Holographic Inspection of Jet Engine Composite Fan Blades

770975

02/01/1977

Event
Aerospace Meeting
Authors Abstract
Content
A holographic inspection method was developed for composite spar/shell fan blades, such as an experimental fan blade and an advanced fan blade. This method was employed to insure the quality of newly fabricated blades. Holographic inspection also was used to indicate initiation and growth of cracks as a result of resonant fatigue testing and spin testing. Metallographic examinations were conducted to show the good correlation between the holographic data and actual blade structures.
Meta TagsDetails
DOI
https://doi.org/10.4271/770975
Pages
7
Citation
Delgrosso, E., and Carlson, C., "Holographic Inspection of Jet Engine Composite Fan Blades," SAE Technical Paper 770975, 1977, https://doi.org/10.4271/770975.
Additional Details
Publisher
Published
Feb 1, 1977
Product Code
770975
Content Type
Technical Paper
Language
English