reciprocating wear in a steam environment

1
Friction vs Time 0 0.2 0.4 0.6 0.8 1 1.2 0 10 20 30 40 50 Time, h Friction Coefficient 3000 h pre-exposure 500 h pre-exposure No pre-exposure Abstract: Tests to simulate the wear between sliding components in a steam power plant have been performed. A low frequency constant load wear apparatus, housed inside a furnace was modified to incorporate a steam environment. The materials tested were pre-exposed in a flowing steam furnace at temperature for either 500 or 3000 hours to provide some simulation of long term ageing. Tests were also performed on as-received material for comparison purposes. The duration of each wear test was 50 hours. Apparatus A schematic diagram of the wear test apparatus is shown below. It has the following features: A split furnace Two arms which hold the samples The top arm moves relative to the fixed bottom arm An LVDT measures the distance travelled Another LVDT measures the wear of the specimen Two load cells measure the normal and frictional forces The two arms are water-cooled The temperature of the furnace and the specimens are measured in-situ by sheathed thermocouples The top and bottom arms have been designed to rotate so that the two contacting surfaces can be made parallel Specimens The samples were designed to ‘push’ fit into the arms. The top sample is a block with a protruding stub which is rubbed against a flat bottom sample. Materials The materials tested are listed in the table below: Software Software was written to control the experiment (cycle speed, water top-up, start and end times) as well as to acquire the measurement data (load, friction, wear, temperature, time, etc.) A typical screen shot showing during a test is shown to the right. Friction During testing, the horizontal and vertical loads and the horizontal and vertical displacements were logged. The vertical load is constant during a test and the horizontal load gives a measure of the friction force generated at the contact interface that can be used to calculate friction coefficients. A good method for displaying this is through ‘friction loops’ (displayed on the right hand side of the figure above) where the friction coefficient is plotted against horizontal displacement. The average friction coefficient for each complete friction loop was also calculated from the integral, and the trend is plotted against time. Typical examples of the friction trends are shown in the figures to the right for a Ni-Cr-Co alloy stub rubbed against a flat HVOF Cr2C3 plate. Both specimens were tested in the as received condition. Initial and final friction coefficient loops are plotted against horizontal direction, shown in (a) and (b) respectively. The average friction coefficient was plotted against time, shown in (c). Results All but one of the tests were performed in a steam environment. One test was carried out without steam for comparative purposes. The graph below shows that the addition of steam reduces the friction coefficient. The graph below shows a comparison of friction results for different materials in the as-received condition: The following graph shows a comparison between materials that have been pre-aged for 3000 hours in a steam environment. Tests were performed on as-received and pre-exposed specimens to compare the effect of ‘aged’ material. Results are presented in the following figures for two different materials. For the Co-Ni-Cr-W alloy against stellite material, ageing increases the friction. By contrast, with the MCrAlY coating, pre-ageing markedly decreases the friction coefficient. The following table shows a summary of the final friction coefficient results with respect to material and ageing treatment: Visual Inspection of the Wear Scar Despite the attention given to sample alignment in the design of the test system, it was found that full contact was not always achieved over the sample surfaces. The following figures show examples of good and bad alignment: Conclusions The work presented here reveals that the addition of steam in a tribological environment clearly influences the friction between both as-received and aged materials. The majority of materials experienced an increase in friction coefficient with age, the only exception being the MCrAlY coated stub, due to its lubricious properties which form during testing. Acknowledgements The authors are grateful to Jim Banks and David Laing for their technical expertise, and would like to acknowledge funding from the Technology Strategy Board and from the Department of Business Innovation and Science for the work reported in this paper. Reciprocating wear in a steam environment L. J. Brown, M. G. Gee & J. W. Nunn National Physical Laboratory, Teddington, Middlesex, TW11 0LW, UK Stub Material Coating on Stub Plate Material Coating on Plate Pre- exposure, h Co-Ni-Cr-W alloy - Stellite - 0 Co-Ni-Cr-W alloy - Stellite - 500 Co-Ni-Cr-W alloy - Stellite - 3000 Co-Ni-Cr-W alloy - Stellite HVOF Cr 2 C 3 0 Co-Ni-Cr-W alloy - Stellite HVOF Cr 2 C 3 500 Co-Ni-Cr-W alloy - Stellite HVOF Cr 2 C 3 3000 Ni-Cr-Co alloy - Stellite - 0 Ni-Cr-Co alloy - Stellite - 500 Ni-Cr-Co alloy - Stellite - 3000 Ni-Cr-Co alloy - Stellite HVOF Cr 2 C 3 0 Ni-Cr-Co alloy - Stellite HVOF Cr 2 C 3 500 Ni-Cr-Co alloy - Stellite HVOF Cr 2 C 3 3000 Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr 2 C 3 0 Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr 2 C 3 500 Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr 2 C 3 3000 Stub Material Coating on Stub Plate Material Coating on Plate Pre- exposure, h Final Friction Co-Ni-Cr-W alloy - Stellite - 0 0.5 Co-Ni-Cr-W alloy - Stellite - 500 0.8 Co-Ni-Cr-W alloy - Stellite - 3000 0.95 Co-Ni-Cr-W alloy - Stellite HVOF Cr 2 C 3 0 0.68 Co-Ni-Cr-W alloy - Stellite HVOF Cr 2 C 3 500 0.9 Co-Ni-Cr-W alloy - Stellite HVOF Cr 2 C 3 3000 - Ni-Cr-Co alloy - Stellite - 0 0.65 Ni-Cr-Co alloy - Stellite - 500 0.65 Ni-Cr-Co alloy - Stellite - 3000 0.85 Ni-Cr-Co alloy - Stellite HVOF Cr 2 C 3 0 0.7 Ni-Cr-Co alloy - Stellite HVOF Cr 2 C 3 500 0.85 Ni-Cr-Co alloy - Stellite HVOF Cr 2 C 3 3000 1.2 Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr 2 C 3 0 0.95 Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr 2 C 3 500 0.95 Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr 2 C 3 3000 1.0 www.npl.co.uk Bad alignment Good alignment 0 0.2 0.4 0.6 0.8 1 1.2 0 10 20 30 40 50 Time, h Friction Coefficient No Steam With Steam 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 0 10 20 30 40 50 Time, h Friction Coefficient Ni-Cr-Co, MCrAlY/HVOF Cr 2 C 3 Ni-Cr-Co/HVOF Cr 2 C 3 Ni-Cr-Co/Stellite Ni-Cr-Co/Stellite Co-Ni-Cr-W/HVOF Cr 2 C 3 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 0 10 20 30 40 50 Time, h Friction Coefficient Ni-Cr-Co /HVOF Cr 2 C 3 Ni-Cr-Co MCrAlY/HVOF Cr 2 C 3 Co-Ni-Cr-W/Stellite Ni-Cr-Co/Stellite 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 0 10 20 30 40 50 Time, h Friction Coefficient 500 h pre-exposure No pre-exposure 3000 h pre-exposure 1 -3 Horizontal Displacement Friction -1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.8 1 -3 -2 -1 0 1 2 3 Horizontal Displacement Friction 1 -3 Horizontal Displacement Friction -1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.8 1 -3 -2 -1 0 1 2 3 Horizontal Displacement Friction 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 0 10 20 30 40 50 60 Time, h Friction Coefficient Plot of Friction Loops a) Initial Friction, b) Final Friction and c) Overall Friction vs. Time Co-Ni-Cr-W MCrAlY (a) (b) (c)

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Page 1: Reciprocating wear in a steam environment

Friction vs Time

0

0.2

0.4

0.6

0.8

1

1.2

0 10 20 30 40 50

Time, h

Fric

tion

Coe

ffici

ent

3000 h pre-exposure

500 h pre-exposure

No pre-exposure

Abstract:Tests to simulate the wear between sliding components in

a steam power plant have been performed. A low frequency

constant load wear apparatus, housed inside a furnace was

modifi ed to incorporate a steam environment.

The materials tested were pre-exposed in a fl owing steam

furnace at temperature for either 500 or 3000 hours to

provide some simulation of long term ageing. Tests were also

performed on as-received material for comparison purposes.

The duration of each wear test was 50 hours.

ApparatusA schematic diagram of the wear test apparatus is shown below. It has the following features:

• A split furnace

• Two arms which hold the samples

• The top arm moves relative to the fi xed bottom arm

• An LVDT measures the distance travelled

• Another LVDT measures the wear of the specimen

• Two load cells measure the normal and frictional forces

• The two arms are water-cooled

• The temperature of the furnace and the specimens are measured in-situ by sheathed thermocouples

• The top and bottom arms have been designed to rotate so that the two contacting surfaces can be made parallel

SpecimensThe samples were designed to ‘push’ fi t into the arms. The top sample is a block with a protruding stub which is rubbed against a fl at bottom sample.

MaterialsThe materials tested are listed in the table below:

SoftwareSoftware was written to control the experiment (cycle speed, water top-up, start and end times) as well as to acquire the measurement data (load, friction, wear, temperature, time, etc.) A typical screen shot showing during a test is shown to the right.

FrictionDuring testing, the horizontal and vertical loads and the horizontal and vertical displacements were logged. The vertical load is constant during a test and the horizontal load gives a measure of the friction force generated at the contact interface that can be used to calculate friction coeffi cients.

A good method for displaying this is through ‘friction loops’ (displayed on the right hand side of the fi gure above) where the friction coeffi cient is plotted against horizontal displacement.

The average friction coeffi cient for each complete friction loop was also calculated from the integral, and the trend is plotted against time. Typical examples of the friction trends are shown in the fi gures to the right for a Ni-Cr-Co alloy stub rubbed against a fl at HVOF Cr2C3 plate. Both specimens were tested in the as received condition. Initial and fi nal friction coeffi cient loops are plotted against horizontal direction, shown in (a) and (b) respectively. The average friction coeffi cient was plotted against time, shown in (c).

ResultsAll but one of the tests were performed in a steam environment. One test was carried out without steam for comparative purposes. The graph below shows that the addition of steam reduces the friction coeffi cient.

The graph below shows a comparison of friction results for different materials in the as-received condition:

The following graph shows a comparison between materials that have been pre-aged for 3000 hours in a steam environment.

Tests were performed on as-received and pre-exposed specimens to compare the effect of ‘aged’ material. Results are presented in the following fi gures for two different materials. For the Co-Ni-Cr-W alloy against stellite material, ageing increases the friction. By contrast, with the MCrAlY coating, pre-ageing markedly decreases the friction coeffi cient.

The following table shows a summary of the fi nal friction coeffi cient results with respect to material and ageing treatment:

Visual Inspection of the Wear ScarDespite the attention given to sample alignment in the design of the test system, it was found that full contact was not always achieved over the sample surfaces. The following fi gures show examples of good and bad alignment:

ConclusionsThe work presented here reveals that the addition of steam in a tribological environment clearly infl uences the friction between both as-received and aged materials.

The majority of materials experienced an increase in friction coeffi cient with age, the only exception being the MCrAlY coated stub, due to its lubricious properties which form during testing.

AcknowledgementsThe authors are grateful to Jim Banks and David Laing for their technical expertise, and would like to acknowledge funding from the Technology Strategy Board and from the Department of Business Innovation and Science for the work reported in this paper.

Reciprocating wear in a steam environmentL. J. Brown, M. G. Gee & J. W. Nunn

National Physical Laboratory, Teddington, Middlesex, TW11 0LW, UK

Stub MaterialCoating

on Stub

Plate

Material

Coating

on Plate

Pre-

exposure, h

Co-Ni-Cr-W alloy - Stellite - 0Co-Ni-Cr-W alloy - Stellite - 500Co-Ni-Cr-W alloy - Stellite - 3000Co-Ni-Cr-W alloy - Stellite HVOF Cr2C3 0Co-Ni-Cr-W alloy - Stellite HVOF Cr2C3 500Co-Ni-Cr-W alloy - Stellite HVOF Cr2C3 3000

Ni-Cr-Co alloy - Stellite - 0Ni-Cr-Co alloy - Stellite - 500Ni-Cr-Co alloy - Stellite - 3000Ni-Cr-Co alloy - Stellite HVOF Cr2C3 0Ni-Cr-Co alloy - Stellite HVOF Cr2C3 500Ni-Cr-Co alloy - Stellite HVOF Cr2C3 3000Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr2C3 0Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr2C3 500Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr2C3 3000

Stub MaterialCoating

on Stub

Plate

Material

Coating

on Plate

Pre-

exposure, h

Final

Friction

Co-Ni-Cr-W alloy - Stellite - 0 0.5Co-Ni-Cr-W alloy - Stellite - 500 0.8Co-Ni-Cr-W alloy - Stellite - 3000 0.95Co-Ni-Cr-W alloy - Stellite HVOF Cr2C3 0 0.68Co-Ni-Cr-W alloy - Stellite HVOF Cr2C3 500 0.9Co-Ni-Cr-W alloy - Stellite HVOF Cr2C3 3000 -

Ni-Cr-Co alloy - Stellite - 0 0.65Ni-Cr-Co alloy - Stellite - 500 0.65Ni-Cr-Co alloy - Stellite - 3000 0.85Ni-Cr-Co alloy - Stellite HVOF Cr2C3 0 0.7Ni-Cr-Co alloy - Stellite HVOF Cr2C3 500 0.85Ni-Cr-Co alloy - Stellite HVOF Cr2C3 3000 1.2Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr2C3 0 0.95Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr2C3 500 0.95Ni-Cr-Co alloy MCrAlY Stellite HVOF Cr2C3 3000 1.0

www.npl.co.uk

Bad alignment

Good alignment

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With Steam

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Ni-Cr-Co, MCrAlY/HVOF Cr2C3

Ni-Cr-Co/HVOF Cr 2 C 3

Ni-Cr-Co/Stellite Ni-Cr-Co/Stellite Co-Ni-Cr-W/HVOF Cr 2 C 3

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Ni-Cr-Co /HVOF Cr 2 C 3 Ni-Cr-Co MCrAlY/HVOF Cr 2 C 3

Co-Ni-Cr-W/Stellite

Ni-Cr-Co/Stellite

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3000 h pre-exposure

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Plot of Friction Loops a) Initial Friction, b) Final Friction and c) Overall Friction vs. Time

Co-Ni-Cr-W

MCrAlY

(a)

(b)

(c)