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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 807
NUT FACTOR ANALYSIS OF ALUMINIUM IVD COATED AND CADMIUM
ELECTROPLATED HIGH STRENGTH FASTENERS
Neethu P1, Sankaravelayutham P2, Dr. Rajeev N3
1Mtech student, Dept. of Mechanical Engineering, NSS college of Engineering, Kerala, India
2Scientist, EFA, Vikram Sarabhai Space Centre, ISRO, TVM, India
3Associate Professor, Dept. of Mechanical Engineering, NSS college of Engineering, Kerala, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - Fasteners are defined as machine elements that
can be easily installed and removed with hand or power tools.
Different types of fasteners are used inaerospaceapplications.
For high strength fasteners, different types of coatings are
used for improving surface protection and achieving desired
mechanical and surface properties. Nut factor analysis of
aluminium IVD and MOS2 coated fasteners and cadmium
coated fasteners has been carried out using friction test.
Fasteners made out of high strength alloy steel materials
namely 35NCD16 is used in this study.
Key Words: (Size 10 & Bold) Key word1, Key word2, Key
word3, etc (Minimum 5 to 8 key words)…
1. INTRODUCTION
Fasteners are machine elements that can be easily installed
and removed with hand or power tools. Screws, bolts, nuts
and rivets are common types of fasteners. The terms bolts
and screws do not refer to specific types of fasteners, but
rather how they are used (i.e. the application). Selecting the
right fastener material from the vast array of materials
available is required and careful consideration may need to
be given to strength, temperature, corrosion, vibration,
fatigue and many other variables. There are three major
steel fasteners used in industries: stainless steel, carbon
steel, and alloy steel.
Most of the fasteners are coated with different kind of
materials using different processes to improve their
functional properties. Ion Vapor Deposition (IVD) is a
physical vapor deposition process for applying pure
aluminum coatings to various partsforcorrosion protection.
A vacuum vessel of various sizes, called an Ivadizer is used
for coating process. Its useful service temperature limit is
925ºF. Cadmium is the most common aerospace fastener
plating material. Plating is done by electro-deposition
process. Since cadmium melts at 600ºF, its useful service
temperature limit is 450ºF.
35NCD16 is a high strength low alloy mainly used in Shear
bolt for light alloy structure of launch vehicles. 35NCD16
fasteners are classified into class II, based on the ultimate
tensile strength (1250MPa).
In this paper nut factor analysis of aluminium IVDandMOS2
coated fasteners andcadmiumcoatedfastenersisdoneusing
friction test. Friction test is conducted for each in Al.IVDand
MOS2 coated fasteners & Cd plated fasteners.AluminumIVD
coated and Cadmium coated M14 bolts made of
35NCD16material is used for this study.
2. EXPERIMENTAL DETAILS
Friction test is conducted for each in Al. IVD and MOS2
coated fasteners & Cd plated fasteners. Nut factor
computations done corresponding to preload steps of 50KN
(39% YS), 77KN (60% YS), 86KN (67% YS) and 116 KN
(75% UTS). Test sample details:
M14 x 1.5 x 33 L HSHCS – PS15760 -35NCD16 - Al. IVD &
MOS2 coated
M14 x 1.5 x 33 L HSHCS – PS14012 -35NCD16 – Cd plated
2.1 Experimental setup for friction test
Generally 60% of YS is the design preload for M14 fasteners
and the same works out to 77 KN. At present,thesefasteners
are applied with a torque of 144 Nm to achieve the desired
preload. Hence torque tension tests were done with
computation steps at 50 KN, 77 KN, 86 KN and 116 KN. The
test setup is given in Fig1.The equipment has preload force
transducer and the thread friction torque transducer fitted
with strain gauges connected to a full Wheatstone bridge.
The thread friction torque transducer is braced against the
preload force transducer using an axial bearing, which
allows the thread friction torque to be measured
independently. The shaft of the torque/angle transducer is
fitted with strain gauges, and the sensor signals and supply
voltage are coupled via extremely low-wear slip rings. An
incremental encoder disc with 360 apertures is also fittedto
the transducer shaft for measurements of angle of rotation.
Nut factor can be calculated using the equation:
T= K*F*D where
K = nut factor,
F= force / preload,
D= diameter of the fastener,
T= torque
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 808
Figure 1: Schatz Torque Tension Testing Machine
2.2 Results and discussion
Table 1 and 2 shows the results of friction for Aluminium
IVD and MOS2 coated fasteners. Table 3 and 4 shows the
results of friction for Cadmium plated fasteners.
Table 1. Friction test results of aluminium IVD and MOS2
coated fasteners
Sl no
Force
50KN 77KN
Torque
Nm
Nut factor Torque
Nm
Nut factor
1 96.7 0.13809 135.58 0.12569
2 92.07 0.13148 130.74 0.12125
3 94.62 0.13512 124.54 0.1155
4 86.97 0.12419 111.17 0.10306
5 94.83 0.13542 124.54 0.1155
6 89.52 0.12778 121.42 0.11261
7 80.72 0.11522 117.21 0.10866
8 101.49 0.09412
9 111.43 0.1033
Kmin 0.11522 0.09412
Kmax 0.13542 0.12569
Kaverage 0.12961 0.11086
Table 2. Friction test results of aluminium IVD and
MOS2 coated fasteners
Sl no
Force
86KN 116KN
Torque
Nm
Nut factor Torque
Nm
Nut factor
1 147.5 0.122521 185.12 0.11398
2 140.52 0.116684 166.8 0.1027
3 133.91 0.111195 168.73 0.10386
4 118.35 0.098274 141.56 0.08716
5 135.42 0.112384 178.31 0.10976
6 132.3 0.109858 169.93 0.1046
7 126.31 0.104848 160.3 0.0987
8 107.63 0.089342 129.96 0.08002
9 121.73 0.101081 160.98 0.09912
Kmin 0.089342 0.08002
Kmax 0.122521 0.11398
Kaverage 0.1073541 0.09999
Average nut factor of aluminium IVD coated fastener =
(0.12961+0.11086+0.1073541+0.09999)/4=0.111955
Chart 1. Torque vs nut factor - Al. IVD and MOS2 coated
fasteners
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 809
Table 3. Friction test results of Cadmium plated fasteners
Sl no
Force
50KN 77KN
Torque
Nm
Nut factor Torque
Nm
Nut factor
1 174.35 0.249022 259.24 0.240451
2 131.83 0.188291 213.24 0.197785
3 165.66 0.23661 261.01 0.24209
4 118.82 0.169709 181.9 0.168716
5 157.9 0.225526 244.82 0.227076
6 176.64 0.252292 262.46 0.243438
7 197.72 0.282401 296.55 0.275057
8 190.28 0.271774 296.87 0.275354
9 201.47 0.287757 295.88 0.274436
Kmin 0.169709 0.168716
Kmax 0.287757 0.275354
Kaverage 0.240376 0.238267
Table 4. Friction test results of Cadmium plated fasteners
Sl
no
Force
86KN 116KN
Torque
Nm
Nut factor Torque
Nm
Nut factor
1 282.34 0.234474 344.95 0.212389
2 238.21 0.197826 301.6 0.185698
3 287.08 0.238328 349.12 0.214957
4 203.86 0.169299 273.24 0.168237
5 270.32 0.224492 337.98 0.208098
6 289.42 0.24027 362.23 0.22299
7 321.01 0.266589 384.72 0.236713
8 329.13 0.273332 402.41 0.247768
9 323.3 0.26849 396.01 0.243828
Kmin 0.169299 0.168237
Kmax 0.273332 0.247768
Kaverage 0.23478889 0.215630889
Average nut factor of cadmium coated fastener =
(0.240376+0.238267+0.2347889+0.215630889)/4=0.24
Chart 2. : Torque vs nut factor - cadmium coated fasteners
3. CONCLUSIONS
Friction test is conducted for each in Al. IVD and MOS2
coated fasteners & Cd plated M14 fasteners and nut factors
for each step is calculated. Average nut factor of aluminium
IVD and MOS2 coated fasteners and cadmium plated
fasteners is calculated. Nut factor of fasteners varied with
coating, threading tolerance, surface roughness, lubrication
and material selection. . From the results it is found the
average nut factor of Aluminium IVD and MOS2 coated
fastener is lower than cadmium plated fastener.
ACKNOWLEDGEMENT
The authors are thankful to Vikram Sarabhai Space Centre,
Indian Space Research Organization, Thiruvananthapuram
and NSS College of Engineering, Palakkad for providing
facilities for research and conducting experiments.
REFERENCES
[1] Technical reference guide, Fastenal industrial and
construction supplies, 2005.
[2] Daniel H. Herring, "The Heat Treatment of Fasteners,"
Fastener Technology International, 2008.
[3] Abhay K. Jha, "Hydrogen embrittlement of 3.5Ni–1.5Cr–
0.5Mo steel fastener," Engineering Failure Analysis, no.
15, pp. 431-439, 2008.
[4] Bickford, J.H and Nassar S.A, 1998 “Handbook of Bolts
and Bolted joints”,Marcel Dekker,New York
[5] K. Gangadhara Reddy, "Failure of cadmium plated
maraging steel tension bolt," Engineering Failure
Analysis , no. 8, pp. 263-269, 2001.
[6] Barret, Fastener Design Manual, NASA reference
publication 1228, 1990.
[7] D. Croccolo, M. De Agostinis,N. Vincenzi,” Experimental
analysis on the tightening torque – preloading force
relationship in threaded fasteners”, Canada : s.n, 2010.
IMECE2010-37153.

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  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 807 NUT FACTOR ANALYSIS OF ALUMINIUM IVD COATED AND CADMIUM ELECTROPLATED HIGH STRENGTH FASTENERS Neethu P1, Sankaravelayutham P2, Dr. Rajeev N3 1Mtech student, Dept. of Mechanical Engineering, NSS college of Engineering, Kerala, India 2Scientist, EFA, Vikram Sarabhai Space Centre, ISRO, TVM, India 3Associate Professor, Dept. of Mechanical Engineering, NSS college of Engineering, Kerala, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Fasteners are defined as machine elements that can be easily installed and removed with hand or power tools. Different types of fasteners are used inaerospaceapplications. For high strength fasteners, different types of coatings are used for improving surface protection and achieving desired mechanical and surface properties. Nut factor analysis of aluminium IVD and MOS2 coated fasteners and cadmium coated fasteners has been carried out using friction test. Fasteners made out of high strength alloy steel materials namely 35NCD16 is used in this study. Key Words: (Size 10 & Bold) Key word1, Key word2, Key word3, etc (Minimum 5 to 8 key words)… 1. INTRODUCTION Fasteners are machine elements that can be easily installed and removed with hand or power tools. Screws, bolts, nuts and rivets are common types of fasteners. The terms bolts and screws do not refer to specific types of fasteners, but rather how they are used (i.e. the application). Selecting the right fastener material from the vast array of materials available is required and careful consideration may need to be given to strength, temperature, corrosion, vibration, fatigue and many other variables. There are three major steel fasteners used in industries: stainless steel, carbon steel, and alloy steel. Most of the fasteners are coated with different kind of materials using different processes to improve their functional properties. Ion Vapor Deposition (IVD) is a physical vapor deposition process for applying pure aluminum coatings to various partsforcorrosion protection. A vacuum vessel of various sizes, called an Ivadizer is used for coating process. Its useful service temperature limit is 925ºF. Cadmium is the most common aerospace fastener plating material. Plating is done by electro-deposition process. Since cadmium melts at 600ºF, its useful service temperature limit is 450ºF. 35NCD16 is a high strength low alloy mainly used in Shear bolt for light alloy structure of launch vehicles. 35NCD16 fasteners are classified into class II, based on the ultimate tensile strength (1250MPa). In this paper nut factor analysis of aluminium IVDandMOS2 coated fasteners andcadmiumcoatedfastenersisdoneusing friction test. Friction test is conducted for each in Al.IVDand MOS2 coated fasteners & Cd plated fasteners.AluminumIVD coated and Cadmium coated M14 bolts made of 35NCD16material is used for this study. 2. EXPERIMENTAL DETAILS Friction test is conducted for each in Al. IVD and MOS2 coated fasteners & Cd plated fasteners. Nut factor computations done corresponding to preload steps of 50KN (39% YS), 77KN (60% YS), 86KN (67% YS) and 116 KN (75% UTS). Test sample details: M14 x 1.5 x 33 L HSHCS – PS15760 -35NCD16 - Al. IVD & MOS2 coated M14 x 1.5 x 33 L HSHCS – PS14012 -35NCD16 – Cd plated 2.1 Experimental setup for friction test Generally 60% of YS is the design preload for M14 fasteners and the same works out to 77 KN. At present,thesefasteners are applied with a torque of 144 Nm to achieve the desired preload. Hence torque tension tests were done with computation steps at 50 KN, 77 KN, 86 KN and 116 KN. The test setup is given in Fig1.The equipment has preload force transducer and the thread friction torque transducer fitted with strain gauges connected to a full Wheatstone bridge. The thread friction torque transducer is braced against the preload force transducer using an axial bearing, which allows the thread friction torque to be measured independently. The shaft of the torque/angle transducer is fitted with strain gauges, and the sensor signals and supply voltage are coupled via extremely low-wear slip rings. An incremental encoder disc with 360 apertures is also fittedto the transducer shaft for measurements of angle of rotation. Nut factor can be calculated using the equation: T= K*F*D where K = nut factor, F= force / preload, D= diameter of the fastener, T= torque
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 808 Figure 1: Schatz Torque Tension Testing Machine 2.2 Results and discussion Table 1 and 2 shows the results of friction for Aluminium IVD and MOS2 coated fasteners. Table 3 and 4 shows the results of friction for Cadmium plated fasteners. Table 1. Friction test results of aluminium IVD and MOS2 coated fasteners Sl no Force 50KN 77KN Torque Nm Nut factor Torque Nm Nut factor 1 96.7 0.13809 135.58 0.12569 2 92.07 0.13148 130.74 0.12125 3 94.62 0.13512 124.54 0.1155 4 86.97 0.12419 111.17 0.10306 5 94.83 0.13542 124.54 0.1155 6 89.52 0.12778 121.42 0.11261 7 80.72 0.11522 117.21 0.10866 8 101.49 0.09412 9 111.43 0.1033 Kmin 0.11522 0.09412 Kmax 0.13542 0.12569 Kaverage 0.12961 0.11086 Table 2. Friction test results of aluminium IVD and MOS2 coated fasteners Sl no Force 86KN 116KN Torque Nm Nut factor Torque Nm Nut factor 1 147.5 0.122521 185.12 0.11398 2 140.52 0.116684 166.8 0.1027 3 133.91 0.111195 168.73 0.10386 4 118.35 0.098274 141.56 0.08716 5 135.42 0.112384 178.31 0.10976 6 132.3 0.109858 169.93 0.1046 7 126.31 0.104848 160.3 0.0987 8 107.63 0.089342 129.96 0.08002 9 121.73 0.101081 160.98 0.09912 Kmin 0.089342 0.08002 Kmax 0.122521 0.11398 Kaverage 0.1073541 0.09999 Average nut factor of aluminium IVD coated fastener = (0.12961+0.11086+0.1073541+0.09999)/4=0.111955 Chart 1. Torque vs nut factor - Al. IVD and MOS2 coated fasteners
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 809 Table 3. Friction test results of Cadmium plated fasteners Sl no Force 50KN 77KN Torque Nm Nut factor Torque Nm Nut factor 1 174.35 0.249022 259.24 0.240451 2 131.83 0.188291 213.24 0.197785 3 165.66 0.23661 261.01 0.24209 4 118.82 0.169709 181.9 0.168716 5 157.9 0.225526 244.82 0.227076 6 176.64 0.252292 262.46 0.243438 7 197.72 0.282401 296.55 0.275057 8 190.28 0.271774 296.87 0.275354 9 201.47 0.287757 295.88 0.274436 Kmin 0.169709 0.168716 Kmax 0.287757 0.275354 Kaverage 0.240376 0.238267 Table 4. Friction test results of Cadmium plated fasteners Sl no Force 86KN 116KN Torque Nm Nut factor Torque Nm Nut factor 1 282.34 0.234474 344.95 0.212389 2 238.21 0.197826 301.6 0.185698 3 287.08 0.238328 349.12 0.214957 4 203.86 0.169299 273.24 0.168237 5 270.32 0.224492 337.98 0.208098 6 289.42 0.24027 362.23 0.22299 7 321.01 0.266589 384.72 0.236713 8 329.13 0.273332 402.41 0.247768 9 323.3 0.26849 396.01 0.243828 Kmin 0.169299 0.168237 Kmax 0.273332 0.247768 Kaverage 0.23478889 0.215630889 Average nut factor of cadmium coated fastener = (0.240376+0.238267+0.2347889+0.215630889)/4=0.24 Chart 2. : Torque vs nut factor - cadmium coated fasteners 3. CONCLUSIONS Friction test is conducted for each in Al. IVD and MOS2 coated fasteners & Cd plated M14 fasteners and nut factors for each step is calculated. Average nut factor of aluminium IVD and MOS2 coated fasteners and cadmium plated fasteners is calculated. Nut factor of fasteners varied with coating, threading tolerance, surface roughness, lubrication and material selection. . From the results it is found the average nut factor of Aluminium IVD and MOS2 coated fastener is lower than cadmium plated fastener. ACKNOWLEDGEMENT The authors are thankful to Vikram Sarabhai Space Centre, Indian Space Research Organization, Thiruvananthapuram and NSS College of Engineering, Palakkad for providing facilities for research and conducting experiments. REFERENCES [1] Technical reference guide, Fastenal industrial and construction supplies, 2005. [2] Daniel H. Herring, "The Heat Treatment of Fasteners," Fastener Technology International, 2008. [3] Abhay K. Jha, "Hydrogen embrittlement of 3.5Ni–1.5Cr– 0.5Mo steel fastener," Engineering Failure Analysis, no. 15, pp. 431-439, 2008. [4] Bickford, J.H and Nassar S.A, 1998 “Handbook of Bolts and Bolted joints”,Marcel Dekker,New York [5] K. Gangadhara Reddy, "Failure of cadmium plated maraging steel tension bolt," Engineering Failure Analysis , no. 8, pp. 263-269, 2001. [6] Barret, Fastener Design Manual, NASA reference publication 1228, 1990. [7] D. Croccolo, M. De Agostinis,N. Vincenzi,” Experimental analysis on the tightening torque – preloading force relationship in threaded fasteners”, Canada : s.n, 2010. IMECE2010-37153.