The Analysis of Two-phase Flow in a Lean Direct Injection Gas-turbine Combustor

2019 ◽  
Vol 47 (3) ◽  
pp. 204-211
Author(s):  
Kyobin Lee ◽  
Jong-Chan Kim ◽  
Hong-Gye Sung
Keyword(s):  
Gas Turbine ◽  
Two Phase Flow ◽  
Direct Injection ◽  
Phase Flow ◽  
Gas Turbine Combustor ◽  
Two Phase ◽  
Lean Direct Injection

OPTICAL MEASUREMENTS OF THE REACTING TWO-PHASE FLOW IN A REALISTIC GAS TURBINE COMBUSTOR AT ELEVATED PRESSURES

2006 ◽  
Vol 16 (5) ◽  
pp. 475-492 ◽  
Author(s):  
Thomas Behrendt ◽  
Martin Carl ◽  
Johannes Heinze ◽  
Christoph Hassa
Keyword(s):  
Gas Turbine ◽  
Two Phase Flow ◽  
Optical Measurements ◽  
Phase Flow ◽  
Gas Turbine Combustor ◽  
Two Phase ◽  
Elevated Pressures

Combustion Dynamics Behavior in a Single-Element Lean Direct Injection (LDI) Gas Turbine Combustor

2014 ◽  
Author(s):  
Cheng Huang ◽  
Rohan Gejji ◽  
William Anderson ◽  
Changjin Yoon ◽  
Venkateswaran Sankaran
Keyword(s):  
Gas Turbine ◽  
Direct Injection ◽  
Single Element ◽  
Gas Turbine Combustor ◽  
Combustion Dynamics ◽  
Lean Direct Injection

Combustion Dynamics in a Single-Element Lean Direct Injection Gas Turbine Combustor

2019 ◽  
Vol 192 (12) ◽  
pp. 2371-2398 ◽  
Author(s):  
Cheng Huang ◽  
Rohan Gejji ◽  
William Anderson ◽  
Changjin Yoon ◽  
Venkateswaran Sankaran
Keyword(s):  
Gas Turbine ◽  
Direct Injection ◽  
Single Element ◽  
Gas Turbine Combustor ◽  
Combustion Dynamics ◽  
Lean Direct Injection

REVAP® Cycle: A New Evaporative Cycle Without Saturation Tower

1997 ◽  
Vol 119 (4) ◽  
pp. 893-897 ◽  
Author(s):  
J. De Ruyck ◽  
S. Bram ◽  
G. Allard
Keyword(s):  
Heat Exchange ◽  
Gas Turbine ◽  
Two Phase Flow ◽  
Curve Analysis ◽  
Phase Flow ◽  
Two Phase ◽  
Flow Heat ◽  
Turbine Equipment ◽  
Composite Curve ◽  
A Performance

A new evaporative cycle layout is disclosed that is shown to have a performance similar to the HAT cycle, but where the saturation tower has been eliminated. This new cycle is a result of a combined exergetic and composite curve analysis discussed in a previous paper, assuming one intercooler and no reheat (De Ruyck et al., 1995). The new cycle uses two-phase flow heat exchange in the misty regime, which is a well-known process. Existing aeroderivative gas turbine equipment can be adapted for application of this cycle, which therefore needs a minimum of development.

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