Upstream Fractionation Layout for Higher-Yield Aviation Fuel
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Solution Overview
Problem
Traditional aviation fuel production processes face inefficiencies due to the direct processing of large-size compounds in isomerization and hydrocracking units, leading to complex operating conditions, reduced yield, and the need for managing molecular sizes and freeze points, with a drag stream of unconverted compounds being unsuitable for jet fuel use.
Innovation Solution
A refining system configuration that reverses the conventional order of dewaxing reactions (hydrocracking and isomerization) and positions the fractionator upstream, allowing for targeted compound processing, recycling unsuitable compounds, and optimizing each reaction step to maximize aviation fuel yield.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Productivity
If large-size compounds are directly processed in isomerization and hydrocracking units, then aviation fuel production can proceed, but operating conditions become overly complex and molecular size management becomes problematic
Solution Approach 1:
The patent applies preliminary action by implementing a fractionation unit upstream of the isomerization and hydrocracking units. This fractionation unit pre-separates the feedstock into different molecular size ranges (C5-10, C10-16, C16-24, C24+) before these streams enter the reaction units. By performing this separation in advance, the subsequent isomerization and hydrocracking units receive feedstock already sized appropriately for their specific functions, eliminating the need for complex real-time molecular size management and simplifying operating conditions while maintaining productivity.
2Speed
If single pass hydrocracking is used, then processing speed is maintained, but a drag stream of unconverted compounds must be removed reducing yield
Solution Approach 1:
The patent applies segmentation by dividing the hydrocracking process into multiple passes with intermediate fractionation steps. After the initial hydrocracking pass, the output is fractionated into different molecular size ranges. The heavier fractions (C16-24, C24+) that were not fully converted are separated and recycled back to the hydrocracking unit for additional processing passes. This segmented approach allows the system to maintain high processing speed through continuous operation while progressively converting unconverted compounds into usable aviation fuel ranges, eliminating the need to discard drag streams and thereby increasing overall yield.
3Ease of manufacture
If fractionator is positioned downstream of reaction units, then conventional processing flow is maintained, but over-cracking occurs producing undesired light ends
Solution Approach 1:
The patent applies inversion by reversing the conventional process configuration. Instead of placing the fractionation unit downstream after isomerization and hydrocracking units, the fractionation unit is positioned upstream before these reaction units. This inverted configuration allows the system to first separate the feedstock into appropriate molecular size ranges, then process each fraction through isomerization and hydrocracking. This prevents over-cracking because each reaction unit receives feedstock already sized for its optimal operation, and any light ends produced can be easily separated and recycled back to the fractionation inlet rather than being lost as undesired byproducts.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
This configuration enhances aviation fuel yield by converting all compounds to suitable sizes, reduces over-cracking, and minimizes light end production, achieving higher efficiency and yield with lower operational severity and capital costs.
Implementation Method 1
fractionating a renewable diesel feedstock in a fractionator to produce a C8− fraction, a C8-18 fraction, and a C18+ fraction
Implementation Method 2
providing the C8-18 fraction to an isomerization reactor to produce an aviation fuel product
Implementation Method 3
supplying at least a portion of the C18+ fraction to a hydrocracking reactor to produce a hydrocracked product
Data Source
AI summary
Embodiments of systems and methods to produce aviation fuel are disclosed. An example of a method to produce aviation fuel includes fractionating a renewable diesel feedstock in a fractionator to produce a C8− fraction, a C8-18 fraction, and a C18+ fraction. Additionally, the method includes providing the C8-18 fraction to an isomerization reactor to produce an aviation fuel product. The method includes supplying at least a portion of the C18+ fraction to a hydrocracking reactor to produce a hydrocracked product. The method further includes recycling at least a portion of the hydrocracked product to the fractionator for fractionating along with the renewable diesel feedstock.


