journal article·2024-05Open access

Hypergravity-exacerbated cracking in high-speed rotating 7075 aluminum blades

Yilin Jiao, Fafa Yang, Haoqi Niu, Lilin Xie, Yadi Zhai, Ang Li, Yanhui Chen

Abstract

On Earth, high-speed rotating blades and rotors experience hypergravity, which is mainly derived from centrifugal force. Aluminum alloys are widely used in high-speed rotating machines. In particular, 7075 aluminum has excellent properties, providing it with great potential for application in high-temperature rotating parts. In this work, the cracking behavior and microstructural evolution characteristics of high-speed rotating blades under different stresses were studied. A specifically designed instrument and blades with multiple necks were assembled, and the stress was tuned by adding weight to the blade tip. Each rotating blade cracked on its root neck, indicating that the gradient hypergravitational force decreased from the root to the tip. The degree of high-temperature cracking obviously increased with a sawtooth-like tip, but the degree of low-temperature cracking did not obviously increase with a smooth tip. A comparison under a constant uniaxial force required a greatly increased ultimate cracking strength that was approximately 10–18 times greater than that under hypergravitational force at the same temperature. Force analysis indicated that the coupling of hypergravitational forces in the normal direction and torsional forces in the tangential direction accelerated cracking. A uniaxial force caused grains to extend along the blade direction. However, a tangential force cut these extended grains to accelerate cracking and grain refining. In this study, real-world simulated service conditions for commercial alloys rotating at high speeds and a new understanding of the mechanical properties of alloys under various severe conditions were provided.
Source: openalex_inverted_index · Quality: baseline

Research context

OpenAlex topics: Aluminum Alloy Microstructure Properties · Microstructure and mechanical properties · Metallurgy and Material Forming

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (33)

Show source-provided references
1. Hypergravity experiments on multiphase media evolution10.1007/s11431-022-2125-x ↗
2. Hypergravity experiments: revolutionary methods for discovering multiphase evolution
3. Supergravity process for enriching and separating Ag from Sn-Ag–Zn melts10.1016/j.cep.2019.107591 ↗
4. Investigation of microgravity effect on solidification of medium-low-melting-point alloy by drop tube experiment10.1007/s11431-008-0128-3 ↗
5. Enrichment and separation behaviors of impurities from stripped copper wire with super-gravity fields10.1016/j.cep.2023.109483 ↗
6. Supergravity process for enriching and separating Ag from Sn–Ag–Zn melts10.1016/j.cep.2019.107591 ↗
7. Efficient separation of lead and antimony metals from the Pb-Sb alloy by super-gravity technology10.1016/j.jallcom.2019.07.211 ↗
8. Novel and efficient purification of scrap Al-Mg alloys using supergravity technology10.1016/j.wasman.2020.09.027 ↗
9. Cleaner approach to the recycling of metals in waste printed circuit boards by magnetic and gravity separation10.1016/j.jclepro.2019.119235 ↗
10. Fundamental research on recovering metals from hot-dip Zn-Al-Mg dross by supergravity separation10.1007/s42243-023-00989-3 ↗
11. Influence of super-gravity coefficient on spatial distribution of solidification structure in Al-14.5Si alloys10.1016/j.jmrt.2021.10.106 ↗
12. Alloy design for aircraft engines10.1038/nmat4709 ↗
13. Hypergravity suppressed thermal diffusion at the Cu-Sn couple interface10.1016/j.jallcom.2022.167231 ↗
14. Stress and deformation of rocket gas turbine disc under different loads using finite element modelling10.1016/j.jppr.2013.01.002 ↗
15. Stress analysis of rotating composite solid disc
16. Stress analysis of rotating composite solid disc
17. Thermo-mechanical modeling of a high pressure turbine blade of an airplane gas turbine engine10.1016/j.prostr.2016.02.026 ↗
18. Failure analysis of turbine disc of an aero engine10.1016/j.engfailanal.2004.12.028 ↗
19. Evaluation of service conditions of high pressure turbine blades made of DS Ni-base superalloy by artificial neural networks
20. ICME framework for damage assessment and remaining creep life prediction of in-service turbine blades manufactured with Ni-based superalloys10.1007/s40192-019-00161-4 ↗
21. Assessment of degradation equivalent operating time for aircraft gas turbine engines10.1017/aer.2019.153 ↗
22. Development of a super high efficiency motor with boron aluminum alloy rotor10.1016/j.proeng.2017.01.288 ↗
23. Analysis of the efficiency of an automotive alternator by replacing Mild steel into aluminum as a material for rotor10.1016/j.matpr.2020.06.439 ↗
24. Experimental study on process of precision forging of an aluminium-alloy rotor10.1016/j.jmatprotec.2005.06.009 ↗
25. Microstructure evolution and microhardness of TiAl based alloy blade by vacuum suction casting10.1016/j.vacuum.2019.02.028 ↗
26. Production issues in the manufacturing of TiAl turbine blades by investment casting10.1016/j.prostr.2020.04.012 ↗
27. A review of selective laser melting of aluminum alloys: processing, microstructure, property and developing trends10.1016/j.jmst.2018.09.004 ↗
28. Review of recent trends and developments in aluminium 7075 alloy and its metal matrix composites (MMCs) for aircraft applications10.1016/j.rineng.2023.101372 ↗
29. Effects of different initial states on dynamic tensile properties and microstructure of 7075 aluminum alloy10.1016/j.msea.2023.145939 ↗
30. Micro-structural evolution subjected to combined tension–torsion deformation for pure copper10.1016/j.msea.2014.04.083 ↗
31. Effect of microstructure on torsion properties of Ti–5Al–5Mo–5V–3Cr–1Zr alloy10.1016/j.msea.2016.11.049 ↗
32. Experimental study on pure titanium subjected to different combined tension and torsion deformation processes10.1016/j.msea.2016.10.106 ↗
33. Mode III and Mode I fatigue crack propagation behaviour under torsional loading10.1007/BF00542053 ↗