The combustion characteristics of the self-stabilized dual-swirler cup in the unconfined case
which is suitable for the tangential trapped vortex combustor
were investigated experimentally.The self-stabilized dual-swirler cup is characterized in that
the dual-swirler with radial holes is employed
and the fuel sprays from a pressure nozzle in the center.According to the different swirl numbers and air flux distributions of the swirler
different layouts are developed.In the experiment under normal temperature and pressure
RP-3
for example
was used as the fuel.Results show that
the flame stability increases and the length and shape of the flame remain unchanged with the decrease of the air flux distribution of the internal swirl and increase of its swirl number.
Lean blowout mechanism of coupled recirculation zone in concentric staged combustor
Combustor Dome Design with Three Swirlers for Widening the Operation Stability Range
The Effect of Fuel-Circumferential-Staging on Lean Blowout Limit at Idle Condition
The Effect of Flow Field and Fuel Spray of Combustor with Swirl Cup on Lean Blowout Limit at Idle Condition
Test on effect of swallowing water on component performance of reverse⁃flow combustor
Related Author
ZOU Bo-wen
XU Quan-hong
CAO Wen-yu
ZHANG Chi
LIN Yu-zhen
YUAN Yi-xiang
LIN Yu-zhen
LIU Gao-en
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Beijing University of Aeronautics and Astronautics
Shanghai JiaoTong University
Hunan Aviation Powerplant Research Institute, Aero Engine Corporation of China
Sichuan Gas Turbine Establishment,Aero Engine Corporation of China