AIRCRAFT INTERIOR EQUIPMENT COMPONENT AND AIRCRAFT INTERIOR EQUIPMENT COMPONENT SYSTEM

An aircraft interior equipment component (10) with a frame (12) which comprises two rigid frame sections (14a-h) and a joint (16a-h) connecting the rigid frame sections (14a-h) to one another, and with a sheetlike section (18) which is supported by the frame (12) and is formed by a flexible and/or f...

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Bibliographische Detailangaben
1. Verfasser: HOETZELDT STEPHAN
Format: Patent
Sprache:eng
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Zusammenfassung:An aircraft interior equipment component (10) with a frame (12) which comprises two rigid frame sections (14a-h) and a joint (16a-h) connecting the rigid frame sections (14a-h) to one another, and with a sheetlike section (18) which is supported by the frame (12) and is formed by a flexible and/or foldable membrane (20) connected to the frame (12).