Parallel Operation of Compact, Efficient Turbogenerators for Robust Tactical Energy Independence

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$747,955.00
Award Year:
2012
Program:
SBIR
Phase:
Phase II
Contract:
FA8650-12-C-2226
Agency Tracking Number:
O2-1151
Solicitation Year:
2010
Solicitation Topic Code:
OSD10-EP1
Solicitation Number:
2010.2
Small Business Information
Mechanical Solutions, Inc.
11 Apollo Drive, Whippany, NJ, -
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
015334899
Principal Investigator:
Charles Prisco
Principal Engineer
(518) 320-8552
cjp@mechsol.com
Business Contact:
Karen Rizzi
General Manager
(973) 326-9920
ksr@mechsol.com
Research Institution:
Stub




Abstract
The project goal is to enable the electrical outputs of multiple, very compact turbogenerators in the 10-50 kW range to be combined ("mechanically paralleled") in order to create a compact, stable, reliable, and efficient microgrid capable of providing up to 500 kW of"island"power that can be subject to rapid transients, without suffering degradation. To accomplish this, MSI has assembled a team of experienced and accomplished individuals in the fields of electrical control, high rotational speed electrical power generation, and rotordynamics and mechanical behavior, and has established a cooperative relationship with a DoD contractor/ supplier of microturbine generators. Analytical methods are being applied that consist of simplified but robust approaches in Phase I and high fidelity numerical techniques in Phase II involving comprehensive nonlinear finite element and finite difference multiphysics (i.e. simultaneous electromagnetic/stress/deflection/vibration) analysis of detailed component and fully assembled system geometries. Specialized testing will be used to validate the analysis and simulation tools. Phase II will conclude with a demonstrated rapid paralleling control system applicable to a wide range of systems, a modified set of small turbojet generators operating as a microgrid, plus rotor system design modifications and a scaling methodology applicable to larger turbojet generators.

* information listed above is at the time of submission.

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