Nested core gas turbine engine
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United States of America Patent
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Nov 18, 2003
Grant Date -
Dec 5, 2002
app pub date -
Sep 5, 2001
filing date -
Sep 5, 2000
priority date (Note) -
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Abstract
A gas turbine engine comprising a combustion chamber section, a turbine section, and a compressor section. The turbine section surrounds the combustion chamber and the compressor section surrounds the turbine section.
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