Browse Topic: Jet fuel

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Aircraft and Aircraft Engine Fuel Pump Low Lubricity Fluid Endurance TestARP1797B (Current)11/26/2025
This procedure is intended to apply to fuel pumps. This procedure will be defined in terms of recommended test fluid, test setup, test conditions, and test method. This procedure may be used for other fuel system components, by testing in conjunction with the pump, which normally supplies the component inlet flow, or a substitute test pump of similar capacity. This procedure may be used, with variations in test conditions and test fluid for performing pump evaluation tests. Tests at progressively increasing pump speeds and pressures will provide design limitation data. Alternate test periods on a test pump and another pump, of a design for which actual service durability is known, will provide useful comparison data.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Aviation Lubricant Tribology Evaluator (ALTE) Method to Determine the Lubricating Quality of Gas Turbine LubricantsARP6255A (Current)11/26/2025
Employing ‘ball-on-cylinder’ philosophy, a non-rotating steel ball is held in a vertically mounted chuck and using an applied load is forced against an axially mounted steel cylinder. The test cylinder is rotated at a fixed speed while being partially immersed in a lubricant reservoir. This maintains the cylinder in a wet condition and continuously transports a lubricating film of test fluid to the ball and cylinder interface. The diameter of the wear scar generated on the test ball is used as a measure of the fluid’s lubricating properties. The apparatus can be used, by adjusting the operating conditions, to reproduce two different wear mechanisms; mild and severe wear, the ALTE therefore has the ability to assess a lubricant’s performance in that regard.
E-34 Propulsion Lubricants Committee
SAE TOMORROW TODAY: A Breakthrough in Sustainable Aviation Fuel1350202/17/2025
We often hear about sustainable fuel options when it comes to vehicles, but what about aerospace? With aviation fuel demand expected to rise to 160 billion gallons per year by 2050, new and innovative Sustainable Aviation Fuel (SAF) pathways are certainly needed. In response, CleanJoule has developed a proprietary manufacturing process that produces SAF with 10% higher energy density than average Jet A fuel. This process utilizes abundant biomass residue to create a cost-effective, drop-in replacement for conventional jet fuel. To learn more, we sat down with Mukund Karanjikar CEO, to discuss CleanJoule's mission is to create accessible, affordable and abundant SAF and reduce the aerospace industry's reliance on fossil fuels. We'd love to hear from you. Share your comments, questions and ideas for future topics and guests to podcast@sae.org. Don't forget to take a moment to follow SAE Tomorrow Today--a podcast where we discuss emerging technology and trends in mobility with the leaders
Hineman, Marcie
Experimental and Numerical Investigation of Combustion and Noise, Vibrations, and Harshness Emissions in a Drone Jet Engine Fueled with Synthetic Paraffinic Kerosene01-17-01-000608/14/2023
Emissions and effects of climate change have prompted study into fuels that reduce global dependence on traditional fuels. This study seeks to investigate engine performance, thermochemical properties, emissions, and perform NVH analysis of Jet-A and S8 using a single-stage turbojet engine at three engine speeds. Experimental Jet-A results were used to validate a CFX simulation of the engine. Engine performance was quantified using thermocouples, pressure sensors, tachometers, flow meters, and load cells fitted to the engine. Emissions results were collected using an MKS Multigas Emissions Analyzer that examined CO, CO₂, H₂O, NOx, and THC. NVH analysis was conducted using a multifield, free-field microphone, and triaxial accelerometer. This study found that Jet-A operates at higher temperatures and pressures than S8, and S8 requires higher fuel flow rates than Jet-A, leading to poorer efficiency and thrust. S8 produced stronger vibrations over 5 kHz compared to Jet-A. S8 showed a
Soloiu, Valentin, Mcafee, John, Ilie, Marcel, Rowell, Aidan, Willis, James, Dillon, Nicholas
Evaluation and Comparison of Performance, Combustion characteristic, NOx and Particle Emission of JP-8, Gasoline and Diesel fuels in a Military Heavy duty 38.8 liters Compression Ignition Diesel Injection Engine Applying with EGR2021-01-118309/21/2021
Global emissions and stringent emission legislations have compelled us to search for alternative fuels for heavy-duty diesel engines. Evaluating the effect of JP-8 and gasoline on heavy-duty diesel engine performance and emissions is important for military combat vehicles under the "multi-fuel strategy program". Performance and fuel economy penalties are well established with the operation of a heavy-duty diesel engine with JP-8 and gasoline. Experimental studies have also suggested that JP-8 and gasoline have great potential for lowering NOx emissions. In the presented experimental study, the impact of using JP-8 and gasoline was evaluated on a military heavy-duty diesel engine. Engine combustion characteristics, performance, and emissions, especially NOx and nanoparticle emissions, were evaluated. All these parameters were compared for diesel, JP-8 and gasoline fuels by applying 7% EGR with supercharging at different load conditions for a heavy-duty, 12-cylinder, 580 kW, and 38.8
Pandey, Anand, Nandgaonkar, Milankumar, Varghese, Anil, sambasivan, Suresh, sonawane, C
DRYING OF THERMOSETTING COMPOSITE MATERIALSARP4977 (Current)05/14/2021
This SAE Aerospace Recommended Practice (ARP) describes standard methods for drying commercial aircraft composite structures prior to repair and gives general guidelines on use and applicability. It addresses the removal of liquids that have collected inside the structures through open damage, microcracks, or porosity and the removal of absorbed moisture from the composite material. The methods described in this document shall only be used when specified in an approved repair document or with the agreement of the original equipment manufacturer (OEM) or regulatory authority. If this document is used for the drying of materials other than thermosetting composite materials, the fitness for this purpose must be determined by the user.
AMS CACRC Commercial Aircraft Composite Repair Committee
Q&A21TOFHP02_1102/01/2021
Commercial vehicles run under a wide range of operating conditions and duty cycles - not all are well-suited for battery-electric propulsion, particularly in the near term. For those hard-to-electrify vehicles, renewable diesel is a viable option to reduce greenhouse-gas emissions “practically overnight,” according to Matt Leuck, technical manager for Renewable Road Transportation in North America for Neste, which claims to be the world's largest producer of renewable diesel and jet fuel. Preparing to participate in the “Low/Zero Carbon Fuels” technical session during the SAE Government/Industry Digital Summit on February 2-3, Leuck said that Neste sees strong, sustained growth for renewable diesel in medium- and heavy-duty road vehicles, as well as in other segments such as mobile machines used at mines and construction sites. “In fact, demand growth has the potential to increase fivefold in the decades ahead,” he shared. “This growth is driven by two key things: end-users are setting
Gehm, Ryan
Connectors, Fiber Optic, Advanced, Circular or Rectangular, Plug and Receptacle, Environment Resistant, Removable Termini/Contacts, General Specification ForAS5590B (Current)11/30/2020
This specification covers the performance requirements for a plug and receptacle. The connector inserts may contain multiple termini or multiple termini and electrical contacts. The connectors use removable termini, or removable termini and electrical contacts, and are capable of operating within a temperature range of −65 to +200 °C (see 1.2.1.1). These connectors are supplied under AS9100 reliability assurance program.
AS-3 Fiber Optics and Applied Photonics Committee
Connectors, Fiber Optic, Advanced, Circular or Rectangular, Plug and Receptacle, Environment Resistant, Removable Termini/Contacts, General Specification ForAS5590B-TEST-REC (Historical)11/30/2020
This specification covers the performance requirements for a plug and receptacle. The connector inserts may contain multiple termini or multiple termini and electrical contacts. The connectors use removable termini, or removable termini and electrical contacts, and are capable of operating within a temperature range of −65 to +200 °C (see 1.2.1.1). These connectors are supplied under AS9100 reliability assurance program.
AS-3 Fiber Optics and Applied Photonics Committee
Vehicle, Magnetic Particle Inspection Petroleum BaseAMS2641D (Current)10/09/2020
This specification covers two types of refined hydrocarbon compounds in the form of liquids. This specification only covers newly manufactured materials.
AMS K Non Destructive Methods and Processes Committee
Fluid, Jet ReferenceAMS2629F (Current)03/12/2020
This specification covers a mixture of liquid hydrocarbons and soluble additives.
AMS G9 Aerospace Sealing Committee
Green Jet Fuel Additive Made from Acetone Plus LightTBMG-3617303/01/2020
A domestically generated additive was made by taking biomass-derived acetone — common nail polish remover — and using light to upgrade it to higher-mass hydrocarbons. It can be blended with conventional jet fuel to fly while providing environmental benefits.
Engineered Solutions for Enclosure Sealing and InsulationTBMG-3566812/01/2019
In the aerospace and defense industries, enclosure sealing and insulation needs to meet challenging and complex requirements. For example, the EMI gaskets that are used in military touchscreens must shield sensitive electronics from electromagnetic interference (EMI) while providing electrical conductivity and ensuring environmental sealing. These enclosure gaskets must also cushion the unit from mechanical shock and avoid interfering with the display's touch function.
Low- to High-Temperature Reaction Transition in a Small-Bore Optical Gasoline Compression Ignition (GCI) Engine03-12-05-003108/19/2019
Abstract This study shows the development of low-temperature and high-temperature reactions in a gasoline-fuelled compression ignition (GCI) engine realizing partially premixed combustion for high efficiency and low emissions. The focus is how the ignition occurs during the low- to high-temperature reaction transition and how it varies due to single- and double-injection strategies. In an optically accessible, single-cylinder small-bore diesel engine equipped with a common-rail fuel injection system, planar laser-induced fluorescence (PLIF) imaging of formaldehyde (HCHO-PLIF), hydroxyl (OH-PLIF), and fuel (fuel-PLIF) has been performed. This was complemented with high-speed imaging of combustion luminosity and chemiluminescence imaging of cool flame and OH*. The diagnostics were performed for two different fuels including conventional diesel as a reference case and then a kerosene-based jet fuel which is a low-ignition quality fuel with cetane number of 30, firstly with single near top
Goyal, Harsh, Zhang, Yilong, Kook, Sanghoon, Kim, Kenneth S., Kweon, Chol-Bum
Identification and Quantification of Phosphate Ester-Based Hydraulic Fluid in Jet Fuel04-12-01-000303/13/2019
Phosphate ester-based hydraulic fluids are commonly used in aviation, due to their fire-resistant properties. However, contamination of jet fuel with hydraulic fluid may cause serious engine failure, hot corrosion of metals, and swelling of elastomer and polymer seals. Identifying and quantifying hydraulic fluids in jet fuels using chromatography is challenging since common hydraulic fluids, such as ExxonMobil™ HyJet™ V and Skydrol™ LD-4, are composed of tri-butyl phosphate, the main peak of which overlaps with peaks from jet fuels in chromatograms. In this work, three techniques to separate and differentiate the jet fuel peaks from the tri-butyl phosphate peaks were developed. Two methods are based on a solid phase extraction (SPE) procedure followed by identification and quantification, which is carried out using a gas chromatograph equipped with a mass spectrometer or a flame ionization detector. The third technique is single-staged, where the separation and analysis are carried out
Stamker Gertopski, Diana, Tartakovsky, Konstantin, Rabaev, Moshe
Sleeve, Hose Assembly, Fire ProtectionAS1072F (Current)01/07/2019
This standard defines the requirements for bulk protective sleeve to provide fire resistance for aircraft hose assemblies, which will enable these assemblies to meet the requirements of AS1055. NOTE: Use of this sleeve does not eliminate the need to demonstrate that the sleeved assemblies will meet the applicable requirements of AS1055.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Novel Turboelectric Aircraft DesignTBMG-2886105/01/2018
NASA Langley Research Center has developed a novel aircraft design that can carry 150+ passengers over a range of 3,500 nautical miles. Key features include a turboelectric propulsion system, twin underwing turbofans, and a rear-fuselage, electrically driven, boundary layer ingesting fan. The design is developed for single-aisle-class aircraft (the largest commercial transport class in the world) to significantly reduce fuel burn compared to current aircraft.
The Application of New Approaches to the Analysis of Deposits from the Jet Fuel Thermal Oxidation Tester (JFTOT)2017-01-229310/08/2017
Studies of diesel system deposits continue to be the subject of interest and publications worldwide. The introduction of high pressure common rail systems resulting in high fuel temperatures in the system with the concomitant use of fuels of varying solubilizing ability (e.g. ULSD and FAME blends) have seen deposits formed at the tip of the injector and on various internal injector components. Though deposit control additives (DCAs) have been successfully deployed to mitigate the deposit formation, work is still required to understand the nature and composition of these deposits. The study of both tip and internal diesel injector deposits (IDID) has seen the development of a number of bench techniques in an attempt to mimic field injector deposits in the laboratory. One of the most used of these is the Jet Fuel Thermal Oxidation Tester or JFTOT (ASTM D3241). The tester was originally designed to assess the oxidation of jet fuel, based on the principle that low stability fuels produce
Barker, Jim, Reid, Jacqueline, Angel Smith, Sarah, Snape, Colin, Scurr, David, Langley, Graham, Patel, Krina, Carter, Anastarsia, Lapthorn, Cris, Pullen, Frank
Kilohertz Mie Scattering and OH* Chemiluminescence Imaging of JP-8 Multiple Injections Using a 250 MPa Fuel Injector2017-01-083203/28/2017
The objective of the study was to investigate the spray and combustion characteristics of Jet Propellant-8 (JP-8) using a high-pressure fuel injector which is capable of up to 250-MPa fuel injection pressure. Experiments were performed in a constant-pressure flow-through combustion chamber at the ambient conditions of 825 K and 6 MPa for the oxygen concentration of 0 and 21%. JP-8 was injected over a range of fuel injection pressures from 50 to 250 MPa for single injection events to establish a baseline operation. Pilot and post injections were used to study the effect of multiple injections on spray and combustion of the high-pressure fuel injector. Both pilot and post injection separation times and quantities were systematically varied. JP-8 spray and combustion events were imaged at 75 kHz using a combination of Mie scattering and OH* chemiluminescence imaging. The Mie scattering results showed that spray atomization and mixing was enhanced with increasing fuel injection pressure
Temme, Jacob, Coburn, Vincent, Kweon, Chol-Bum
Fluid, Jet ReferenceAMS2629E (Historical)02/08/2017
This specification covers a mixture of liquid hydrocarbons and soluble additives.
AMS G9 Aerospace Sealing Committee
Energy Storage for Commercial Hybrid Electric Aircraft2016-01-201409/20/2016
Energy storage options for a hybrid electric commercial single aisle aircraft were investigated. The propulsion system features twin Geared Turbofan™ engines in which each low speed spool is assisted by a 2,500 HP electric motor during takeoff and climb. During cruise, the aircraft is powered solely by the turbine engines which are sized for efficient operation during this mission phase. A survey of state of the art energy storage options was conducted. Battery, super-capacitor, and flywheel metrics were collected from the literature including Specific Energy (Wh/kg), Volumetric Energy Density (Wh/L), Specific Power (W/kg), Cost ($/kWh), and Number of Cycles. Energy storage in fuels was also considered along with various converters sized to produce a targeted quantity of electric power. The fuel and converters include fuel cells (both proton exchange membrane and solid oxide operating on hydrogen or on jet fuel) and a turbogenerator (jet fuel or LNG). The various energy storage options
Rheaume, Jonathan M., Lents, Charles
Ball-On-Cylinder (BOC) Aircraft Turbine Fuel Lubricity TesterAIR1794A (Historical)05/13/2016
This metric SAE Aerospace Information Report (AIR) details a ball-on-cylinder (BOC) test device and specifies a method of rating the relative lubricity of aviation turbine fuel samples. The BOC produces a wear scar on a stationary steel ball by forcing it with a fixed load against a fuel wetted steel test ring in a controlled atmosphere. The test ring is rotated at a fixed speed so its surface is wetted by a momentary exposure to the fluid under test. The size of the wear scar is a measure of the test fluid lubricity and provides a basis for predicting friction or wear problems.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Spray Characterization and Ignition Delay Measurements of JP-8 and IPK in a Constant-Pressure Flow Chamber2016-01-073604/05/2016
This research compares the spray development and combustion characteristics of jet propellant 8 (JP-8) and iso-paraffinic kerosene (IPK) through a range of diesel engine in-cylinder operating conditions. Non-reacting spray experiments were performed in a constant-pressure flow chamber with 99% nitrogen gas composition at constant temperature (900 K) and densities ranging from 11-56 kg/m3. Near-simultaneous, high-speed Mie and schlieren images of the spray were acquired to measure the liquid and vapor penetration lengths of the non-reacting jet. Reacting experiments, consisting of photodiode measurements and intensified high-speed movies of OH* chemiluminescence, were performed at the same thermodynamic conditions as the non-reacting experiments, except with a 21%/79% oxygen/nitrogen ambient gas composition. Measurements of the rate of injection, issued from a single-hole axial common-rail fuel injector, showed negligible differences between the fuels. The non-reacting liquid length of
Tess, Michael, Kurman, Matthew, Kweon, Chol-Bum
A Technical Evaluation of New Renewable Jet and Diesel Fuels Operated in Neat Form in Multiple Diesel Engines2016-01-082904/05/2016
The US Navy is in the process of evaluating Catalytic Hydrothermal Conversion Jet fuel (CHCJ-5) for inclusion in the JP-5 specification, MIL-DTL-5624, and evaluating Catalytic Hydrothermal Conversion Diesel fuel (CHCD-76) for inclusion in the F-76 specification, MILDTL-16884. CHC fuels are produced from renewable feedstocks such as triglycerides, plant oils, and fatty acids. A Catalytic Hydrothermolysis process chemically converts these feedstocks into a mixture of paraffins, cycloparaffins, aromatics, olefins, and organic acids. The resulting mixture is then hydroprocessed and fractionated to produce a kerosene (or diesel) product having a distillation profile comparable to traditional petroleum derived fuels. The end product is a fuel that is able to meet the jet (or diesel) chemical and physical MIL-SPEC requirements without blending with conventional petroleum fuels. Detailed physical and chemical characterizations are presented showing these new renewable fuels in neat form have
McDaniel, Andrew, Dickerson, Terrence, Luning-Prak, Dianne, Hamilton, Len, Cowart, Jim
Fusible-Core PolymerTBMG-2313810/01/2015
Egmond Plastic Alkmaar, The Netherlands +31-72-5614644
Water Solubility in Different Alternative Jet Fuels: A Comparison with Petroleum-Based Jet Fuel2015-01-256309/15/2015
The paper presents an extensive assessment of the hygroscopic characteristics of a number of alternative jet fuel blends. These are blended with conventional Jet A-1 to conform with current aviation standards at a 50:50 ratio by volume, except for DSHC (Direct Sugar to Hydrocarbon), which is blended at 10% DSHC and 90% Jet A-1. Given the lack of information available on the water solubility of alternative jet fuels, an effective analysis of experimental data about this characteristic in six different alternatives was performed. These included four ASTM approved alternatives (two Fischer-Tropsch (FT) synthetics from coal and natural gas, one HEFA (Hydroprocessed Esters and Fatty Acids) derived from camelina and DSHC. An extra two alternatives currently under consideration for ASTM approval were also tested; ReadiJet and an ATJ (Alcohol to Jet). Water solubility-temperature curves were created and compared to the Jet A-1 reported in the CRC (Coordinating Research Council) Handbook of
Charro, Alberto, Baena, Solange, Lam, Joseph K-W
Finite Element Analysis Simulation of a Fireproof Test for an Aircraft Propulsion Engine Mount Structure Made of Titanium2015-01-262109/15/2015
Aviation regulations requires that engine mounts, and other flight structures located in designated fire zones must be constructed of fireproof material so that they are capable of withstanding the effects of fire. Historically, steel is defined as being inherently fireproof, however, titanium was not. Therefore, a fireproof test was conducted using 6AL-4V titanium structure for the attachment of the propulsion system on a mid-size business jet to satisfy FAA Federal Aviation Requirement 25.865. To determine if the titanium structure would be able to support normal operating loads during the fire event, finite element analysis was performed on the titanium structure simulating the fire test. The fire test simulates a fire on the aircraft from the propulsion system by using a burner with jet fuel exposing the component to a 2000 °F (1093°C) flame. The 2000 °F (1093°C) Flame is calibrated based on FAA Advisory Circular AC20-135. The 2000 °F (1093°C) flame is modeled as a series of
Leicht, Douglas
The Jet Fuel Hydrodynamic Cavitation Bubble Size with Cavitation Power and Energy from Rayleigh-Plesset Equation2015-01-238909/15/2015
Cavitation erosion in aircraft engine and control systems is a major concern in hydrodynamic power units. In developing turbulent flow of low pressure and high velocities, a certain amount of cavitation erosion is not unusual. Cavitation can occur with the presence of fuel vapor or air bubbles dissolved in the fuel tank that are transported through the system. Cavitation erosion is caused by collapse of the bubble, which occurs violently and creates a pressure shock wave of fluid. Striking a solid surface, the shock wave can cause progressive damage if it persists. A kinetic cavitation power rate is developed to make a meaningful estimation of the cavitation erosion rate theoretically, which then can be validated with laboratory experiments. Theoretically, we manipulate parameters such as bubble size, collapse pressure, and energy for a given fuel system design, finding variation within each component of the system. However, cavitation erosion rates vary wildly even when relative
Ni, William W., Cass, Michael, Bartholme, Daniel
Characterization of the Ultrafine and Black Carbon Emissions from Different Aviation Alternative Fuels2015-01-256209/15/2015
This study reports gaseous and particle (ultrafine and black carbon (BC)) emissions from a turbofan engine core on standard Jet A-1 and three alternative fuels, including 100% hydrothermolysis synthetic kerosene with aromatics (CH-SKA), 50% Hydro-processed Esters and Fatty Acid paraffinic kerosene (HEFA-SPK), and 100% Fischer Tropsch (FT-SPK). Gaseous emissions from this engine for various fuels were similar but significant differences in particle emissions were observed. During the idle condition, it was observed that the non-refractory mass fraction in the emitted particles were higher than during higher engine load condition. This observation is consistent for all test fuels. The 100% CH-SKA fuel was found to have noticeable reductions in BC emissions when compared to Jet A-1 by 28-38% by different BC instruments (and 7% in refractory particle number (PN) emissions) at take-off condition. BC emissions from this fuel were lower than from Jet A-1 by 45-50% (and 25-26% in refractory PN
Chan, Tak W., Chishty, Wajid, Davison, Craig, Buote, David
Effects of Ice Accretion in an Aircraft Protective Mesh Strainer of a Fuel Pump2015-01-244909/15/2015
This paper focuses on the investigation of the nature, process and effects of ice accretion on different feed pump strainers upstream of the aircraft feeding system. A suitable test rig was designed to circulate Jet A-1 containing water/ice contaminants at cold temperatures through the strainers. Following an extensive literature review, a number of screening tests were performed. These provided a strong base for an exhaustive study of fuel icing in the dynamic environment offered by the test rig. The effects of the rate of fuel cooling on the nature of ice were examined. As expected, it was observed that the yield of ice generated on the mesh screen increased with the water concentration in the fuel. It was also revealed that at higher cooling rates, a crust of snow formed on top of softer ice on the mesh screen. This phenomenon induced a slight drop in pressure across the mesh screen, indicating that the permeability of the crust layer is lower, but still allowed the passage of fuel
Baena, Solange, Lam, Joseph K-W, Lawson, Craig
Start-up and Steady-State Performance of a New Renewable Alcohol-To-Jet (ATJ) Fuel in Multiple Diesel Engines2015-01-090104/14/2015
A new Alcohol To Jet (ATJ) fuel has been developed using a process which takes biomass feedstock to produce a branched butanol molecule. Further dehydration, reforming and hydro-treating produced principally a highly branched C12 iso-paraffin molecule. This ATJ fuel with a low cetane value (DCN = 18) was blended with Navy jet fuel (JP5) in various quantities and tested in order to determine how much ATJ could be blended before diesel engine operation became problematic (the US Navy and Marine Corps may use jet fuel in their diesel engines). Blends of 20%, 30% and 40% ATJ (by volume) were tested with jet fuel. The Derived Cetane Number (DCN) falls from 45 for the base JP5 to 38 with the 40% ATJ component blended in. Engine start performance was evaluated on two Yanmar engines and a Waukesha CFR diesel engine and showed that engine start times increased steadily with increasing ATJ content. Longer start times with increasing ATJ content were the result of some engine cycles with poor
Dickerson, Terrence, McDaniel, Andrew, Williams, Sherry, Luning-Prak, Dianne, Hamilton, Len, Bermudez, Eric, Cowart, Jim
A Fuel Surrogate Validation Approach Using a JP-8 Fueled Optically Accessible Compression Ignition Engine2015-01-090604/14/2015
An experimental fuel surrogate validation approach is proposed for a compression ignition application, and applied to validate a Jet-A POSF 4658 fuel surrogate. The approach examines the agreement of both physical and chemical properties of surrogate and target fuels during validation within a real compression-ignition engine environment during four sequential but distinct combustion phases. In-cylinder Mie Scattering measurements are applied to evaporating sprays to compare the behavior of the surrogate, its target fuel, and for reference, n-heptane. Early mixture formation and low temperature reaction behavior were investigated using 2-D broadband chemiluminescence imaging, while high temperature ignition and combustion chemistry were studied using OH chemiluminescence imaging. The optical measurements were combined with cylinder pressure-based combustion analysis, including ignition delay and premixed burn duration, to validate the global behavior of the surrogate. Engine-out UHC
Yu, Xin, Luo, Xi, Jansons, Marcis, Kim, Doohyun, Martz, Jason, Violi, Angela
Flying on VegetationTBMG-2074410/01/2014
Fuel is expensive for airlines. According to sources interviewed for this article, fuel accounts for 30 to 50% of operating costs, depending on the size of the aircraft. And fuel prices remain volatile.
Propulsion: Energy Sources14AERP10_0110/01/2014
Flying on Vegetation: Airlines, aircraft companies, and other stakeholders are taking the long view in developing sustainable alternatives to petroleum-based jet fuels. Fuel is expensive for airlines. According to sources interviewed for this article, fuel accounts for 30 to 50% of operating costs, depending on the size of the aircraft. And fuel prices remain volatile. At the same time, there are few alternatives to powering aircraft. While land transport has some available options-think electric vehicles and hydrogen fuel cells-aviation depends on liquid fuels with high energy density. Emissions are another concern. According to the Air Transport Action Group (ATAG), aviation is responsible for 2% of global manmade CO2 emissions.
Morey, Bruce
The Compatibility Study of Aircraft Fuel Tank Elastomers with Synthesized Paraffinic Kerosine and its Blends2014-01-900109/01/2014
The synthetic paraffinic kerosine (SPK) produced via HEFAs is of great interest for civil aviation industry as it exhibits an excellent thermal oxidative stability with significantly lower particulate matter emission. However, due to its aromatic free characteristics, the widespread use of SPK is limited by its compatibility with non-metal materials such as fuel tank elastomers. In this research the compatibility of SPK and its blends with widely used aircraft fuel tank elastomers were systematically studied. Experimental results demonstrated the volume swellability of all selected materials showed a linear relationship with volume percentage of No.3 jet fuel in SPK blend. The increase of volume percentage of No.3 jet fuel in the SPK blend increased volume swellability for all materials except fluorosilicone gasket. The alkyl benzenes and naphthalenes in the blend acted as the hydrogen donors, which facilitated the formation of polymer matrix and led to the increase of the distance
Chen, Kai
Comparison of Soot Formation For Diesel and Jet-A in a Constant Volume Combustion Chamber Using Two-Color Pyrometry2014-01-125104/01/2014
The measurement of the two-color line of sight soot and KL factor for NO.2 diesel and jet-A fuels was conducted in an optical constant volume combustion chamber by using a high speed camera under 1000 K ambient temperature and varied oxygen concentration conditions. The ambient conditions were set as follows: four oxygen cases including 10%, 15%, 18% and 21% at 1000 K ambient temperature. KL factor and soot temperature were determined based on the two-color pyrometry technique using two band-pass filters with wavelengths of 650 nm and 550 nm. The results show that low soot temperature is observed in the upstream inner flame along the centerline, which is surrounded by high soot temperature regions, and a high KL factor is found in the same region with a low soot temperature. The results under different times suggest that soot temperature is higher for high O2 conditions during the entire flame development; meanwhile, both integrated KL factor and soot area decrease with the increase of
Jing, Wei, Roberts, William, Fang, Tiegang
Experimental Validation and Combustion Modeling of a JP-8 Surrogate in a Single Cylinder Diesel Engine2014-01-137604/01/2014
This paper presents the results of an experimental investigation on a single cylinder engine to validate a two-component JP-8 surrogate. The two-component surrogate was chosen based on a previous investigation where the key properties, such as DCN, volatility, density, and lower heating value, of the surrogate were matched with those of the target JP-8. The matching of the auto-ignition, combustion, and emission characteristics of the surrogate with JP-8 was investigated in an actual diesel engine environment. The engine tests for the validation of the surrogate were conducted at an engine speed of 1500 rpm, a load of 3 bar, and different injection timings. The results for the cylinder gas pressure, ignition delay period, rate of heat release, and the CO, HC, and NOx emissions showed a good match between the surrogate and the target JP-8. However, the engine-out particulate matter for the surrogate was lower than that for the JP-8 at all tested conditions. These findings are presented
Shrestha, Amit, Joshi, Umashankar, Zheng, Ziliang, Badawy, Tamer, Henein, Naeim, Sattler, Eric, Schihl, Peter
Role of Volatility in the Development of JP-8 Surrogates for Diesel Engine Application2014-01-138904/01/2014
Surrogates for JP-8 have been developed in the high temperature gas phase environment of gas turbines. In diesel engines, the fuel is introduced in the liquid phase where volatility plays a major role in the formation of the combustible mixture and autoignition reactions that occur at relatively lower temperatures. In this paper, the role of volatility on the combustion of JP-8 and five different surrogate fuels was investigated in the constant volume combustion chamber of the Ignition Quality Tester (IQT). IQT is used to determine the derived cetane number (DCN) of diesel engine fuels according to ASTM D6890. The surrogate fuels were formulated such that their DCNs matched that of JP-8, but with different volatilities. Tests were conducted to investigate the effect of volatility on the autoignition and combustion characteristics of the surrogates using a detailed analysis of the rate of heat release immediately after the start of injection. In addition, the effect of volatility on the
Zheng, Ziliang, Lee, PO-I, Shrestha, Amit, Badawy, Tamer, Lai, Ming-Chia, Henein, Naeim, Sattler, Eric
2013 Create the Future Design: Transportation & Automotive Category WinnerTBMG-1774411/01/2013
Carl Lawrence, Becky English, Graham Hill, John Murino, Elaine Thorndike, Gaby Aweida, Carl Talkington, Rob Kammerling, Kim Hedberg, Nancy Balch, Ilse Gayl and Ron Gremban Swift Tram, Inc., Boulder, CO
Comparison and Evaluation of Wear, Performance and Emission of Diesel, Karanja Oil Biodiesel and JP-8 in a Military 585 kW CIDI Engine2013-01-265810/14/2013
Investigating the impact of Karanja oil biodiesel and JP-8 fuel on diesel engine performance, emission and wear are very important for military track and wheeled vehicles due to their great potential as alternative fuels. In the present study, a military 585 kW CIDI engine was fuelled and tested with diesel, Karanja oil biodiesel and JP-8 respectively. The performances of fuels were evaluated in terms of brake horse power, specific fuel consumption, brake specific energy consumption, brake mean effective pressure, thermal efficiency and heat release rates. The emission of carbon monoxide (CO), unburnt hydrocarbon (UHC), and oxides of nitrogen NOx with the three fuels were also compared. Both Karanja oil, after transesterification and JP-8 exhibit the properties (density, viscosity and calorific value) within acceptable limits of ASTM standard. Performance of both JP-8 and pure Karanja oil biodiesel were slightly lower than diesel. Emissions of CO and UHC were found lower with both
Pandey, Anand Kumar, Nandgaonkar, Milankumar
Camelina-Based Biofuel Shows Advantages in Turboprop13AERD1001_0210/01/2013
Researchers within the government of Canada see the need to improve the emissions performance of the Rolls-Royce T56 engine, which despite its age, remains a workhorse for its military aircraft fleet. In the United States, more than 200 billion gallons of liquid fuel is produced each year in a ratio of about 7:2:1 for gasoline, diesel, and jet fuel, respectively. With international air traffic expected to increase in the long term, the cost of aviation fuel will continue to rise unless current production can be increased. To address the global fuel challenges and economic sustainability, the International Air Transport Association (IATA) in June 2009 committed the airline industry to achieving a continuous improvement in fuel efficiency of 1.5% per year from 2009 to 2020, reaching carbon-neutral growth by 2020, and achieving a 50% absolute reduction in carbon emissions by 2050.
The Development of Novel Fuel Dehydrating Icing Inhibitors2013-01-216909/17/2013
Dissolved water is a normal component of jet fuel which is vapourised during combustion; however, free water is a contaminant that can starve engines, freeze to form ice crystals capable of blocking fuel feeds, support microbial growth, and contribute towards corrosion. Jet fuel may be protected from the potentially hazardous effects of free-water using biocides and icing/corrosion inhibitors. This investigation seeks to identify novel chemical approaches to the dual management of both water contamination and ice formation in jet fuel. The strategy of using organic molecules as dehydrating agents remains a relatively neglected approach perhaps because of the complexity of the physical organic chemistry involved in developing and refining these systems. However, organic molecules with well characterised dehydrating properties - such as ortho esters, acetals, hemiacetals, ketals, and hemiketals - present themselves as an excellent starting-point for the development and optimisation of
Repetto, Sonia L., Costello, James F., De Lacy Costello, Benjamin, Ratcliffe, Norman M., Lam, Joseph K.-W.
Immediate Impacts on Particulate and Gaseous Emissions from a T56 Turbo-Prop Engine Using a Biofuel Blend2013-01-213109/17/2013
Adoption of hydro-processed esters and fatty acid biojet fuels is a critical component for the sustainability of the aviation industry. Aviation biofuels reduce pollution and provide alternatives to conventional fossil fuels. A study of the impacts of biofuels on emissions from a T56 turbo-prop engine was undertaken as a joint effort among several departments of the Government of Canada. In this study, particulate (including particle number and black carbon (BC) mass) and regulated gaseous emissions (CO2, CO, NO, NO2, THC) were characterized with the engine operating on conventional F-34 jet fuel and jet fuel blended with camelina-based hydro-processed biojet fuel (C-HEFA) by 50% in volume. Emissions characterization, conducted after 20-hour ground engine durability tests, showed immediate significant reductions in particle number and BC mass when the engine was operated on the C-HEFA blend. Operating at high speed ground idle (HSGI) using the C-HEFA blend reduced particle number and
Chan, Tak W., Pham, Vinh, Chalmers, Jennifer, Davison, Craig, Chishty, Wajid, Poitras, Pierre
Calculation of Heating Value for Diesel Fuels Containing Biodiesel2013-01-113904/08/2013
Biodiesel, a fuel comprised of mono-alkyl esters of long-chain fatty acids also known as Fatty Acid Methyl Esters(FAME), derived from vegetable oils or animal fats, has become an important commercial marketplace automotive fuel in the United States (US) and around the world over last few years. FAME biodiesels have many chemical and physical property differences compared to conventional petroleum based diesel fuels. Also, the properties of biodiesel vary based on the feedstock chosen for biodiesel production. One of the key differences between petroleum diesel fuels and biodiesel is the energy content. The energy content, or heating value, is an important property of motor fuel, since it directly affects the vehicle fuel economy. While the energy content can be measured by combustion of the fuel in a bomb calorimeter, this analytical laboratory testing is time consuming and expensive. It would be more convenient to estimate the energy content from other commonly measured fuel
Lopes, Shailesh Martin, Furey, Robert, Geng, Pat
Combustion and Emissions Characteristics of JP-8 Blends and ULSD #2 with Similar CN in a Direct Injection Naturally Aspirated Compression Engine2013-01-168204/08/2013
"The Single Fuel Forward Policy" legislation enacted in the United States mandates that deployed U.S. military ground vehicles must be operable with aviation fuel (JP-8). This substitution of JP-8 for diesel raises concerns about the compatibility of this fuel with existing reciprocating piston engine systems. This study investigates the combustion, emissions, and performance characteristics of blends of JP-8 and Ultra Low Sulfur Diesel (ULSD) fuels with similar cetane numbers (CN), 48 (JP-8) and 47(ULSD), respectively, in a direct injection (DI) compression ignition engine over the load range of 3-8 bar imep at 1400 rpm. The results showed that JP-8 blends and ULSD had ignition delays ranging from approximately 1.0-1.4 ms and an average combustion duration time in the range of 47-65 CAD. Cylinder maximum heat flux values were found to be between 2.0 and 4.4 MW/m₂, with radiation flux increasing much faster than convection flux while increasing the imep. Combustion maximum bulk
Soloiu, Valentin, Ochieng, Henry, Weaver, Jabeous, Duggan, Marvin, Harp, Spencer, Vlcek, Brian, Jenkins, Craig, Jansons, Marcis
Investigation of Low-Temperature Combustion in an Optical Engine Fueled with Low Cetane Sasol JP-8 Fuel Using OH-PLIF and HCHO Chemiluminescence Imaging2013-01-089804/08/2013
Low cetane JP-8 fuels have been identified as being difficult to use under conventional diesel operation. However, recent focus on low-temperature combustion (LTC) modes has led to an interest in distillate hydrocarbon fuels having high volatility and low autoignition tendency. An experimental study is performed to evaluate low-temperature combustion processes in a small-bore optically-accessible diesel engine operated in a partially-premixed combustion mode using low-cetane Sasol JP-8 fuel. This particular fuel has a cetane number of 25. Both single and dual injection strategies are tested. Since long ignition delay is a consequence of strong autoignition resistance, under the conditions examined, low cetane Sasol JP-8 combustion can only take place with a double injection strategy: one pilot injection event in the vicinity of exhaust TDC and one main injection event near firing TDC. In this work, the effects of autoignition properties are examined by comparing the behavior of a high
Zha, Kan, Yu, Xin, Lai, Ming-Chia, Jansons, Marcis
Control of Fuel Octane for Knock Mitigation on a Dual-Fuel Spark-Ignition Engine2013-01-032004/08/2013
A two-port fuel-injection (PFI) system is added to a Rotax 914 four-cylinder spark-ignition engine to allow two fuels of different reactivity to be injected simultaneously in order to vary the fuel octane number during engine operation. Engine performance using the dual-fuel PFI system is compared to that using injection of primary-reference-fuel (PRF) blends via a single-PFI system for fuel octane ratings of 50, 70, and 87 octane. The on-the-fly octane control of dual-PFI system is found to control fuel-octane well enough to produce maximum indicated mean effective pressure (IMEPn) results within ± 2% of single-PFI PRF IMEPn results. IMEPn is compared among dual-PFI blends from 20 to 87 octane, neat n-heptane, neat JP-8, and JP-8/isooctane blends. Maximum IMEPn for these fuels is established for the Rotax 914 engine operating from 2500 to 5800 rev/min. IMEPn limitations for dual-PFI blends of JP-8 and isooctane are investigated at typical general-aviation cruise-power requirements to
Baranski, Jacob, Anderson, Eric, Grinstead, Keith, Hoke, John, Litke, Paul
Advanced Glow Plug for Heavy Fuels Applications2013-01-171604/08/2013
With current DoD goals of switching to a common battlefield logistics fuel, there is a significant push to develop technologies that allow small, high-powered engines such as used in unmanned aerial, marine, and ground vehicles, typically fueled by volatile fuels such as gasoline, to operate on heavy fuels such as JP-8. In this paper, the feasibility of catalytic glow plugs as an enabling component for the use of heavy fuels both as a retrofit to existing engines as well as new engine designs is demonstrated. Compared to standard spark igniters and non-catalytic glow plugs, the use of catalytic glow plugs will provide benefits including lower required compression ratio, improved igniter life, reduced energy requirements, and overall reduction in system weight and size. The catalytic glow plugs were shown to have a significant increase in surface temperature (180+°C) with impingement of a fuel spray and this increase was maintained over many cycles of impingement. Engine testing
Baird, Benjamin, Etemad, Shahrokh
Sleeve, Hose Assembly, Fire ProtectionAS1072E (Historical)01/02/2013
This standard defines the requirements for bulk protective sleeve to provide fire resistance for aircraft hose assemblies, which will enable these assemblies to meet the requirements of AS1055. NOTE: Use of this sleeve does not eliminate the need to demonstrate that the sleeved assemblies will meet the applicable requirements of AS1055.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Biofuel advances12AERD1024_0110/24/2012
The aerospace industry remains committed to getting off the ground with alternatives to jet fuel. As nations grapple with emissions, oil-security, and energy-price matters, aggressive investment, regulation, and corporate involvement have propelled the alternative-fuels industry to commercial relevance. Alternative fuels today have a total capacity capable of replacing 4.8% of current oil capacity. However, growth has slowed significantly. Since 2005, annual capacity growth has been roughly 22%; but growth through 2015 will be about 5% per year. As supply grows and logistical hurdles associated with feedstock and fuels increase, a new crop of technologies is emerging to add to the growing alternative-fuels space.
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