Renewable Aviation Fuel Yield via C8-C14 Feedstock Isomerization

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Solution Overview

Problem

Current processes for producing aviation fuel from renewable sources face a trade-off between cold-flow properties and the yield of naphtha and light ends, resulting in lower aviation fuel component yield and increased production of naphtha and light ends.

Innovation Solution

Selecting a renewable feedstock rich in fatty acids with 8-14 carbon atoms, hydrogenating and deoxygenating it to produce normal paraffins, and then isomerizing these paraffins to generate a product stream rich in branched paraffins, which improves the yield and cold-flow properties of the aviation fuel while reducing naphtha and light ends.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If higher severity operation is used in the isomerization/cracking reactor to produce aviation fuel from renewable feedstocks, then cold-flow properties are improved, but the yield of aviation fuel decreases and naphtha and light ends increase

Engineering Contradiction:
Improvecold-flow propertiesVSAvoidaviation fuel yield
Core Design Contradiction:
TemperatureVSProductivity

Solution Approach 1:

The patent changes the carbon chain length parameter of the feedstock from conventional C15-C18 to C8-C14. This parameter change allows the process to achieve good cold-flow properties without requiring high-severity operation, thereby maintaining high aviation fuel yield while meeting cold-flow specifications.

Inventive Principle:
Principle #35Parameter changes

2Temperature

If higher severity operation is used in the isomerization/cracking reactor, then cold-flow properties are improved, but naphtha and light ends production increases

Engineering Contradiction:
Improvecold-flow propertiesVSAvoidnaphtha and light ends
Core Design Contradiction:
TemperatureVSLoss of substance

Solution Approach 1:

The patent changes the feedstock carbon chain length parameter to C8-C14, which inherently produces better cold-flow properties without requiring high-severity cracking. This reduces unwanted naphtha and light ends formation while achieving the desired cold-flow performance.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If feedstocks with longer carbon chains (C15-C18) are used, then the process is simpler, but the aviation fuel yield is lower and cold-flow properties are poorer

Engineering Contradiction:
Improveprocess simplicityVSAvoidaviation fuel yield
Core Design Contradiction:
Ease of manufactureVSProductivity

Solution Approach 1:

The patent selects feedstocks with C8-C14 carbon chain lengths, which are ideal for producing aviation fuel. This parameter optimization achieves high yield and superior cold-flow properties while maintaining process simplicity through standard hydroprocessing and isomerization operations.

Inventive Principle:
Principle #35Parameter changes

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 approach enhances the yield and cold-flow properties of aviation fuel, achieving higher yields and lower freeze points compared to using feedstocks with longer carbon chains, while maintaining compliance with ASTM D7566 HEFA SPK specifications.

Implementation Method 1

hydrogenating and deoxygenating it to produce normal paraffins

Methodology Applied
Scientific EffectHydrogenation: Hydrogenation

Implementation Method 2

hydrogenating and deoxygenating in a first reaction zone in the presence of hydrogenating and deoxygenating catalyst

Methodology Applied
Scientific EffectDeoxygenation: Reduction

Implementation Method 3

isomerizing these paraffins to generate a product stream rich in branched paraffins

Methodology Applied
Scientific EffectIsomerization: Catalysis

Data Source

PatentUS9914880B2Method of increasing the yield of aviation fuel from renewable feedstocks
Publication Date: 2018.03.13 UOP LLC
  • US9914880B2 patent drawing
  • US9914880B2 patent drawing
  • US9914880B2 patent drawing

AI summary

A method of increasing the yield of renewable aviation fuel is described. A renewable feedstock rich in fatty acids having between 8 and 14 carbon atoms is selected, and the selected feedstock is hydrogenated and deoxygenated in a first reaction zone to provide an effluent rich in normal paraffins having between 9 and 15 carbon atoms. The normal paraffins are isomerized in a second reaction zone to isomerize at least a portion of the normal paraffins. The isomerization reaction mixture may be separated into a product stream comprising a product rich in branched paraffins having between 9 and 15 carbon atoms, which has a higher yield than a product stream made using a renewable feedstock rich in fatty acids having more than 15 carbon atoms.