SBIR Phase I:A Ground-Based Sensor Array for Wake Vortex Detection

Award Information
Agency: National Science Foundation
Branch: N/A
Contract: 0945388
Agency Tracking Number: 0945388
Amount: $149,981.00
Phase: Phase I
Program: SBIR
Awards Year: 2010
Solitcitation Year: 2010
Solitcitation Topic Code: IC
Solitcitation Number: NSF 09-541
Small Business Information
MAC
1777 Highland Drive, Suite B, Ann Arbor, MI, 48108
Duns: 969868298
Hubzone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Dominique Fourguette
 MS
 (323) 256-0547
 dfourguette@michiganaerospace.com
Business Contact
 Dominique Fourguette
Title: MS
Phone: (323) 256-0547
Email: dfourguette@michiganaerospace.com
Research Institution
N/A
Abstract
This Small Business Innovation Research (SBIR) Phase I project seeks to develop a low-cost, easily-deployable sensor suite capable of providing the entire flow velocity field of wake vortices produced by airplanes near airports. Large aircraft produce strong air vortices at their wingtips, a significant hazard for smaller following aircraft. Without observing the vortices, aircraft must be widely-spaced on takeoff and landing. Current systems for airport wake-vortex measurement, such as wind anemometers, Radar Acoustic Sounding Sensors (RASS) and pulsed Light Detection and Ranging (LIDAR), do not capture the detailed flow-field of the vortex, so hazardous situations like counter-rotating vortices may not be detected. The new technique is based on the use of a sensor suite located at specific points near the runway to map the vortical flow. This Phase I effort includes a demonstration of the concept using existing laboratory data (consisting of 2-D mappings of vortical wall flows), and trade studies and design of the sensor suite. The sensor concept will be prototyped and tested in Phase II in an airport setting. The broader impact/commercial potential of this project will be increased safety during take-off and landing, especially for small aircraft. Present practice is to allow a fixed amount of spacing after a particular aircraft type to allow the vortices it produces to dissipate, plus an added safety margin. The ability to directly observe the vortices will allow following distances to be based on actual conditions, allowing adaptive spacing, thus enhancing safety. In comparison with competing, more complex and more delicate LIDAR and radar-based systems, the low cost of this instrumentation will allow smaller airports, not just the largest ones, to be equipped with this technology. Such smaller airports using this capability can increase their flight capacity, thus potentially relieving larger hubs, especially if an emergency evacuation were to be declared. Larger airports can use the technology to increase overall safety, especially for smaller aircraft, allowing them to land and take off with confidence amongst the larger airliners. This effort will also increase our understanding of vortical wall flows, ubiquitous in windy conditions combined with rugged terrain. Derivative versions of this equipment will be useful for other applications, such as for emergency teams required to operate in hazardous-access, windy conditions.

* information listed above is at the time of submission.

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