High Temperature Permanent Magnet Actuator Motor

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA8650-08-M-2871
Agency Tracking Number: F081-058-0137
Amount: $99,938.00
Phase: Phase I
Program: SBIR
Awards Year: 2008
Solicitation Year: 2008
Solicitation Topic Code: AF081-058
Solicitation Number: 2008.1
Small Business Information
SATCON APPLIED TECHNOLOGY, INC.
27 Drydock Avenue, Boston, MA, 02210
DUNS: 187659425
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Gerald Foshage
 Project Manager
 (617) 897-2448
 gerald.foshage@satcon.com
Business Contact
 Erin Corcoran
Title: Contracts Specialist
Phone: (617) 897-2437
Email: erin.corcoran@satcon.com
Research Institution
N/A
Abstract
A transition from a centralized, hydraulically based power source to a multi-source electric power base is eliciting a need for an electrically powered aircraft. This electrical power base will be composed on multiple, independently operated electric units, working together to power the craft. A premeditated obstacle to this innovative approach is achieving a level of power density that will meet weight and volume criteria in aircraft application. High power density electrical machines innately present thermal management issues. These issues stem from condensed power dissipation in a smaller volume and surface area. The temperatures associated with this application demand attention in the motor design and selection of materials that will meet life requirements of an application. SatCon Applied Technology proposes to meet these challenges by developing a motor with high power density, magnet and insulation systems that withstands the aircraft high temperature environment. A feasibility study of permanent magnet formulation, temperature sensitivity, and affecting environmental variables will be conducted. The end result will be a comprehensive understanding of long life insulation systems capable of withstanding high temperatures in a compact motor design. Cooling methods appropriate to manage temperatures in the aircraft will be evaluated and the most appropriate solution implemented.

* information listed above is at the time of submission.

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