Systole
发表于 2025-3-21 19:04:22
书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0284582<br><br> <br><br>书目名称Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0284582<br><br> <br><br>
Archipelago
发表于 2025-3-21 23:49:52
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Organization
发表于 2025-3-22 00:41:57
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.
的事物
发表于 2025-3-22 05:15:44
Design, Fabrication and Testing of CMC Combustor Liner,Ra = 0.3~0.5. After the inner and outer liners and other components have been densified and processed, the SiC rivets are used for on-line riveting, which achieves a connection result equivalent to “metal riveting” after CVI-SiC deposition, improves the ability of components to maintain the profile,
察觉
发表于 2025-3-22 09:41:22
Design, Fabrication and Testing of CMC Turbine Blisk, 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.
确保
发表于 2025-3-22 15:24:30
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确保
发表于 2025-3-22 19:25:56
High-Temperature Mechanical Properties of Ceramic-Matrix Composites,forms, i.e., three-dimensional four-directional (3D4D) braided, two-dimensional plain-woven (2DPW) and stain woven (2DSW) lamination, are investigated at elevated temperature of 1400 °C. The high-temperature mechanical properties of SiC/SiC composites, e.g., tensile strength, compressional strength,
Gobble
发表于 2025-3-22 21:44:21
Design, Fabrication and Testing of CMC High-Pressure Turbine Guide Vane,nalysis of the turbine guide vane was at first analyzed. The SiC/SiC high-pressure turbine single/twin guide vanes were fabricated using the chemical vapor infiltration (CVI) method. Thermal shock experiments of SiC/SiC high-pressure turbine guide vanes were carried out on the third-generation turbi
Cloudburst
发表于 2025-3-23 04:26:24
Design, Fabrication and Testing of CMC Combustor Liner, was at first analyzed. The SiC/SiC combustor liner with the dimension of 296.48 mm (maximum diameter of outer liner) × 149.85 mm (minimum diameter of inner liner) × 100.46 mm (height), a wall thickness of 3–10 mm (including splicing structure) was fabricated using the CVI process. The surface of th
Ischemic-Stroke
发表于 2025-3-23 07:01:07
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