Foreign Object Damage to Fan Rotor B

Foreign Object Damage to Fan Rotor Blades of Aeroengine Part Ⅰ: Experimental Study of Bird Impact

The conditions of experiment for bird impact to blades have been improved. The experiment of bird impact to the fan rotor blades of an aeroengine is carried out. Through analyzing the transient state response of blades impacted by bird and the change of blade profile before and after the impact, the anti-bird impact performance of blades in the first fan rotor is verified. The basis of anti-foreign object damage design for the fan rotor blades of an aeroengine is provided.

作 者： Guan Yupu Zhao Zhenhua Chen Wei Gao Deping   作者单位： College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China  刊 名： 中国航空学报（英文版）  ISTIC 英文刊名： CHINESE JOURNAL OF AERONAUTICS  年，卷(期)： 2007 20(5)  分类号： V2  关键词： aerospace propulsion system   bird impact experiment   fan rotor blade   transient response  

【Foreign Object Damage to Fan Rotor B】相关文章：

Welcome the foreign festivals05-04

Simulation Analysis of Indoor Gas Explosion Damage04-27

The reconstruction of diffractive object digital hologram at a short distance04-27

Fever of Foreign Language Training Schools05-04

THE PLATFORM FOR GUANGDONG FOREIGN-INVESTED ENTERPRISES04-26

Damage and Seismic Intensity in the Meizoseismal Region of the Ms 8.0 Wenchuan Earthquake,Sichuan, China04-27

b2b推广活动方案09-27

Generation of Hydroxyl Radicals and Its Relation to Cellular Oxidative Damage in Plants Subjected to Water Stress04-27

拼音b的教案01-05

B级我最大梅赛德斯-奔驰B-Class04-27