Stress Technology, Inc.

Address

1800 BRIHTON-HENRIETTA
Rochester, NY, 14623

Information

DUNS:
# of Employees: 29

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. N/A

    Amount: $719,480.00

    N/A

    SBIRPhase II1999Air Force Department of Defense
  2. A PROBABILISTIC DIAGNOSTIC AND PROGNOSTIC SYSTEM (ProDaPS) FOR GAS TURBINE ENGINES

    Amount: $99,759.00

    Stress Technology Incorporated proposes a Probabilistic Diagnostic and Prognostic System (ProDaPS) capable of probabilistic assessment of engine sensor signals, mechnanical and performance diagnostics ...

    SBIRPhase I1998Air Force Department of Defense
  3. USAF Engine Maintenance Cost Analysis Based on Probabilistic

    Amount: $99,968.00

    To aid the USAF in meeting it's IHPTET maintenance cost reduction goals, Stress Technology Incorporated proposes a probabilistic engineering, risk-based economic assessment tool for analyzing maintena ...

    SBIRPhase I1998Air Force Department of Defense
  4. Engine Diagnostic, Trend Monitoring, and Life Management

    Amount: $747,086.00

    The purpose of this program is to demonstrate a novel approach to condition-based diagnosis and life management for gas-turbine engines. The long term goal is to eliminate heavy, labor intensive on-bo ...

    SBIRPhase II1995Air Force Department of Defense
  5. Engine Diagnostic, Trend Monitoring, and Life Management

    Amount: $78,455.00

    N/A

    SBIRPhase I1994Air Force Department of Defense
  6. COMPUTER AIDED STRUCTURAL AND LIFE ANALYSIS OF TURBINE ENGINE COMPONENTS

    Amount: $705,533.00

    A COMPUTER BASED PROGRAM FOR STRUCTURAL ANALYSIS AND LIFE PREDICTION OF HIGH TEMPERATURE TURBINE ENGINE COMPONENTS IS PROPOSED, USING EXISTING COMPUTER ROUTINES WHICH HAVE BEEN DEMONSTRATED BY STI TO ...

    SBIRPhase II1991Air Force Department of Defense
  7. COMPUTER AIDED STRUCTURAL AND LIFE ANALYSIS OF TURBINE ENGINE COMPONENTS

    Amount: $49,212.00

    N/A

    SBIRPhase I1990Air Force Department of Defense
  8. COMPRESSOR SYSTEM DESIGN METHODOLOGY

    Amount: $49,701.00

    A PROGRAM TO FURTHER THE DEVELOPMENT OF A COMPUTER BASED DESIGN ANALYSIS CODE FOR COMPRESSOR SYSTEMS IS PROPOSED TO ASSIST THE UNITED STATES AIR FORCE IDENTIFY NEXT GENERATION ENGINES WITH IMPROVED TH ...

    SBIRPhase I1989Air Force Department of Defense
  9. LIGHTWEIGHT TURBINE BLADE ATTACHMENT

    Amount: $48,573.00

    PROPOSED HEREIN IS A PROGRAM TO DEVELOP AN IMPROVED METHOD FOR TURBINE BLADE DISK ATTACHMENTS. A DESIGN CONCEPT IS PRESENTED TO ALLOW EASY REMOVAL AND REPLACMENT OF BLADES, REDUCE THE MASS OF THE ATTA ...

    SBIRPhase I1989Navy Department of Defense

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