Corrosion impairment experimental study of aluminum alloy LY11 propellers in a certain airplane
|更新时间:2026-07-07
|
Corrosion impairment experimental study of aluminum alloy LY11 propellers in a certain airplane
Vol. 25, Issue 2, (2010)
作者机构:
1. 北京航空航天大学 能源与动力工程学院,北京,100191
2. 中国人民解放军海军潜艇学院 防救指挥与工程教研室,青岛,266071
作者简介:
基金信息:
DOI:
CLC:
Published:2010
稿件说明:
移动端阅览
GU Yuan, SHI Duo-qi, YANG Xiao-guang, et al. Corrosion impairment experimental study of aluminum alloy LY11 propellers in a certain airplane[J]. 2010, 25(2).
DOI:
GU Yuan, SHI Duo-qi, YANG Xiao-guang, et al. Corrosion impairment experimental study of aluminum alloy LY11 propellers in a certain airplane[J]. 2010, 25(2).DOI:
Corrosion impairment experimental study of aluminum alloy LY11 propellers in a certain airplane
The test of simulation part of a propeller of airplane at different rust corrosion impairment conditions on the experiment machine and electromagnetic table was conducted
whilst the rule of impairment surface ratio A changes with low-cycle loading N
and the change rule of vibration frequency in line with the ratio of corrosion impairment depth
corrosion length and corrosion impairment area were given.The experiment shows that
when the loads and the temperature are the same
the property of material
shot-peen process and the operating environment are impartment factors for corrosion impairment of propellers;and the damnification area A and damnification depth H have more influence on the vibration frequency of propellers of airplane.The most limit depth ratio is 0.14
and the most limit damnification depth of simulation part is 0.7mm.The ratio of damnification area is 0.015
and the most limit damnification area of simulation part is 3.006mm2.