Methods and Systems for Assessing Damage to a Structure and Determining Repair Information

An example computer-implemented method of assessing damage to a structure includes receiving information of damage to the structure, and identifying a damage type for the damage. Following, the damage type and the information is compared with a first reference having allowable damage limits of the s...

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Bibliographische Detailangaben
Hauptverfasser:	Keller, Russell, Lin, John, Lewis, Arne, Brewer, Carlyn, Greene, Kelly, Yovanof, Nicolette, Duong, Cong
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDEDFOR ELSEWHERE AVIATION CHECKING-DEVICES COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GENERATING RANDOM NUMBERS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS PHYSICS REGISTERING OR INDICATING THE WORKING OF MACHINES TIME OR ATTENDANCE REGISTERS TRANSPORTING VOTING OR LOTTERY APPARATUS
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Beschreibung
Zusammenfassung:	An example computer-implemented method of assessing damage to a structure includes receiving information of damage to the structure, and identifying a damage type for the damage. Following, the damage type and the information is compared with a first reference having allowable damage limits of the structure for that damage type, a second reference having damage repair information and associated damage repair processes, and a database having historical repair information for the damage type. Based on the damage type and the information indicating that the damage is outside the allowable damage limits described in the first reference and also does not have any associated damage repair process described in the second reference and the database does not include historical repair information for the damage type, expanded repair information is provided for a repair solution based on a material type and loading of the structure.