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Fan Noise Screening Rig for New Open Rotor and Propeller Concepts

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX10CC83P
Agency Tracking Number: 094311
Amount: $99,760.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A2.10
Solicitation Number: N/A
Timeline
Solicitation Year: 2009
Award Year: 2010
Award Start Date (Proposal Award Date): 2010-01-29
Award End Date (Contract End Date): 2010-07-29
Small Business Information
358 East Fillmore Avenue
St. Paul, MN 55107-1289
United States
DUNS: 041776824
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Robert Week
 Principal Investigator
 (651) 220-1205
 rweek@aerosysengr.com
Business Contact
 Peter Maye
Title: Business Official
Phone: (651) 220-1339
Email: pmaye@aerosysengr.com
Research Institution
N/A
Abstract

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.

* Information listed above is at the time of submission. *

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