NASA SBIR 2011 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 11-2 A2.03-9148
PHASE 1 CONTRACT NUMBER: NNX12CF19P
SUBTOPIC TITLE: Aero-Acoustics
PROPOSAL TITLE: Deployable Engine Air-Brake for Drag Management Applications

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
ATA Engineering, Inc.
11995 El Camino Real
San Diego, CA 92130 - 2566
(858) 480-2000

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Parthiv N Shah
parthiv.shah@ata-e.com
11995 El Camino Real, Suite 200
San Diego, CA 92130 - 2566
(858) 480-2101

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 6

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
ATA Engineering, Inc., (ATA) proposes a Phase II SBIR program to demonstrate an innovative engine air-brake (EAB) technology that uses a deployable swirl vane mechanism to switch the operation of a turbofan engine nozzle from a conventional mode to a "drag management" mode. Equivalent drag (via thrust reduction) results from the strong radial pressure gradient created by swirl vanes that are aerodynamically "invisible" during conventional operation and introduced during a drag management maneuver. Such "drag on demand" enables operational benefits such as slower, steeper, and/or aeroacoustically cleaner flight on approach, addressing NASA's need for active and passive control of aeroacoustic noise sources for conventional and advanced aircraft configurations. In Phase I ATA successfully designed an integrated vane-nozzle for a NASA high bypass ratio nozzle. To advance the technology readiness level (TRL) , ATA has formed a partnership with Williams International (WI), a manufacturer of small jet engines and industry leader in the small business jet market. The ATA/WI team will apply the Phase I design approach to the WI FJ44-4 mixed flow turbofan which is selected as a demonstration test article to move the TRL to 5–6 by the end Phase II.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The most immediate opportunity for this system is to assist NASA in the development of next generation quiet aircraft, including tube and wing (current generation +1) and integrated airframe propulsion system configurations (current generation +2). On approach, these aircraft are likely to have airframe noise levels that are comparable to or in excess of the engines. A quiet air brake device will allow noise reduction by creating drag without the associated unsteady flow structures of devices such as flaps, slats, and undercarriage. In addition, these devices will enable steep approaches, thereby locating the noise source further from the affected communities. Further development of the technology could lead to advanced thrust reverser applications whereby the deployable exit guide vanes can actuate to a closed position to function as thrust reverser blocker doors. An additional application for swirling exhaust flows is in the area of wake vortex avoidance and induced drag management. For example, swirling outflow devices placed on wing tips could be used to counter- or co-swirl relative to the bound vortex that is shed by a finite wing, resulting in potential induced drag reduction or increase (possibly of value in a quiet drag sense). This may prove to have applications in designing more fuel efficient and quiet aircraft in the future.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The commercial potential for this system extends beyond NASA's development programs related to next-generation quiet aircraft. Two complementary potential commercial markets exist for the technology: (1) implementation as a complementary technology in retrofit (ejector) hush kits on older aircraft engines in order to meet current and future noise requirements, and (2) implementation in future jet engines as an integral part of the engine design; i.e., modifying traditional engine exit guide vanes or bypass nozzles with a variable mechanism that generates a swirling outflow in drag management mode. The first market has immediate potential (within the next five to seven years), while the second market, although potentially much larger from a quantity standpoint, is a longer-term endeavor (likely seven to ten years before practical implementation in a new engine that would be part of the first N+2 prototypes). The retrofit market provides a simpler and faster implementation and is an opportunity to demonstrate the effectiveness of the technology to the community before upselling the technology or its derivatives to the engine Original Equipment Manufacturers (OEMs). Another potential application is integration of the technology into tactical UAV and cruise missile platforms that demand high levels of power generation while simultaneously requiring maneuverability and thrust control.

TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
Aerodynamics
Atmospheric Propulsion
Deployment


Form Generated on 09-03-12 17:04