AF lab investigating microscopic crack formation in aircraft

Dr. Adam Pilchak, materials research engineer at the Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio, loads a piece of a fractured titanium disk into a scanning electron microscope. By looking at the microscopic features on the fracture surface, researchers are able to determine how the crack initiated and spreads through the component to cause the failure. (Air Force photo/Michele Eaton)

Dr. Adam Pilchak, materials research engineer at the Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio, loads a piece of a fractured titanium disk into a scanning electron microscope. By looking at the microscopic features on the fracture surface, researchers are able to determine how the crack initiated and spreads through the component to cause the failure. (Air Force photo/Michele Eaton)

WRIGHT-PATTERSON AIR FORCE BASE, Ohio --

The B-52 is one of the oldest legacy aircraft in the Air Force. Since the 1950s, this aircraft has led the force in its dominance as the world’s best.

However, just as humans begin to age, so do aircraft. Repeated loading and unloading, changes in air pressure, exposure to altitude and more, contribute to what is referred to as “metal fatigue,” resulting in small, microscopic cracks in engine, wing or tail structures that can have detrimental effects on safety.

Research scientists from the Metals Branch of the Materials and Manufacturing Directorate at Air Force Research Laboratory, understand the critical importance of metal fatigue and aircraft safety. To better address this critical issue, they are studying the earliest stages of crack formation in turbine engine materials in order to alleviate cracks leading to unexpected fatigue failure.  Greater understanding of crack origins leads to more effective aircraft inspection procedures, wherein maintenance teams are able to determine metal fatigue at an earlier stage and mitigate the life-limiting effects before they become a safety problem.

“The Air Force routinely inspects engine components for cracks, but it is possible to miss microscopically small cracks with current inspection methods. We want to be confident that an undetectable crack does not grow to failure before the next inspection,” said Dr. Adam Pilchak, a research scientist in the Metals Branch. “Because crack growth rates can vary considerably depending on how a material is processed, it is important to understand the worst-case scenario that leads to the shortest fatigue lifetime.”

Using a scanning electron microscope, or SEM, Pilchak and his team are able to magnify the surfaces of fractured laboratory samples or components taken from aircraft engine surfaces up to 50,000 times to precisely determine where a crack initiated. By studying the details of the crack initiation sites and the material on which cracks form, it is possible to modify the way materials are processed, ultimately improving safety.

 

“Our team is using a novel methodology in SEM to quantify, non-destructively, the cracking mechanisms during early stages of fatigue. The information from these characterizations can help reduce sustainment costs and improve fleet readiness, without compromising safety,” said Vikas Sinha, a materials scientist in the branch.

 

Pilchak and his team of researchers presented their research at the International Metallographic Contest at Microscopy and Microanalysis 2016, where they were awarded first place for research in electron microscopy as well as the Jacquet-Lucas Award for excellence in metallography.

“Studying fatigue in a controlled laboratory setting can really help determine the root cause of a failure in the field,” said Pilchak. “Ultimately, understanding how cracks initiate and grow can save lives.”