Surge elimination control method for aero-engine
The invention relates to the field of aero-engines, in particular to a surge elimination control method for an aero-engine. The method comprises the steps: cutting of oil supply of a main combustion chamber, and quitting surge elimination; designing ignition oil supply control , wherein the engine i...
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Main Authors | , , , , , , |
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Format | Patent |
Language | Chinese English |
Published |
28.09.2021
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Subjects | |
Online Access | Get full text |
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