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公开(公告)号：US20240158100A1
公开(公告)日：2024-05-16
申请号：US18493939
申请日：2023-10-25
发明人： Frank SCHNEIDER , Hannes MÜLLER , Michael REMPE , Tim LÜBBERT , Frederik ALBERS
摘要： The present disclosure relates to a method for servicing an aircraft by a ground service unit. The method comprises reading a wireless parameter signal from a transponder at the aircraft, decoding the wireless parameter signal to derive at least one aircraft parameter of a water supply system and/or a waste system of the aircraft, moving a servicing equipment interface to a service panel of the aircraft, connecting the servicing equipment interface to a coupling at the service panel, servicing the aircraft via the servicing equipment interface corresponding to the at least one aircraft parameter, and writing a service parameter into the transponder at the aircraft.
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公开(公告)号：US20240141630A1
公开(公告)日：2024-05-02
申请号：US18493884
申请日：2023-10-25
发明人： Frederik ALBERS , Frank SCHNEIDER , Hannes MÜLLER , Axel SCHREINER , Tim LÜBBERT , Michael REMPE
摘要： A water supply system for a plurality of water consumer units in an aircraft. The system includes a main tank configured to store a main supply of water, a main water pipe connected to an outlet of the main tank, and a plurality of water networks, each configured to conduct water from the main tank to at least one of the plurality of water consumer units. The plurality of water consumer units is partitioned in a first group of water consumer units and at least a second group of water consumer units. Each of the plurality of water networks includes a conveying device configured to convey water to each water consumer unit of one of the groups. The water supply system further includes a cross-feed valve configured to fluidically connect or separate the plurality of water networks downstream of the conveying devices in the plurality of water networks.
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公开(公告)号：US20240101243A1
公开(公告)日：2024-03-28
申请号：US18526601
申请日：2023-12-01
发明人： Frank SCHNEIDER , Frederik ALBERS , Sonja PAWELLEK
摘要： A line assembly for installation in an aircraft fuselage includes a first line section having a first diameter, a second line section having a second diameter, a set of first line brackets, and a set of second line brackets. The first line brackets include a first receiving space configured to hold the first line section and a first support portion for attaching the first line brackets to a fuselage structural part. The second line brackets include a second receiving space configured to hold the second line section and a second support portion for attaching the second line brackets to the first line section. The second line section includes a higher flexibility than the first line section. The second line section is attached to the first line section through a plurality of second line brackets arranged at a distance to and independent from the first line brackets.
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公开(公告)号：US20230139167A1
公开(公告)日：2023-05-04
申请号：US17973832
申请日：2022-10-26
发明人： Frank SCHNEIDER , Frederik ALBERS , Sonja PAWELLEK
摘要： A line assembly for installation in an aircraft fuselage includes a first line section having a first diameter, a second line section having a second diameter, a set of first line brackets, and a set of second line brackets. The first line brackets include a first receiving space configured to hold the first line section and a first support portion for attaching the first line brackets to a fuselage structural part. The second line brackets include a second receiving space configured to hold the second line section and a second support portion for attaching the second line brackets to the first line section. The second line section includes a higher flexibility than the first line section. The second line section is attached to the first line section through a plurality of second line brackets arranged at a distance to and independent from the first line brackets.
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公开(公告)号：US20220412606A1
公开(公告)日：2022-12-29
申请号：US17848997
申请日：2022-06-24
发明人： Michael REMPE , Frederik ALBERS , Frank SCHNEIDER , Axel SCHREINER , Tim LÜBBERT
摘要： A system for heating up water for a consumer unit in an aircraft, having a water reservoir and a control unit. The water reservoir has a heating device to heat water held in the water reservoir to a consumer temperature. The control unit controls the heating device so water in the water reservoir is automatically heated to or above a disinfection temperature at which germ formation in the water reservoir is eliminated or suppressed, and a temperature of the water in the water reservoir is maintained at or above the disinfection temperature for a disinfection period, the heating to the disinfection temperature being effected only during flight phases or portions of flight phases of the aircraft during which use of the consumer unit by a user is not to be expected. A corresponding method and an aircraft having such a system are disclosed.
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