Lambda Research

Company Information
Address 5521 Fair Lane
Cincinnati, OH, 45227-3401


DUNS: 084756105

# of Employees: 21

Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N

Award Charts

Award Listing

  1. Characterization and Modeling of Residual Stress and Cold Work Evolution in PM Nickel Base Disk Superalloy

    Amount: $99,995.00

    Powder metal (PM) superalloys used for critical compressor and turbine disk applications are prone to fatigue failures in stress concentration features such as holes and radii, as well as from corrosi ...

    SBIRPhase I2011National Aeronautics and Space Administration
  2. Stress Corrosion Cracking Mitigation and Fatigue Strength Improvement of Light Water Reactor Components Using Low Plasticity Burnishing (LPB)

    Amount: $99,958.00

    Stress corrosion cracking (SCC) and fatigue can dramatically reduce the service life of light water reactor (LWR) components, including pressure vessels, steam generator nozzles, pressurized nozzles, ...

    SBIRPhase I2009Department of Energy
  3. LPB as a Crack Initiation Resistant Surface Treatment Process for Case Hardened Steels

    Amount: $69,987.00

    The goal of the proposed SBIR work is to develop Low plasticity burnishing (LPB) as a manufacturing process to increase the high cycle fatigue (HCF) strength of case carburized steels by creating a cr ...

    SBIRPhase I2009Army Department of Defense
  4. Residual Stress Measurements Program to Support Condition Based Maintenance (CBM) of Critical Rotating Components of Propulsion Systems

    Amount: $79,858.00

    Surface enhancement processes are extensively used to introduce compressive residual stresses (CRS) and enhance the fatigue performance in titanium and nickel alloy rotating components for Navy propul ...

    SBIRPhase I2007Navy Department of Defense
  5. Design Tools for Fatigue Life Prediction in Surface Treated Aerospace Components

    Amount: $1,384,920.00

    The goal of this program is to develop a validated design tool to predict fatigue behavior in components subjected to residual compression inducing surface treatments. This design tool will be based o ...

    SBIRPhase II2007Navy Department of Defense
  6. Design Tools for Fatigue Life Prediction in Surface Treated Aerospace Components

    Amount: $149,943.00

    Although surface treatments like low plasticity burnishing (LPB) and laser shock processing (LSP) impart deep compressive residual stresses that significantly improve damage tolerance, credit for the ...

    SBIRPhase I2005Navy Department of Defense
  7. Component Surface Treatments for Engine Fatigue Enhancement

    Amount: $749,951.00

    The feasibility of improving damage tolerance of the F119 4th stage compressor IBR blades with low plasticity burnishing (LPB) was successfully demonstrated in Phase I. Fatigue results for Ti-6246 bla ...

    SBIRPhase II2003Air Force Department of Defense
  8. Affordable Compressor Blade Fatigue Life Extension Technology

    Amount: $740,237.00

    "Improved damage tolerance is critical to achieving reduced engineownership costs and increasing safety and fleet readiness. InPhase I, low plasticity burnishing (LPB) was successfullydemonstrated to ...

    SBIRPhase II2002Navy Department of Defense
  9. Component Surface Treatments for Engine Fatigue Enhancement

    Amount: $99,973.00

    "The 4th stage compressor IBR of the JSF F119 engine is fatigue limited. Surface enhancement, by the introduction of compressive residual stress, is a practical means of improving fatigue performance ...

    SBIRPhase I2002Air Force Department of Defense
  10. Optical Powering Of Systems

    Amount: $69,967.00

    Low Plasticity Burnishing (LPB) has been shown to provide twice the HCF strength ofshot peening, and four times the strength after FOD in Ti-6Al-4V and IN718 laboratoryspecimens exposed to turbine eng ...

    SBIRPhase I2001Navy Department of Defense

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