Characteristics of compressed air with water spray cooling action radius

Author(s):  
G. Jia ◽  
W. Xu ◽  
Y. Shi ◽  
M. Cai
2017 ◽  
Vol 18 (2) ◽  
pp. 211 ◽  
Author(s):  
Jia Guanwei ◽  
Cai Maolin ◽  
Shi Yan ◽  
Xu Weiqing

1998 ◽  
Vol 69 (6) ◽  
pp. 240-246 ◽  
Author(s):  
Vigdis Olden ◽  
Miroslav Raudenský ◽  
Kristin Onsrud ◽  
Wolfgang Hummel

1980 ◽  
Vol 39 (2) ◽  
pp. 900-905
Author(s):  
L. I. Urbanovich ◽  
V. A. Goryainov ◽  
V. V. Sevost'yanov ◽  
Yu. G. Boev ◽  
V. M. Niskovskikh ◽  
...  

2001 ◽  
Author(s):  
J. Ward ◽  
M. de Oliveira ◽  
D. R. Garwood ◽  
R. A. Wallis

Abstract The desired mechanical properties of the nickel-based or titanium forgings used in gas turbines for aircraft and power generation applications can be controlled by varying the rate of cooling from the so-called solution temperature during an initial heat treatment process. The use of dilute air-water spray cooling of these forgings is a technique which can provide heat transfer rates lying between those associated with conventional oil quenching or convective air-cooling. Air assisted atomisation can result in fine sprays over a wide range of water flow rates and it has a further advantage in that the air “sweeps” the surface and hence helps to prevent the build up of deleterious vapour films at high surface temperatures. The paper presents experimental data for the heat transfer rates associated with the use of these sprays to cool surfaces from temperatures of approximately 800°C. Many forgings contain surface recesses, which can lead to build up or “pooling” of the water so that the effect of variations in surface geometry is also reported. Periodic interruption of the water flow is a technique which can be employed to provide additional control of the heat transfer rate, particularly at temperatures below 500°C so that data is also presented for pulsed sprays.


Author(s):  
I Ritchey ◽  
E H Fisher ◽  
G D Agnew

Aerodervative gas turbines intercooled by water spray injection systems have recently entered service. A calculation framework is presented which permits the effect of water spray injection for both intercooling and inlet chilling to be evaluated and compared with conventional cooling techniques for a range of cycles. The calculations are based on representative performance maps for compressors and turbines, focusing upon the actual performance benefits that can be realized from existing turbomachinery. The principal conclusions are that spray intercooling can give a greater power boost than conventional intercooling for a given compressor operating envelope spray inlet chilling can give performance benefits comparable with absorption chilling and intercooling is more attractive at ambient temperatures below 15°C, whereas inlet chilling is preferable at higher temperatures.


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