| Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions | |
Fan XJ(范学军) ; Zhong FQ(仲峰泉); Yu G(俞刚); Li JG(李建国); Sun CJ; Fan XJ
| |
| Source Publication | Journal of Propulsion and Power
 |
| 2009 | |
| Volume | 25Issue:6Pages:1226-1232 |
| ISSN | 0748-4658 |
| Abstract | Catalytic cracking of China no. 3 aviation kerosene using a zeolite catalyst was investigated under supercritical conditions. A three-stage heating/cracking system was specially designed to be capable of heating 0.8 kg kerosene to a temperature of 1050 K and pressure of 7.0 MPa with maximum mass flow rate of 80 g/s. Sonic nozzles of different diameters were used to calibrate and monitor the mass flow rate of the cracked fuel mixture. With proper experiment arrangements, the mass flow rate per unit throat area of the cracked fuel mixture was found to well correlate with the extent of fuel conversion. The gaseous products obtained from fuel cracking under different conditions were also analyzed using gas chromatography. Composition analysis showed that the average molecular weight of the resulting gaseous products and the fuel mass conversion percentage were a strong function of the fuel temperature and were only slightly affected by the fuel pressure. The fuel conversion was also shown to depend on the fuel residence time in the reactor, as expected. Furthermore, the heat sink levels due to sensible heating and endothermic cracking were determined and compared at varying test conditions. It was found that at a fuel temperature of similar to 1050 K, the total heat sink reached similar to 3.4 MJ/kg, in which chemical heat sink accounted for similar to 1.5 MJ/kg. |
| Keyword | Fueled Supersonic Combustor Model Combustor Injection |
| DOI | 10.2514/1.41966 |
| Indexed By | SCI |
| Language | 英语 |
| WOS ID | WOS:000272497300008 |
| WOS Keyword | FUELED SUPERSONIC COMBUSTOR ; MODEL COMBUSTOR ; INJECTION |
| WOS Research Area | Engineering |
| WOS Subject | Engineering, Aerospace |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/33537 |
| Collection | 高温气体动力学国家重点实验室 |
| Corresponding Author | Fan XJ |
| Recommended Citation GB/T 7714 | Fan XJ,Zhong FQ,Yu G,et al. Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions[J]. Journal of Propulsion and Power,2009,25,6,:1226-1232. |
| APA | 范学军,仲峰泉,俞刚,李建国,Sun CJ,&Fan XJ.(2009).Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions.Journal of Propulsion and Power,25(6),1226-1232. |
| MLA | 范学军,et al."Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions".Journal of Propulsion and Power 25.6(2009):1226-1232. |
| Files in This Item: | Download All | |||||
| File Name/Size | DocType | Version | Access | License | ||
| S02.pdf（2295KB） | 开放获取 | -- | View Download | |||
Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.
Edit Comment