SBIR/STTR Research Award

Design Environment to Improve Fatigue Resistance Through Engineered Residual Stresses

Award identifier a054c34594da8d71d32c11d24c5bc391fff2e5b001a05b3e74407c5fee188394Awarding agency Department of Defense · Air Force

Award amount

$749,788

Program and phase

SBIR · Phase II

Award year

2009

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Impact Technologies
Proposal award date
2009-07-01
Contract end date
2011-07-01
UEI
T1JNUWJLN5M1
Solicitation number
2008.1
Topic code
AF081-089

Research abstract

The Air Force has identified a need for the development of predictive design tools that can be used to accurately determine the fatigue life of components containing both applied and engineered residual stresses and determine the optimal location and processing parameters for residual stress introduction. Impact Technologies proposes to develop an integrated analysis tool that will achieve this objective. The technical approach is based on integrating design capabilities for modeling for residual stress prediction, computational fracture mechanics based damage progression, and life prediction calculations. The approach will also take into consideration statistical variants due to modeling accuracy, loading conditions, and material behavior. This integrated approach will allow for the identification of component high stress/life-limiting regions, determination of engineered residual stress process application regions, and the computation of damage tolerance effects due to different residual stress inducing processes. BENEFIT: The development of this system would be attractive to the military as well as industry. The technology will be generic enough to be applied to any metallic structural component that contains material processing-induced stresses and documented material properties. Advanced tools that can accurately predict fatigue life of structural components subjected to residual stress while reducing experimental testing requirements can contribute to F-22 ASIP goals. In addition to F-22, this technology would be applicable to all metallic airframe structural components and could include critical drive and propulsion system components that utilize residual stress-inducing material processing. The introduction of residual stresses to increase fatigue life is used extensively in commercial aircraft structures, automotive applications, propulsion system turbines and mechanical drive components, and power generation turbines and drive components. This represents significant commercial potential for a fully developed successful Phase III product transition.

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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