Bio-jet fuel range in biofuels derived from hydroconversion of palm olein over Ni/zeolite catalysts and freezing point of biofuels/Jet A-1 blends

Fuel ◽  
2021 ◽  
Vol 293 ◽  
pp. 120472
Author(s):  
Pachara Chintakanan ◽  
Tharapong Vitidsant ◽  
Prasert Reubroycharoen ◽  
Prapan Kuchonthara ◽  
Tetsuya Kida ◽  
...  
2018 ◽  
Vol 2 (8) ◽  
pp. 1863-1869 ◽  
Author(s):  
Jiawei Xie ◽  
Lei Zhang ◽  
Xiangwen Zhang ◽  
Peijuan Han ◽  
Junjian Xie ◽  
...  

Biofuels synthesized from lignocellulose-derived platform chemicals are very attractive for sustainable development.


2016 ◽  
Vol 10 (4) ◽  
pp. 485-492 ◽  
Author(s):  
Anna Iakovlieva ◽  
◽  
Oksana Vovk ◽  
Sergii Boichenko ◽  
Kazimierz Lejda ◽  
...  

The work is devoted to the development of alternative jet fuel blended with rapeseed oil-derived biocomponents and study of their physical-chemical properties. The modification of conventional jet fuel by rapeseed oil esters was chosen for this work among the variety of technologies for alternative jet fuels development. The main characteristics of conventional jet fuel and three kinds of biocomponents were determined and compared to the standards requirements to jet fuel of Jet A-1 grade. The most important or identifying physical-chemical properties of jet fuels were determined for the scope of this study. Among them are: density, viscosity, fractional composition, freezing point and net heat of combustion. The influence of rapeseed oil-derived biocomponents on the mentioned above characteristics of blended jet fuels was studied and explained.


Catalysts ◽  
2019 ◽  
Vol 9 (11) ◽  
pp. 886 ◽  
Author(s):  
Wei Wang ◽  
Shaoying Sun ◽  
Fengan Han ◽  
Guangyi Li ◽  
Xianzhao Shao ◽  
...  

Diesel and jet fuel range cycloalkanes were obtained in ~84.8% overall carbon yield with cyclopentanone and furfural, which can be produced from hemicellulose. Firstly, 2,5-bis(furan-2-ylmethyl)-cyclopentanone was prepared by the aldol condensation/hydrogenation reaction of cyclopentanone and furfural under solid base and selective hydrogenation catalyst. Over the optimized catalyst (Pd/C-CaO), 98.5% carbon yield of 2,5-bis(furan-2-ylmethyl)-cyclopentanone was acquired at 423 K. Subsequently, the 2,5-bis(furan-2-ylmethyl)-cyclopentanone was further hydrodeoxygenated over the M/H-ZSM-5(Pd, Pt and Ru) catalyst. Overall, 86.1% carbon yield of diesel and jet fuel range cycloalkanes was gained over the Pd/H-ZSM-5 catalyst under solvent-free conditions. The cycloalkane mixture obtained in this work has a high density (0.82 g mL−1) and a low freezing point (241.7 K). Therefore, it can be mixed into diesel and jet fuel to increase their volumetric heat values or payloads.


2020 ◽  
Vol 44 (1) ◽  
Author(s):  
R. El-Araby ◽  
E. Abdelkader ◽  
G. El Diwani ◽  
S. I. Hawash

Abstract Background Biomass fuels (bio-jet fuel) have recently attracted considerable attention as alternatives to conventional jet fuel. They have become the focus of aircraft manufacturers, engines, oil companies, governments and researchers alike. This study is concerned with the production of biojet fuel using waste cooking oil (WCO). Batch reactor is used for running the experimental study. The catalytic cracking products are investigated by GC mass spectra. Final products from different reaction conditions are subjected to fractional distillation. The (Bio kerosene) fraction was compared with the conventional jet A-1 and showed that it met the basic jet fuel specifications. Optimum reaction conditions are obtained at (450 °C), pressure of (120 bars), catalyst dose (2.5% w/v), reaction time (60 min) and hydrogen pressure 4 atmosphere. The aim of this study is to produce bio aviation fuel according to specifications and with a low freezing point from waste cooking oil in one step using a laboratory prepared catalyst and with a low percentage of hydrogen to complete the process of cracking and deoxygenation in one reactor, which is naturally reflected positively on the price of the final product of bio aviation fuel. Results The results indicated that the product obtained from WCO shows promising potential bio aviation fuels, having a low freezing point (− 55 °C) and that all bio kerosene’s specifications obtained at these conditions follow the international standard specifications of aviation turbine fuel. Conclusion Biojet fuel obtained from WCO has fairly acceptable physico-chemical properties compared to those of petroleum-based fuel. Adjustment of the hydro catalytic cracking reaction conditions was used to control quantities and characteristics of produced bio aviation fuel. Taking into consideration the economic evaluation WCO is preferable as raw material for bio aviation fuel production due to its low cost and its contribution in environmental pollution abatement. Blend of 5% bio aviation with jet A-1 (by volume) can be used in the engine without any modifications and a successful test of blended aviation fuel with 10% bio aviation has been achieved on Jet-Cat 80/120 engine.


2015 ◽  
Vol 129 ◽  
pp. 139-146 ◽  
Author(s):  
Toshiaki Hanaoka ◽  
Tomohisa Miyazawa ◽  
Katsuya Shimura ◽  
Satoshi Hirata

2020 ◽  
Vol 1008 ◽  
pp. 231-244
Author(s):  
Rehab M. El-Maghraby

Aviation industry is considered one of the contributors to atmospheric CO2emissions. It is forced to cut off carbon dioxide emission starting 2020. Current trends in bio-jet production involve mega projects with million dollars of investments. In this study, bio-jet fuel production by blending bio-diesel with traditional jet fuel at different concentrations of bio-diesel (5, 10, 15, 20 vol. %) was investigated. This blending technique will reduce bio-jet production cost compared to other bio-jet techniques. Bio-diesel was originally produced by the transesterification of non-edible vegetable oil (renewable sources), so, its blend with jet fuel will has a reduced carbon foot print. The blend was tested to ensure that the end product will meet the ASTM D1655 international specifications for Jet A-1 and Jet A and can be used in aircrafts.Available data on biodiesel blending with jet fuel in the literature is not consistent, there are many contradictory results. Hence, more investigations are required using locally available feedstocks. The main physicochemical properties for Jet A-1 and Jet A according to ASTM D1655 were tested to check if the blend will be compatible with existing turbojet engine systems. Different tests were conducted; vacuum distillation, smoke point, kinematic viscosity, density, flash point, total acidity and freezing point. In addition, heating value of the blend was calculated. The result was then compared with calculated value using blending indices available in the literature. Blending indices were able to predict the laboratory measured specifications for the studied blends.It was found that only 5% bio-diesel- 95% jet fuel blend (B5) meets ASTM standard for Jet A. Hence, biodiesel can be safely used as a blend with fossil-based jet for a concentration of up to 5% without any change in the ASTM specifications. Freezing point is the most important constrain for this blending technique. Higher blends of biodiesel will cause the bio-jet blend to fail ASTM specifications. In general, blending technique will reduce the cost impact that may have been incurred due to change in infrastructure when using other production techniques.


2021 ◽  
Author(s):  
Anup Rana ◽  
Leandro Cid Gomes ◽  
João Rodrigues ◽  
Hugo Arrou-Vignod ◽  
Johan Sjölander ◽  
...  

The hemiterpene isoprene is a volatile C<sub>5</sub> hydrocarbon, with industrial applications. It is generated today from fossil resources, but can also be made in biological processes. We have utilized engineered photosynthetic cyanobacteria for direct, light-driven production of bio-isoprene from carbon dioxide, and show that isoprene in a subsequent photochemical step, using simulated or natural solar light, can be dimerized into limonene, paradiprene, and isomeric C<sub>10</sub>H<sub>16</sub> hydrocarbons (monoterpenes) in very high yields (above 90% after 44 hours) under sensitized conditions. The optimal sensitizer in our experiments is di(naphth-1-yl)methanone which we can use with a loading of merely 0.1 mol%, and it is easily recycled for subsequent photodimerization cycles. The isoprene dimers generated are a mixture of [2+2], [4+2] and [4+4] cycloadducts, and after hydrogenation this mixture is nearly ideal as a jet fuel drop-in. Importantly, the photodimerization can be carried out at ambient conditions. The high content of hydrogenated [2+2] dimers in our isoprene dimer mix lowers the flash point below the threshold (38 °C), yet, these dimers can be converted thermally into [4+2] and [4+4] dimers. When hydrogenated these monoterpenoids fully satisfy the criteria for drop-in jet fuels with regard to energy density, flashpoint, kinematic viscosity, density, and freezing point.


2019 ◽  
Vol 207 ◽  
pp. 441-447 ◽  
Author(s):  
Genkuo Nie ◽  
Yiying Dai ◽  
Yanan Liu ◽  
Junjian Xie ◽  
Si Gong ◽  
...  

Author(s):  
Yang Lin ◽  
Yuzhen Lin ◽  
Chi Zhang ◽  
Quanhong Xu ◽  
Chih-Jen Sung ◽  
...  

For application to aircraft turbines, the present work experimentally examines the physical and combustion-related properties of an F-T synthetic jet fuel relative to the Chinese standard jet fuel, RP-3. This fuel, derived from coal feedstock, is characterized in terms of its physical properties such as density, flash point, freezing point, surface tension, viscosity, and heating value in accordance with Chinese National Standard Testing Methods. Subsequently, several important characteristics relevant to its use in aircraft turbine engines are investigated using a single cup model combustor rig, including atomization, ignition, blowout, and exhaust emissions experiments are carried out. Preliminary results suggest that the use of coal-derived synthetic jet fuel will not result in adverse effects on the performance of an aircraft turbine combustor relative to conventional aviation kerosene. These initial results support the conclusion that full-scale engine testing is warranted to further investigate the performance of F-T synthetic jet fuels in practical systems, and to determine its ability to act as a “drop-in” replacement for traditional aviation fuel.


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