HYBRID AIRCRAFT FUSELAGE CELL STRUCTURE

FIELD: transport.SUBSTANCE: invention relates to aircraft engineering. Proposed aircraft structure comprises skin panel with dual shell, skin single-piece panel, stiffness element arranged between skin panels and lengthwise strip to load transition section. said lengthwise trap is located in the are...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MJULLER MARKUS, JERN PAUL, DOL'TSINSKI VOL'F-DITRIKH, KHARTVIG ARNE, VEBER MARKUS JORG, PROVE JENS-UL'RIKH, KHEL'TSH NORBERT
Format: Patent
Sprache:eng ; rus
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