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Optimization of Turbine Engine Performance Using Shape Memory Alloy Pressure…

Award Information

Agency:
Department of Defense
Branch:
Defense Advanced Research Projects Agency
Award ID:
53273
Program Year/Program:
2002 / SBIR
Agency Tracking Number:
01SB1-0028
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Orbital Research Inc
4415 Euclid Avenue Suite 500 Cleveland, OH 44103-
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 2002
Title: Optimization of Turbine Engine Performance Using Shape Memory Alloy Pressure Transducers
Agency / Branch: DOD / DARPA
Contract: DAAH01-02-C-R185
Award Amount: $369,997.00
 

Abstract:

Currently, active cooling of pressure transducers is required in high temperature sections of turbine engines, which limit their use to ground-based engine tests. Lacking high temperature pressure measurement capabilities, turbine engines must operatewithin a wide engine performance margin, which limits the true performance capability of the engine, reduces fuel economy and aircraft range. A flight-ready, high temperature pressure transducer would enable advanced engine controls for improved aircraftand engine performance, extended range and fuel efficiency, reduced emissions, and engine health monitoring capabilities. The Phase I program successfully demonstrated a fast response, high temperature shape memory alloy (HTSMA) pressure sensing elementsuitable for harsh turbine engine applications without the need for active cooling. This Phase II program will build upon these successful results to produce a flight-ready, HTSMA pressure transducer that will be tested in turbine engine ground or flighttests at Pratt & Whitney's test facility. Orbital Research has received much interest though our working relationships with key turbine engine organizations and manufacturers, such as the Propulsion Instrumentation Working Group and Pratt & Whitney.Continued collaboration with Orbital Research's turbine engine industry team will ensure product readiness and reliability in harsh turbine engine environments.

Principal Investigator:

Joseph Snyder
Sr. Materials Engineer
4404495785
snyder@orbitalresearch.com

Business Contact:

Frederick Lisy
Vice President
4404495785
lisy@orbitalresearch.com
Small Business Information at Submission:

Orbital Research, Inc.
673G Alpha Drive Cleveland, OH 44143

EIN/Tax ID: 341672688
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No