Small Business Innovation Research/Small Business Tech Transfer
Non-Thermal Soot Denuder, Phase I
Project Introduction
We propose to develop a non-thermal soot denuder for measuring chemical components of the nucleation mode particulate matter emissions from gas turbine engines, in combination with an Aerodyne Aerosol Mass Spectrometer (AMS). This proposed approach will effectively eliminate the contribution of soot particles to the AMS-measured volatile PM mass spectrum. It is capable of identifying the semi-volatile composition of the nucleation mode particles based on their characteristic mass spectra and also determining the particle size distribution in aerodynamic diameter.
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Anticipated Benefits
This proposed apparatus can be easily transferred from a soot denuder into a non-thermal nanoparticle purifier and could become a continuous and environment-friendly method to purify and size-select the desired nanoparticles in the same time. Such technique would have a great impact on the mass production of high-quality nanoparticles. The material and operational cost of this instrument is so low that there is little financial burdening to add it to the current available nanoparticle synthesis scheme. The primary NASA need for this technology is in its research programs to monitor nucleation mode particulate emissions from aircraft engines. In addition to AMS, other particle measurement instruments with an aerodynamic lens such as Aerodynamic Particle Sizer (APS), which NASA has used in its previous field missions, can also be integrated with the proposed soot denuder to monitor soot particles without the influence of non-refractory coating.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Aerodyne Research, Inc | Lead Organization | Industry | Billerica, Massachusetts |
Glenn Research Center
(GRC)
|
Supporting Organization | NASA Center | Cleveland, Ohio |
Primary U.S. Work Locations
-
Massachusetts
-
Ohio
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- Aerodyne Research, Inc
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Start: Feb 2011
End: Sep 2011
Technology Maturity (TRL)
| Start: | 4 |
| Current: | 8 |
| Estimated End: | 8 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX01 Propulsion Systems
- TX01.3 Aero Propulsion
- TX01.3.2 Turbine Based Combined Cycle
Target Destination
Earth
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