Using method of tool for repairing aero-engine axial flow casing runner
The invention relates to a using method of a tool for repairing an aero-engine axial flow casing runner. The tool for repairing the aero-engine axial flow casing runner comprises a first protection ring matched with a second-stage stationary blade mounting groove, a second protection ring matched wi...
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Main Author | |
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Format | Patent |
Language | Chinese English |
Published |
18.08.2023
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to a using method of a tool for repairing an aero-engine axial flow casing runner. The tool for repairing the aero-engine axial flow casing runner comprises a first protection ring matched with a second-stage stationary blade mounting groove, a second protection ring matched with a third-stage stationary blade mounting groove, a spigot protection ring and a plurality of plugs matched with stationary blade mounting holes, the outer wall of the first protection ring is in small clearance fit with the inner wall of the second-stage stationary blade mounting groove, and the outer wall of the second protection ring is in small clearance fit with the inner wall of the third-stage stationary blade mounting groove. The outer wall of the second protection ring is in small clearance fit with the inner wall of a third-stage stationary blade mounting groove, the spigot protection ring is connected to a left-end spigot of the axial flow casing in a sleeving mode, and during assembling, the first prot |
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Bibliography: | Application Number: CN202310633458 |