SBIR/STTR Research Award

A Dynamic Failure Mode Simulation Environment (FMECA++) for EHM Design and Analysis

Award identifier a643ec6f898c138df3fdb04cf2043a2ba4b6e15cedf21c1186f8b307e02106f3Awarding agency Department of Defense · Air Force

Award amount

$599,258

Program and phase

SBIR · Phase II

Award year

2005

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Impact Technologies
Proposal award date
2005-05-10
Contract end date
2007-09-10
UEI
T1JNUWJLN5M1
Solicitation number
2003.1
Topic code
AF03-169

Research abstract

Impact Technologies, in cooperation with Pratt & Whitney and Qualtech Systems Inc., propose to develop and commercialize a simulation-based design application for dynamic failure mode and effects analysis (FMECA++) that specifically focuses on designing and verifying EHM technologies for legacy and new acquisition engines. The proposed FMECA++ design software will be capable of; 1.) Automated failure mode insertion and propagation analysis, 2.) EHM algorithm design and verification, 3.) Full dynamic engine simulations, 4.) Embedded code generation for the ICF and 5.) Direct interfacing with the QSI TEAMS Product. In order to address this multi-scale modeling functionality, the Impact team will leverage the COTS software suite by Mathworks called Simulink/Stateflow and use XML data schema for integration with the QSI software. Utilizing the Simulink software as the core analysis engine, the design software will be capable of providing full functionality from the specific EHM algorithm level to the higher-level engine health management reasoners. The Impact team believes this innovative approach to EHM design/analysis will truly represent the next generation in capability needed for the VAATE Intelligent Engine focus area and can be directly incorporated into the AFRL’s ICF facility. In addition, the JSF Program Office (JPO) has recently supported a program at Impact focused on vehicle-level modeling and will be leveraged during this Phase II program, thus reducing our Phase II proposed cost by over $150K. The end goal is to create a comprehensive simulation-based design tool to support dynamic fault propagation analysis; EHM cost/benefit analysis, as well as EHM testing and validation that enables EHM design and trade studies much earlier in the overall design process where significant cost savings can be realized. A realistic application of the software will be based on comprehensive EHM analysis for the Pratt & Whitney F119 and F135 engines.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

232 SBIR/STTR records share this UEI (1999–2014). Reported award amounts total $76,299,884. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, Department of Homeland Security, Department of Transportation

Agency intelligence

Department of Defense

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