Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Geanina Laura Pintilei"'
Autor:
Geanina Laura, Pintilei1 laura_rares082008@yahoo.com, Abrudeanu, Marioara1, Corneliu, Munteanu2, Ionuț Vasile, Crîșmaru2, Mihaela, Vladu1, Iustin, Popa1
Publikováno v:
TEHNOMUS. 2015, p452-456. 5p.
Publikováno v:
Procedia Technology. 19:247-253
Usually equipments that work at low and cryogenic temperatures are made of stainless steel due to their good mechanical and anti corrosion properties. The best stainless steels for this kind of applications are the ones that present an austenitic mic
Autor:
Marioara Abrudeanu, Dragomir-Stanciu Daniel, Geanina Laura Pintilei, Corneliu Munteanu, Ionut Vasile Crismaru
Publikováno v:
Procedia Technology. 19:276-283
The behavior of the material subjected to thermal shock is influenced by its phase stability, its micro structural properties and its thermal expansion properties. This paper analysis the behavior of an 99,5% purity Al2O3 deposited on a Ti alloy subj
Autor:
Ionuț Vasile, Crîșmaru1 crismaru.ionut@yahoo.com, Geanina Laura, Pintilei1, Biniuc Carmen, Papatoiu1, Marius, Imbrea1, Sorin Claudiu, Iacob Strugariu1, Corneliu, Munteanu1
Publikováno v:
TEHNOMUS. 2013, p58-63. 6p.
Autor:
Ionuț Vasile, Crîșmaru1 crismaru.ionut@yahoo.com, Geanina Laura, Pintilei1, Lozneanu, Marian Vasile1, Constantin, Paulin1, Biniuc Carmen, Papatoiu1, Corneliu, Munteanu1
Publikováno v:
TEHNOMUS. 2013, p280-285. 6p.
Autor:
Carmen Biniuc Papatoiu, Sorin Iacob Strugaru, Corneliu Munteanu, Alexandru Bârcă, Geanina Laura Pintilei, Constantin Paulin
Publikováno v:
Advanced Materials Research. 837:705-710
This paper presents the results of dilatometry and DTA analyses performed on a Ni base super alloy sample on which a ZrO2/20%Y2O3 coating was deposited. The tests were done at similar temperatures as those present in a gas turbine engine at the inlet
Autor:
Sorin Iacob Strugaru, Corneliu Munteanu, Eduard Sebastian Bârcă, Valentin Nica, Geanina Laura Pintilei, Florin Brânza
Publikováno v:
Advanced Materials Research. 837:711-717
This paper presents a concept of thermal barrier coating used to prevent exfoliation and increase the maximum working temperature of a turbine engine. The coating consist of a ZrO2/20%Y2O3 ceramic layer and a NiCrAlY adherent layer, deposited by atmo