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Patent AT-E400497-T1: [Translated] STRUCTURAL ELEMENT FOR AN AIRCRAFT

Published by National Center for Biotechnology Information (NCBI) | U.S. Department of Health & Human Services | Catalog Last Checked: September 10, 2026 at 07:47 PM | Dataset Last Updated: September 06, 2025
The structural element for the floor in an aircraft fuselage (2) has a passive component (3), as the lateral carrier to support the floor, and active piezo electric ceramics (20-22) to pass controlled forces into the passive component. A control (31), with an electronic measurement and evaluation function, is electrically connected (24-26) to the piezo electric ceramics, to pass voltage signals for them to expand or contract (27-30) according to the forces on the fuselage floor as the aircraft maneuvers in flight.

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