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公开(公告)号：US10577107B2
公开(公告)日：2020-03-03
申请号：US15816521
申请日：2017-11-17
Applicant: Airbus Operations GmbH
Inventor： Marc Spille , Matthias Reiss , Wilhelm Lutzer , Oliver Kiehne , Michael Kempa , Norbert Kaufeld
Abstract: A system for suctioning fluid is disclosed. In a cabin monument, a vacuum source and a vacuum interface unit is provided. At least one flexible hose provides a connection to the vacuum interface unit, having at least one first fluid line having a connection element. The end connection element connects to a unit to be evacuated. The vacuum interface unit includes an adapter for connection to the at least one fluid line, and a trigger unit. At least one valve unit and a control unit for controlling the at least one valve unit reside in the cabin monument. The control unit controls the valve unit at least indirectly based on a trigger signal generated by the trigger unit. Thus, a flexible positioning of a unit to be evacuated for waste compaction is possible. The disclosure also relates to a vehicle, in particular an aircraft, having such a suctioning system.
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公开(公告)号：US10343781B2
公开(公告)日：2019-07-09
申请号：US14243073
申请日：2014-04-02
Applicant: Airbus Operations GmbH
Inventor： Torsten Truemper , Matthias Reiss
Abstract: An aircraft cooling system including a cooler which is adapted to supply cooling energy to an aircraft device to be cooled, and a heat transfer arrangement which is adapted to transfer waste heat generated by the cooler to a cabin air extraction system. The heat transfer arrangement comprises a heat transfer circuit, in which a liquid heat transfer medium heated by the waste heat of the cooler circulates.
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公开(公告)号：US11794903B2
公开(公告)日：2023-10-24
申请号：US17482586
申请日：2021-09-23
Applicant: Airbus Operations GmbH
Inventor： Rafael Mortensen Ernits , Oliver Kiehne , Matthias Reiss , Oliver Delaplanche , Markus Tiemann , Dennis Keiser
IPC: B64D11/04 , B64D11/00 , F24H9/20 , F24H15/223 , F24H1/00
CPC classification number: B64D11/04 , B64D11/0007 , F24H9/2021 , F24H15/223 , F24H1/009
Abstract: A system for providing temperature-controlled water in an aircraft has a tank, a water temperature-controlling unit, a control unit, and a power supply terminal. The water temperature-controlling unit can be coupled to the tank to heat or to cool water situated therein. The control unit is connected to the water temperature-controlling unit to activate the water temperature-controlling unit for controlling the temperature of water in the tank to a predefined temperature. The power supply terminal can be connected to an on-board voltage source for the water temperature-controlling unit and the control unit to be supplied with electrical voltage. The system is in the form of a coherent and self-contained unit which can be integrated into a standard parking place of a galley of the aircraft. The tank is mounted so as to be exchangeable or the system has a water discharge connection which is coupled to the tank.
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公开(公告)号：US20220219822A1
公开(公告)日：2022-07-14
申请号：US17612462
申请日：2020-05-20
Applicant: Airbus Operations GmbH
Inventor： Matthias Reiss , Michael Bauer , Rafael Mortensen Ernits , Michael Freitag
Abstract: A system for automatically adapting operating parameters of a galley device on the basis of provided supply items for on-board catering for a vehicle, in particular an aircraft, includes a galley device that has an identification device that is designed to identify a supply item; and a control device for controlling the galley device, wherein the control device is designed to provide operating parameters for the identified supply item and to operate the galley device in accordance with the operating parameters.
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公开(公告)号：US10899376B2
公开(公告)日：2021-01-26
申请号：US16136903
申请日：2018-09-20
Applicant: Airbus Operations GmbH
Inventor： Michael Bauer , Norbert Kaufeld , Matthias Reiss , Oliver Kiehne , Simon Stock , Rafael Mortensen Ernits
Abstract: An electrically driven trolley combination for an aircraft cabin with an independently usable, manually movable trolley and an electrical operating apparatus. The trolley has a base section, a main section extending from the base section, and wheels with the trolley supported on a cabin floor by the wheels and manually movable over the cabin floor being pushed or pulled. The electrical operating apparatus can be detachably coupled to the trolley and has a frame, a driveable rolling device on the frame and by which the electrical operating apparatus can be supported on a cabin floor and rolled, a coupling apparatus on the frame for detachably coupling the electrical operating apparatus to the trolley and having an engagement section and a movement section, the engagement section being selectively movable between a first position and a second position by the movement section, an electrical drive device, and a control device.
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Patent Agency Ranking
公开(公告)号：US20190084604A1
公开(公告)日：2019-03-21
申请号：US16136903
申请日：2018-09-20
Applicant: Airbus Operations GmbH
Inventor： Michael Bauer , Norbert Kaufeld , Matthias Reiss , Oliver Kiehne
Abstract: An electrically driven trolley combination for an aircraft cabin with an independently usable, manually movable trolley and an electrical operating apparatus. The trolley has a base section, a main section extending from the base section, and wheels with the trolley supported on a cabin floor by the wheels and manually movable over the cabin floor being pushed or pulled. The electrical operating apparatus can be detachably coupled to the trolley and has a frame, a driveable rolling device on the frame and by which the electrical operating apparatus can be supported on a cabin floor and rolled, a coupling apparatus on the frame for detachably coupling the electrical operating apparatus to the trolley and having an engagement section and a movement section, the engagement section being selectively movable between a first position and a second position by the movement section, an electrical drive device, and a control device.
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7.发明申请公开(公告)号：US20140298824A1
公开(公告)日：2014-10-09
申请号：US14243067
申请日：2014-04-02
Applicant: Airbus Operations GmbH
Inventor： Torsten Truemper , Matthias Reiss
CPC classification number: B64D13/08 , B64D13/06 , B64D2013/0629 , F25B21/04 , Y02B30/52 , Y02T50/56
Abstract: An aircraft cooling system including a cooler having a cold transfer circuit, in which a cold transfer medium circulates. The cooler supplies cooling energy to an aircraft device to be cooled. The aircraft cooling system further includes a heat transfer arrangement having a heat transfer circuit, in which a heat transfer medium circulates and which is thermally coupled to the cold transfer circuit of the cooler via a heat exchanger, in order to absorb waste heat generated by the cooler and transfer it to a cabin air extraction system. The heat transfer arrangement further includes at least one heat pump which brings about an increase of the heat energy transfer from the cold transfer medium circulating in the cold transfer circuit of the cooler to the heat transfer medium circulating in the heat transfer circuit, at least in certain operating phases of the aircraft cooling system.
Abstract translation: 一种飞机冷却系统，包括具有冷传递电路的冷却器，其中冷转印介质循环。 冷却器为要冷却的飞行器装置提供冷却能量。 飞机冷却系统还包括具有传热回路的传热装置，其中传热介质循环并且经由热交换器热耦合到冷却器的冷传递回路，以便吸收由热交换器产生的废热 冷却器并将其转移到客舱空气抽取系统。 传热装置还包括至少一个热泵，其使从在冷却器的冷传递回路中循环的冷转移介质到在传热回路中循环的传热介质的热能传递增加至少在 飞机冷却系统的某些运行阶段。
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公开(公告)号：US20240409199A1
公开(公告)日：2024-12-12
申请号：US18734448
申请日：2024-06-05
Applicant: Airbus Operations GmbH
Inventor： Matthias Reiss , Rafael Mortensen Ernits , Oliver Kiehne , Birte Pupkes , Dennis Keiser , Michael Freitag , Jakob Payk , Bastian Schäfer , Tobias Dahms , Alejandro Rego Hevia
IPC: B64C1/06
Abstract: A structural element for a passenger cabin of an aircraft is built using biomimicry methods. The structural element includes a generative structure, and a functional component. The generative structure includes at least one accommodating space. The functional component is arranged within the at least one accommodating space. The generative structure includes a load topology optimized structure based on a bioinspired generative design that is configured to enable the structural integrity of the structural element while simultaneously providing integrated functionalities via the functional component. Further, an interior component for an aircraft is disclosed that includes at least one such structural element, and an aircraft including at least one structural element. For example, an aircraft galley may include a structural component that may therefore, for example, include integrated wiring, plumbing or other functionalities.
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公开(公告)号：US11501249B2
公开(公告)日：2022-11-15
申请号：US16371413
申请日：2019-04-01
Applicant: Airbus Operations GmbH
Inventor： Michael Bauer , Matthias Reiss , Norbert Kaufeld , Tobias Dahms , Heinrich Hoelscher , Rafael Mortensen Ernits , Michael Freitag
IPC: G06Q10/08 , B65G1/04 , B64D11/00 , B64D11/04 , G06F3/0488
Abstract: A system for stock management for on-board catering for a vehicle, in particular for an aircraft, includes a galley which is provided with a control unit for controlling the galley, wherein the control unit is designed to make available stock management data of the galley; a service unit for transporting supplies within the vehicle, wherein the stock management data comprise a stock record of the supplies transported with the service unit; and at least one operator control element which is communicatively connected to the control unit of the galley via a wireless data connection and is designed to record removal of a supply item from the service unit and/or reception of a supply item into the service unit, and to bring about updating of the stock record of the transported supplies on the basis thereof.
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公开(公告)号：US10479505B2
公开(公告)日：2019-11-19
申请号：US15586424
申请日：2017-05-04
Applicant: Airbus Operations GmbH
Inventor： Wilhelm Lutzer , Matthias Reiss , Oliver Kiehne , Michael Kempa , Marc Spille , Holger Czopka
Abstract: A fluid-disposing system for a galley sink includes: a galley sink for a galley cabin monument, a self-regulating valve, a control unit, a sensor, and a signal connection between the sensor and the control unit. The valve input is connected to a fluid line, connected to a drainage opening of the galley sink. The valve is arranged underneath the drainage opening, such that fluid from the galley sink can flow through the associated drainage opening into the fluid line. The valve output is designed to be couplable with a source of negative pressure. The valve is designed to automatically open at a predetermined amount M1 of fluid in the fluid line, such that fluid can flow out of the fluid line, and to automatically close at a predetermined amount M2 of fluid in the fluid line, such that the predetermined amount M2 of fluid remains in the fluid line.
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