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مکانیک::
توبورشارژری
Liquid Cooled Turbocharged Propulsion System for
This paper provides a technical assessment of a liquid cooled turbocharged, reciprocating engine concept capable of meeting the requirements for a HALE vehicle.
A properly designed spark ignition engine with a two or three stage series turbocharger system utilizing state-of-the-art aerodynamic design can meet the challenges presented at these altitudes.
A version of the turbocharged spark ignition engine is capable of providing high thermal efficiency with the least BSAC and minimum turbomachinery weight.
A turbocharged spark ignition internal combustion engine such as the Voyager 200 or 300 series engine operating on aviation gasoline offers an efficient propulsion system strategy for high altitude long endurance flight.
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