← Back to NASA Technology Projects
Fan Noise Screening Rig for New Open Rotor and Propeller Concepts
Completed
TRL 3 (started at 1, targeting 3)
Description
Recent advancements in open rotor engine concepts warrant continued research, however the cost of wind tunnel tests is not insignificant. Because the jet noise of an open rotor engine, or even that of a geared fan, is very low in relation to the fan noise, it is evident that fan noise reduction technology is now just as important as jet noise reduction. A low cost test system is needed that would allow for comprehensive technology screening of open rotor concepts permitting more testing to be conducted at a lower overall cost. The approach to developing such a system will be to maximize the use of current technology in the selection and development of components. The first step to achieving this goal will be a design study that will include the following activities: define test criteria, further investigate drive motor and bearing technology, perform dynamic and structural analysis, define services such as power, cooling, lubrication, health monitoring, prepare fabrication estimate.
Benefits
The test technology resulting from this study may allow for derivative test rigs to be constructed for test in other non-NASA test facilities. Examples include the GE Aviation Cell 41 acoustic test facility in Evendale, Ohio or the Boeing Corporation Low Speed Aero-acoustic Facility (LSAF) in Seattle, Washington. Additionally, a modular, transportable test apparatus may be conceived of that would allow for testing a common rig in different test sites.
A fundamental enterprise goal of NASA is to develop new and less expensive research and test technologies for the advancement of aerodynamics. The test rig resulting from this study would provide a less expensive technology screening facility capable of demonstrating new open rotor or propeller concepts. A potential site for use of this test rig may be in the NASA Glenn Research Center Aero-Acoustic Propulsion Lab (AAPL).
Details
| Technology area | Flight Vehicle Systems > Aeroscience > Aeroacoustics |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Aero Systems Engineering, Inc., St. Paul, MN |
| Start date | 2010-01-29 |
| End date | 2010-07-29 |
Project contacts
Listed on TechPort itself — the most direct way to ask about this specific project.
How to get involved
This is early/mid-stage (TRL 3) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.