TURBINE ENGINE AND GAS TURBINE ENGINE ASSEMBLING METHOD

摘要

PROBLEM TO BE SOLVED: To provide an improved turbine engine structure on demand for improving efficiency and output which has greatly advanced the development of the turbine engine structure, the efficiency including both operating efficiency and manufacturing efficiency. SOLUTION: This gas turbine engine comprises a rotor group supported by a center shaft 28. A plurality of retainer segments 210A, 210B have a first face 214 for engaging with the rotor group and a second face 212 for engaging with the center shaft to transmit pre-compressive force from the center shaft 28 to the rotor group. COPYRIGHT: (C)2006,JPO&NCIPI