METHOD OF BALANCING A SPOOL OF A GAS TURBINE ENGINE
A method of balancing a spool of a gas turbine engine, the spool including a forward rotor assembly and an aft rotor assembly separated by a spacer, the method comprising: balancing the forward rotor assembly and the aft rotor assembly independently from one another using conventional balancing tech...
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Format: | Patent |
Sprache: | eng ; fre |
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