NASA SBIR 2019-II Solicitation

Proposal Summary

 19-2- A1.03-3403
 Low Emissions/Clean Power - Environmentally Responsible Propulsion
 An Enhanced Software Toolkit for OpenNCC to Reduce NOx in Commercial Supersonic Transport Combustors
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Combustion Research and Flow Technology
6210 Keller's Church Road
Pipersville, PA 18947
(215) 766-1520

PRINCIPAL INVESTIGATOR (Name, E-mail, Mail Address, City/State/Zip, Phone)
Andrea Zambon
6210 Keller's Church Road
Pipersville, PA 18947 - 1020
(215) 766-1520

BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Neeraj Sinha
6210 Keller's Church Road
Pipersville, PA 18947 - 1020
(215) 766-1520

Estimated Technology Readiness Level (TRL) :
Begin: 4
End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words)

The innovation proposed is a second-generation Software Toolkit enabling improved predictions of oxides of nitrogen (NOx) as well as particulate matter like soot in high-fidelity yet computationally-tractable Computational Fluid Dynamics (CFD) analyses of combustor concepts applicable to Commercial Supersonic Transport (CST) designs. Given the technical challenges to meet the more stringent NOx emission limits at the higher CST cruising altitudes and the unique characteristics of the CST thermodynamic cycle, the proposed innovation intends to enhance the capabilities of the first-generation Software Toolkit for NASA’s OpenNCC CFD code. The second-generation Software Toolkit will feature (i) enhanced predictive accuracy of the primary turbulent flame with real fuels, NOx and soot, (ii) computational efficiency and (iii) software portability, e.g., to NASA’s OpenNCC. Since CST combustor concepts will operate at higher temperatures and with higher fuel flow rates, a detailed understanding of flame dynamics is required, in particular within the context of parametric or trade studies. Given the competing performance and emission targets to be considered, a large number of design parameters needs to be considered, including both geometric parameters as well as parameters associated with combustor operation, for instance use of alternative fuels as a means to reduce NOx emissions. The significance of the innovation is that it addresses NASA’s core needs for an economically feasible and environmentally acceptable propulsion technology suitable for a supersonic commercial aircraft. Historically, commercial supersonic transport has received significant opposition with respect to economic viability (e.g., due to excessive fuel consumption) and environmental impact, both in terms of sonic boom and noise generation for communities along the flight path as well as negative effects on the climate and on public health.

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

This product addresses (i) NASA’s core needs for an economically feasible and environmentally acceptable CST propulsion technology, (ii) NASA ARMD core needs for enabling safe and reliable operation of next-generation (e.g., "N+3" and beyond) ultra low-emission conventional gas-turbine engine as well hybrid electric aircraft propulsion and (iii) core needs of NASA’s vision for next-generation aircraft systems with hybrid integrated wing/body systems with significant improvements in engine performance, emissions and noise reduction.

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

The commercial market includes the broad aerospace, power-generation and defense industry. Commercial aircraft gas turbine engines are the primary driver for this product. Other applications encompass power-generation turbines and IC/HCCI/diesel engines. DoD applications include gas-turbine engines, scramjets, RDEs, augmentors, UAVs propulsion systems and rocket engines.

Duration: 24

Form Generated on 05/04/2020 06:28:48