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Aero Engine

BIFURCATION BUCKLING OF A CORRUGATED JET PIPE LINER FOR AN AERO-ENGINE AFTERBURNER

BIFURCATION BUCKLING OF A CORRUGATED JET PIPE LINER FOR AN AERO-ENGINE AFTERBURNER

... the aero-engine jetpipe liner are reported in the open ...turbine engine were acquired by a bench test and the liner wall temperature calculation model was improved ...turbine engine and ...

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Multi pipe Routing in Bundles for Aero engine using MOPSO

Multi pipe Routing in Bundles for Aero engine using MOPSO

... This paper studies the optimization of pipe layout for multi-pipe routing in bundles by taking the complex equipment: aero-engine as an example. The MOPSO algorithm is applied on multi-objectives to obtain ...

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Structural Design Analysis of Bypass Casing for an Aero Engine

Structural Design Analysis of Bypass Casing for an Aero Engine

... an aero engine in cooling and noise ...an aero engine. It houses the core engine of an aero engine which comprises of High pressure compressor unit (HPC), Combustion ...

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Simulation of Secondary Flow in Lubrication Pipe with End Bends of an Aero Engine

Simulation of Secondary Flow in Lubrication Pipe with End Bends of an Aero Engine

... in aero engine lubrication ...in aero engine pipes due to complicated engine ...in aero engine has one pressure, scavenge and vent ...an aero engine is ...

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Literature Review on Innovative Technologies for Temperature Measurement of Aero Engine Component

Literature Review on Innovative Technologies for Temperature Measurement of Aero Engine Component

... of aero engine ...improved engine operating efficiency gas turbine is design to operate at higher temperature which is just few degree below the melting point of material so accurate temperature ...

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Fuzzy scheduling control for gas turbine aero engine: a multiobjective approach

Fuzzy scheduling control for gas turbine aero engine: a multiobjective approach

... Abstract—This paper investigates the use of a nonconventional approach to control a gas turbine aero-engine. The rationale be- hind this study is the need to develop advanced tools and tech- niques that can ...

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Research on Numerical Simulation of Three dimensional Icing for Aircraft and Aero engine

Research on Numerical Simulation of Three dimensional Icing for Aircraft and Aero engine

... The three-dimensional icing calculation research code designed in this paper is developed on the platform of FLUENT. Use FLUENT secondary development features—User-Defined Function (UDF), According to the needs of ...

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Logical Knowledge-based Advanced Cost Estimation Methodology (LKACEM) Applied to Metal Matrix Composite Aero-Engine Blisk

Logical Knowledge-based Advanced Cost Estimation Methodology (LKACEM) Applied to Metal Matrix Composite Aero-Engine Blisk

... As composites have become a choice for many designers, engineers and project planners for use in structural and non-structural parts, their in-depth study has become important. Detailed analysis of the material ...

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A coupled 1D film hydrodynamics and core gas flow model for air oil flows in aero engine bearing chambers

A coupled 1D film hydrodynamics and core gas flow model for air oil flows in aero engine bearing chambers

... of aero-engine transmissions components requires the supply and efficient distribution of sufficient oil to lubricate and cool components such as bearings, gears and their ...these aero-engine ...

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Experimental study of the pressure loss in aero engine air oil separators

Experimental study of the pressure loss in aero engine air oil separators

... Aero-engine bearings require a steady supply of oil for lubrication and cooling. Ideally, all of the oil running through the bearings is recycled to minimise the total weight of the oil carried on board. At ...

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Research on Early Fault Self Recovery Monitoring of Aero Engine Rotor System

Research on Early Fault Self Recovery Monitoring of Aero Engine Rotor System

... In order to increase robustness of the AERS (Aero-engine Rotor System) and to solve the problem of lacking fault samples in fault diagnosis and the difficulty in identifying early weak fault, we proposed a ...

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Characterization of Air Plasma Sprayed Al PO4 and Laser-Sealed ZrO2-MgO Coatings on Ni-Base Supper Alloys of Aero-Engine

Characterization of Air Plasma Sprayed Al PO4 and Laser-Sealed ZrO2-MgO Coatings on Ni-Base Supper Alloys of Aero-Engine

... Gas and steam turbines operate in the environments where the ingestions of solid particles are inevitable and results in erosion of materials. In the recent times gas turbine technology for power generation and for ...

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Power System Analysis of an Aero Engine

Power System Analysis of an Aero Engine

... The engine has a thrust range of 82 to 109 ...the engine flow approaches a maximum value to be ...the engine are also analyzed from reverse-engineering ...and aero-propulsive generation ...

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Design, construction, and testing of an aero-engine starter-generator for the more-electric aircraft

Design, construction, and testing of an aero-engine starter-generator for the more-electric aircraft

... Abstract: This study describes the design, construction, and testing of an aero-engine starter-generator and its associated power electronic converter. A high-speed, permanent magnet machine and a ...

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Research on Assemblability Evaluation Method of Aero engine Based on Assembly Data Model

Research on Assemblability Evaluation Method of Aero engine Based on Assembly Data Model

... Aero-engine design is a system engineering that requires constant verification and iterations to achieve final use and assembly requirements. If the spatial positional relationship between the assembly ...

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Multi-Objective Meta Heuristic Optimization Algorithm with Multi Criteria Decision Making Strategy for Aero-Engine Controller Design

Multi-Objective Meta Heuristic Optimization Algorithm with Multi Criteria Decision Making Strategy for Aero-Engine Controller Design

... the aero-engine controller design and optimization ...of aero-engine ...the engine and controller illustrate that the optimized controllers successfully satisfy the engine’s control ...

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Design and Implementation of Fuel Metering Unit for an Aero Engine

Design and Implementation of Fuel Metering Unit for an Aero Engine

... an Aero engine. Fuel flow of an engine varies with an ambient condition such as temperature, pressure and the amount of fuel flow to the engine is different at various ...and engine ...

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Stress Analysis of Aero Engine Spur Gear

Stress Analysis of Aero Engine Spur Gear

... ABSTRACT: The context of this paper pertained to Aircraft gear design, which gives details about reduction of contact stresses in aero engine spur gears. Also discussed about changing the geometrical ...

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Impact Damage of Aero Engine after UAV Ingestion

Impact Damage of Aero Engine after UAV Ingestion

... the aero engine blade is established through the software SolidWorks, and then the 3D model is imported to the finite element pre-processing software HyperMesh for ...

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Measurement of CO2 concentration and temperature in an aero engine exhaust plume using wavelength modulation spectroscopy

Measurement of CO2 concentration and temperature in an aero engine exhaust plume using wavelength modulation spectroscopy

... Typically, 2f/1f spectra are analysed using the methodology described by Sun et al. [17], where the entire modulated experimental signal is recorded and processed using a software LIA that is also used to demodulate a ...

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