Difference between revisions of "Sustainable Aviation Fuel"

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==Figures of Merit==
==Figures of Merit==
The table below show a list of FOMs by which solar electric aircraft can be assessed. The first four (shown in bold) are used to assess the aircraft itself. They are very similar to the FOMs that are used to compare traditional aircraft which are propelled by fossil fuels, the big difference being that 2SEA is essentially emissions free during flight operations. The other rows represent subordinated FOMs which impact the performance and cost of solar electric aircraft but are provided as outputs (primary FOMs) from lower level roadmaps at level 3 or level 4, see the DSM above.
The table below show a list of FOMs by which sustainable aviation fuel can be assessed. The first four (shown in bold) are identified as main FoMs for sustainable aviation fuel with the following reasons: 1)one of the biggest disadvantages of SAF is its cost. 2) In present, SAF blend ratio to the current jet fuel is up to 50%, and this blend ratio needs to be improved for net zero emission. 3) CO2 emission when producing SAF is also needs to be assessed to fairly evaluate the net CO2 emission. The other five FoMs are used for the trade-off of the technology choice used for SAF production.  


[[File:Section 4_.JPG]]
[[File:saf_fom_tab.JPG]]


Besides defining what the FOMs are, this section of the roadmap should also contain the FOM trends over time dFOM/dt as well as some of the key governing equations that underpin the technology. These governing equations can be derived from physics (or chemistry, biology ..) or they can be empirically derived from a multivariate regression model. The table below shows an example of a key governing equation governing (solar-) electric aircraft.
The figure below is an expected SAF blending ratio improvement, assuming the net zero CO2 emission by 2050.


[[File:Section 4_2.JPG]]
[[File:saf_scurve.JPG]]
 
As mentioned above, the cost is a key to assess SAF. We summarize the governing equations given in the literature in the following table.
 
[[File:saf_goveq_tab.JPG]]
 
The following figure is the example of the SAF cost with a HEFA and a FT. The utopia point is left-bottom in those figures.
 
[[File:saf_cost_ex.JPG]]

Revision as of 23:30, 11 October 2023

Technology Roadmap Sections and Deliverables

Our technology roadmap identifier is shown as:

  • 2SAF - Sustainable Aviation Fuel

This indicates that we are dealing with a “level 2” roadmap at the product level, where “level 1” would indicate a market level roadmap and “level 3” or “level 4” would indicate an individual technology roadmap.

Roadmap Overview

Sustainable aviation fuel (SAF) is a strong candidate to deal with global warming in the context of aviation, using low carbon footprint resources such as biomass and waste oil. SAF has a good compatibility with the present aircraft. SAF has similar characteristics to the current jet fuel and can be mixed with it, so the architecture of aircraft does not need to change. On the other hand, another strong alternative for low carbon footprint fuel is hydrogen, which needs the rearchitecting of the aircraft because of its small density and temperature, affecting the vehicle size. The following figure coming from FAA shows SAF is the key toward the ambitious goal of "net zero CO2 emissions" in aviation.

File:Netzero aviation.jpeg Source: netzero

For producing SAF, there are several pathways depending on feedstock and the way of conversion from feedstock to SAF. However, each pathway has advantages and disadvantages such as cost, scalability, and technological readiness. This roadmap tries to identify the impactful technologies on the feasibility of SAF, and show their development plan.

Design Structure Matrix (DSM) Allocation

SAF Hierarchy.png

The above 1SAF tree shows the relationship between other technologies related to the SAF. Specifically, the enabling technologies to SAF, by either the introduction of new materials or a new process are considered. The enabling of SAF with the novel use of existing materials are shown with the connection of SAF to 2HEF, 2ATJ, 2FTC, 2PTF, 3BAF, 3CLS, 3CNB, and 3WCO. The enabling of SAF through the introduction of new processes are shown through SAF connections to 3ROI, 3NTF, 3HPS, 3SEX, 3FNT, 3GAS, 3FTS, 3ELS, 3ICS, and 3MES. In the DSM, the connections between the Level 3 technologies are beyond the scope of considerations for the current investigations for SAF and therefore not populated.

Roadmap Model using OPM

The Object-Process-Diagram (OPD) of the 2SAF - Sustainable Aviation Fuel roadmap in the figure below. This diagram shows the processes (Pretreating, and SAF Converting) for producing SAF with the representative pathways with different feedstocks. We include four different SAF producing categories: 1) Hydroprocessed Esters and Fatty Acids(HEFA) with recycled oils, bio-oils, and animal fat, 2) Alcohol-to-Jet(AtJ) with cellulose, 3) Fischer-Tropsch(FT) with coal, natural gas, and biomass, and 4) Power-to-Liquid(PtL) with water and CO2.

Saf overview opd.png

The object-process language (OPL) is also shown as follows.

Saf overview opl1.png Saf overview opl2.png

Figures of Merit

The table below show a list of FOMs by which sustainable aviation fuel can be assessed. The first four (shown in bold) are identified as main FoMs for sustainable aviation fuel with the following reasons: 1)one of the biggest disadvantages of SAF is its cost. 2) In present, SAF blend ratio to the current jet fuel is up to 50%, and this blend ratio needs to be improved for net zero emission. 3) CO2 emission when producing SAF is also needs to be assessed to fairly evaluate the net CO2 emission. The other five FoMs are used for the trade-off of the technology choice used for SAF production.

File:Saf fom tab.JPG

The figure below is an expected SAF blending ratio improvement, assuming the net zero CO2 emission by 2050.

File:Saf scurve.JPG

As mentioned above, the cost is a key to assess SAF. We summarize the governing equations given in the literature in the following table.

File:Saf goveq tab.JPG

The following figure is the example of the SAF cost with a HEFA and a FT. The utopia point is left-bottom in those figures.

File:Saf cost ex.JPG