A method and system for calculating the accumulated damage on a component of an aircraft, the method comprising determining the weight of the aircraft at a predetermined point of a flight cycle, calculating, based at least partially on the determined weight of the aircraft, a calculated damage inflicted on the component during the flight cycle, obtaining historic data indicating the damage inflicted on the component before the flight cycle and calculating the accumulated damage of the component, based on the calculated damage inflicted on the component during the flight cycle and the historic data.
L'invention concerne un procédé et un système pour calculer les dommages accumulés sur un composant d'un aéronef, le procédé comprenant la détermination du poids de l'aéronef à un point prédéterminé d'un cycle de vol, le calcul, sur la base au moins partiellement du poids déterminé de l'aéronef, d'un dommage calculé infligé sur le composant pendant le cycle de vol, l'obtention de données historiques indiquant les dommages infligés sur le composant avant le cycle de vol et le calcul des dommages accumulés du composant, sur la base des dommages calculés infligés sur le composant pendant le cycle de vol et des données historiques.
METHOD AND SYSTEM FOR CALCULATING ACCUMULATED DAMAGE ON A STRUCTURAL COMPONENT
PROCÉDÉ ET SYSTÈME DE CALCUL DE DOMMAGES ACCUMULÉS SUR UN COMPOSANT STRUCTURAL
2024-07-25
Patent
Elektronische Ressource
Englisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte |
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