SBIR-STTR Award

High Power Density TAG Motors for Hybrid Electric Air Platforms
Award last edited on: 7/8/2010

Sponsored Program
SBIR
Awarding Agency
DOD : DARPA
Total Award Amount
$849,000
Award Phase
2
Solicitation Topic Code
SB082-011
Principal Investigator
S Paul Dev

Company Information

D-Star Engineering Corporation (AKA: D-Star Aerospace)

4 Armstrong Road
Shelton, CT 06484
   (203) 925-7630
   mailroom@dstarengineering.com
   www.dstarengineering.com
Location: Single
Congr. District: 03
County: Fairfield

Phase I

Contract Number: ----------
Start Date: ----    Completed: ----
Phase I year
2009
Phase I Amount
$99,000
The project aims to develop a strategy for a dramatically lighter and more efficient electric motor, with initial emphasis on a 7 hp class, 12” diameter fan for VTOL UAVs. For this, D-STAR is proposing a new motor architecture that combines and enhances the best features of contemporary motor architectures. For the Phase 1, the project tasks include : preliminary design and layout of the TAG Motor, electro-magnetic design and optimization of the copper armatures, electronic design of the motor drive circuits, design iteration and optimization, and reporting & planning.

Keywords:
Motor Generator Permanent Magnet High Power Efficiency

Phase II

Contract Number: ----------
Start Date: ----    Completed: ----
Phase II year
2010
Phase II Amount
$750,000
DARPA SBIR solicitation SB082-011 seeks the design and development of high power density electric motors for hybrid electric air platforms, indicating a need for a prototype motor rated at 7 hp, weight less than 1.4 lbs, efficiency greater than 95% and operating at speeds less than 10,000 revolutions per minute (RPM), to be used for a ducted fan of less than 12 inches in diameter with a targeted speed of 8,400 RPM. During Phase 1, D-STAR Engineering engaged in preliminary and analytical design and optimization of such a motor, labeled the TAG Motor, and indicated its feasibility. Upon invitation by DARPA, D-STAR has prepared a proposal for detailed mechanical design and development of a prototype for such a motor. Technical details of the TAG Motor are included in relevant sections of this proposal.

Keywords:
Motor Light Weight High Efficiency Fan Hybrid Uav