Research on the Fatigue Performance of TC6 Compressor Blade under the CCF Effect
This paper studied the influence of high and low combined fatigue (CCF) on compressor blade fatigue performance. We investigated the coupling between low cycle fatigue (LCF) loading from centrifugal force with high cycle fatigue (HCF) loading from vibration and determined the blade disc vibration fr...
Saved in:
Main Authors: | Zhang Yakui, Guo Shuxiang |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2018-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2018/7154784 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Performance analytic model and method for CCF multi-channel mechanism
by: YAN Jun-rong, et al.
Published: (2009-01-01) -
CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR
by: YIN ZhiPeng, et al.
Published: (2016-01-01) -
SIMULATION OF FATIGUE CRACK INITIATION LIFE OF TC4 TITANIUM ALLOY BASED ON ITS MESOSCOPIC PROPERTIES
by: JIANG Ze, et al.
Published: (2021-01-01) -
Transition Effect on the Flow Dynamics in a Compressor Blade Passage
by: Ryszard Szwaba, et al.
Published: (2021-01-01) -
Research on the law of engine compressor blade crack propagation based on operation data
by: SHI LiZhong, et al.
Published: (2024-06-01)