Exchanger Structure-Induced Flow Maldistribution and Performance Deterioration

2013 ◽  
pp. 275-307
Author(s):  
Li-Zhi Zhang
Keyword(s):  
Performance Deterioration ◽  
Induced Flow ◽  
And Performance ◽  
Flow Maldistribution

scholarly journals The Dynamics of Suspended Solid Particles in a Two Stage Gas Turbine

1986 ◽  
Author(s):  
W. Tabakoff ◽  
A. Hamed
Keyword(s):  
Flow Field ◽  
Gas Turbine ◽  
Turbine Blades ◽  
Three Dimensional ◽  
Suspended Solid ◽  
Solid Particles ◽  
Two Stage ◽  
Particle Momentum ◽  
Performance Deterioration ◽  
And Performance

Gas turbine engines operating in dusty environments are exposed to erosion and performance deterioration. In order to provide the basis for calculating the erosion and performance deterioration of turbines using pulverized coal, an investigation is undertaken to determine the three dimensional particle trajectories in a two stage turbine. The solution takes into account the influence of the variation in the three dimensional flow field. The change in particle momentum due to their collision with the turbine blades and casings is modeled using empirical equations derived from experimental Laser Doppler Velocimetry (LDV) measurements. The results show the three dimensional trajectory characteristics of the solid particles relative to the turbine blades. The results also show that the particle distribution in the flow field are determined by particle-blade impacts. The results obtained from this study indicate the turbine blade locations which are subjected to more blade impacts and hence more erosion damage.

Compressor Erosion and Performance Deterioration

1987 ◽  
Vol 109 (3) ◽  
pp. 297-306 ◽  
Author(s):  
W. Tabakoff
Keyword(s):  
Axial Flow ◽  
Solid Particles ◽  
Atmospheric Environment ◽  
Jet Engines ◽  
Particle Trajectories ◽  
Performance Deterioration ◽  
The Difference ◽  
And Performance ◽  
Flow Compressor ◽  
Particle Separator

Aircraft engines operating in areas where the atmosphere is polluted by small solid particles are typical examples of jet engines operating under hostile atmospheric environment. The particles may be different kinds of sand, volcanic ashes or others. Under these conditions, the gas and particles experience different degrees of turning as they flow through the engine. This is mainly due to the difference in their inertia. This paper presents the results of an investigation of the solid particle dynamics through a helicopter engine with inlet particle separator. The particle trajectories are computed in the inlet separator which is characterized by considerable hub and tip contouring and radial variation in the swirling vane shape. The nonseparated particle trajectories are determined through the deswirling vanes and the five stage axial flow compressor. The results from this study include the frequency of particle impacts and the erosion distribution on the blade surfaces.

Development of the General Electric LM 1500 Gas Turbine as a Marine Power Plant

1966 ◽  
Vol 88 (2) ◽  
pp. 144-152
Author(s):  
E. E. Stoeckly
Keyword(s):  
Power Plant ◽  
Gas Turbine ◽  
Marine Environment ◽  
Hot Corrosion ◽  
Power Plants ◽  
Sea Salt ◽  
Marine Propulsion ◽  
Performance Deterioration ◽  
Aircraft Type ◽  
And Performance

Many unique advantages have stemmed from the use of aircraft-type gas turbine power plants in selected marine propulsion applications; and, as expected, special problems have arisen because of the marine environment, primarily in the areas of parts integrity resulting from cold and hot corrosion and performance deterioration due to compressor fouling. Sulfur in the fuel, together with sea salt in the fuel and combustion air, creates major problems. Programs directed to reduce the detrimental effects, and the results attained are described.

Experimental Investigation of Manifold Induced Flow Maldistribution in U-and Z-Turn Flow Configurations

2011 ◽  
Vol 110-116 ◽  
pp. 4677-4683 ◽  
Author(s):  
Sachin B. Ingle ◽  
R.S. Maurya
Keyword(s):  
Experimental Study ◽  
Pipe Flow ◽  
Flow Distribution ◽  
Peripheral Region ◽  
Pressure Drops ◽  
Uniform Flow Distribution ◽  
Channel Velocity ◽  
Induced Flow ◽  
Flow Configurations ◽  
Flow Maldistribution

In many process equipments and mechanical system where a flow needs to be distributed among several outlets, the design is generally based on the assumption that the fluid is uniformly divided among them but practically in never happens. A non-uniform flow distribution imposes a serious design limitation in terms of rise in pressure drops and decrease in thermal performance of the system. Reynolds number being a characterizing parameter of pipe flow is expected to play a significant role in flow maldistribution pattern also. This paper present an experimental study performed on multi channel U-and Z-turn flow configurations where the flow is varied in the practical range of 20000 < Re < 35000. Result shows the presence of maldistribution. It is found that the Re plays an important role in characterizing the flow in terms of channel velocity, axial velocity in header and flow distribution pattern in a specific channel. Maldistribution effect is found to be dominant in the central region in U-turn flow and peripheral region in Z-turn configurations.

Sign in / Sign up

Export Citation Format

Share Document