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AbstractIn this chapter, the design, fabrication and testing of CMC turbine blisk were investigated. The service performance analysis of the turbine blisk was at first analyzed. The spider web structure (SWS) fiber preform was adopted as the reinforcement elements of the turbine blisk. The BN interphase and SiC matrix were deposited on the SWS fiber preform, and during the fabrication, the on-line machining were conducted to control the shape and dimension of the blisk. The environmental barrier coatings (EBCs) were prepared on the surface of the SiC/SiC turbine blisk using the atmospheric plasma spraying (APS) method. The XCT scan was conducted to characterize the internal defects in the SiC/SiC turbine blisk. The mechanical performance evaluation, over rotation test and engine bench test were performed, respectively. Finally, the SiC/SiC turbine blisk was installed on an aircraft and completed the first flight testing, which verified the feasibility of the SiC/SiC turbine rotor for gas turbine engine application and accumulated valuable experience for the subsequent development of CMC hot-section components. ReferencesBhat BN (2018) Aerospace materials and applications. American Institute of Aeronautics and Astronautics Google Scholar Cranford SW, Tarakanova A, Pugno NM et al (2012) Nonlinear material behaviour of spider silk yields robust webs. Nature 482(7383):72–76CAS PubMed Google Scholar Freeman TJ, Engel TZ (2019) Turbine blisk including ceramic matrix composite blades and methods of manufacture. 10280768B2, US Google Scholar Li L (2020) Interfaces of ceramic-matrix composites. Design, characterization and damage effects. Wiley-VCH, Weinheim, Germany Google Scholar Liu X, Xu Y, Guo X, Luo X, Li L, Zeng Y, Liu C (2022) Fabrication and testing of spider web structure SiC/SiC turbine blisk. J Chin Ceram Soc 50(8):2205–2211CAS Google Scholar Liu X, Xu Y, Li J, Luo X, Guo X, Hu X, Cao X, Li L, Liu C, Dong N, Liu Y (2023) Design, fabrication and testing of ceramic-matrix composite turbine blisk. Acta Materiae Compositae Sinica 40:1702–1712 Google Scholar Nozhnitsky YA (2018) The problem of ensuring reliability of gas turbine engines. IOP Conf Ser: Mater Sci Eng 302:012082 Google Scholar Ogawa A, Hashimoto R, Zhou F (2001) Rotational test of C/C blisk rotors. In: The 13th international conference on composite materials. Beijing, China. Google Scholar Download references Author informationAuthors and AffiliationsSchool of Materials Science and Engineering, Northwestern Polytechnical University, Xi’an, Shaanxi, ChinaXiaochong LiuCollege of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, ChinaLongbiao LiAuthorsXiaochong LiuYou can also search for this author in PubMed Google
