Tech Integration-dev Group Inc

Company Information

Company Name
Tech Integration-dev Group Inc
Address
1 Progress Rd
Billerica, MA, 01821
Phone
n/a
URL
n/a
DUNS
n/a
Number of Employees
n/a

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$499,500.00
10
SBIR Phase II
$1,599,949.00
4
Chart code to be here

Award List

  1. ACTIVE CANCELLATION OF INTERIOR AND EXTERIOR PROPELLER DRIVER AIRCRAFT NOISE USING AN EXTERIOR SOURCE

    Amount: $200,000.00

    WE PROPOSE TO DEVELOP, FOR AIRCRAFT DEPLOYMENT, AN ACTIVE CANCELLATION TECHNIQUE THAT HAS SHOWN PROMISE IN PRELIMINARYLABORATORY TESTING. THE SYSTEM CONSISTS OF A PROVEN CANCELLATION ALGORITHM FOR REP ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  2. HELICOPTER VIBRATION MONITORING USING UNIFIED FAULT-STRUCTURE-SENSOR ANALYSIS

    Amount: $500,000.00

    VIBRATION MONITORING R&D HAS BEEN SIGNAL PROCESSING ORIENTED AND PROBLEMS ARISE BECAUSE TECHNIQUES DEVELOPED FOR ONE MACHINE ARE NOT TRANSFERABLE TO OTHERS. TIDG PROPOSES A UNIFIED APPROACH TO MONITOR ...

    SBIR Phase II 1990 NavyDepartment of Defense
  3. ADVANCED INTEGRATED SOLID STATE FLIGHT LOAD SENSORS

    Amount: $399,949.00

    MODERN MICROELECTRONICS ARE MAKING POSSIBLE THE ACQUISITION AND PROCESSING OF EXTENSIVE FLIGHT DATA, BUT THE SENSORS FOR ACQUIRING SUCH DATA ARE UNSUITABLE FOR THE TASK, DUE TO THEIR ENVIRONMENTAL SUS ...

    SBIR Phase II 1990 ArmyDepartment of Defense
  4. HIGH FREQUENCY HIGH TEMPERATURE LOW NOISE VIBRATION SENSOR AND CALIBRATORS

    Amount: $50,000.00

    AS SHIPS BECOME QUIETER, IMPROVED CAPABILITIES FOR MEASURING VIBRATION IN HIGH-FREQUENCY, HIGH-TEMPERATURE, LOW-NOISE ENVIRONMENTS ARE NEEDED. TIDG PROPOSES A UNIFIED APPROACH TO THE MEASUREMENT TECHN ...

    SBIR Phase I 1988 NavyDepartment of Defense
  5. CONTINUOUS ON-BOARD NON-DESTRUCTIVE MONITORING OF DEGRADATION IN STIFFNESS AND STRENGTH OF FIBER COMPOSITES

    Amount: $50,000.00

    COMPOSITE MATERIALS ARE BEING IMPLEMENTED INTO A VARIETY OF CRITICAL AEROSPACE APPLICATIONS. DAMAGE DEVELOPMENT OCCURS TO THESE COMPOSITES DUE TO CYCLIC LOADING FATIGUE AND ENVIRONMENTAL EFFECTS. COND ...

    SBIR Phase I 1989 National Aeronautics and Space Administration
  6. ACTIVE CANCELLATION OF ROTOR ACOUSTIC SIGNATURES

    Amount: $50,000.00

    A HIGHLY EFFICIENT CONCEPT IS PROPOSED WHICH WILL SUBSTANTIALLY REDUCE ACOUSTIC SIGNATURES OF HELICOPTERS AND TILT ROTOR AIRCRAFT. THE CONCEPT CAN BE INCORPORATED INTO FUTURE HELICOPTER DESIGNS WITHOU ...

    SBIR Phase I 1989 Defense Advanced Research Projects AgencyDepartment of Defense
  7. AUTOMATIC FAULT DETECTION AND FAILURE PREDICTION FOR SPACECRAFT SYSTEMS

    Amount: $500,000.00

    TIDG PROPOSES TO DEVELOPE AN INTEGRATED FAULT DETECTION AND FAILURE PREDICTION SYSTEM FOR SPACECRAFT MECHANICAL, ELECTRICAL AND STRUCTURAL SYSTEMS. OUR APPROACH USES OUR PROVEN PATTERN RECOGNITION FAU ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  8. PROGNOSTIC METHODS FOR ROTORCRAFT CONDITION MONITORING

    Amount: $50,000.00

    PROGNOSTIC METHODS (TIME TO FAILURE PREDICTION) REQUIRE KNOWLEDGE OF FAILURE MODES, EARLY DETECTION OF CHANGE, AND LEARNING FROM EXPERIENCE. IN PREVIOUS AND ONGOING GOVERNMENT SUPPORTED RESEARCH, TIDG ...

    SBIR Phase I 1990 ArmyDepartment of Defense
  9. HIGH GAIN ACOUSTIC SENSOR SYSTEMS FOR AIRCRAFT NOISE SIGNATURE DETECTION

    Amount: $50,000.00

    PASSIVE ACOUSTIC DETECTION SYSTEMS HAVE DEMONSTRATED POTENTIAL TO DETECT AND TRACK LOW-FLYING AIRCRAFT. SIGNAL-PROCESSING TECHNIQUES HAVE PROGRESSED TO THE POINT WHERE DETECTION AND CLASSIFICATION CAP ...

    SBIR Phase I 1991 Air ForceDepartment of Defense
  10. ENHANCED METHODS FOR PLANETARY GEAR SYSTEMS

    Amount: $50,000.00

    DIAGNOSTIC FAULT DETECTION REQUIRES KNOWLEDGE OF FAILURE MODES, RECOGNITION OF MEASURABLE FAULT PATTERNS, AND IMPLEMENTATION OF OPTIMIZED SIGNAL PROCESSING. MANY OF TODAY'S ROTORCRAFT TRANSMISSIONS US ...

    SBIR Phase I 1991 National Aeronautics and Space Administration

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