Aero-engine blade tip clearance passive control device and aero-engine
The invention relates to an aero-engine blade tip clearance passive control device and an aero-engine. The aero-engine blade tip clearance passive control device comprises a high-temperature alloy ring, a honeycomb structure and a high-temperature shape memory alloy wire, and the honeycomb structure...
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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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