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公开(公告)号：US12134473B2
公开(公告)日：2024-11-05
申请号：US18199087
申请日：2023-05-18
Applicant: Airbus Operations GmbH
Inventor： Wilhelm Lutzer , Ulrich Rieger , Eberhard Gumbert , Carsten Ohlfest , Holger Brilsky , Gerke Popken
Abstract: A wastewater tank arrangement for an aircraft, including a wastewater tank and a drain pipe having a first end and an opposite second end, the drain pipe fastened with its first end to the wastewater tank and having a second end for connection to a service panel in the aircraft structure. Providing a wastewater tank arrangement can effectively compensate tolerances between the wastewater tank and the service panel, and can effectively compensate installation and manufacturing tolerances during the course of the initial installation, in that the wastewater tank arrangement has a tolerance compensation device configured to connect the second end of the drain pipe to the service panel and compensate tolerances between the second end of the drain pipe and the service panel.
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公开(公告)号：US11691734B2
公开(公告)日：2023-07-04
申请号：US17217140
申请日：2021-03-30
Applicant: Airbus Operations GmbH
Inventor： Wilhelm Lutzer , Ulrich Rieger , Eberhard Gumbert , Carsten Ohlfest , Holger Brilsky , Gerke Popken
CPC classification number: B64D11/02 , B64D11/04 , F16L27/1012 , F16L27/11
Abstract: A wastewater tank arrangement for an aircraft, including a wastewater tank and a drain pipe having a first end and an opposite second end, the drain pipe fastened with its first end to the wastewater tank and having a second end for connection to a service panel in the aircraft structure. Providing a wastewater tank arrangement can effectively compensate tolerances between the wastewater tank and the service panel, and can effectively compensate installation and manufacturing tolerances during the course of the initial installation, in that the wastewater tank arrangement has a tolerance compensation device configured to connect the second end of the drain pipe to the service panel and compensate tolerances between the second end of the drain pipe and the service panel.
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公开(公告)号：US20250010993A1
公开(公告)日：2025-01-09
申请号：US18762798
申请日：2024-07-03
Applicant: Airbus Operations GmbH
Inventor： Carsten Ohlfest , Frank Schneider , Matthias Hegenbart , Kenneth Boenning , Axel Zimmermann , Frederik Albers , Sonja Pawellek , Stefan Wenderoth , Brice Peyres
Abstract: An aircraft with a potable water system enabling the connection of monuments to preinstalled aircraft potable water interfaces by customized piping, which is routed within raceways for example directly along seat rails, and an installation method.
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公开(公告)号：US20250010994A1
公开(公告)日：2025-01-09
申请号：US18762976
申请日：2024-07-03
Applicant: Airbus Operations GmbH
Inventor： Carsten Ohlfest , Frank Schneider , Matthias Hegenbart , Kenneth Boenning , Axel Zimmermann , Frederik Albers , Sonja Pawellek , Stefan Wenderoth , Brice Peyres
Abstract: An aircraft with a potable water system to feed potable water from a potable water tank to a consumer equipment of a monument in the aircraft cabin, including potable water interfaces, and at least one monument, with at least one opening in the monument to establish a fluid connection to the consumer equipment, wherein at least one potable water interface is accessible through the at least one opening, and an assembly method for installing a potable water system wherein standard parts of the potable water system are preinstalled and customized parts are installed later on.
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