A lean-burn internally-staged combustor for low emissions that can be used in civil aviation
gas turbines is introduced in this paper. The main stage is designed and optimized in terms …

采用数值和实验方法对一种强剪切空气雾化喷嘴的流场和喷雾特性进行研究.
采用粒子动态分析仪(PDA) 实验研究了不同气液比下强剪切空气雾化喷嘴的速度场和喷雾场 …

This article gives an overview of the current rich-dome combustion system design,
requirements and challenges; followed by the first alternative to rich-domes that have been …

An evaluation of Lagrangian-based, discrete-phase models for multi-component liquid
sprays encountered in the combustors of gas turbine engines is considered. In particular, the …

Micro Gas Turbines (MGT) are an attractive choice for Unmanned Aerial Vehicles (UAV) and
small-scale power generation. Compared with other propulsion systems, MGT have several …

The flow field and spray characteristics of a high shear air-blast nozzle were investigated
numerically and experimentally. Particle dynamics analyzer (PDA) was employed to …

抄録 Trend of the recent combustor technology for civil aircraft engines are reviewed. NOx
reduction is extremely difficult for aircraft engines, which have many strict requirements …