an incision, said incision is raised for said aperture to face in the direction of flight of the aircraft. 4. The modular aircraft liquid transferring system according to claim 3, further comprising a pumping device by means of which the liquid received in a region between said exterior wall and an at least one further interior wall of said receiving element is pumped into said tank module via a central internal line of said receiving element and said hose pipe, said central internal line forming said interior wall of said receiving element. 5. The modular aircraft liquid transferring system according to claim 4, wherein said receiving element comprises a spacer means provided between said central internal line and said exterior wall, provided with said apertures. 6. The modular aircraft liquid transferring system according to claim 1, wherein said receiving element comprises at least one fin for stabilizing purposes. 7. The modular aircraft liquid transferring system according to claim 1, wherein said receiving element comprises weights for weighting the latter. 8. The modular aircraft liquid transferring system according to claim 1, further comprising a mobile discharge device attachable to the side of said bulkhead module facing said filling module. 9. The modular aircraft liquid transferring system according to claim 8, wherein said discharge device serves as a support and for the alignment of said hose pipe, and said receiving element respectively. 10. The modular aircraft liquid transferring system according to claim 1, wherein said tank module, bulkhead module and filling module are designed as a tubular frame structure. 11. The modular aircraft liquid transferring system according to claim 1, wherein said tank module includes at least one vent. 12. The modular aircraft liquid transferring system according to claim 1, further comprising at least one additional tank module including at least one tank container, and at least one collecting tank connectable to said tank container via at least one connecting shaft, wherein said additional tank module being connectable to said tank module downstream of said bulkhead module thereby creating an adjustable array of tank modules.

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Device for receiving liquids in aircraft and/or releasing liquids therefrom

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Device for receiving liquids in aircraft and/or releasing liquids therefrom

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IPC 상세정보(version : 201201)

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