Feasibility of optical interference-based NDE methods to inspect helicopter rotor blades

Dirk M. Findeis; Jasson Gryzagoridis

doi:10.1117/12.385035

5 May 2000 Feasibility of optical interference-based NDE methods to inspect helicopter rotor blades

Dirk M. Findeis, Jasson Gryzagoridis

Author Affiliations +

Proceedings Volume 3994, Nondestructive Evaluation of Aging Aircraft, Airports, and Aerospace Hardware IV; (2000) https://doi.org/10.1117/12.385035
Event: SPIE's 5th Annual International Symposium on Nondestructive Evaluation and Health Monitoring of Aging Infrastructure, 2000, Newport Beach, CA, United States

Abstract

Currently, the NDE procedure for Alouette helicopter rotor blades consists of a visual inspection followed by a manual acoustic inspection procedure by trained personnel using purpose manufactured tapping hammers. The former inspection is aimed at detecting surface cracks and corrosion whereas the latter is intended to inspect the rotor blade for possible areas of delamination between the alloy skin and the leading edge spar or blade root reinforcing strip. This paper investigates the feasibility of using either the authors locally developed Portable Digital Shearography or Electronic Speckle Pattern Interferometry in conjunction with Mechanical Impedance Analysis in order to determine the possible presence and extent of defects more accurately and reliably. Both optical inspection techniques are discussed, their theory and apparatus presented and the inspection procedure described. The principle of Mechanical Impedance Analysis is also outlined and the inspection method described. The successful results of the study as well as defects detected are presented and discussed. Outlining the potential of using this alternative NDE method as an on-site, in-situ inspection procedure concludes the paper.

Citation Download Citation

Dirk M. Findeis and Jasson Gryzagoridis "Feasibility of optical interference-based NDE methods to inspect helicopter rotor blades", Proc. SPIE 3994, Nondestructive Evaluation of Aging Aircraft, Airports, and Aerospace Hardware IV, (5 May 2000); https://doi.org/10.1117/12.385035

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