TURBINE ENGINE INCLUDING BALANCED LOW PRESSURE STAGE COUNT

摘要

A turbine engine (20) includes a compressor section (24) having a high pressure portion (52) and a low pressure portion (44) and a turbine section (28), having a low pressure portion (46) and a high pressure portion (54). A ratio of low pressure portion stages (132) to low pressure compressor portion stages (130) is less than or equal to 1.