Case Studies

Reduction of Aircraft Engine Blade Damage


In 1991, the B-1B Lancer's F101 engine began experiencing titanium turbine blade failures that forced the grounding of the entire B-1 fleet. The primary hazard was foreign object damage (FOD), as ingested ice chunks and other hard objects were producing cracks in the blades that led to failure and irreparable engine damage.

The United States Air Force ordered special manual inspections prior to all B-1 flights, a laborious procedure that involved rubbing the leading edge of each blade with cotton balls, cotton gloves, or dental floss. If inspectors detected even a single snag, the blade was swapped out and replaced before the aircraft was cleared to fly. By 1994, the Air Force was devoting over one million man-hours at a cost of $10 million per year to complete the engine inspections and keep the B-1 flying.


GE Aircraft Engines (GEAE) turned to laser peening as a potential solution to improve the durability of F101 fan blades and decrease the blades' sensitivity to FOD. They tested laser peening on blades that were nothced up to 0.25 inches deep to simulate foreign object damage. The blades were subjected to rigorous fatigue testing, and their performance was compared to similarly notched blades that had only been shot peened. The fatigue life improvement for laser peened blades was unprecedented.

Damage to a typical F101 blade reduces the fatigue strength from 75 ksi to less than 20 ksi - well below the design requirement. However, when laser peened blades are comparably damaged, they retain a fatigue strength of 75 ksi or more. Laser peened blades in the study outperformed shot peened blades by a wide margin, and even lasted longer than pristine, undamaged blades.


Given the overwhelming fatigue life improvement demonstrated by laser peening, the Air Force authorized production development of this revolutionary surface enhancement process. Laser peening was proven to virtually eliminate sensitivity to FOD defects up to 0.25 inches deep, preventing engine failures that endangered critical aircraft and crew. GEAE began laser peening all F101 first stage fan blades in 1997, using four laser peening systems designed and built by LSP Technologies, Inc.

Laser peening adoption proved to be a valuable application for the U.S. Air Force, with tens of millions of dollars saved in blade replacement costs, engine damage repair costs, inspection and maintenance, and cost avoidance from airfoil failures.

Overall, the potential savings offered by laser peening are estimated to approach $1 billion when calculated over all engines in the Air Force fleet.

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