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複合材の最新非破壊検査技術,三菱重工技報 Vol.54 No.4(2017)

(2017) 24 *1 *2 *3 The State-of-the-art Non Destructive Inspection Technology for Composite Materials *1 *3 Mitsuyoshi Uematsu Takahito Shimomukai *2 *3 Yoshiharu Kuze Hiroshi Takemoto *2 *3 Seiji Kobayashi Shogo Tanaka Time-Reversal

三菱重工技報 Vol.54 No.4 (2017) 25 が整備され,適用が徐々に進んでいるものの国内で実機に適用されている例は少ない。

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Transcription of 複合材の最新非破壊検査技術,三菱重工技報 Vol.54 No.4(2017)

1 (2017) 24 *1 *2 *3 The State-of-the-art Non Destructive Inspection Technology for Composite Materials *1 *3 Mitsuyoshi Uematsu Takahito Shimomukai *2 *3 Yoshiharu Kuze Hiroshi Takemoto *2 *3 Seiji Kobayashi Shogo Tanaka Time-Reversal

2 |1. CFRP GFRP 787 A350 50 / |2. CFRP (2017) 25 PAUT Probability Of Detection POD (a)

3 POD (b) POD |3. Time-Reversal T/R PAUT / MHz ZETEC T/R PAUT T/R PAUT T/R PAUT PAUT T/R

4 (2017) 26 T/R PAUT OCT: Optical Coherence Tomography OCT Santec IVS-300 SN UV 90 OCT LBI.

5 Laser Bond Inspection FAA (1) (2017) 27 weak bond ENCOMB LBI EMAT: Electromagnetic AcousticTransducer LBI LSP Technology G1C LBI 80 800 (2)

6 Go/No Go (2017) 28 |4. T/R PAUT OCT LBI AI (1) Federal Aviation Administration, Composite Aircraft Structure, AC 20-107B (2009) (2) National Aerospace Standard, Certification & Qualification of Nondestructive TestPersonnel, NAS410 (2014)


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