INTEGRATED TAIL CONE AND MOUNTED GENERATOR
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United States of America Patent
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Issued Date -
Sep 17, 2020
app pub date -
Mar 15, 2019
filing date -
Mar 15, 2019
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Abstract
A gas turbine engine including: a tail cone; a low pressure compressor; a low pressure turbine; a low speed spool interconnecting the low pressure compressor and the low pressure turbine; an electric generator located within the tail cone, the electric generator being operably connected to the low speed spool; a structural support housing at least partially enclosing the electric generator, the structural support housing being located within the tail cone; and a mounting system located within the tail cone between the structural support housing and the tail cone, wherein the mounting system attaches the tail cone to the structural support housing.
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