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Company Information:

Company Name:
Tech Integration-dev Group Inc
Address:
1 Progress Rd
Billerica, MA 01821
Phone:
N/A
URL:
N/A
EIN:
N/A
DUNS:
N/A
Number of Employees:
N/A
Woman-Owned?:
No
Minority-Owned?:
No
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
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
Award Amount:
$49,500.00
Agency:
NASA
Principal Investigator:
Nathan B Higbie , Principal Investigator
Abstract:
N/a

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

Award Year / Program / Phase:
1987 / SBIR / Phase II
Award Amount:
$200,000.00
Agency:
NASA
Principal Investigator:
Nathan B Higbie , Principal Investigator
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
Award Amount:
$50,000.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Nathan B Higbie
Abstract:
N/a

HIGH FREQUENCY HIGH TEMPERATURE LOW NOISE VIBRATION SENSOR AND CALIBRATORS

Award Year / Program / Phase:
1988 / SBIR / Phase I
Award Amount:
$50,000.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Nathan b higbie
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
Award Amount:
$50,000.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Philip Harvey
Abstract:
N/a

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

Award Year / Program / Phase:
1989 / SBIR / Phase I
Award Amount:
$50,000.00
Agency:
NASA
Principal Investigator:
Gino A Pinto
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
Award Amount:
$50,000.00
Agency / Branch:
DOD / DARPA
Principal Investigator:
George P Succi
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
Award Amount:
$500,000.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Nathan B Higbie
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
Award Amount:
$399,949.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Philip Harvey
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
Award Amount:
$50,000.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Nathan B Higbie
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
Award Amount:
$50,000.00
Agency:
NASA
Principal Investigator:
Nathan B. Higbie , Director Of Development
Abstract:
N/a

AUTOMATIC FAULT DETECTION AND FAILURE PREDICTION FOR SPACECRAFT SYSTEMS

Award Year / Program / Phase:
1991 / SBIR / Phase II
Award Amount:
$500,000.00
Agency:
NASA
Principal Investigator:
Nathan B. Higbie , Director Of Development
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
Award Amount:
$50,000.00
Agency / Branch:
DOD / USAF
Principal Investigator:
George F Succi , Principal Investigator
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
Award Amount:
$50,000.00
Agency:
NASA
Principal Investigator:
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