A system which includes a first light beam locating sensor associated with a first position to be located on a wing of an aircraft. The first light beam locating sensor senses a first light beam at an identifiable position on the first light beam locating sensor. A processor is configured to receive a first signal from the first light beam locating sensor wherein the first signal includes a first identifiable position on the first light beam locating sensor. The processor is configured to determine a location of the first position on the wing and perform a first comparison of the location of the first position on the wing to a predetermined analyzed location of the first position on the wing.
SYSTEM AND METHOD FOR CORRECTING WING TWIST OF AN AIRCRAFT
SYSTEM UND VERFAHREN ZUR KORREKTUR DER SCHRÄNKUNG EINES FLÜGELS
SYSTÈME ET PROCÉDÉ DE CORRECTION DE LA TORSION D'AILE D'UN AÉRONEF
27.04.2022
Patent
Elektronische Ressource
Englisch
SYSTEM AND METHOD FOR CORRECTING WING TWIST OF AIRCRAFT
Europäisches Patentamt | 2018
|SYSTEM AND METHOD FOR CORRECTING WING TWIST OF AN AIRCRAFT
Europäisches Patentamt | 2018
|System and method for correcting wing twist of an aircraft
Europäisches Patentamt | 2018
|