Investigation of casting–ceramic shell mold interface thermal resistance during solidification process of nickel based superalloy

D Szeliga, K Kubiak, W Ziaja, R Cygan… - … Thermal and Fluid …, 2017 - Elsevier
The study of thermal resistance (TR) at the casting-mold interface has been performed to
describe the solidification process aimed at the improvement of technology and the …

Rapid prototyping in manufacturing of core models of aircraft engine blades

P Rokicki, G Budzik, K Kubiak, J Bernaczek… - Aircraft Engineering …, 2014 - emerald.com
Purpose–The purpose of this paper is to present the advantages of computer-aided
design/rapid prototyping (CAD/RP) usage in designing and manufacturing of the core …

Modeling of directional solidification of columnar grain structure in CMSX-4 nickel-based superalloy castings

D Szeliga, K Kubiak, A Burbelko, M Motyka… - Journal of materials …, 2014 - Springer
The paper presents the analysis of numerical simulation of the Bridgman directional
solidification process performed on CMSX-4 rods. The numerical simulation was studied …

Effect of Y content on interface reaction and wettability between a nickel-base single crystal superalloy melt and ceramic mould

Y Zi, J Meng, C Zhang, Y Yang, Y Zhou… - Journal of Alloys and …, 2019 - Elsevier
In this paper, the effect of Y content on interface reaction and wettability between a nickel-
base single crystal supperalloy melt and ceramic mould were studied by means of sessile …

Assessing the condition of gas turbine rotor blades with the optoelectronic and thermographic methods

M Bogdan, J Błachnio, A Kułaszka, M Derlatka - Metals, 2019 - mdpi.com
Gas turbines and their blades in particular might be damaged in the course of the aviation
turbojet engine operation process. The degradation process of the blade microstructure is …

[PDF][PDF] Increased temperature impact on durability of gas turbine blades

J BłAchnio, M BogdAn, D Zasada - Eksploatacja i Niezawodność, 2017 - bibliotekanauki.pl
The paper presents the research results of a microstructure of the turbine rotor blades made
of nickel-based super alloys. The purpose of the research was to determine the high …

Interfacial reaction mechanism between ceramic mould and single crystal superalloy for manufacturing turbine blade

J Yao, L Dong, Z Wu, L Wang, B Shen, X Yang - Materials, 2022 - mdpi.com
Single crystal superalloys are the preferred materials for manufacturing turbine blades of
advanced aero-engines, due to their excellent high temperature comprehensive …

[PDF][PDF] Geometric accuracy of aircraft engine blade models constructed by means of the generative rapid prototyping methods FDM and SLA

G Budzik - Advances in Manufacturing Science and …, 2010 - advancesmst.prz.edu.pl
S umm ar y The article presents an analysis of the incremental model building process in the
RP methods (FDM and SLA) with regard to the accuracy of construction of aircraft engine …

[PDF][PDF] Functional properties of aluminide layer deposited on Inconel 713 LC Ni-based superalloy in the CVD process

M Yavorska, J Sieniawski… - Archives of Metallurgy and …, 2011 - bibliotekanauki.pl
In the paper there was established the influence of temperature and process time on the
functional properties of aluminide layer deposited on nickel based-Inconel 713 LC …

Analysis of causes of decohesion of a gas turbine blade made of EI 867‐WD alloy

J Błachnio - Aircraft Engineering and Aerospace Technology, 2011 - emerald.com
Purpose–The purpose of this paper is to present results of laboratory testing work on causes
of a service failure/damage to an aircraft turbojet's gas‐turbine blade made of the EI 867 …