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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Bibliographic Details
Main Authors QIU DONGMEI, WANG GUORUN, PAN YIFEI
Format Patent
LanguageChinese
English
Published 28.09.2021
Subjects
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