Gas compressor whole blade ring correction method

The invention provides a gas compressor whole blade ring correction method. The method includes the following steps of firstly, part assembling, secondly, part fixing, thirdly, tool locking, fourthly, heating performed in a furnace and fifthly correction completion. The thermal correction technology...

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Bibliographische Detailangaben
Hauptverfasser: AO BIN, SHI QIA, WAN LONG, GUO XIANGMIN, LI CHANG, WANG YUEXIN, QIN GUIFEN, LUO YUNFEN
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention provides a gas compressor whole blade ring correction method. The method includes the following steps of firstly, part assembling, secondly, part fixing, thirdly, tool locking, fourthly, heating performed in a furnace and fifthly correction completion. The thermal correction technology is adopted, the deformation requirement of a brazed gas compressor whole blade ring is met, and meanwhile operation is convenient, cost is low, and the quality of engine parts is guaranteed.