Suppr超能文献

使用铂负载的Y型沸石-AlO复合催化剂对正十七烷进行加氢裂化生产可持续航空燃料。

Production of Sustainable Aviation Fuel by Hydrocracking of -Heptadecane Using Pt-Supported Y-Zeolite-AlO Composite Catalysts.

作者信息

Mitsuoka Shunma, Murata Kosuke, Hashimoto Tadanori, Chen Ning, Jonoo Yuki, Kawabe Sho, Nakao Keita, Ishihara Atsushi

机构信息

Division of Chemistry for Materials, Graduate School of Engineering, Mie University, 1577 Kurima Machiya-Cho, Tsu City, Mie Prefecture 514-8507, Japan.

Zeolite Group, Institute of Inorganic Materials, Nanyo Office, Tosoh Corporation, 4560 Kaisei-Cho, Shunan City, Yamaguchi Prefecture 746-8501, Japan.

出版信息

ACS Omega. 2024 Jan 8;9(3):3669-3674. doi: 10.1021/acsomega.3c07678. eCollection 2024 Jan 23.

Abstract

Hydrocracking of fat or Fischer-Tropsch (FT) wax from biomass to produce the jet fuel of sustainable aviation fuel has been one of the key reactions. -Heptadecane, which is one of the model diesel fractions produced from fat or FT wax, has hardly been used for hydrocracking of hydrocarbon for jet fuel production, while -hexadecane has often been used as one of the model compounds for this reaction. In the present study, a HY-zeolite (50 wt %, SiO/AlO = 100)-AlO (50 wt %) composite-supported Pt (0.5 wt %) catalyst [0.5Pt/Y(100)35A] was tested for hydrocracking of -heptadecane using a fixed-bed flow reactor at a H pressure of 0.5 MPa, H flow rate of 300 mL/min, WHSV of 2.3 h, and a catalyst weight of 2 g. Fine-tuning of the temperature to 295 °C achieved the highest selectivity of 74% for the jet fuel fraction C8-C15 with the high conversion of 99%. The jet fuel yield reached 73%, which was almost an ideal maximum yield of 75%. Similar hydrocracking of -hexadecane has just reported the maximum yield of 51% for jet fuel fraction. Further, 0.5Pt/Z(110)35A, which has a composition similar to that of 0.5Pt/Y(100)35A except for the type of zeolite, could not give as high yield of jet fuel as 0.5Pt/Y(100)35A because the rapid conversion to lighter fractions than the jet fuel occurred by the slight increase in the reaction temperature even at a lower temperature range.

摘要

将来自生物质的脂肪或费托(FT)蜡进行加氢裂化以生产可持续航空燃料的喷气燃料,一直是关键反应之一。十七烷是由脂肪或FT蜡生产的典型柴油馏分之一,几乎未被用于烃类加氢裂化以生产喷气燃料,而十六烷常被用作该反应的典型化合物之一。在本研究中,使用固定床流动反应器,在氢气压力0.5MPa、氢气流速300mL/min、重时空速2.3h⁻¹以及催化剂重量2g的条件下,对一种HY型沸石(50wt%,SiO₂/Al₂O₃ = 100)-Al₂O₃(50wt%)复合载体负载的Pt(0.5wt%)催化剂[0.5Pt/Y(100)35A]进行了十七烷加氢裂化测试。将温度微调至295℃时,喷气燃料馏分C₈ - C₁₅的选择性最高可达74%,转化率高达99%。喷气燃料产率达到73%,几乎是理想的最大产率75%。类似的十六烷加氢裂化报道的喷气燃料馏分最大产率仅为51%。此外,0.5Pt/Z(110)35A,其组成与0.5Pt/Y(100)35A相似,只是沸石类型不同,由于即使在较低温度范围内反应温度略有升高,就会快速转化为比喷气燃料更轻的馏分,所以无法获得与0.5Pt/Y(100)35A一样高的喷气燃料产率。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ce59/10809707/94030c480254/ao3c07678_0001.jpg

文献AI研究员

20分钟写一篇综述,助力文献阅读效率提升50倍。

立即体验

用中文搜PubMed

大模型驱动的PubMed中文搜索引擎

马上搜索

文档翻译

学术文献翻译模型,支持多种主流文档格式。

立即体验