To provide an air vehicle soundness diagnostic system which enables peeling of an adhesion structure and progress of the peeling etc. in an airframe of an air vehicle to be diagnosed, and to provide an air vehicle soundness diagnostic method.SOLUTION: An air vehicle soundness diagnostic system 10 includes a control part 40 for performing a structure soundness monitoring of an airframe 2 of an air vehicle 1. The control part 40 has: a first risk evaluation part 50 which evaluates a risk of occurrence of damage of the airframe 2 based on a correlation between a signal data set 106 based on measurement data 101 measured by a measuring instrument 20 and reference data 105 stored in a storage part 30; a second risk evaluation part 60 which evaluates the risk of the occurrence of the damage of the airframe 2 based on behavior of time series variation of the signal data set 106; and a maintenance evaluation part 70 which evaluates life, repair timing, and a maintenance plan of the airframe 2 based on the behavior of the time series variation of the signal data set 106.SELECTED DRAWING: Figure 1
【課題】航空機の機体における接着構造の剥離及び剥離の進展等を診断することを可能にする航空機の健全性診断装置及びその方法を提供すること。【解決手段】航空機の健全性診断装置10は、航空機1の機体2の構造健全性モニタリングを行う制御部40を備える。制御部40は、計測器20が計測した計測データ101に基づく信号データセット106と記憶部30に記憶された基準データ105との相関関係に基づいて、機体2の損傷発生のリスクを評価する第1リスク評価部50と、信号データセット106の時系列変化の挙動に基づいて、機体2の損傷発生のリスクを評価する第2リスク評価部60と、信号データセット106の時系列変化の挙動に基づいて、機体2の寿命、修理の時期、及びメンテナンスの計画を評価するメンテナンス評価部70と、を有する。【選択図】図1
AIR VEHICLE SOUNDNESS DIAGNOSTIC SYSTEM AND AIR VEHICLE SOUNDNESS DIAGNOSTIC METHOD
航空機の健全性診断装置及び航空機の健全性診断方法
2019-05-09
Patent
Electronic Resource
Japanese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 |
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