Aero-engine compressor rotor pin assembling tool and using method thereof

• Main Authors: ZHU ZHAOXIA, YE CAIMING, HE JIN, HUANG MAOLIN, LI WEN, XI GANG, LIU MAOLIN, HUANG JUNHUA, MU ZHENNAN, GUO HAOBANG
• Format: Patent
• Language: Chinese; English
• Published: 30.05.2023
• Subjects: HAND TOOLS; MANIPULATORS; PERFORMING OPERATIONS; PORTABLE POWER-DRIVEN TOOLS; TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FORFASTENING, CONNECTING, DISENGAGING OR HOLDING; TRANSPORTING

The invention relates to the technical field of air compressor rotor assembling, and discloses an aero-engine air compressor rotor pin assembling tool which comprises a handle and a hitting rod, the handle is provided with a through hollow inner cavity for the hitting rod to stretch in, and the through tail end of the hollow inner cavity of the handle is provided with a guide hole for a pin to be installed in. The end face of the guide hole in the handle is an inclined face with a dip angle which is matched with the outer circle surface of a compressor rotor. The beating rod comprises a force application end and a press-in end which are sequentially connected, the force application end is located outside the hollow inner cavity of the handle, and the end face of the press-in end makes contact with the pin and transmits force applied by the force application end to the pin; the length difference value of the central axis of the hollow inner cavity of the handle and the length of the press-in end of the beating