Small Engines Designed for High Efficiency, High Power Density and Quiet Operations

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: W31P4Q-09-C-0129
Agency Tracking Number: 08SB2-0250
Amount: $98,902.00
Phase: Phase I
Program: SBIR
Awards Year: 2008
Solicitation Year: 2008
Solicitation Topic Code: SB082-010
Solicitation Number: 2008.2
Small Business Information
2197 Brookwood Dr., South Elgin, IL, 60177
DUNS: 130455335
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Jack Jerovsek
 Principal Investigator
 (616) 837-8975
 bakereng@pathwaynet.com
Business Contact
 Mike Boruta
Title: Project Manager
Phone: (847) 628-4769
Email: kineticresearch@sbcglobal.net
Research Institution
N/A
Abstract
The Nutating Disk Engine is a new technology with significant advantages, and multiple potential military and commercial applications. Development work has focused on a dual-disk version of the engine, including a demonstrator prototype. Second-generation prototype is currently in development. This DARPA program provides an opportunity design a single-disk version. Development work to date has lead to the conclusion that a single-disk version is not only feasible, but desirable. The single-disk Nutating Engine offers several advantages including improved power density, reduced component count, direct routing between compressor outlets and prechamber, and the elimination of coupling hardware. The proposed Meyer Nutating Disk Engine will be a single disk engine designed to produce an output of 8-10 Hp at 4,500 rpm, and run on heavy fuel. The compact size packages this engine within a 5.75” diameter and 5.95” overall length. The engine weighs 5.6 lbs. with a projected power density of 1.46 Hp/lb. Heavy fuel operation allows it to operate efficiently at reduced rpm and light loads. Quiet operation is also expected. The single-disk engine will be designed and analysis performed during Phase I, ultimately leading to the production of a demonstration engine, paired with a generator, during the Phase II effort.

* Information listed above is at the time of submission. *

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