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authorJoshua Drake <joshua.ellis.drake@gmail.com>2024-11-01 17:02:39 -0500
committerJoshua Drake <joshua.ellis.drake@gmail.com>2024-11-01 17:02:39 -0500
commitaa03b369272ec6d5b47600b72f8c673848f0860a (patch)
tree27009c1b62794961791ad8e6283497d92727af3a /background.tex
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@@ -41,6 +41,9 @@ Turboshaft style engines are most often used in helicopters, and are characteriz
\end{figure}
\section{Generator Theory}
\section{Battery Theory}
+\begin{equation}\label{battC}
+ I_{Battery}=\frac{V_{Battery}-V_{Supply}}{R_{Battery}}
+\end{equation}
\section{Turboelectric Theory}
NASA defines turboelectric systems as being at the least a turboshaft coupled to an electric generator, which power electric motors which then drive propellers. This configuration can be further categorized in accordance with whether the turbine engine drives a load directly.
These systems, refered to as "Partial Turbo Electric" \cite{nasa_prop_overview}, employ the use of either turbofans or turboprops in addition to being coupled to electric generators.