Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Júlio César Gomes Santos"'
Autor:
Getúlio de Vasconcelos, Júlio César Gomes Santos, Jéssica Fernanda Azevedo, Viviane Teleginski Mazur, Daniele Cristina Chagas, Maurício Marlon Mazur
Publikováno v:
Engenharia Mecânica: Inovações Tecnológicas de Elevado Valor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bdd13241ad4fe707888a7953c1975ec
https://doi.org/10.22533/at.ed.8262109021
https://doi.org/10.22533/at.ed.8262109021
Autor:
Daniele Cristina Chagas, Júlio César Gomes Santos, Ana Claudia Costa de Oliveira, Getúlio de Vasconcelos, Jéssica Fernanda Azevedo, Viviane Teleginski
Publikováno v:
Materials Science Forum. 869:685-688
The high temperature environments where aeronautical turbine blades are exposed makes mandatory the use of ceramic coatings. A bond coat comprised by a MCrAlY alloy (M=Co, Ni) is necessary to match the blade metallic substrate with the ceramic, also
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e2a83afef1a77f3562fa5edeb78b42fd
https://doi.org/10.4028/www.scientific.net/msf.869.685
https://doi.org/10.4028/www.scientific.net/msf.869.685
Autor:
Júlio César Gomes Santos, Getúlio de Vasconcelos, Daniele Cristina Chagas, Viviane Teleginski, Ana Claudia Costa de Oliveira, Jéssica Fernanda Azevedo, Rudimar Riva
Publikováno v:
Surface and Coatings Technology. 260:251-259
article i nfo Ceramic coatings are employed to avoid the oxidation effect on turbine blade metallic substrate and as well as, increase turbine work temperature, improving its performance on metallic substrates to increase their lifetime. A bond coat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d0ec3cc271c5c6cde50217b61700a6e2
https://doi.org/10.1016/j.surfcoat.2014.06.076
https://doi.org/10.1016/j.surfcoat.2014.06.076
Autor:
Antunes Andre Da Silva, Jorge Otubo, Júlio César Gomes Santos, Leonardo Kyo Kabayama, Odair Doná Rigo, Afonso Paulo Monteiro Pinheiro
Publikováno v:
Materials Science Forum. 643:15-18
The rocket propellant ignition system uses electro-explosive device actuated by wire electrode. Those wires are usually made by Fe-Ni based alloy with controlled thermal expansion inserted into a ceramic feed-through and are connected to thin resisti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::723d5c256c1315bd980cc9b20dca4206
https://doi.org/10.4028/www.scientific.net/msf.643.15
https://doi.org/10.4028/www.scientific.net/msf.643.15