Rotorcraft On-Blade Pressure and Strain Measurements Using Wireless Optical Sensor System

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$99,999.00
Award Year:
2007
Program:
SBIR
Phase:
Phase I
Contract:
NNC07QA09P
Award Id:
83765
Agency Tracking Number:
066244
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
11750 Beltsville Drive, Suite 300, Beltsville, MD, 20705
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
061997029
Principal Investigator:
GangWang
Principal Investigator
(240) 790-0600
wangg@technosci.com
Business Contact:
AmyHizoune
Business Official
(240) 790-0609
aph@technosci.com
Research Institute:
n/a
Abstract
Experimental measurements of rotor blades are important for understanding the aerodynamics and dynamics of a rotorcraft. This understanding can help in solving on-blade problems as well as in designing and optimizing the blade profiles for improved aerodynamics and noise attenuation in the next generation rotorcraft. Therefore, a Wireless Optical Pressure/Strain Sensor (WOPSS) system for helicopter on-blade pressure and strain measurement is proposed to utilize the benefits of low coherence interferometry system to create an innovative real-time pressure and strain measurement technique. Leveraging past and current experiences with fiber optic sensor development, a proof-of-concept of optical pressure/strain sensor system with wireless data acquisition and transfer capability will be demonstrated at the end of Phase I. The distributed optical pressure/strain sensor measurements will be used to obtain real-time dynamic pressure fields and mode shapes and displacements by integrating strain data for the helicopter rotor blade. Phase I efforts will conduct optical pressure and strain sensor design analysis to meet on-blade pressure and strain measurement requirements and demonstrate a proof-of-concept prototyped wireless optical pressure and strain sensor package.

* information listed above is at the time of submission.

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