in:(PUPKES BIRTE)

AIRCRAFT CABIN DISMANTLING AND RECYCLING US18331025
[Matthias REISS, Antje TERNO, Thorsten OTTO, Matthias POGGENSEE, Sonja REHSÖFT, Axel BECKER, Maite GONZALEZ EIZAGUIRRE, Rafael MORTENSEN ERNITS, Dennis KEISER, Michael FREITAG, Birte PUPKES] DE Hamburg An aircraft cabin dismantling and recycling system including: a device (10) for transferring aircraft cabin parts to secondary utilization is provided that includes a data input (12), a data processor (14) and an output interface (16). The data input provides cabin base types from a database and initial equipment installation states of the aircraft cabin from an installation state database. The data processor is configured to identify a cabin base type for a current part of the aircraft cabin; assign an initial equipment installation state of the aircraft cabin; estimate changes of the current part and determine a current parameter; identify implementable transferring options for the current part of the aircraft cabin from a database of transferring options based on the current parameter, and select one of the identified transferring options.
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DE102021003051A
[MORTENSEN ENITS RAFAEL, KEISER DENNIS, PUPKES BIRTE, BÖROLD AXEL, SPRODOWSKI TOBIAS, FREITAG MICHAEL, JATHE NICOLAS, SCHWEERS DIRK, LÜTJEN MICHAEL, ROHDE ANN-KATHRIN, PANTER LARS, ZEITLER WALDEMAR, BRODA EIKE] DE
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Bionic Structural Element with Integrated Functionality for a Passenger Cabin of an Aircraft, Interior Component for an Aircraft, and Aircraft US18734448
[Matthias Reiss, Rafael Mortensen Ernits, Oliver Kiehne, Birte Pupkes, Dennis Keiser, Michael Freitag, Jakob Payk, Bastian Schäfer, Tobias Dahms, Alejandro Rego Hevia] DE Hamburg 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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BIONIC STRUCTURAL ELEMENT WITH INTEGRATED FUNCTIONALITY FOR A PASSENGER CABIN OF AN AIRCRAFT, INTERIOR COMPONENT FOR AN AIRCRAFT, AND AIRCRAFT EP24177941.2
[HEVIA, Alejandro Rego, REISS, Matthias, ERNITS, Rafael Mortnesen, KIEHNE, Oliver, PAYK, Jakob, SCHÄFER, Bastian, DAHMS, Tobias, PUPKES, Birte, KEISER, Dennis, FREITAG, Michael] Kreetslag 10, 21129 Hamburg, DE Disclosed herein is a structural element (100) for a passenger cabin of an aircraft (200) that is build using biomimicry methods. The structural element (100) comprises a generative structure (110), and a functional component (120). The generative structure (110) comprises at least one accommodating space (111). The functional component (120) is arranged within the at least one accommodating space (111). The generative structure (110) comprises a load topology optimized structure based on a bioinspired generative design that that is configured to enable the structural integrity of the structural element (100) while simultaneously providing integrated functionalities via the functional component (120). Further, an interior component (200) for an aircraft (300) is disclosed that comprises at least one such structural element (100), and an aircraft (300) comprising at least one structural element (100). For example, an aircraft galley may include a structural component (100) that may therefore, for example, include integrated wiring, plumbing or other functionalities. <img id="iaf01" file="imgaf001.tif" wi="65" he="82" img-content="drawing" img-format="tif" />
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AIRCRAFT CABIN DISMANTLING AND RECYCLING EP22177908.5
[REISS, Matthias, TERNO, Antje, OTTO, Thorsten, POGGENSEE, Matthias, REHSÖFT, Sonja, BECKER, Axel, GONZALEZ EIZAGUIRRE, Maite, MORTENSEN ERNITS, Rafael, KEISER, Dennis, FREITAG, Michael, PUPKES, Birte] DE,21129 Hamburg,Kreetslag 10; The present invention relates to aircraft cabin dismantling and recycling. In order to provide improved guidance relating to aircraft cabins when they are no longer used in their initial purpose, a device (10) for transferring aircraft cabin parts to secondary utilization is provided that comprises a data input (12), a data processor (14) and an output interface (16). The data input is configured to provide a plurality of cabin base types from a database. The data input is also configured to provide a plurality of initial equipment installation states of the aircraft cabin from an installation state database. The initial equipment installation state comprises data of at least one of the group of: material, construction, equipment and installation. The data input is further configured to provide a plurality of implementable transferring options from a database of transferring options. The data processor is configured to identify a cabin base type for a current part of the aircraft cabin by selecting one of the plurality of cabin base types from a database. The data processor is also configured to assign, based on the identified cabin base type, one of the plurality of initial equipment installation states of the aircraft cabin. The data processor is further configured to estimate changes of the current part over the identified cabin base type for at least one of the group of: material, construction, equipment and installation. The data processor is furthermore configured to determine at least one current parameter of the group of: material, construction, equipment and installation for the current part of the aircraft cabin based on the assigned initial equipment installation state and the estimated changes. The data processor is still further configured to identify implementable transferring options for the current part of the aircraft cabin from a database of transferring options based the at least one determined current parameter. The data processor is as well configured to select at least one of the identified transferring options for the current part of the aircraft cabin. The output interface is configured to provide the selected identified transferring option.
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