scholarly journals An Experimental Study on the Spray Characteristics of a Rotating Fuel Nozzle of a Slinger Combustor for Different Flow Rates and Rotating Speeds

2021 ◽  
Vol 25 (4) ◽  
pp. 59-70
Author(s):  
Hyeon-Seok Shim ◽  
Jonggeun Bae ◽  
Jupyoung Kim ◽  
Shaun Kim ◽  
Donghyun Kim ◽  
...  
Author(s):  
Angela Gerlach ◽  
Dorian Perlitz ◽  
Flemming Lykholt-Ustrup ◽  
Christian Brix Jacobsen ◽  
Paul Uwe Thamsen

This paper analyzes the clogging behavior of a vortex pump with different impeller designs. The influence of blade outlet angle, blade number, and impeller diameter were tested. Non-woven textiles in different concentrations served as the clogging material. The results suggest that a smaller outlet blade angle, a higher blade number, and a larger impeller diameter allow pumping more textiles. Impellers that were capable of pumping more textiles, however, were less efficient. Overall, pumping textiles causes efficiency losses. However, this could not be only related to increased power consumption. Flow rates under clogging operation were close to the flow rates under clear water operation irrespective of the amount of clogging material and the impellers design. Further, in all tests clogging material accumulated at the suction mouth in the casing.


2018 ◽  
Vol 142 ◽  
pp. 717-722 ◽  
Author(s):  
Rong Xue ◽  
Yixiao Ruan ◽  
Xiufang Liu ◽  
Liang Chen ◽  
Xingqun Zhang ◽  
...  

Fuel ◽  
2012 ◽  
Vol 97 ◽  
pp. 390-399 ◽  
Author(s):  
Raul Payri ◽  
Antonio García ◽  
Vicent Domenech ◽  
Russell Durrett ◽  
Alejandro H. Plazas

2021 ◽  
Vol 33 (9) ◽  
pp. 091902
Author(s):  
Junjian Tian ◽  
Yu Liu ◽  
Fengyu Li ◽  
Kai Han ◽  
Wenliang Zhou ◽  
...  

1992 ◽  
Vol 114 (2) ◽  
pp. 454-461 ◽  
Author(s):  
S. H. Bhavnani ◽  
J. M. Khodadadi ◽  
J. S. Goodling ◽  
J. Waggott

Results are presented for an experimental study of fluid flow in models of gas turbine disk cavities. Experiments were performed on 70-cm-dia disks for rotational Reynolds numbers up to 2.29 × 106. Velocity and pressure distributions are presented and compared to previous theoretical and experimental studies for a free disk, and an unshrouded plane Rotor–Stator disk system. Minimum coolant flow rates for the prevention of ingress, determined for the case of a simple axial rim seal, compare well with previously published data.


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