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Company Information:

Name: Tech Integration-dev Group Inc
Address: 1 Progress Rd
Billerica, MA 01821
Located in HUBZone: No
Woman-Owned: No
Minority-Owned: No
URL: N/A
Phone: 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

Award List:

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

Award Year / Program / Phase: 1985 / SBIR / Phase I
Agency: NASA
Principal Investigator: Nathan B Higbie , Principal Investigator
Award Amount: $49,500.00

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

Award Year / Program / Phase: 1987 / SBIR / Phase II
Agency: NASA
Principal Investigator: Nathan B Higbie , Principal Investigator
Award Amount: $200,000.00
Abstract:
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 repetitive noise that uses a synch pulse from the engine, a high power sound source mounted near the… More

HELICOPTER VIBRATION MONITORING USING UNIFIED FAULT-STRUCTURE-SENSOR ANALYSIS

Award Year / Program / Phase: 1987 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Nathan B Higbie
Award Amount: $50,000.00

HIGH FREQUENCY HIGH TEMPERATURE LOW NOISE VIBRATION SENSOR AND CALIBRATORS

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Nathan b higbie
Award Amount: $50,000.00
Abstract:
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 technology that includes improvements in sensors, mounting techniques, and calibration. high-frequency… More

ADVANCED INTEGRATED SOLID STATE FLIGHT LOAD SENSORS

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / ARMY
Principal Investigator: Philip Harvey
Award Amount: $50,000.00

CONTINUOUS ON-BOARD NON-DESTRUCTIVE MONITORING OF DEGRADATION IN STIFFNESS AND STRENGTH OF FIBER COMPOSITES

Award Year / Program / Phase: 1989 / SBIR / Phase I
Agency: NASA
Principal Investigator: Gino A Pinto
Award Amount: $50,000.00
Abstract:
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. condition monitoring of these composites is therefore needed in order to assess the composite's… More

ACTIVE CANCELLATION OF ROTOR ACOUSTIC SIGNATURES

Award Year / Program / Phase: 1989 / SBIR / Phase I
Agency / Branch: DOD / DARPA
Principal Investigator: George P Succi
Award Amount: $50,000.00
Abstract:
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 without any obvious, weight or performance penalties. the concept will produce reduction of sound… More

HELICOPTER VIBRATION MONITORING USING UNIFIED FAULT-STRUCTURE-SENSOR ANALYSIS

Award Year / Program / Phase: 1990 / SBIR / Phase II
Agency / Branch: DOD / NAVY
Principal Investigator: Nathan B Higbie
Award Amount: $500,000.00
Abstract:
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 monitoring r&d which will use modeling and data to predict fault signatures, use cepstral and other forms… More

ADVANCED INTEGRATED SOLID STATE FLIGHT LOAD SENSORS

Award Year / Program / Phase: 1990 / SBIR / Phase II
Agency / Branch: DOD / ARMY
Principal Investigator: Philip Harvey
Award Amount: $399,949.00
Abstract:
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 susceptibility, fragility, and incompatibility with field replacement requirements. thus, the… More

PROGNOSTIC METHODS FOR ROTORCRAFT CONDITION MONITORING

Award Year / Program / Phase: 1990 / SBIR / Phase I
Agency / Branch: DOD / ARMY
Principal Investigator: Nathan B Higbie
Award Amount: $50,000.00
Abstract:
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 has proven techniques for early fault detection of rotorcraft mechanical faults and is currently… More

AUTOMATIC FAULT DETECTION AND FAILURE PREDICTION FOR SPACECRAFT SYSTEMS

Award Year / Program / Phase: 1990 / SBIR / Phase I
Agency: NASA
Principal Investigator: Nathan B. Higbie , Director Of Development
Award Amount: $50,000.00

AUTOMATIC FAULT DETECTION AND FAILURE PREDICTION FOR SPACECRAFT SYSTEMS

Award Year / Program / Phase: 1991 / SBIR / Phase II
Agency: NASA
Principal Investigator: Nathan B. Higbie , Director Of Development
Award Amount: $500,000.00
Abstract:
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 fault detection techniques that we developed for navy helicopter gearboxes coupled with new research in… More

HIGH GAIN ACOUSTIC SENSOR SYSTEMS FOR AIRCRAFT NOISE SIGNATURE DETECTION

Award Year / Program / Phase: 1991 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: George F Succi , Principal Investigator
Award Amount: $50,000.00
Abstract:
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 capabilities are quite extensive for certain aircraft targets. other targets have proven to be more… More

ENHANCED METHODS FOR PLANETARY GEAR SYSTEMS

Award Year / Program / Phase: 1991 / SBIR / Phase I
Agency: NASA
Principal Investigator:
Award Amount: $50,000.00
Abstract:
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 use planetary-gear reduction systems; these systems pose a complex problem in the diagnostics field… More