Eddy Current Inspection System Print E-mail
Jun 01 2006
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Concurrent with the ECIS upgrade was the implementation of an inspection process known as the “sewing stitch.” The sewing stitch inspection technique significantly increases the efficiency and productivity of inspecting dovetail slots on F100- GE-129 high-pressure turbine disks. Using this new technique during scheduled maintenance operations, OC-ALC maintainers demonstrated a 65% decrease in inspection time.

ECIS’ original implementation occurred in the 1980s at the San Antonio Air Logistics Center, Kelly AFB, Texas, under the laboratory’s Retirement for Cause program. Eddy current inspections are critical for early crack detection and ensuring safety throughout the AF fleet. Engineers upgraded ECIS in the late 1990s, replacing obsolete system components and upgrading the station computer. The system continues to provide the AF with the enhanced inspection capability needed for conducting safety inspections under the AF structural integrity program.

Prior to the 1980s, AF maintainers replaced all engine disks when they reached a predetermined number of operating hours—a necessity since eddy current inspection technology did not yet exist. Even after manufacturing processes improved the quality and durability of aircraft engine disks, the philosophy and time frame established for retiring the disks remained unchanged. Recent advances in sensor technology, computing speed, and computational analysis now enable engineers to determine conditions under which an engine disk can continue to operate safely. By gathering more accurate measurements and processing those measurements intelligently, ECIS allows the AF to safely increase the operating life span of engine components.

In addition to increasing engine component safety, ECIS’ improved inspection techniques generate substantial cost savings. Since the price tag for one engine rotor disk can range from $25,000 to several hundreds of thousands of dollars, the AF may ultimately save hundreds of millions of dollars by keeping disks in service longer.

Dr. Howard Sizek and Dr. Paul R. Riggle (Anteon Corporation), of the Air Force Research Laboratory’s Materials and Manufacturing Directorate, wrote this article. For more information, contact TECH CONNECT at (800) 203-6451 or place a request at http://www.afrl.af.mil/techconn_index.asp. Reference document ML-H-05-19.



 

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