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
| @type | dcat:Dataset |
|---|---|
| accessLevel | public |
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"009:25"
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"fn": "NIH/NCBI Data Team",
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| description | 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. |
| distribution |
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"description": "Access the complete Patent AT-E400497-T1: [Translated] STRUCTURAL ELEMENT FOR AN AIRCRAFT on the official website.",
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|
| identifier | https://healthdata.gov/api/views/8mup-uu3e |
| issued | 2025-09-05 |
| keyword |
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"chemistry",
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| landingPage | https://healthdata.gov/d/8mup-uu3e |
| modified | 2025-09-06 |
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| publisher |
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| theme |
[
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|
| title | Patent AT-E400497-T1: [Translated] STRUCTURAL ELEMENT FOR AN AIRCRAFT |
