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標題: Titlebook: Ceramic Coatings for High-Temperature Environments; From Thermal Barrier Amirhossein Pakseresht,Kamalan Kirubaharan Amirtha Book 2024 The E [打印本頁]

作者: 矜持    時間: 2025-3-21 20:01
書目名稱Ceramic Coatings for High-Temperature Environments影響因子(影響力)




書目名稱Ceramic Coatings for High-Temperature Environments影響因子(影響力)學科排名




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書目名稱Ceramic Coatings for High-Temperature Environments網(wǎng)絡公開度學科排名




書目名稱Ceramic Coatings for High-Temperature Environments被引頻次




書目名稱Ceramic Coatings for High-Temperature Environments被引頻次學科排名




書目名稱Ceramic Coatings for High-Temperature Environments年度引用




書目名稱Ceramic Coatings for High-Temperature Environments年度引用學科排名




書目名稱Ceramic Coatings for High-Temperature Environments讀者反饋




書目名稱Ceramic Coatings for High-Temperature Environments讀者反饋學科排名





作者: 分期付款    時間: 2025-3-21 22:36

作者: Excise    時間: 2025-3-22 04:22

作者: 羞辱    時間: 2025-3-22 08:01
Trends and Perspectives in Mitigating CMAS Infiltration in Thermal Barrier Coatinggnesium-aluminosilicate (CMAS) damage the TBC and reduce its durability. After presenting the SPS process, its application to thermal barrier coatings and industrialization challenges of the process, the chapter discusses the effects of CMAS infiltration on TBC and the methodologies used to characte
作者: 發(fā)酵    時間: 2025-3-22 09:37

作者: 前奏曲    時間: 2025-3-22 16:53
Zirconia-Based Thermal Barrier Coatings Systems for Aero-Industry of the structure characteristics of obtained ceramic materials, emphasizing the need for reduced thermal conductivity as well as the critical need to predict the life span. This chapter will provide a short review on the present status of the research of ceramics composites coatings used as thermal
作者: 前奏曲    時間: 2025-3-22 20:26
Multilayered Coatings by Thermal Spray for High-Temperature Applicationsttention on three aspects for the enhancement of protective coatings: i) the optimization of multilayered TBC/EBC architecture, ii) assessment of the damage of TBC/EBC subjected to thermal cycling and molten silicates attack, and iii) exploration of candidate materials for the fabrication of novel c
作者: expunge    時間: 2025-3-23 01:04

作者: Bucket    時間: 2025-3-23 01:45
Environmental Barrier Coatings (EBCs) for Silicon-Based Ceramics and Compositesnding strength with CMCs can prolong the service life of EBCs. Therefore, EBCs are usually composed of three layers: the bonding layer, interlayer, and topcoat. Nowadays, EBCs have promoted to the third generation. The topcoat of EBCs in direct contact with the environment is crucial. Rare-earth sil
作者: 嘮叨    時間: 2025-3-23 07:18

作者: inconceivable    時間: 2025-3-23 10:18

作者: Lament    時間: 2025-3-23 16:55

作者: Alienated    時間: 2025-3-23 21:29

作者: Blood-Clot    時間: 2025-3-23 23:42

作者: 才能    時間: 2025-3-24 05:34
High-Temperature W/ZrC Composite Coatingse. The reaction of zirconium carbide with oxygen can enhance oxidation resistance through the formation of ZrO. layer which can be melted at a higher temperature (2677?℃), covering the surface to avoid further oxidation of substrates. Several methods have been reported to deposit the composite on co
作者: 強制性    時間: 2025-3-24 06:52
Book 2024ting methods along with the properties and applications of emerging high entropy UHTCs...With contributions from international researchers active in the field, this edited book features the most recent and up-to-date literature references for a broad readership consisting of academic and industrial
作者: 烤架    時間: 2025-3-24 11:03
https://doi.org/10.1007/978-3-658-05444-1industrial TBC manufacturing, under a large variety of operating environments. During the last decades, many ceramic oxides with potential enhanced properties were investigated and fabricated TBCs were tested at laboratory scale. However, prolonged high-temperature service requires further validatio
作者: 性上癮    時間: 2025-3-24 17:58
Summary, Conclusion and Outlook,gnesium-aluminosilicate (CMAS) damage the TBC and reduce its durability. After presenting the SPS process, its application to thermal barrier coatings and industrialization challenges of the process, the chapter discusses the effects of CMAS infiltration on TBC and the methodologies used to characte
作者: Overthrow    時間: 2025-3-24 23:05
Mitgliederprojekte in der Automobilindustriee alone for TBC top coat because of its low coefficient of thermal elongation compared with bond coat and substrate. However, Al.O. coating together with other TBC materials on the metal substrate using different methods and designs can improve the mechanical and thermal properties of TBC while prov
作者: TATE    時間: 2025-3-25 01:04
Anlage der empirischen Untersuchung of the structure characteristics of obtained ceramic materials, emphasizing the need for reduced thermal conductivity as well as the critical need to predict the life span. This chapter will provide a short review on the present status of the research of ceramics composites coatings used as thermal
作者: aqueduct    時間: 2025-3-25 06:42
Anlage der empirischen Untersuchungttention on three aspects for the enhancement of protective coatings: i) the optimization of multilayered TBC/EBC architecture, ii) assessment of the damage of TBC/EBC subjected to thermal cycling and molten silicates attack, and iii) exploration of candidate materials for the fabrication of novel c
作者: extemporaneous    時間: 2025-3-25 11:31

作者: 浮雕寶石    時間: 2025-3-25 12:19

作者: CHOP    時間: 2025-3-25 16:44

作者: 甜得發(fā)膩    時間: 2025-3-25 21:15

作者: Maximize    時間: 2025-3-26 01:51
Distributed Organizing in Practice of C/C materials for protecting aerospace structures from thermal shock in re-entry missions. In particular, advanced coating treatments using ceramic-based (SiC-Al.O.-ZrO.) refractory varnishes, even reinforced by ceramic filling nanoparticles (SiO. powder), are analyzed by space environment simul
作者: arousal    時間: 2025-3-26 07:12
https://doi.org/10.1007/978-3-658-06155-5-temperature ceramic coatings and fibre-reinforced ultra-high-temperature ceramic materials. UHTC coatings are extremely useful as thermal shock absorbers, surface seals and leak minimisers. The carbothermal reduction method is the oldest method employed for the synthesis of UHTCs. However, many oth
作者: Vaginismus    時間: 2025-3-26 12:29
https://doi.org/10.1007/978-3-658-06441-9top of it to protect the substrate against oxidation at ultra-high temperatures. HfO. also has a very high melting point which further protects the underlying coating and substrate. These characteristics make hafnium carbide very promising as an anti-ablation coating for ultra-high-temperature appli
作者: 發(fā)源    時間: 2025-3-26 14:06

作者: 上下倒置    時間: 2025-3-26 17:21

作者: 統(tǒng)治人類    時間: 2025-3-26 23:20

作者: 言外之意    時間: 2025-3-27 02:37

作者: KIN    時間: 2025-3-27 08:11

作者: 宇宙你    時間: 2025-3-27 10:13

作者: Flounder    時間: 2025-3-27 17:01

作者: defuse    時間: 2025-3-27 20:47
Summary, Conclusion and Outlook,production costs while improving the efficiency of aero-engines. One way to achieve this is by developing a thermal barrier coating (TBC) on the hottest components of the turbine to increase its inlet temperature. Different methods are used to deposit TBC, including air plasma spray (APS) and electr
作者: EVEN    時間: 2025-3-27 22:59
A Model of External Knowledge Absorption,hereby improving thermal efficiency and extending its service life. The selection of TBCs materials is crucial including high melting point, low thermal conductivity, corrosion resistance, thermal expansion coefficient, substrate matching, and no phase transformation or sintering during service. Ytt
作者: 使更活躍    時間: 2025-3-28 02:55
Mitgliederprojekte in der Automobilindustriece expectation of gas turbine engines for an economical and environmental aspect, researchers focus on the development of materials which can tolerate high temperatures, high stress, and the evolution of ceramic coatings. In this respect, thermal barrier coatings (TBC) play a major role in protectin
作者: Bravado    時間: 2025-3-28 09:08

作者: Focus-Words    時間: 2025-3-28 12:58

作者: 正式演說    時間: 2025-3-28 16:56

作者: LIEN    時間: 2025-3-28 22:47
https://doi.org/10.1007/978-3-658-06123-4t mechanical properties at elevated temperatures. However, corrosive gas and foreign particles in the service environment, such as water vapor/oxygen and some silicate dusts may attack silicon-based ceramics, which finally result in lifetime recession and sometimes severe failure. Therefore, Environ
作者: 代理人    時間: 2025-3-29 00:32
https://doi.org/10.1007/978-3-658-06123-4eneration gas-turbine engines. However, hot steam and volcanic ash degrade the mechanical properties of silicon carbide. Environmental barrier coatings (EBCs) play an important role in mitigating corrosion under the harsh operating conditions required for next-generation turbines. In addition to cor
作者: 不能仁慈    時間: 2025-3-29 04:27
https://doi.org/10.1007/978-3-658-06123-4igh-temperature application in aerospace propulsion systems. However, this composite material is susceptible to high-temperature oxidation in oxygen-containing environment. Coating with Si-based ceramics or ultra-high temperature ceramic (UHTC) materials is proven to be an efficient method for impro
作者: 一再遛    時間: 2025-3-29 11:16

作者: ostensible    時間: 2025-3-29 12:06
Distributed Organizing in Practicespace industry for thermal protection systems (TPS) to face the dramatic thermo-mechanical stress suffered by spacecraft structures during re-entry into Earth atmosphere. A branch of current aerospace research is focused in finding ever more effective coating solutions to preserve CMCs from oxidatio
作者: gorgeous    時間: 2025-3-29 18:07
https://doi.org/10.1007/978-3-658-06155-5nd hypersonic concepts and the related applications have resulted in the search for new categories of materials capable of withstanding very high temperature. The borides, nitrides and carbides of various transition metals can be employed for synthesising ultra-high-temperature ceramic (UHTC) coatin
作者: prick-test    時間: 2025-3-29 20:50

作者: consent    時間: 2025-3-30 02:45

作者: 打火石    時間: 2025-3-30 06:22

作者: 牽連    時間: 2025-3-30 09:52
Trends and Perspectives in Mitigating CMAS Infiltration in Thermal Barrier Coatingproduction costs while improving the efficiency of aero-engines. One way to achieve this is by developing a thermal barrier coating (TBC) on the hottest components of the turbine to increase its inlet temperature. Different methods are used to deposit TBC, including air plasma spray (APS) and electr
作者: 對待    時間: 2025-3-30 16:08

作者: 刺激    時間: 2025-3-30 19:35





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