GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
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United States of America Patent
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app pub date -
Oct 1, 2015
filing date -
Jun 2, 2008
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Abandoned
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Abstract
A gas turbine engine according to an example of the present disclosure includes, among other things, a fan section, a low spool that includes a low pressure compressor section, the low pressure compressor section including three (3) or more stages, and a high spool including a high pressure compressor section. The high pressure compressor section includes between eight to thirteen (8-13) stages. A gear train is defined along an engine axis. The low spool is operable to drive the fan section through the gear train.
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