Development of an Engine Air-Brake for Quiet Drag Applications

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX09CA33C
Agency Tracking Number: 075394
Amount: $599,315.00
Phase: Phase II
Program: SBIR
Awards Year: 2009
Solicitation Year: 2007
Solicitation Topic Code: A2.03
Solicitation Number: N/A
Small Business Information
11995 El Camino Real, San Diego, CA, 92130-2566
DUNS: 133709001
HUBZone Owned: N
Woman Owned: Y
Socially and Economically Disadvantaged: N
Principal Investigator
 Parthiv Shah
 Principal Investigator
 (858) 480-2101
 parthiv.shah@ata-e.com
Business Contact
 Ronan Cunningham
Title: Business Official
Phone: (858) 480-2015
Email: ronan.cunningham@ata-e.com
Research Institution
N/A
Abstract
A novel quiet engine air-brake (EAB) is proposed in response to NASA's solicitation for active and passive noise control concepts for conventional and advanced aircraft. The EAB concept is applicable to 1) next-generation, conventional tube and wing aircraft (current generation +1) and 2) advanced integrated airframe/propulsion system configurations (current generation +2, +3). Potential retrofit opportunities are also envisioned. Phase 1 analysis on NASA's Source Diagnostic Test (SDT) fan stage suggests that an EAB could realize three to four decibels overall noise reduction under the approach flight path by generating a swirling exhaust with drag equivalent to one to two turbofan-sized bluff bodies per powerplant. Such drag generation could enable slower and/or steeper and/or aero-acoustically cleaner approach trajectories. A Phase II development program is proposed to 1) perform aerodynamic designs of dual-stream, swirling bypass flow nozzles and experimentally assess their performance and noise, 2) develop conceptual aero-designs that address current engine architecture issues such as pylon duct bifurcations, and 3) develop a prototype design of an EAB for validation in a model-scale rig. The final deliverable to NASA will be a written report presenting design, analysis and experimental results from blown nozzle testing, plus a prototype EAB design.

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

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