NASA SBIR 2014 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 14-2 A4.01-9539
PHASE 1 CONTRACT NUMBER: NNX14CL38P
SUBTOPIC TITLE: Ground Test Techniques and Measurement Technologies
PROPOSAL TITLE: Development of a "Digital Bridge" Thermal Anemometer for Turbulence Measurements

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Vigyan, Inc.
30 Research Drive
Hampton, VA 23666 - 1325
(757) 865-1400

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Amber Favaregh
favaregh@vigyan.com
30 Research Drive
Hampton, VA 23666 - 1325
(757) 865-1400

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Eugene Richard White
rwhite@vigyan.com
30 Research Drive
Hampton, VA 23666 - 1325
(757) 865-1400 Extension :202

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 2
End: 5

Technology Available (TAV) Subtopics
Ground Test Techniques and Measurement Technologies is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Thermal anemometry (a.k.a. hot-wire anemometry) has been a key experimental technique in fluid mechanics for many decades. Due to the small physical size and high frequency response of the sensors (resulting in excellent spatial and temporal resolution), the technique has been widely used for studies of turbulent flows. Even with the advent of nonintrusive techniques such as Laser Doppler Velocimetry (LDV) and Particle Image Velocimetry (PIV), hot wire anemometry is uniquely capable of extremely high frequency response and fine spatial resolution measurements. ViGYAN has demonstrated a fundamental change to the anemometer configuration, with two related aspects. First, the circuitry to power the sensor and establish its operating point is packaged immediately adjacent to the sensor, i.e. in the typical probe holder, removing the effect of the cable connecting the sensor to an external anemometer. Second, modern analog-digital conversion hardware has been employed to the maximum extent possible, including directly driving the sensor. Data transmission is fully digital, immune to environmental variations or electrical noise. Based on these results, the Phase II work will deploy this "Digital Bridge" system using a Digital Signal Processing (DSP) device connected via fiber-optic cable the miniaturized "probe holder" electronics. The DSP will be controlled by a generic PC with software to control the system and acquire/store data. A production-ready version will be developed and delivered; facilities, expertise, and resources are available to fabricate and deliver production units at the conclusion of Phase II. Production designs for ruggedized units will also be done for use in wind tunnels that operate at higher dynamic pressures and extreme temperatures.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
A primary objective of the Digital Bridge design is, of course, to improve the performance of thermal anemometry in demanding aerospace applications, particularly wind tunnels. Any NASA wind tunnel, from small low-speed facilities to highly complex installations such as the National Transonic Facility (NTF) at NASA LaRC are candidates for this technology. The miniaturized, localized, and substantially digitized electronics package could be used for acquisition and processing of signals from hot film arrays, often used for boundary layer studies in both wind tunnel and flight environments. Other potential research applications could include planetary atmosphere measurements.
One of the key issues here has been the large number of sensors, but the digital bridge approach lends itself to effective multiplexing of a large number of sensors across a smaller number of anemometers. Such an approach would allow for the use of hot wire sensors analogous to the shift to electronically scanned pressure (ESP) transducers widely used in wind tunnels.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
There are many commercial and educational wind tunnels in the U.S. and around the world that could use the Digital Bridge. Looking to broader markets, the majority of air mass flow sensors for automotive applications rely on thermal anemometry in one way or another. The monitoring and control of heating, ventilation, and air conditioning (HVAC) systems is also done with thermal anemometry systems. A digital bridge approach will offer improved environmental tolerance and greater reliability for both applications, with its digital outputs being easily integrated into the overall automotive or industrial control systems used.
There are a number of applications for hot wire sensors in medical instrumentation . It should be noted that a requirement in many of these systems is electrical isolation; our use of fiber optic instrumentation cables would be very useful in such environments.

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
Biological (see also Biological Health/Life Support)
Cryogenic/Fluid Systems
Data Acquisition (see also Sensors)
Entry, Descent, & Landing (see also Planetary Navigation, Tracking, & Telemetry)
Health Monitoring & Sensing (see also Sensors)
Medical
Nondestructive Evaluation (NDE; NDT)
Pressure & Vacuum Systems
Thermal

Form Generated on 04-14-15 17:14