Environmentatlly Benign Disposal of Substances
Small Business Information
P.o. Box 1468, Princeton, NJ, 08542
Dr. Moshe Lavid
AbstractResearch into the possible unconventional engine candidates that e2cclude the use of pistons, rotors (Wankel type), lever arm mechanisms, and conventional aerodynamic turbine components, reveals a surprisingly vast array of pumping machinery. Therefore, this Phase I feasibilty study will provide the opportunity to investigate a variety of design approaches potentially capable of meeting the current RPV/UAV heavy fuel propulsion requirements. Inherent specific perfor- mance limitations of piston and turbine engines dictates scale reduction will demand greater design discipline relative to the physics that govern their performance. The preferred system concept incorporates a combination of innovative translations of rotary to reciprocating motion resulting in a compact design of high mechanical efficiency. High thermal efficiency will be achieved by the incorporation of low surface/volume geometry. The design makes extensive use of synergism.
* information listed above is at the time of submission.