Corrosion prevention and control program are vital for the continued airworthiness of aging aircraft. 摘要腐性防護與控制方案是確保老齡飛機持續適航性的基本結構維護方案。
With increasing the heat-treatment temperature, the adhesive strength and corrosion resistance of the films declined. 熱處理溫度進(jìn)一步增加，鍍層的結合強度下降，耐蝕性變化不大。
Zinc based alloy electrodeposits have been emphasized for their excellent corrosion resistance. 鋅基合金電鍍層由于具有優(yōu)良的耐蝕性而受到人們的關(guān)注。
