Gas jet flow characteristic of high-pressure methane pulsed injection of single-hole cylindrical nozzle

Fuel ◽  
2019 ◽  
Vol 257 ◽  
pp. 116081 ◽  
Author(s):  
Yan Lei ◽  
Jiaxing Liu ◽  
Tao Qiu ◽  
Yunqiang Li ◽  
Yupeng Wang ◽  
...  
2021 ◽  
Author(s):  
Long Liu ◽  
Tianyang Dai ◽  
Qian Xiong ◽  
Yuehua Qian ◽  
Bo Liu

Abstract With increasingly stringent emissions limitation of greenhouse gas and atmospheric pollutants for ship, the direct injection of natural gas on the cylinder head with high-pressure injection is an effective method to make a high power output and decrease harmful gas emissions in marine natural gas dual fuel engines. However, the effects on mixing characteristics of high-pressure natural gas underexpanded jet have not been fully understood. Especially, the injection pressure is up to 30 MPa with large injection quantity and critical surrounding gas conditions for the low-speed two-stroke marine engine. Therefore, this research is focused on the flow and mixing process of the natural gas jet with high-pressure injection under the in-cylinder conditions of low-speed two-stroke marine engine. The gas jet penetration, the distribution of velocity and density, the equivalence ratio and air entrainment have been analyzed under different nozzle hole diameters by numerical simulation. The effects of surrounding gas conditions including pressure, temperature and swirl ratio on air entrainment and equivalence ratio distribution were studied in detail. From the numerical simulation, it is found that the mixing characteristics of natural gas jet can be improved under in-cylinder conditions of higher ambient temperature and swirl ratio, which is relevant to the low-speed two-stroke marine engine.


2007 ◽  
Vol 56 (12) ◽  
pp. 6918
Author(s):  
物理学报
Keyword(s):  

Author(s):  
K. Michael Du¨sing ◽  
Andrea Ciani ◽  
Adnan Eroglu

Alstoms GT24 and GT26 engines feature a unique sequential combustion system [1, 2]. This system consists of a premixed combustor (called EV), which is followed by a high pressure turbine, a reheat combustor (called SEV) and a low pressure turbine (Figure 1). Recently improvements in NOx performance of the SEV have been demonstrated. Starting with relatively simple methods numerous design variants have been tested and down selected. Further down-selection has been done with methods of increased complexity. Overall a fast and cost effective development process has been assured. During the development process the variation coefficient and unmixedness measured and calculated for mixing only systems (CFD and water channel) has proven to be a reliable indicators for low NOx emissions for the real combustion system on atmospheric and high pressure test rigs. To demonstrate this a comparison of both quantities against NOx emissions is shown. The paper focuses on the NOx results achieved during this development and its relation to mixing quantities. Using this relation, together with a detailed understanding of the flow characteristic in the SEV burner, reductions in NOx emissions for GT24 and GT26 SEV burner and lance hardware can be reached using relatively simple methods.


2000 ◽  
Vol 71 (4) ◽  
pp. 585-591 ◽  
Author(s):  
D.N. Kozlov ◽  
B. Hemmerling ◽  
A. Stampanoni-Panariello
Keyword(s):  
Jet Flow ◽  
Gas Jet ◽  

Author(s):  
V. A. Soukhanovskii ◽  
M. G. Bell ◽  
W. R. Blanchard ◽  
J. K. Dong ◽  
R. C. Gernhardt ◽  
...  

Sign in / Sign up

Export Citation Format

Share Document