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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Format: | Patent |
Sprache: | chi ; eng |
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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. |
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