Study of aldehydes, Co and characterization of particles resulting from oil contamination of aircraft bleed air

Doctor of Philosophy === Department of Mechanical and Nuclear Engineering === Byron Jones === Contamination of aircraft bleed air with engine oil and/or hydraulic fluid results in a “fume event” in the aircraft cabin. Exposure to contaminated bleed air may have acute and/or chronic adverse health ef...

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Main Author: Nayyeri Amiri, Shahin
Language:en_US
Published: 2018
Subjects:
CO
Online Access:http://hdl.handle.net/2097/39129
id ndltd-KSU-oai-krex.k-state.edu-2097-39129
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spelling ndltd-KSU-oai-krex.k-state.edu-2097-391292018-11-08T15:52:33Z Study of aldehydes, Co and characterization of particles resulting from oil contamination of aircraft bleed air Nayyeri Amiri, Shahin Aldehydes CO Characterization of particles aircraft bleed air Doctor of Philosophy Department of Mechanical and Nuclear Engineering Byron Jones Contamination of aircraft bleed air with engine oil and/or hydraulic fluid results in a “fume event” in the aircraft cabin. Exposure to contaminated bleed air may have acute and/or chronic adverse health effects based on the intensity of various chemicals which are released during such a fume event. ASHRAE Standard 161, Air Quality within Commercial Aircraft, includes a requirement for bleed air sensors to detect contamination from lubricating oil. One potential approach to meeting this requirement is through particle detection. In the research reported here, the end goal is to provide data needed to develop an automated detection apparatus for contaminated bleed air through oil particle detection. Consequently, the type and concentration of different chemicals as well as the number and size distribution of particles were determined for bleed air with different rates of contamination under various turbine engine operating conditions. Multiple fume events were simulated by using a four-part experimental program to develop a detailed characterization of particles that result when bleed air is contaminated with lubricating oil. 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 (high bleed air temperature) the concentration distribution and particle size does not vary much with power (temperature) and generally depends on the rate of contamination. Moreover, at elevated power levels, the peak particle concentration takes place in the range of 50 to 70 nanometers and the bulk of the particles form at less than 150 nanometers. At very low contamination rates very ultrafine particles can be generated in the size of 10 nanometers or less. As a result, detection is needed for a range of sizes ranging from about 100 nanometers to 10 nanometers. 2018-08-10T15:46:35Z 2018-08-10T15:46:35Z 2018-08-01 2018 August Dissertation http://hdl.handle.net/2097/39129 en_US
collection NDLTD
language en_US
sources NDLTD
topic Aldehydes
CO
Characterization of particles
aircraft bleed air
spellingShingle Aldehydes
CO
Characterization of particles
aircraft bleed air
Nayyeri Amiri, Shahin
Study of aldehydes, Co and characterization of particles resulting from oil contamination of aircraft bleed air
description Doctor of Philosophy === Department of Mechanical and Nuclear Engineering === Byron Jones === Contamination of aircraft bleed air with engine oil and/or hydraulic fluid results in a “fume event” in the aircraft cabin. Exposure to contaminated bleed air may have acute and/or chronic adverse health effects based on the intensity of various chemicals which are released during such a fume event. ASHRAE Standard 161, Air Quality within Commercial Aircraft, includes a requirement for bleed air sensors to detect contamination from lubricating oil. One potential approach to meeting this requirement is through particle detection. In the research reported here, the end goal is to provide data needed to develop an automated detection apparatus for contaminated bleed air through oil particle detection. Consequently, the type and concentration of different chemicals as well as the number and size distribution of particles were determined for bleed air with different rates of contamination under various turbine engine operating conditions. Multiple fume events were simulated by using a four-part experimental program to develop a detailed characterization of particles that result when bleed air is contaminated with lubricating oil. 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 (high bleed air temperature) the concentration distribution and particle size does not vary much with power (temperature) and generally depends on the rate of contamination. Moreover, at elevated power levels, the peak particle concentration takes place in the range of 50 to 70 nanometers and the bulk of the particles form at less than 150 nanometers. At very low contamination rates very ultrafine particles can be generated in the size of 10 nanometers or less. As a result, detection is needed for a range of sizes ranging from about 100 nanometers to 10 nanometers.
author Nayyeri Amiri, Shahin
author_facet Nayyeri Amiri, Shahin
author_sort Nayyeri Amiri, Shahin
title Study of aldehydes, Co and characterization of particles resulting from oil contamination of aircraft bleed air
title_short Study of aldehydes, Co and characterization of particles resulting from oil contamination of aircraft bleed air
title_full Study of aldehydes, Co and characterization of particles resulting from oil contamination of aircraft bleed air
title_fullStr Study of aldehydes, Co and characterization of particles resulting from oil contamination of aircraft bleed air
title_full_unstemmed Study of aldehydes, Co and characterization of particles resulting from oil contamination of aircraft bleed air
title_sort study of aldehydes, co and characterization of particles resulting from oil contamination of aircraft bleed air
publishDate 2018
url http://hdl.handle.net/2097/39129
work_keys_str_mv AT nayyeriamirishahin studyofaldehydescoandcharacterizationofparticlesresultingfromoilcontaminationofaircraftbleedair
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