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Patent AT-E400497-T1: [Translated] STRUCTURAL ELEMENT FOR AN AIRCRAFT
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.
Complete Metadata
| bureauCode |
[ "009:25" ] |
|---|---|
| identifier | https://healthdata.gov/api/views/8mup-uu3e |
| issued | 2025-09-05 |
| landingPage | https://healthdata.gov/d/8mup-uu3e |
| programCode |
[ "009:066" ] |
| theme |
[ "NIH" ] |
