Research Papers: Gas Turbines: Coal, Biomass, and Alternative Fuels

Validation of an Infrared Extinction Method for Fuel Vapor Concentration Measurements Towards the Systematic Comparison Between Alternative and Conventional Fuels for Aviation

[+] Author and Article Information
Johannes Fritzer1

 Graz University of Technology, Institute for Thermal Turbomachinery and Machine Dynamics, Infeldgasse 25A, 8010 Graz, Austria

Fabrice Giuliani

 Graz University of Technology, Institute for Thermal Turbomachinery and Machine Dynamics, Infeldgasse 25A, 8010 Graz, Austria

Alain Strzelecki, Virginel Bodoc

 ONERA -French Aerospace Lab, 2. Avenue Edouard Belin, 31055 Toulouse Cedex 4, France


Corresponding author.

J. Eng. Gas Turbines Power 134(1), 011401 (Oct 27, 2011) (8 pages) doi:10.1115/1.4004144 History: Received April 12, 2011; Revised April 27, 2011; Published October 27, 2011; Online October 27, 2011

Due to increasing oil prices and the obvious influence of the combustion of fossil fuel-derivatives on climate change on the one hand and the steady growth of transportation needs on the other, it is necessary to develop alternatives to oil for aviation. For this purpose a specific research program on the investigation of adequate alternative fuels for aviation has been founded by the European Commission’s Framework Program. The project Alfa Bird (Alternative Fuels and Bio-fuels in Aircraft Development) focuses on an identification of possible alternative fuels to kerosene, the investigation of the adequacy of the selected ones, an evaluation of the environmental and economic impact of them, and finally the creation of a future perspective for the industrial use of the “best” alternative. The main part of the investigation activities at TU Graz, in cooperation with ONERA Centre de Toulouse and Fauga-Mauzac on these specific topics consists of the analysis of the evaporation of the previously chosen fuel types in comparison to fully synthetic jet fuel. Therefore qualitative measurements to obtain vapor concentration gradients will be done using the infrared extinction (IRE) measurement method. Based on a simplified Beer–Bouguer–Lambert law the integral vapor concentrations can be obtained. The main hypothesis is that if the line-of-sight extinction due to Mie-scattering is similar for both infrared and visible wavelengths because of the presence of the spray, only infrared light will be absorbed by the fuel vapor, being transparent to visible light. This contribution focuses on the validation of the infrared measurement technique on a well characterized spray. The tests are performed under controlled boundary conditions. Therefore an existing IRE test arrangement at ONERA Toulouse using an ultrasonic atomizer injecting n-octane at atmospheric conditions has been analyzed. Error sources related to misalignments in the hardware have been considered and an iterative alignment method of the laser beams followed by a beam diameter and diffraction analysis have been performed. Optimizing the setup to obtain a stable operation point has been successful. Improved experimental results at this operation point were compared with existing simulation results for the evaporation of the ultrasonic atomizer used. The achieved data has shown good accordance to the existing simulation results.

Copyright © 2012 by American Society of Mechanical Engineers
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Figure 1

Absorption spectrum of gasoline

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Figure 2

Optical thickness ratio/area mean diameter

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Figure 3

(1) Injector, (2) pinhole

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Figure 4

Schematic of the test bench

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Figure 5

Ultrasonic atomizer Sonics USVC 130 AT

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Figure 6

Radial evolution of droplet size (μm) distribution

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Figure 7

Mean values of the droplet diameters determined by PDA

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Figure 8

Beam diameter measurement

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Figure 9

Beam diameter/diffraction analysis with razorblade

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Figure 10

Calculation of the circular aperture diffraction

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Figure 11

Laser beam analysis with razorblade in vertical direction

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Figure 12

Laser beam analysis with razorblade in horizontal direction

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Figure 13

Extinction measurements/variation of the fuel mass flow (25/2030/35 ml/min)

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Figure 14

Extinction measurements/variation of the injection parameter (28/31/35% amplitude)

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Figure 15

Stable extinction measurements at 35 ml/min

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Figure 16

Comparison of deconvolution results with simulation results




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