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VEXTEC Corporation

Company Information
Address
5123 VIRGINIA WAY STE C21
BRENTWOOD, TN 37027-7519
United States


http://www.vextec.com

Information

UEI: K8DXK85LFYM4

# of Employees: 6


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Optimal Durability and Reliability Testing of Gas Turbine Components

    Amount: $749,215.00

    This proposal outlines the development of innovative technologies applied in a practical and cost effective methodology for determining gas turbine engine reliability. The approach is to produce a set ...

    SBIRPhase II2008Department of Defense Air Force
  2. Optimal Durability and Reliability Testing of Gas Turbine Components

    Amount: $99,946.00

    Through the traditional design and development cycles, prototype hardware components are built, tested, and the design is then modified for unforeseen shortcomings revealed in testing. These cycles a ...

    SBIRPhase I2007Department of Defense Air Force
  3. Integrally Bladed Rotor (IBR) Sustainment

    Amount: $99,996.00

    Integrally bladed rotors (IBRs) have become prevalent in new military gas turbine engines. IBRs replace rotors with inserted blades. As with other types of unitized structures, IBRs greatly reduce par ...

    SBIRPhase I2007Department of Defense Air Force
  4. Digital Electronics Health Prognosis

    Amount: $1,141,380.00

    A comprehensive Air System PHM approach will be developed for avionics digital circuits. As a mission is flown, temperature and vibration data indicate the stresses imposed on the electronics. This te ...

    SBIRPhase II2007Department of Defense Navy
  5. Three-Dimensional Nonlinear Structural Analysis Methods for Gas Turbine Engine Metallic Components and Component Assemblies

    Amount: $1,191,010.00

    The objective of this Phase II program is to implement, demonstrate and validate the computational techniques that were developed in Phase I that can be used for materials-damage based prognosis of ga ...

    SBIRPhase II2007Department of Defense Air Force
  6. Physics Based Gear Health Prognosis via Modeling Coupled with Component Level Tests

    Amount: $69,999.00

    PHM investments can successfully diagnose up to 70% of damage fault indications. The cost of empirically-based testing is very high and must be reworked for every gear system design change. Physics-ba ...

    STTRPhase I2007Department of Defense Navy
  7. Software for the Design and Certification of Unitized Airframe Components

    Amount: $742,566.00

    This SBIR Phase II will demonstrate the feasibility for a unitized component structural design tool that allows for holistic risk assessment. The analysis will transform the FEA predicted stress (or s ...

    STTRPhase II2007Department of Defense Air Force
  8. Real-Time Management of Turbine Engine Usage Data

    Amount: $748,976.00

    This SBIR program will develop a novel software methodology for the management of gas turbine usage data in real time for accurate prediction of engine life. The approach will be flexible enough to al ...

    SBIRPhase II2006Department of Defense Air Force
  9. Vehicle Enterprise Computational Reliability Software (ECRS)

    Amount: $1,957,570.00

    As the Army’s current fielded ground combat and combat support systems continue to age, there are increasing performance and reliability issues being encountered by our troops. Vehicles and equipmen ...

    SBIRPhase II2006Department of Defense Army
  10. Three-Dimensional Nonlinear Structural Analysis Methods for Gas Turbine Engine Metallic Components and Component Assemblies

    Amount: $99,992.00

    Air Force engines are required to satisfy both safe-life and fatigue crack growth (damage tolerant) design criteria under the engine structural integrity program (ENSIP). To achieve this requirement, ...

    SBIRPhase I2006Department of Defense Air Force
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