Method and tool structure for disassembling interference fit structure of turbine rotor

The invention belongs to the technical field of disassembling tools of gas turbine engines, and particularly relates to a method and tool structure for disassembling an interference fit structure of a turbine rotor. The tool structure comprises a hard cushion piece, an arc-shaped abutting piece and...

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Hauptverfasser: ZHOU JIANGFENG, ZHAO FENGJU, CAI YU, WANG HAILIN, DU ZHINENG, MAO CHUNPING, TAO SIYI, CAI PENG, XU SHIHUI, WANG MING
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creator ZHOU JIANGFENG
ZHAO FENGJU
CAI YU
WANG HAILIN
DU ZHINENG
MAO CHUNPING
TAO SIYI
CAI PENG
XU SHIHUI
WANG MING
description The invention belongs to the technical field of disassembling tools of gas turbine engines, and particularly relates to a method and tool structure for disassembling an interference fit structure of a turbine rotor. The tool structure comprises a hard cushion piece, an arc-shaped abutting piece and an ejection screw. The flange part of the arc-shaped abutting piece can abut against the outer edge of the shaft neck disc part of the turbine shaft. The ejection screw can abut against the front cushion face of the hard cushion piece. A flange plate part is arranged on the front side of the disc face of the turbine disc, and the flange plate back groove is formed between the flange plate part and the disc face of the turbine disc. The ejection screw is in threaded fit with the arc-shaped abutting piece and can push the arc-shaped abutting piece away from the hard cushion piece. According to the scheme, the tool structure and the disassembling method have the advantages of being simple, good in manufacturability, l
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subjects HAND TOOLS
MANIPULATORS
PERFORMING OPERATIONS
PORTABLE POWER-DRIVEN TOOLS
TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FORFASTENING, CONNECTING, DISENGAGING OR HOLDING
TRANSPORTING
title Method and tool structure for disassembling interference fit structure of turbine rotor
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