Analysis and Testing of a Composite Fuselage Shield for Open Rotor Engine Blade-Out Protection

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The Federal Aviation Administration is working with the European Aviation Safety Agency to determine the certification base for proposed new engines that would not have a containment structure on large commercial aircraft. Equivalent safety to the current fleet is desired by the regulators, which means that loss of a single fan blade will not cause hazard to the Aircraft. The NASA Glenn Research Center and The Naval Air Warfare Center (NAWC), China Lake, collaborated with the FAA Aircraft Catastrophic Failure Prevention Program to design and test lightweight composite shields for protection of the aircraft passengers and critical systems from a released blade that could impact the fuselage. In the test, two composite blades were pyrotechnically released from a running engine, each impacting a composite shield with a different thickness. The thinner shield was penetrated by the blade and the thicker shield prevented penetration. This was consistent with pre-test predictions. This paper documents the live fire test from the full scale rig at NAWC China Lake and describes the damage to the shields as well as instrumentation results.

Authors

• Pereira, J. Michael NASA Glenn Research Center
• Emmerling, William Federal Aviation Administration
• Seng, Silvia Naval Air Warfare Center
• Frankenberger, Charles Naval Air Warfare Center
• Ruggeri, Charles R. NASA Glenn Research Center
• Revilock, Duane M. NASA Glenn Research Center
• Carney, Kelly S. NASA Glenn Research Center

Keywords

• safety
• jet engine
• composite materials