Invention Application
US20160024958A1 GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE 审中-公开
燃气涡轮发动机,低压低压涡轮

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
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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