Detailed Performance Comparison of a Dump and Short Faired Combustor Diffuser System

Author:

Carrotte J. F.1,Denman P. A.1,Wray A. P.1,Fry P.2

Affiliation:

1. Department of Transport Technology, Loughborough University, Loughborough, Leics, United Kingdom

2. Combustion Department, Rolls Royce plc, Derby, United Kingdom

Abstract

A rectangular model simulating four sectors of a combustion chamber was used to compare the performance of a standard dump diffuser, of overall length 180 mm, with that of a faired design 25.5 mm shorter. The performance of each system was assessed in terms of total pressure loss and static pressure recovery between prediffuser inlet and the annuli surrounding the flame tube. Since the program objective was to test design concepts only, no allowance was made for the presence of burner feed arms or flame tube support pins. In addition, tests were performed with relatively low levels of inlet turbulence and no wake mixing effects from upstream compressor blades. Relative to the dump design, the mass weighted total pressure loss to the outer and inner annuli was reduced by 30 and 40 percent, respectively, for the faired diffuser. Measurements around the flame tube head were used to identify regions of high loss within each system and account for the differences in performance. Within a dump diffuser the flow separates at prediffuser exit resulting in a free surface diffusion around the flame tube head and a recirculating flow in the dump cavity. This source of loss is eliminated in the faired system where the flow remains attached to the casings. Furthermore, the faired system exhibited similar velocity magnitudes and gradients around the combustor head despite its shorter length.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Numerical Characterization on the Influence of Flame Tube Geometry and Dump Gap in the Diffuser Performance at High Altitudes;Proceedings of the National Academy of Sciences, India Section A: Physical Sciences;2023-12-18

2. Computational Investigation on the Influence of Dump Gap and Novel Flame Tube Geometries in the Hybrid Diffuser Performance;Handbook of Research on Aspects and Applications of Incompressible and Compressible Aerodynamics;2022-06-24

3. Liner dome shape effect on the annulus flow characteristics with and without swirl for a can-combustor model;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2007-05-01

4. Enhanced External Aerodynamic Performance of a Generic Combustor Using An Integrated OGV/Prediffuser Design Technique;Journal of Engineering for Gas Turbines and Power;2006-02-01

5. An Experimental/Computational Study of Airflow in the Combustor–Diffuser System of a Gas Turbine for Power Generation;Journal of Engineering for Gas Turbines and Power;1998-01-01

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