Multiaxial fatigue damage and reliability assessment of aero-engine compressor blades made of TC4 titanium alloy

2021 ◽  
pp. 107107
Author(s):  
Bingqiang Li ◽  
Honggen Zhou ◽  
Jinfeng Liu ◽  
Chao Kang
2010 ◽  
Vol 177 ◽  
pp. 338-341
Author(s):  
Ming Sheng Li ◽  
Yong Zhong Fan ◽  
Shu Juan Zhang

In this study, composite metastable (Ti0.49Al0.49Y0.02)N, (Ti0.44Al0.44Cr0.1Y0.02)N and (Ti0.34Al0.34Cr0.3Y0.02)N coatings were respectively deposited on a wrought martensite steel 1Cr11Ni2W2MoV for aero-engine compressor blades by arc ion plating technique with a pulse substrate bias. All the coatings have B1NaCl phase structure with a (220) preferred orientation and dense structures. The introduction of chromium into the coatings gave rise to a minute shrinkage of crystal lattice and a decrease of crystal size. Annealed at 800°C, Oxidation-resistance of the coatings improved with increased Cr content. But heat-treated at 900°C, the incorporation of Cr gave rise to obvious decrease of oxidation-resistance.


2012 ◽  
Vol 490-495 ◽  
pp. 2814-2818
Author(s):  
Xiao Qiang Shi ◽  
Shu Sheng Zhang ◽  
Shan Li ◽  
Rui Xue Ma

For improving currently the low manufacturing level and the long cycle of the production reparation period of aero-engine compressor blades, the rapid response production preparation system for compressor blades was proposed. Blade product line data was managed based on the process main model by the PDM platform to finish data sharing and integration. With the support of the process master model technology and the technical maturity, the cooperation of the process design and the process equipment design was achieved. Three subsystems about blade production were developed and integrated based on the PDM. It is proved that the system can improve the efficiency of the CNC processing and quality of compressor blades, meanwhile it can improve the utilization rate of CNC equipments, and excavate the potential of blade production lines.


2007 ◽  
Vol 546-549 ◽  
pp. 1789-1794 ◽  
Author(s):  
Ming Sheng Li ◽  
Chang Jie Feng ◽  
Fu Hui Wang ◽  
Wei Tao Wu

Composite metastable Ti0.5Al0.5N, Ti0.49Al0.49Y0.02N and Ti0.48Al0.48Y0.04N coatings were deposited on a wrought martensite steel 1Cr11Ni2W2MoV for aero-engine compressor blades by arc ion plating respectively all coatings possessed a dense surface and the same B1NaCl phase structure and the lattice parameter increased with increase of the incorporated element Y. Oxidation-resistance of (Ti,Al,Y)N coatings at 800 for up to 500 hr was investigated and the results showed that the introduction of yttrium into the coatings dramastically improved the oxidation-resistance of the coatings in air. The presence of Y in the nitride coatings suppresses the outer diffusion of Fe through the nitride coating. And the oxide of yttrium may segregate to the grain boundaries of oxides, suppressing the outward diffusion of metallic elements in coating and the inward diffusion of oxygen. Besides, the existence of adequate Y in the coatings is in favor of suppression of the growth of oxide crystals, formation layered oxide scale and decrease of compressive stress of oxidation.


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