Demonstration of Novel Sampling Techniques for Measurement of Turbine Engine Volatile and Non-Volatile Particulate Matter (PM) Emissions
WP-201317
Objective
Particulate matter (PM) is an Environmental Protection Agency (EPA) designated criteria pollutant regulated by the National Ambient Air Quality Standards (NAAQS) under the Clean Air Act (CAA). In September, 1997, the U.S. EPA revised the PM regulation to include more stringent standards for PM less than 2.5 micrometers (PM2.5) in diameter. Most health and environmentally harmful PM2.5 result from the combustion of fossils fuels in stationary (e.g. power plants) and mobile sources, such as aircraft and ground vehicles. Although it has been recognized that Department of Defense (DoD) operations, particularly aircraft, produce significant PM2.5 emissions, quantification of these has been a tremendous challenge. The high uncertainty in estimates of military aircraft on regional PM2.5 inventories may cause unnecessary restrictions, resulting in increased operational costs and adverse impacts to the overall mission. For instance, military training could be restricted to certain hours of the day or limited to a few days a week in order to reduce the adverse impact of aircraft operations on local air quality. In addition, state regulators could require that a new weapon system or use of an alternative (non-petroleum derived) fuel within their jurisdiction require assessment of PM2.5 emissions to ensure that these will not impact the attainment or maintenance designation level of the region. Therefore, the reliable characterization of military aircraft PM emissions is of upmost importance to determine the burden on the local environment.
The overall objective of this program is to demonstrate the performance of several innovative devices to condition aircraft turbine engine exhaust to allow improved characterization of volatile and nonvolatile PM (total number, mass and composition) using conventional instrumentation. Total PM include non-volatile PM, which are emitted at engine exit temperatures and pressures (i.e., soot) and volatile PM, which are formed via gas-to-particle conversion in the atmosphere (i.e., condensed organics and sulfur species). Although challenging, significant progress on methods for characterizing non-volatile PM has been achieved by the Society of Automotive Engineers (SAE) E-31 committee. This will lead to a measurement standard in an Aerospace Recommended Report (ARP) by late 2013. In contrast, with the exception of a position paper by the SAE E-31 committee in 2005, measurement of volatile PM has not been addressed. Characterization of volatile PM is recognized to be extremely difficult due to its unstable thermodynamic state (including susceptibility to condensation in sampling lines), and the high influence of atmospheric conditions on the resulting physical and chemical properties.
Technology Description
The approach in this program is to promote the controlled condensation of volatile species extracted at the engine exit plane for subsequent characterization and quantitation of volatile PM. PM characterization includes: particle number, size, mass, chemical composition and elemental/organic carbon fraction. These will be compared to PM sampled at 30 m where significant volatile PM have formed. Demonstration of a device to separate the volatile and nonvolatile PM for analysis will also be performed in this project to support the development of the nonvolatile PM ARP.
Benefits
These demonstrations will take place at two test sites and will employ turbine engines representative of newer and legacy technologies. Successful demonstration of the devices will significantly increase the understanding of volatile PM formation for subsequent characterization, and may lead to the development of standard methodologies for the measurement of total and non-volatile PM emissions from aircraft turbine engines. Reliable estimates of aircraft PM2.5 exhaust to state and federal regulating agencies will prevent unnecessary and costly restrictions on the use of weapon systems, and operations at military bases, while providing accurate data for cost-effective emission mitigating strategies. (Anticipated Project Completion - 2015)
Points of Contact
Principal Investigator
Mr. Edwin Corporan
Air Force Research Laboratory (AFRL)
Phone: 937-255-2008
Fax: 937-255-3893
Document Types
- Fact Sheet - Brief project summary with links to related documents and points of contact.
- Final Report - Comprehensive report for every completed SERDP and ESTCP project that contains all technical results.
- Cost & Performance Report - Overview of ESTCP demonstration activities, results, and conclusions, standardized to facilitate implementation decisions.
- Technical Report - Additional interim reports, laboratory reports, demonstration reports, and technology survey reports.
- Guidance - Instructional information on technical topics such as protocols and user’s guides.
- Workshop Report - Summary of workshop discussion and findings.
- Multimedia - On demand videos, animations, and webcasts highlighting featured initiatives or technologies.
- Model/Software - Computer programs and applications available for download.
- Database - Digitally organized collection of data available to search and access.
