Keywords: G. قطعات موتور هواپیما; A. Intermetallics; B. Elastic properties; Fracture; Mechanical properties; G. Aero-engine components;
مقالات ISI G. قطعات موتور هواپیما (ترجمه نشده)
مقالات زیر هنوز به فارسی ترجمه نشده اند.
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در صورتی که به ترجمه آماده هر یک از مقالات زیر نیاز داشته باشید، می توانید سفارش دهید تا مترجمان با تجربه این مجموعه در اسرع وقت آن را برای شما ترجمه نمایند.
Keywords: G. قطعات موتور هواپیما; A. Molybdenum silicides; B. Oxidation; C. Coatings, intermetallic and otherwise; C. Vapour deposition; G. Aero-engine components;
Heat treatment of laser metal deposited TiAl TNM alloy
Keywords: G. قطعات موتور هواپیما; A. Intermetallics; B. Annealing; Phase transformation; C. Casting; Heat treatment; Laser processing and cladding; D. Microstructure; G. Aero-engine components;
Stability of lamellar structure of directionally solidified NiAl-28Cr-6Mo eutectic alloy at different withdrawal rates and temperatures
Keywords: G. قطعات موتور هواپیما; A. Intermetallics (aluminides); B. Thermal stability; C. Crystal growth; D. Microstructure; G. Aero-engine components;
Experimental determination of the phase diagrams of the Co-Ni-X (X = W, Mo, Nb, Ta) ternary systems using diffusion multiples
Keywords: G. قطعات موتور هواپیما; A. Intermetallics; B. Phase stability; C. Heat treatment; D. Microstructure; F. Electron microprobe; G. Aero-engine components;
Microstructure control and mechanical properties from isothermal forging and heat treatment of Ti–22Al–25Nb (at.%) orthorhombic alloy
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on Ti3Al; B. Creep; C. Isothermal forging; F. Electron microscopy, scanning; G. Aero-engine components
Investigations on the microstructure and room temperature fracture toughness of directionally solidified NiAl–Cr(Mo) eutectic alloy
Keywords: G. قطعات موتور هواپیما; A. Nickel aluminides, based on NiAl; B. Crack propagation; B. Fracture toughness; C. Crystal growth; D. Microstructure; G. Aero-engine components
Effect of alloying elements on the behaviour of TiAl-based alloys
Keywords: G. قطعات موتور هواپیما; A. Intermetallics; B. Fracture toughness; B. Oxidation; G. Aero-engine components; G. Automotive uses, including engines;
The effects of ultrasonic nanocrystal surface modification (UNSM) on pack aluminizing for the fabrication of Pt-modified aluminide coatings at low temperatures
Keywords: G. قطعات موتور هواپیما; A. Aluminides, miscellaneous; B. Oxidation; C. Surface finishing; G. Aero-engine components
High-temperature oxidation behavior of Mo-Si-B-based and Co-Re-Cr-based alloys
Keywords: G. قطعات موتور هواپیما; A. Molybdenum silicides; A. Multiphase intermetallics; B. Oxidation; G. Aero-engine components;
In-situ neutron diffraction study of thermal phase stability in a γ-TiAl based alloy doped with Mo and/or C
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Order/disorder transformations; B. Phase diagrams; D. Site occupancy; F. Diffraction; G. Aero-engine components;
Effect of Dy on the microstructures of directionally solidified NiAl–Cr(Mo) hypereutectic alloy at different withdrawal rates
Keywords: G. قطعات موتور هواپیما; A. Nickel aluminides, based on NiAl; A. Rare-earth intermetallics; C. Crystal growth; D. Microstructure; G. Aero-engine components
Influence of fiber alignment on creep in directionally solidified NiAl-10Mo in-situ composites
Keywords: G. قطعات موتور هواپیما; A. Nickel aluminides, based on NiAl; B. Creep (properties and mechanisms); C. Crystal growth; E. Mechanical properties, theory; G. Aero-engine components;
High speed ball nose end milling of γ-TiAl alloys
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; C. Machining; G. Aero-engine components;
An in-situ high-energy X-ray diffraction study on the hot-deformation behavior of a β-phase containing TiAl alloy
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; C. Thermomechanical treatment; F. Diffraction; G. Aero-engine components;
Optimized coating procedure for the protection of TiAl intermetallic alloy against high temperature oxidation
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Oxidation; C. Coatings; G. Aero-engine components
Fabrication and characterization of in-situ TiAl matrix composite with controlled microlaminated architecture based on SiC/Al and Ti system
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Phase transformation; C. Reaction synthesis; D. Microstructure; G. Aero-engine components
High temperature creep behaviour in the γ titanium aluminide Ti–45Al–2Mn–2Nb
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides; A. Intermetallics; B. Creep; G. Aero-engine components; B. Oxidation
Isothermal oxidation behaviour of TiAl–Cr–Nb–B alloys produced by induction melting
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Oxidation; G. Aero-engine components; G. Automotive uses, including engines (and other transportation uses)
Electrochemical synthesis of Nb5Si3 intermetallic compound from molten calcium chloride salt
Keywords: G. قطعات موتور هواپیما; A. Intermetallics, miscellaneous; F. Electrochemical characterization; G. Aero-engine components
Effect of withdrawal rate on the microstructure of directionally solidified NiAl–Cr(Mo) hypereutectic alloy
Keywords: G. قطعات موتور هواپیما; A. Nickel aluminides, based on NiAl; A. Composites; C. Crystal growth; D. Microstructure; G. Aero-engine components
Fracture of convoluted and lamellar α2 + γ TiAl alloys
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Fracture toughness; D. Microstructure; G. Aero-engine components;
Diffusion aluminide coatings for TiAl intermetallic turbine blades
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Oxidation; C. Coatings, intermetallic and otherwise; F. Electron microscopy, scanning; G. Aero-engine components
Phase continuity in high temperature Mo–Si–B alloys: A FIB-Tomography Study
Keywords: G. قطعات موتور هواپیما; A. Molybdenum silicides; F. Tomography; D. Microstructure; F. Electron microscopy, scanning; G. Aero-engine components
Emission mitigation potential of lightweight intermetallic TiAl components
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; C. Near-net-shape manufacturing; G. Aero-engine components; G. Environmental applications
Electron beam melting of Ti-48Al-2Cr-2Nb alloy: Microstructure and mechanical properties investigation
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; C. Near-net-shape manufacturing; G. Aero-engine components; C. Heat treatment; F. Mechanical testing;
Effect of a phosphoric acid treatment on the high temperature oxidation behaviour of γ-TiAl: An overall mechanism
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Oxidation; C. Coatings; D. Site occupancy; G. Aero-engine components
Ab initio study of phase transformations in transition-metal disilicides
Keywords: G. قطعات موتور هواپیما; A. Silicides, various; B. Phase transformation, plastic deformation mechanisms; D. Defects: dislocation geometry and arrangement; E. Ab-initio calculations; G. Aero-engine components
Development of a turbulence-free casting technique for titanium aluminides
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; C. Melting; C. Casting; G. Aero-engine components; G. Energy systems
On the influence of boron-addition on TLP bonding time in a Ni3Al-based intermetallic
Keywords: G. قطعات موتور هواپیما; A. Nickel aluminides, based on Ni3Al; C. Joining; G. Aero-engine components
Plastic deformation behavior of Ni3(Ti0.7Nb0.3) single crystals with D019 structure
Keywords: G. قطعات موتور هواپیما; A. Ternary alloy systems; B. Plastic deformation mechanism; B. Yield stress; D. Defects: dislocation geometry and arrangement; G. Aero-engine components
Effect of zirconium addition on cyclic oxidation behavior of platinum-modified aluminide coating on nickel-based superalloy
Keywords: G. قطعات موتور هواپیما; A. Aluminides, miscellaneous; B. Oxidation; G. Aero-engine components
Topological close packed μ phase formation and the determination of diffusion parameters in the Co–Mo system
Keywords: G. قطعات موتور هواپیما; B. Diffusion; A. Intermetallics, miscellaneous; B. Phase diagrams; G. Aero-engine components
Ni and Al diffusion in Ni-rich NiAl and the effect of Pt additions
Keywords: G. قطعات موتور هواپیما; A. Nickel aluminides; B. Diffusion; D. Defects: point defects; G. Aero-engine components; E. Electronic structure calculations
Cyclic oxidation of Pt/Pd-modified aluminide coating on a nickel-based superalloy at 1150 °C
Keywords: G. قطعات موتور هواپیما; A. Aluminides, miscellaneous; B. Oxidation; G. Aero-engine components
Ab initio calculations of elastic properties of Pt–Sc alloys
Keywords: G. قطعات موتور هواپیما; 31.15.A−; 62.20.de; 62.20.dqA. Intermetallics, miscellaneous; B. Elastic properties; E. Ab initio calculations; G. Aero-engine components; G. Furnace furniture
Atomistic modeling of Pt additions to NiAl
Keywords: G. قطعات موتور هواپیما; A. Nickel aluminides, based on NiAl; B. Thermal properties; D. Site occupancy; E. Simulations, atomistic; G. Aero-engine components
Analysis of element-content effects on equilibrium segregation at γ/γ′ interface in Ni-base superalloys using the cluster variation method
Keywords: G. قطعات موتور هواپیما; D. Phase interfaces; E. Phase stability, prediction; B. Order/disorder transformations; D. Site occupancy; G. Aero-engine components
Mechanically alloyed Mo-Si-B alloys with a continuous α-Mo matrix and improved mechanical properties
Keywords: G. قطعات موتور هواپیما; A. Molybdenum silicides; B. Brittleness and ductility; C. Mechanical alloying and milling; D. Microstructure; G. Aero-engine components;
Laser beam weld microstructures in directionally solidified alloy IC 6
Keywords: G. قطعات موتور هواپیما; C. Joining; G. Aero-engine components; C. Laser processing
MoSi2 laminate processed by tape casting: Microstructure and mechanical properties' investigation
Keywords: G. قطعات موتور هواپیما; A. Molybdenum silicides; C. Sintering; F. Mechanical testing; G. Aero-engine components
Solid solution mechanism and thermodynamic properties of Ti–Re alloy system: Experiment and theory
Keywords: G. قطعات موتور هواپیما; A. Intermetallics, miscellaneous; B. Thermodynamic and thermochemical properties; E. Simulations, atomistic; F. Diffraction; G. Aero-engine components
Laser beam weld-metal microstructure in a yttrium modified directionally solidified Ni3Al-base alloy
Keywords: G. قطعات موتور هواپیما; G. Aero-engine components; C. Joining; A. Nickel aluminides, based on Ni3Al; C. Melting;
First-principles study of shear deformation in TiAl and Ti3Al
Keywords: G. قطعات موتور هواپیما; A. Multiphase intermetallics; B. Plastic deformation mechanisms; E. Ab initio calculations; E. Phase stability, prediction; G. Aero-engine components
Intermetallics: Why is it so difficult to introduce them in gas turbine engines?
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; A. Nickel aluminides, based on NiAl; G. Aero-engine components
The effect of long term exposure in oxidising and corroding environments on the tensile properties of two gamma-TiAl alloys
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Oxidation; B. Corrosion; B. Mechanical properties at high temperaturs; G. Aero-engine components;
Effect of composition on the mechanical properties of newly developed Ti2AlNb-based titanium aluminide
Keywords: G. قطعات موتور هواپیما; B. Mechanical properties at high temperatures; G. Aero-engine components;
Microstructure evolution of NiCoCrAlY overlay coating for Ni3Al based alloy IC6 turbine vane during long term engine test
Keywords: G. قطعات موتور هواپیما; A. Nickel aluminides; based on Ni3Al; C. Coatings; Intermetallic and otherwise; D. Microstructure; G. Aero-engine components;
Gamma titanium aluminide, TNB
Keywords: G. قطعات موتور هواپیما; A. Titanium aluminides, based on TiAl; B. Fatigue resistance and crack growth; G. Aero-engine components;