Characterization of Particulate Resulting from Oil Contamination of
Aircraft Bleed Air 01-14-01-0002
This also appears in
SAE International Journal of Aerospace-V130-1EJ
Possible oil contamination of aircraft bleed air is an ongoing operational issue
for commercial aircraft. A sensitive and reliable method to detect
contamination, especially at very low levels, has been elusive due, in part, to
the lack of information about the physical nature of oil that results when
entrained in the bleed air by an engine compressor. While it was expected that
high shear rates in the compressors would result in very finely dispersed
particles, detailed data on the size characteristics of these droplets were not
available, making it difficult to develop reliable detection techniques. The
goal of the reported research was to collect experimental data to provide this
information. The concentration and size distribution of particles were measured
for bleed air with different rates of controlled oil contamination under various
engine operating conditions. Multiple contamination levels were generated by
injecting jet engine lubricating oil into the air intake of two different
turbine engines (Allison 250 C18 and Allison 250 C28B). The resulting
contaminated bleed air was cooled and sampled. In addition, another series of
tests was conducted on a Pratt and Whitney F117-PW-100 engine on board an Air
Force C17 aircraft with oil injected into the first stage of the compressor.
Test results show that oil contamination in the compressor will result in a fog
of very fine droplets in the bleed air under most operating conditions. With
moderately high contamination rates at elevated power levels, the concentration
distribution and particle size does not vary much with power and generally
depends on the rate of contamination. Moreover, at elevated power levels, the
peak particle concentration takes place in the range of 50 nanometers (nm) to 70
nm and the bulk of the particles form at less than 150 nm. At very low
contamination rates, the ultrafine particles generated can be 10 nm or less.
This research shows that detection should focus on the particles less than 100
nm and detection of particles as small as 10 nm may be required for detection of
very low contamination levels.
Citation: Nayyeri, S., Jones, B., and Hosni, M., "Characterization of Particulate Resulting from Oil Contamination of Aircraft Bleed Air," SAE Int. J. Aerosp. 14(1):45-62, 2021, https://doi.org/10.4271/01-14-01-0002. Download Citation
Author(s):
Shahin Nayyeri, Byron Jones, Mohammad Hosni