CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR
A type of aero engine compressor blade model was built based on finite element. Dynamics of the clamped constrained blade was obtained by modal simulation and the influence of centrifugal force on the vibration of blades was researched. And then,the modal test was carried out to validate the model a...
Saved in:
Main Authors: | YIN ZhiPeng, LI QuanTong, GAO XingWei, CHEN PengFei, TANG Ling |
---|---|
Format: | Article |
Language: | zho |
Published: |
Editorial Office of Journal of Mechanical Strength
2016-01-01
|
Series: | Jixie qiangdu |
Subjects: | |
Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2016.03.005 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration Behavior
by: Dirk Hagelstein, et al.
Published: (2000-01-01) -
On the Forced Response of Harmonically and Partially
Mistuned Bladed Disks. Part I: Harmonic Mistuning
by: Marc P. Mignolet, et al.
Published: (2000-01-01) -
ANALYSIS AND TEST OF COMBINED FATIGUE LOADING SYSTEM OF CERTAIN ENGINE FAN BLADE
by: TANG Ling, et al.
Published: (2018-01-01) -
On the Forced Response of Harmonically and Partially Mistuned
Bladed Disks. Part II: Partial Mistuning and Applications
by: Marc P. Mignolet, et al.
Published: (2000-01-01) -
Research on the law of engine compressor blade crack propagation based on operation data
by: SHI LiZhong, et al.
Published: (2024-06-01)