University of Dayton eCommons Honors Theses University Honors Program 5-2017 Design of an Opposed-piston, Opposed-stroke Diesel Engine for Use in Utility Aircraft Luke Kozal University of Dayton Follow this and additional works at: https://ecommons.udayton.edu/uhp_theses Part of the Aerospace Engineering Commons, and the Mechanical Engineering Commons eCommons Citation Kozal, Luke, "Design of an Opposed-piston, Opposed-stroke Diesel Engine for Use in Utility Aircraft" (2017). Honors Theses. 113. https://ecommons.udayton.edu/uhp_theses/113 This Honors Thesis is brought to you for free and open access by the University Honors Program at eCommons. It has been accepted for inclusion in Honors Theses by an authorized administrator of eCommons. For more information, please contact
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[email protected]. Design of an Opposed-piston, Opposed-stroke Diesel Engine for Use in Utility Aircraft Honors Thesis Luke Kozal Department: Mechanical Engineering Advisors: Andrew Murray, Ph.D. David Myszka, Ph.D. Paul Litke, AFRL/RQTC May 2017 Design of an Opposed-piston, Opposed-stroke Diesel Engine for Use in Utility Aircraft Luke Kozal Department: Mechanical Engineering Advisor: Andrew Murray, Ph.D. David Myszka, Ph.D. Paul Litke, AFRL/RQTC May 2017 Abstract The objective of this thesis was to determine the feasibility of using an opposed-piston, opposed-stroke, diesel engine in utility aircraft. Utility aircraft are aircraft that have a maximal takeoff weight of 12,500lbs. These aircraft are often used for transportation of cargo and other goods. In order to handle that weight, many of the aircraft are powered by turboprop engines. Turboprop engines are a style of jet engine with power capabilities ranging from 500 to several thousand horsepower (hp).