Effect of Operating Variables on the Performance of a Highly Loaded Annular Combustor
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S. K. Muduli
,
R. K. Satpathy
Abstract
A highly loaded full-scale annular combustor is studied in the air-flow facility for the effect of operating variables such as compressor discharge velocity and fuel-air ratio on the performance parameters. The combustor is designed to operate at high pressures and high exit temperatures that impose stringent limitations on its performance such as pressure loss, exit temperature profiles and combustion efficiency. The effect of excess air ratio on performance parameters is found to be marginal over the range tested. Increasing the excess air ratio decreases the pressure loss, exit pattern factors and combustion efficiency. The inlet Mach no. is found to influence the pressure loss strongly and exit temperature patterns marginally. Combustion efficiency is found to deteriorate with increase in Mach number. This will in turn affect the integrity and life of hot end components of the aero engine.
©2015 by De Gruyter
Artikel in diesem Heft
- Frontmatter
- Study on Internal Flow and External Performance of a Semi-open Impeller Centrifugal Pump with Different Tip Clearances
- A Numerical Study of Spray Injected in a Gas Turbine Lean Pre-Mixed Pre-Vaporized Combustor
- Coupling Optimization Design of Aspirated Compressor Airfoil and Aspirated Scheme Based on Artificial Bee Colony Algorithm and CST Method
- Propagation of Different Types of Inflow Distortions through a Contra Rotating Fan Stage
- A Method to Determine the Slip Factor of Centrifugal Pumps through Experiment
- Investigation of Blade Angle of an Open Cross-Flow Runner
- Mixing Characteristics of Elliptical and Rectangular Subsonic Jets with Swirling Co-flow
- Effect of Operating Variables on the Performance of a Highly Loaded Annular Combustor
- Numerical Investigations on the Nanosecond Pulse Discharge Process of Disk-Shape Plasma Igniter
- Development of a High Efficiency In-Line Tube Fan Using CFD
Artikel in diesem Heft
- Frontmatter
- Study on Internal Flow and External Performance of a Semi-open Impeller Centrifugal Pump with Different Tip Clearances
- A Numerical Study of Spray Injected in a Gas Turbine Lean Pre-Mixed Pre-Vaporized Combustor
- Coupling Optimization Design of Aspirated Compressor Airfoil and Aspirated Scheme Based on Artificial Bee Colony Algorithm and CST Method
- Propagation of Different Types of Inflow Distortions through a Contra Rotating Fan Stage
- A Method to Determine the Slip Factor of Centrifugal Pumps through Experiment
- Investigation of Blade Angle of an Open Cross-Flow Runner
- Mixing Characteristics of Elliptical and Rectangular Subsonic Jets with Swirling Co-flow
- Effect of Operating Variables on the Performance of a Highly Loaded Annular Combustor
- Numerical Investigations on the Nanosecond Pulse Discharge Process of Disk-Shape Plasma Igniter
- Development of a High Efficiency In-Line Tube Fan Using CFD
