Patent Number: 8,584,464

Title: Gas turbine engine assembly and method of assembling same

Abstract: A method for assembling a gas turbine engine assembly includes providing a core gas turbine engine including a high-pressure compressor, a combustor, and a high-pressure turbine, and coupling a low-pressure compressor between the core gas turbine engine and a motor such that the low-pressure compressor is driven only by the motor.

Inventors: Joshi; Narendra Digamber (Cincinnati, OH), Michael; Michael Eugene (Cincinnati, OH), Reale; Michael Joseph (Milford, OH)

Assignee: General Electric Company

International Classification: F02C 1/00 (20060101); F02C 6/04 (20060101)

Expiration Date: 1/19/12018