標(biāo)題: Titlebook: Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components; Xiaochong Liu,Longbiao Li Book 2024 The Editor(s) (if a [打印本頁(yè)] 作者: Systole 時(shí)間: 2025-3-21 19:04
書(shū)目名稱(chēng)Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components影響因子(影響力)
書(shū)目名稱(chēng)Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components影響因子(影響力)學(xué)科排名
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書(shū)目名稱(chēng)Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components被引頻次
書(shū)目名稱(chēng)Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components被引頻次學(xué)科排名
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書(shū)目名稱(chēng)Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components讀者反饋學(xué)科排名
作者: Archipelago 時(shí)間: 2025-3-21 23:49 作者: Organization 時(shí)間: 2025-3-22 00:41
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.作者: 的事物 時(shí)間: 2025-3-22 05:15
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,作者: 察覺(jué) 時(shí)間: 2025-3-22 09:41
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.作者: 確保 時(shí)間: 2025-3-22 15:24 作者: 確保 時(shí)間: 2025-3-22 19:25
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,作者: Gobble 時(shí)間: 2025-3-22 21:44
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作者: Cloudburst 時(shí)間: 2025-3-23 04:26
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作者: Ischemic-Stroke 時(shí)間: 2025-3-23 07:01 作者: 載貨清單 時(shí)間: 2025-3-23 12:16 作者: Pelvic-Floor 時(shí)間: 2025-3-23 17:54
High-Temperature Mechanical Properties of Ceramic-Matrix Composites, interlaminar shear strength, in-plane shear strength, flexural strength, cyclic fatigue lifetime, and creep life are obtained from experimental data. The high-temperature mechanical properties can support the engineers to better design CMCs hot-section components.作者: 慢跑鞋 時(shí)間: 2025-3-23 19:24 作者: LOPE 時(shí)間: 2025-3-24 01:34 作者: Accessible 時(shí)間: 2025-3-24 03:46
2662-9305 aeroengines were also introduced. The book can better help the engineering designers understand the methods used in design and testing of CMC components.978-981-97-6111-1978-981-97-6109-8Series ISSN 2662-9305 Series E-ISSN 2662-9313 作者: 多嘴 時(shí)間: 2025-3-24 08:24
Family Therapy: In and Out of SYNCwere conducted to investigate the damage mechanisms and failure modes. During thermal shock tests, the surface temperature field of the SiC/SiC guide vane was analyzed. The damage characteristics of the single/twin turbine guide vane after experiencing different thermal shocks were discussed.作者: antenna 時(shí)間: 2025-3-24 10:45
Design, Fabrication and Testing of CMC High-Pressure Turbine Guide Vane,were conducted to investigate the damage mechanisms and failure modes. During thermal shock tests, the surface temperature field of the SiC/SiC guide vane was analyzed. The damage characteristics of the single/twin turbine guide vane after experiencing different thermal shocks were discussed.作者: amyloid 時(shí)間: 2025-3-24 14:50
Book 2024gines. The book focuses on the design, fabrication and testing of different CMC components, e.g., turbine guide vanes, combustor liner, and turbine blisk, etc. The high-temperature mechanical properties, and performance requirements of the aeroengines were also introduced. The book can better help t作者: narcissism 時(shí)間: 2025-3-24 22:15 作者: grounded 時(shí)間: 2025-3-25 01:49
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,作者: 音樂(lè)會(huì) 時(shí)間: 2025-3-25 04:41 作者: cumulative 時(shí)間: 2025-3-25 08:29 作者: 沒(méi)有希望 時(shí)間: 2025-3-25 13:42
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 dimensi作者: Peak-Bone-Mass 時(shí)間: 2025-3-25 16:22
Xiaochong Liu,Longbiao LiFocuses on the design, fabrication and testing of different CMC components in aeroengine.Introduces high-temperature mechanical properties and performance requirements of aeroengine.Helps engineering 作者: Chemotherapy 時(shí)間: 2025-3-25 21:15 作者: 皮薩 時(shí)間: 2025-3-26 02:39 作者: GIST 時(shí)間: 2025-3-26 07:28
Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components978-981-97-6109-8Series ISSN 2662-9305 Series E-ISSN 2662-9313 作者: 褻瀆 時(shí)間: 2025-3-26 11:42 作者: 思想流動(dòng) 時(shí)間: 2025-3-26 15:10
https://doi.org/10.1007/978-981-97-6109-8Ceramic-Matrix Composites (CMCs); Hot-Section Components; Turbine Guide Vanes; Combustor Liner; Turbine 作者: 松緊帶 時(shí)間: 2025-3-26 18:46 作者: mydriatic 時(shí)間: 2025-3-26 21:43
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