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FUEL DEOX SIGNED

Optimisation of an on-board adsorbent/catalyst unit for aviation fuel thermal stability improvement

Total Cost €

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EC-Contrib. €

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Partnership

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 FUEL DEOX project word cloud

Explore the words cloud of the FUEL DEOX project. It provides you a very rough idea of what is the project "FUEL DEOX" about.

representative    association    heat    experiments    advantages    oxygen    serve    weight    board    dissolved    trade    flow    exchanger    experimentally    injection    waste    decrease    deoxygenation    deposit    volume    thermal    catalysts    adding    stability    lubricity    adsorbents    off    reduce    recommend    optimized    engines    sfc    calculation    oxidative    fuel    aftstu    size    performance    compositional    solid    bespoke    cooling    temperature    reactions    regime    reynold    catalyst    tendency    trl5    benefit    jet    elimination    sheffield    longevity    ir       sink    carbonaceous    overboard    employing    engine    simultaneous    enhancement    bulk    regimes    leads    small    investigates    chemistry    experimental    aviation    cycle    deoxygenated    efficiency    respect    offers    absorbing    simulator    fuels    savings    moderate    adsorbent    dumped    hirets    optimise    air    quantum    improvement    contains    device    university    separation    extra    yield    signature    vhbr    medium    shows    bleed   

Project "FUEL DEOX" data sheet

The following table provides information about the project.

Coordinator
THE UNIVERSITY OF SHEFFIELD 

Organization address
address: FIRTH COURT WESTERN BANK
city: SHEFFIELD
postcode: S10 2TN
website: www.shef.ac.uk

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country United Kingdom [UK]
 Total cost 344˙046 €
 EC max contribution 344˙046 € (100%)
 Programme 1. H2020-EU.3.4.5.5. (ITD Engines)
 Code Call H2020-CS2-CFP02-2015-01
 Funding Scheme CS2-RIA
 Starting year 2016
 Duration (year-month-day) from 2016-08-01   to  2018-07-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    THE UNIVERSITY OF SHEFFIELD UK (SHEFFIELD) coordinator 344˙046.00

Map

 Project objective

The research programme proposed by the University of Sheffield experimentally investigates the application of an optimized on-board adsorbent/catalyst unit to reduce the tendency of jet fuel that contains dissolved oxygen to produce solid carbonaceous deposit in the fuel system and injection system at moderate temperature regimes. Improved fuel thermal oxidative stability offers the fuel to serve as a better heat sink, absorbing more waste heat from VHBR engines and using the heat to benefit in the engine performance cycle. This leads to more efficiency in comparison to adding extra cooling systems employing bleed air that is dumped overboard, and could yield around 2% SFC improvement in association with heat exchanger weight and volume savings. Furthermore, the elimination of overboard bleed is a potential to reduce IR signature. To achieve the programme goal, the following project objectives are proposed: 1) Optimise the size of the adsorbents/catalysts unit in small scale, bespoke experimental device with respect to flow regime and bulk fuel temperature following a Design of Experiments approach 2) Simultaneous thermal oxidative stability assessment of deoxygenated fuel using low medium scale test device namely, “High Reynold Thermal Stability (HiReTS)” 3) Compositional analysis of deoxygenated fuels with particular focus on side reactions 4) Fuel lubricity assessment 5) Calculation of adsorbent longevity using available quantum chemistry methods 6) Calculation of trade-off between thermal stability enhancement and lubricity decrease using available quantum chemistry methods 7) Project scale up and use of the optimised adsorbent/catalyst unit in a TRL5 scale engine representative jet fuel system simulator, namely the “Aviation Fuel Thermal Stability Test Unit (AFTSTU)” 8) Recommend future development. The oxygen separation by adsorbent/catalysts shows more advantages in comparison to the other deoxygenation methods being developed for aviation fuel thermal stability enhancement.

 Deliverables

List of deliverables.
A proof of agreements existence Other 2019-05-31 11:59:01

Take a look to the deliverables list in detail:  detailed list of FUEL DEOX deliverables.

 Publications

year authors and title journal last update
List of publications.
2017 Alborzi, E, Blakey, S., Dywer, M., Meijer, A
Design of an Onboard Aviation Fuel Deoxygenator Unit for Improvement of Thermal Stability, IASH 2017 - , Rome
published pages: , ISSN: , DOI:
15th International Symposium on Stability, Handling and Use of Liquid Fuels 2020-04-01
2019 Alborzi, E., Gadsby, P., Blakey, S.
The Effect of Variation in Si/Al Ratio of Zeolite on Aviation Fuel Thermal Stability Improvement
published pages: , ISSN: , DOI:
IASH 2019 – 16th International Symposium on Stability, Handling and Use of Liquid Fuels, Los Angeles 2020-04-01
2019 Ehsan Alborzi, Phil Gadsby, Mohammed S. Ismail, Abdolkarim Sheikhansari, Matthew. R. Dwyer, Anthony J. H. M. Meijer, Simon G. Blakey, Mohamed Pourkashanian
Comparative Study of the Effect of Fuel Deoxygenation and Polar Species Removal on Jet Fuel Surface Deposition
published pages: 1825-1836, ISSN: 0887-0624, DOI: 10.1021/acs.energyfuels.8b03468
Energy & Fuels 33/3 2020-04-01

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