Common Fuel Engines for Powered Parafoils and other Airborne Systems

Award Information
Agency:
Department of Defense
Amount:
$118,881.00
Program:
SBIR
Contract:
DAAD16-02-C-0025
Solitcitation Year:
N/A
Solicitation Number:
N/A
Branch:
Army
Award Year:
2002
Phase:
Phase I
Agency Tracking Number:
A012-1641
Solicitation Topic Code:
N/A
Small Business Information
Gse, Inc.
219 East Enterprise St., P.O. Box 7743, Incline Village, NV, 89450
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
783625692
Principal Investigator
 Greg Stevenson
 CEO
 (775) 831-3917
 gseng4hfe@aol.com
Business Contact
 Dick Grace
Title: VP Operations
Phone: (775) 831-3917
Email: gseng4hfe@aol.com
Research Institution
N/A
Abstract
"The military "Single Fuel Forward" policy under DOD Directive 4140.25 has placed high priority on the implementation of heavy fuel engines (HFE) capable of operating on logistically available kerosene based fuels. (ie: JP-5, JP-8, DF-2) Subsonic airborneapplications defined by maximum endurance and payload capacity require the HFE to have outstanding specific weight ratios below 1.5 lbs/hp as well as excellent fuel economy under .5 lbs/hp-hr. The air dropped mission scenario of the Powered Parafoilfurther complicates the HFE requirement of having to predictably start in-flight during the chute deployment at high altitude. This unattended cold start requirement is unique to the project and is the main focus of this phase I feasibilitystudy/demonstration. The proposed high-speed multi-cylinder compression ignition (CI) diesel relies on cylinder pressure/temperature to self-ignite the fuel. High altitude starting is by an innovative low cost and robust variable compression mechanism withthe assistance of conventional cold start aids. Current logistically available fuels have variable viscosity, lubricity, and cetane values that are critical factors to engine start up, peak performance, and endurance. The proposed approach incorporates aninnovative high-speed diesel injection and combustion system that is specifically designed for multi-fuel operation. The proposed effort matures a much-needed high speed, multi-fuel diesel engine technol

* information listed above is at the time of submission.

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