A Simplified Model of Gas Generator for Active Component Control and Operability Analysis

Award Information
Agency: Department of Defense
Branch: Army
Contract: N/A
Agency Tracking Number: 32823
Amount: $69,618.00
Phase: Phase I
Program: SBIR
Awards Year: 1996
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
4801 S. Lakeshore Dr. Suite, 202, Tempe, AZ, 85282
DUNS: N/A
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Dr. Link C. Jaw
 (602) 752-7909
Business Contact
Phone: () -
Research Institution
N/A
Abstract
The firm proposes to conduct a research on turboshaft engine control and accessory technologies. The specific technology to be developed a simplified, unsteady-flow dynamic model of an engine gas generator which is suitable for the analysis and design of advanced turbine engine controls. Two motivations of the proposed work are: 1) a lack of efficient model to support the design and simulation of advanced engine controls, 2) a lack of attention to the coupling between active compressor and combustor controls. The significance of the proposed work is in three areas: 1) developing an integrated, simplified model of the (unsteady flow and shaft) dynamics of compressor and combustor; 2) allowing systematic analysis of the coupling effects among the three basic components; and 3) conducting control analysis for actuator sizing and sensor/actuator placement.

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

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