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Uniflow Two-Cycle Aero-Diesel Powerplant

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: N/A
Agency Tracking Number: 22848
Amount: $67,850.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 1994
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
P.O. Box 7743, Incline Village, NV, 89452
DUNS: N/A
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Gregory Stevenson
 (702) 831-3917
Business Contact
Phone: () -
Research Institution
N/A
Abstract
This proposal outlines the design and development of a uniflow two stroke Aero-Diesel engine core in response to the NASA SBIR solicitation for a general aviation aircraft propulsion system. The proposed engine will offer increased power density, simplified operation, reduced emissions, noise, and vibration, while enhancing reliability and safety when compared to currently available general aviation aircraft engines. Important innovations are: * Reciprocating, uniflow sleeve valve to control intake and exhaust ports * Hypocycloidal crank design that reduces engine size, weight and vibration * Electronic fuel injection/engine management system. * Governor controlled single lever variable pitch integration system. These innovations are aimed at the NASA supplied objectives "to improve performance, safety and reliability, simplify operations, reduce maintenance and costs, and improve environmental compatibility." and address the limitations with current general aviation powerplants.

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

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