Simulation of Technology for the Production of Axisymmetric Parts for Gas Turbine Engines Made of Heat Resistant Alloys by Means of Reeling under Superplastic Conditions

2020 ◽  
Vol 49 (2) ◽  
pp. 150-158
Author(s):  
R. Yu. Sukhorukov
Keyword(s):  
Gas Turbine ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Heat Resistant

scholarly journals SELECTION OF TOOL HARD ALLOY FOR PROCESSING PARTS OF GAS TURBINE ENGINES

2018 ◽  
pp. 89-93
Author(s):  
E. V. Artamonov ◽  
A. M. Tveryakov ◽  
A. S. Shtin
Keyword(s):  
Hard Alloy ◽  
Gas Turbine ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Heat Resistant ◽  
Materials Used ◽  
Selection Of

The article reports a brief overview of the choice of tool hard alloy for processing heat-resistant materials used for the manufacturing of parts of gas turbine engines DR-59, J-59, and DG-90.

Calculation of temperature fields in the zone of the transverse edge of the drill

2021 ◽  
pp. 79-84
Author(s):  
Keyword(s):  
Gas Turbine ◽  
Temperature Fields ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Heat Resistant ◽  
Edge Temperature ◽  
Hole Machining

The wear of the transverse edge of the drill, the features of the drill web and the calculation determination of the temperature fields in the zone of its operation are investigated. Dependences are obtained for determining the total contact temperatures on the front and rear surfaces of the half-web. The results were used to create CAD for blade hole machining modes with application to the processing of heat-resistant materials of gas turbine engines. Keywords: hole, blade processing, drilling, transverse edge, temperature fields. [email protected]

Preparation, Structure, and Properties of Ni3Al and NiAl Light Powder Alloys for Aerospace

2007 ◽  
Vol 534-536 ◽  
pp. 1585-1588 ◽  
Author(s):  
K.B. Povarova ◽  
O.A. Skachkov
Keyword(s):  
Gas Turbine ◽  
New Technology ◽  
Turbine Engines ◽  
Heat Sources ◽  
Gas Turbine Engines ◽  
Combustion Chambers ◽  
Term Operation ◽  
Heat Resistant ◽  
Turbine Installation

New light super-heat-resistant powder Ni3Al and NiAl-based alloys (of the Ni-Al-Mo-B, Ni-Al-Fe-La, and Ni-Al-Y2O3 systems), as well as a new technology for preparing and processing them have been developed. The density of the alloys was 7.3-7.5 and ~6 g/cm 3, respectively. The Ni3Al sheets were used to prepare shields for combustion chambers in gas-turbine engines by roomtemperature deformation; the shields are intended for the long-term operation at 1100-1200°C and for the short-term use at 1300°C. The activated NiAl powders alloyed with Fe+La were used to produce sintered complex-shape articles, such as combustion stabilizers in a jet unit of combustion chamber of the gas-turbine installation, heat sources, etc. capable of operating at t≤1500°C under low mechanical stresses. At 1100, 1300, and 1500°C, the 100-h strength of the heat-resistant NiAl- (2-7.5) vol. % Y2O3 alloys subjected to directional recrystallization is 70, 35 and ≥10 MPa, respectively. The vanes, in which the length of recrystallized grain is smaller than the vane length by a factor of 1.5-2, were manufactured from these alloys.

scholarly journals Cobalt–Niobium-Carbide Eutectic Alloys for Increasing the Service Life of Gas Turbine Engines

2021 ◽  
Vol 22 (4) ◽  
pp. 678-693
Author(s):  
G. P. Dmitrieva ◽  
T. S. Cherepova ◽  
T. V. Pryadko
Keyword(s):  
Service Life ◽  
Gas Turbine ◽  
Niobium Carbide ◽  
Aircraft Engine ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Eutectic Alloys ◽  
Heat Resistant ◽  
The Creation

This article represents the stages of the creation of new serial wear-proof and heat-resistant (at temperatures up to 1100 °C) cobalt–Nb-carbide cast eutectic alloys of the KhTN (XTN) grade at the G.V. Kurdyumov Institute for Metal Physics of the N.A.S. of Ukraine, comparing them by their main properties, and use in aircraft engine engineering.

Prospects for the creation of high-temperature heatresistant alloys based on refractory matrices and natural composites

2021 ◽  
pp. 64-78
Author(s):  
E. N. Kablov ◽  
Yu. A. Bondarenko ◽  
M. Yu. Kolodyazhny ◽  
V. A. Surova ◽  
A. R. Narsky
Keyword(s):  
High Temperature ◽  
Gas Turbine ◽  
High Heat ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Heat Resistant ◽  
High Temperature Materials ◽  
Natural Composites ◽  
Scientific Technical ◽  
The Creation

The paper presents the scientific, technical and technological aspects in the field of creating new high-temperature materials for parts of the hot section of gas turbine engines (GTE) with operating temperatures exceeding those existing in GTE. More refractory metallic materials for the creation of new high-heat-resistant alloys used for the manufacture of rotor and nozzle blades and other parts of promising gas turbine engines based on NiAl-Ni3Al, Co-Cr-Re, Pt-Al, Nb-Si, Mo-Si-B systems have been investigated. It is shown that, depending on the composition of the selected matrix, the working temperature of heat-resistant alloys increases to 1300-1500°С, which is significantly higher than the existing nickel heat-resistant alloys.

Modeling the structure formation during hot deforming the billets of the parts of gas-turbine engines made of heat-resistant nickel alloy

2016 ◽  
Vol 45 (5) ◽  
pp. 469-475 ◽  
Author(s):  
I. A. Burlakov ◽  
V. A. Valitov ◽  
A. A. Ganeev ◽  
D. M. Zabel’yan ◽  
S. V. Morozov ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Nickel Alloy ◽  
Structure Formation ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Heat Resistant

Specifics of Producing Disk Blanks for Gas-Turbine Engines using Granules of Super Heat-Resistant Nickel Alloys

Metallurgist ◽  
2020 ◽  
Vol 64 (3-4) ◽  
pp. 362-369
Author(s):  
A. M. Volkov ◽  
D. A. Karyagin ◽  
M. N. Letnikov ◽  
M. M. Bakradze ◽  
A. S. Perevozov
Keyword(s):  
Gas Turbine ◽  
Nickel Alloys ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Heat Resistant
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