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Research Papers: Gas Turbines: Turbomachinery

Gas Turbine Fouling Tests: Review, Critical Analysis, and Particle Impact Behavior Map

[+] Author and Article Information
Alessio Suman, Nicola Casari, Elettra Fabbri, Michele Pinelli

Dipartimento di Ingegneria,
Università degli Studi di Ferrara,
Ferrara 44122, Italy

Luca di Mare

St John's College,
University of Oxford,
St Giles,
Oxford OX1 3JP, UK

Francesco Montomoli

Imperial College London,
London SW7 2AZ, UK

Contributed by the Turbomachinery Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received July 29, 2018; final manuscript received August 10, 2018; published online November 29, 2018. Editor: Jerzy T. Sawicki.

J. Eng. Gas Turbines Power 141(3), 032601 (Nov 29, 2018) (18 pages) Paper No: GTP-18-1525; doi: 10.1115/1.4041282 History: Received July 29, 2018; Revised August 10, 2018

Fouling affects gas turbine operation, and airborne or fuel contaminants, under certain conditions, become very likely to adhere to surfaces if impact takes place. Particle sticking implies the change in shape in terms of roughness of the impinged surface. The consequences of these deposits could be dramatic: these effects can shut an aircraft engine down or derate a land-based power unit. This occurrence may happen due to the reduction of the compressor flow rate and the turbine capacity, caused by a variation in the HPT nozzle throat area (geometric blockage due to the thickness of the deposited layer and the aerodynamic blockage due to the increased roughness, and in turn boundary layer). Several methods to quantify particle sticking have been proposed in literature so far, and the experimental data used for their validation vary in a wide range of materials and conditions. The experimental analyzes have been supported by (and have given inspiration to) increasingly realistic mathematical models. Experimental tests have been carried out on (i) a full scale gas turbine unit, (ii) wind tunnel testing or hot gas facilities using stationary cascades, able to reproduce the same conditions of gas turbine nozzle operation and finally, (iii) wind tunnel testing or hot gas facilities using a coupon as the target. In this review, the whole variety of experimental tests performed are gathered and classified according to composition, size, temperature, and particle impact velocity. Using particle viscosity and sticking prediction models, over seventy (70) tests are compared with each other and with the model previsions providing a useful starting point for a comprehensive critical analysis. Due to the variety of test conditions, the related results are difficult to be pieced together due to differences in particle material and properties. The historical data of particle deposition obtained over thirty (30) years are classified using particle kinetic energy and the ratio between particle temperature and its softening temperature. Qualitative thresholds for the distinction between particle deposition, surface erosion, and particle break-up, based on particle properties and impact conditions, are identified. The outcome of this paper can be used for further development of sticking models or as a starting point for new insight into the problem.

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Tarabrin, A. P. , Schurovsky, V. A. , Bodrov, A. I. , and Stalder, J.-P. , 1998, “ Influence of Axial Compressor Fouling on Gas Turbine Unit Performance Based on Different Schemes and With Different Initial Parameters,” ASME Paper No. 98-GT-416.
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Figures

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Fig. 1

Number of occurrences for: (a) particle diameter, (b) velocity, and (c) temperature

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Fig. 2

Viscosity values as a function of the temperature calculated according to the NPL model [77]

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Fig. 3

Critical viscosity method (rebound and sticking regions are divided by the dashed line) calculated according to the NPL model [77]

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Fig. 4

Critical viscosity method for silty particles (six tests with ARD) and coal particles (JPBS A, three tests with JPBS B, JBPP, five tests with Coal (bit) and three tests with Pittsburg) calculated according to the NPL model [77]

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Fig. 5

Classification of volcanic tests according to the total alkali-silica diagram. The black star marker used for Laki tests (Laki 2, 3, 4, and 5) summarizes four different tests.

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Fig. 6

Critical viscosity method for volcanic particles according to the GRD model [80]

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Fig. 7

Comparison of the critical viscosity ratio (μ/μc) calculated according the NPL [77] and GRD [80] viscosity methods where straight dashed line allows the data comparison

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Fig. 8

Critical velocity method for JBPS B 2 as a function of the particle diameter. Lower particle velocity v than critical velocity determines sticky condition.

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Fig. 9

Ekin-Θ plane: deposition tests

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Fig. 10

Ekin-Θ plane including erosion and splashing tests. Particle deposition data are reported with gray dots.

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Fig. 11

Particle impact behavior map

Tables

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