The invention provides a method for inspecting a single closed cavity foam sandwich structure after damage repair. The method comprises the following steps: selecting a target tail rotor blade comprising a tail rotor blade with zero service life or an unused tail rotor blade; based on the target tail rotor blade and a knocking detector, determining a target elastic characteristic value of the knocking detector; and based on the target elastic characteristic value of the knocking detector, determining whether the tail rotor blade subjected to damage repair is debonded or not; according to the method, the layering fault of the tail rotor blade after glue injection repair can be simply, intuitively, quickly and accurately identified, a conclusion whether the fault is qualified or not can be given, and the method can be popularized for inspection after damage repair of the single closed cavity foam sandwich structure.
本申请提供了一种单闭腔泡沫夹层结构损伤修理后检验方法,所述方法包括:选取目标尾桨叶;其中,所述目标尾桨叶包括零寿命的尾桨叶或未使用的尾桨叶;基于所述目标尾桨叶和敲击检测仪,确定所述敲击检测仪的目标弹性特征值;基于所述敲击检测仪的目标弹性特征值,确定损伤修理后的尾桨叶是否脱粘;本申请可以简捷、直观、快速、准确的鉴别出注胶修理后的尾桨叶分层故障,能够给出是否合格结论,可推广单闭腔泡沫夹层结构损伤修理后检验。
Method for inspecting single closed cavity foam sandwich structure after damage repair
一种单闭腔泡沫夹层结构损伤修理后检验方法
2022-01-21
Patent
Elektronische Ressource
Chinesisch
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 |
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