The Effect of Flow Field and Fuel Spray of Combustor with Swirl Cup on Lean Blowout Limit at Idle Condition
|更新时间:2026-07-07
|
The Effect of Flow Field and Fuel Spray of Combustor with Swirl Cup on Lean Blowout Limit at Idle Condition
Vol. 19, Issue 3, (2004)
作者机构:
北京航空航天大学航空发动机气动热力重点实验室,北京,100083
作者简介:
基金信息:
DOI:
CLC:
Published:2004
稿件说明:
移动端阅览
YUAN Yi-xiang, LIN Yu-zhen, LIU Gao-en. The Effect of Flow Field and Fuel Spray of Combustor with Swirl Cup on Lean Blowout Limit at Idle Condition[J]. 2004, 19(3).
DOI:
YUAN Yi-xiang, LIN Yu-zhen, LIU Gao-en. The Effect of Flow Field and Fuel Spray of Combustor with Swirl Cup on Lean Blowout Limit at Idle Condition[J]. 2004, 19(3).DOI:
The Effect of Flow Field and Fuel Spray of Combustor with Swirl Cup on Lean Blowout Limit at Idle Condition
of which one was that with three swirlers (A model)
and the other with two swirlers (B model).Computation was conducted for flow field of these combustors.Flow field and fuel spray of the two designs were measured by Phase Doppler Analysis (PDA).The lean blowout fuel air ratio and flame photo were obtained.The results showed that the A model had better Sauter Mean Diameter (SMD) & uniformity than B model
but it had a worse lean blowout performance
and the flow rate in the inner swirler of A model should decrease to establish a low pressure stagnation region which would be helpful to improve the lean blowout fuel air ratio.
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
Lean blowout mechanism of coupled recirculation zone in concentric staged combustor
Influences of the swirl cup flares design on the small combustor ignition performances
A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory
Related Author
YUAN Yi xiang
LIN Yu zhen
LIU Gao en
HU Guo xin
GONG Jing
ZOU Bo-wen
XU Quan-hong
CAO Wen-yu
Related Institution
Shanghai JiaoTong University
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
China Aviation Powerplant Research Institute, Aviation Industry Corporation of China
National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Jet Propulsion, National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics