Status Report

NASA Tech Transfer Opportunity: Flow Control Devices

By SpaceRef Editor
March 12, 2012
Filed under , ,

TECHNOLOGY TRANSFER OPPORTUNITY FLOW CONTROL DEVICES TWO FLUIDIC OSCILLATORS WITH NO MOVING PARTS OPTIMIZE FLOW CONTROL FOR BETTER SYSTEM PERFORMANCE

Synopsis – Mar 12, 2012

General Information
Solicitation Number: N/A
Reference Number: TTO0971
Posted Date: Mar 12, 2012
FedBizOpps Posted Date: Mar 12, 2012
Recovery and Reinvestment Act Action: No
Original Response Date: Jun 01, 2012
Current Response Date: Jun 01, 2012
Classification Code: 99 — Miscellaneous
NAICS Code: 927110
Set-Aside Code:

Contracting Office Address

NASA/Langley Research Center, Mail Stop 12, Industry Assistance Office, Hampton, VA 23681-0001

Description

NASA Langley Research Center in Hampton, VA solicits interest from companies interested in obtaining license rights to commercialize, manufacture and market the following technology. License rights may be issued on an exclusive or nonexclusive basis and may include specific fields of use.

THE TECHNOLOGY:

NASA Langley develops innovative technologies to control fluid flow in ways that will ultimately result in improved performance and fuel efficiency. Often called as fluidic oscillators, sweeping jet actuators or flip flop oscillators, these flow control devices work based on the Coanda effect. They can be embedded directly into a control surface (such as a wing or a turbine blade) and generate spatially oscillating bursts (or jets) of fluid to improve flow characteristics by enhancing lift, reducing drag, or enhancing heat transfer. Recent studies show upto a 60% performance enhancement with oscillators. NASA offers two new fluidic oscillator designs that address two key limitations of these oscillators: coupled frequency-amplitude and random oscillations. One oscillator effectively decouples the oscillation frequency from the amplitude. The other design enables synchronization of an entire array. The new oscillators have no moving parts– oscillation, decoupling, and synchronization are achieved entirely via internal flow dynamics.

To express interest in this opportunity, please respond to Sean Sullivan, Research Triangle International (RTI), at: NASA Langley Research Center, Strategic Relationships Office (SRSO), 17 West Taylor St., Mail Stop 218, Building 1212, Room 110 Hampton, Virginia, E-mail: Sean.D.Sullivan@NASA.gov, or phone: 757-864-5055. Please indicate the date and title of the FBO notice and include your company and contact information.

RTI is responsible for aggregating and acknowledging all responses. These responses are provided to members of NASA Langley’s Innovative Partnerships Office within the SRO for the purpose of promoting public awareness of our technology products, and conducting preliminary market research to determine public interest in and potential for future licensing opportunities. If direct licensing interest results from this posting, SRO will follow the formal licensing process of posting in the Federal Register as required. No follow-on procurement is expected to result from responses to this Notice.

Point of Contact

Name: Sean Sullivan
Title: Media Specialist
Phone: 757-864-5055
Fax: 757-864-8101
Email: sean.d.sullivan@nasa.gov

SpaceRef staff editor.