Design, fabrication and testing of ceramic-matrix composite turbine blisk

LIU Xiaochong; XU Youliang; LI Jian; LUO Xiao; GUO Xiaojun; HU Xiaoan; CAO Xueqiang; LI Longbiao; LIU Chidong; DONG Ning; LIU Yongsheng

doi:10.13801/j.cnki.fhclxb.20220407.001

Volume 40 Issue 3

Mar. 2023

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LIU Xiaochong, XU Youliang, LI Jian, et al. Design, fabrication and testing of ceramic-matrix composite turbine blisk[J]. Acta Materiae Compositae Sinica, 2023, 40(3): 1696-1706. doi: 10.13801/j.cnki.fhclxb.20220407.001

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LIU Xiaochong, XU Youliang, LI Jian, et al. Design, fabrication and testing of ceramic-matrix composite turbine blisk[J]. Acta Materiae Compositae Sinica, 2023, 40(3): 1696-1706. doi: 10.13801/j.cnki.fhclxb.20220407.001

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Design, fabrication and testing of ceramic-matrix composite turbine blisk

doi: 10.13801/j.cnki.fhclxb.20220407.001

1.
School of Materials Science and Engineering, Northwestern Polytechnical University, Xi′an 710072, China
2.
Hunan Aviation Powerplant Research Institute, Aero Engine Corporation of China, Zhuzhou 412000, China
3.
School of Aircraft Engineering, Nanchang Hangkong University, Nanchang 330063, China
4.
School of Materials Science and Engineering, Wuhan University of Technology, Wuhan 430070, China
5.
College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

Funds: Project Supported by the Major Research Plan of the National Natural Science Foundation of China (92060202); National Natural Science Foundation of China (52172100)

Received Date: 2022-03-07
Accepted Date: 2022-03-31
Rev Recd Date: 2022-03-25

Available Online: 2022-04-08

Publish Date: 2023-03-15

Abstract

Abstract

Turbine rotor is the key component of gas turbine engines. Design, fabrication, and experimental verification of SiC/SiC turbine blisk were investigated. The Spider Web Structure (SWS) SiC preform was used as the reinforcement in turbine blisk. The BN interphase and SiC matrix were deposited on the surface of the SWS SiC fiber preform, respectively. The SiC/SiC turbine blisk was machined by "on-line processing" to form a turbine bisk that meets the design requirements. The environmental barrier coatings (EBCs) were prepared on the surface of SiC/SiC turbine blisk using the atmospheric plasma spraying (APS) method. The CT scan was conducted to characterize the internal defects in SiC/SiC turbine blisk. The mechanical performance evaluation, over rotation test and engine bench test were performed, respectively. The maximum failure strength approached 300 MPa. During the over rotation test, when the rotating speed reached n=104166 r/min, the blade in the turbine blisk broke; and when the rotating speed reached n=108072 r/min, the disk in the turbine blisk broke. During the engine bench test, low cyclic fatigue of N=994 cyclic with maximum speed n_max=60000 r/min and N=100 cyclic with maximum speed n_max=70000 r/min were completed. On January 1, 2022, the SiC/SiC turbine blisk successfully completed the first flight test in Zhuzhou, which is also the first flight test of the domestic SiC/SiC rotor assembly platform and verified the feasibility of SiC/SiC turbine rotor application in gas turbine engines.
- SiC/SiC,
- turbine blisk,
- spider web structure (SWS),
- environmental barrier coatings (EBCs),
- over rotation test,
- engine bench test,
- gas turbine engines
Long Abstrsct
Innovation Points

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References(39)

References

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