DETERMINING BENDING STATE OF AIRCRAFT WING

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United States of America Patent

APP PUB NO 20240174372A1
SERIAL NO

18522340

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An aircraft including a wing, a first pressure sensor and a second pressure sensor, wherein each pressure sensor is configured to measure pressure of a liquid within the wing and has a known position within the wing. The aircraft includes a processing system configured to receive first pressure data from the first pressure sensor, receive second pressure data from the second pressure sensor, and determine a bending state of the wing based on the first pressure data, the second pressure data, and the known positions of the first and second pressure sensors within the wing.

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Patent Owner(s)

Patent OwnerAddress
AIRBUS OPERATIONS LIMITEDPEGASUS HOUSE AEROSPACE AVENUE FILTON BRISTOL BS34 7PA

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Vignola, Dylan Bristol, GB 5 0

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