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Company Information:

Company Name:
SPRUNG-BRETT RDI, INC.
Address:
Baird Research Park, Suite 102C
1576 Sweet Home Road
Amherst, NY
Phone:
(917) 701-4010
URL:
N/A
EIN:
204504249
DUNS:
623374340
Number of Employees:
5
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 $397,148.00 3
SBIR Phase II $748,775.00 1
STTR Phase I $68,936.00 1
STTR Phase II $500,000.00 1

Award List:

High Torque High Efficiency WARP Motor Design for use in Leading Edge Flap Systems

Award Year / Program / Phase:
2006 / STTR / Phase I
Award Amount:
$68,936.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Michael K. Brewster, Director of Research
Research Institution:
UNIV. OF MARYLAND EASTERN SHOR
RI Contact:
I. K. Dabipi
Abstract:
A motor drive actuation system with integrated transmission has been proposed for study and application to electric flap actuation and other high torque low rpm range applications. A new technology is introduced in this proposal with technical and scientific discourse expanding on the fundamental… More

Advanced Development of High Torque WARP Motor for Use in Leading Edge Flap Systems Phase II

Award Year / Program / Phase:
2007 / STTR / Phase II
Award Amount:
$500,000.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Michael K. Brewster, Director of Research
Research Institution:
WAYNE STATE UNIV.
RI Contact:
Nabil G. Chalhoub
Abstract:
Continued development of a motor drive actuation system with integrated transmission has been proposed for further study, experimentation and application development for electric flap actuation and other high torque low rpm range applications. This new technology was introduced in a phase I program… More

High Temperature Permanent Magnet Actuator Motor

Award Year / Program / Phase:
2008 / SBIR / Phase I
Award Amount:
$99,528.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Michael K. Brewster, Director of Research
Abstract:
A novel highly integrated electric actuator with an electrically based thermal management system is proposed for further study and feasibility assessment. A permanent magnet system is initially chosen and several candidate designs are presented for exploration under GFI(Air Force) stipulated… More

High Temperature Permanent Magnet Actuator Motor

Award Year / Program / Phase:
2009 / SBIR / Phase II
Award Amount:
$748,775.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Michael K. Brewster, Director of Research
Abstract:
This proposal describes a novel approach in the design and development of a high temperature resistant electric motor for aerospace actuation applications. A biomorphical inspired adaptive achitecture was conceptualized in Phase I and is proposed to be futher explored in detail in Phase II. … More

High Temperature Electro-Magnetic WARP Actuators (HTEMA)

Award Year / Program / Phase:
2012 / SBIR / Phase I
Award Amount:
$149,258.00
Agency:
DOD
Principal Investigator:
Cecil J. Brewster, President – (917) 701-4010
Abstract:
ABSTRACT: This proposal is the fusion of two major Phase II efforts with NAVAIR and AFRL. Innovative Electro-magnetic motor actuation is merged with a proprietary adaptive thermally dynamic shielding system. BENEFIT: High Temperature (extreme environment) tolerant electric actuation that can… More

Rotary Electromechanical Actuator for Next-Generation Thin-Wing Aircraft Flight Control

Award Year / Program / Phase:
2013 / SBIR / Phase I
Award Amount:
$148,362.00
Agency:
DOD
Principal Investigator:
Michael Brewster, Director of Research – (301) 960-4321
Abstract:
ABSTRACT: The objective of this proposal is to develop a high torque, compact and reliable rotary electromechanical (EMA) actuator for next-generation thin-wing military aircraft flight control. This topic seeks to develop advanced rotary EMA technologies for primary flight control actuation… More