An Integrated Modeling and Fault Simulation Environment for Analyzing Aircraft Subsystem Interactions

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$750,000.00
Award Year:
2003
Program:
SBIR
Phase:
Phase II
Contract:
N68335-04-C-0022
Award Id:
64645
Agency Tracking Number:
N022-0937
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
125 Tech Park Drive, Rochester, NY, 14623
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
073955507
Principal Investigator:
Michael Roemer
Director of Engineering
(585) 424-1990
mike.roemer@impact-tek.com
Business Contact:
Mark Redding
President
(585) 424-1990
mark.redding@impact-tek.com
Research Institution:
n/a
Abstract
Impact Technologies, in cooperation with the Honeywell F-35 PTMS development team, propose the development, customization and implementation of a software simulation environment specifically focused on the integrated modeling of the F-35 PTMS (PowerThermal Management System), but can be applied across various vehicle subsystems. The proposed fault simulation and analysis test bench will be used to rigorously evaluate the failure mode interactions between all LRU and subsystems of systems such as thePTMS. The integrated software simulation demonstrated in Phase I within the Matlab/Simulink software will be further developed and applied to the F-35 PTMS with capability of failure mode modeling, full dynamic simulation, functional subsysteminteraction, and provide PHM algorithm interface

* information listed above is at the time of submission.

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