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Manufacturing and Functional Characterization of Graphite/Metal Composite Materials for High Voltage Electric Motors

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27 August 2024

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28 August 2024

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Abstract
Current paper is aiming to show the obtained results in manufacturing and characterization of graphite-based and metal composite materials suitable to be used in high voltage applications of automotive and/or aviation field. Thus, 4 types of materials have been processed and tested in order to assess their suitability to be used as current collector material for electric engines. The novelty of this work is the presentation of the new innovative technological process for obtaining the carbon/metal composite material used in the manufacture of sliding contacts for current collector heads, as well as the characteristics obtained for this material. All 4 obtained materials have been characterized from structural, mechanical and functional point of view and the most suitable of them has been chosen to be further developed by the end beneficiary.
Keywords: 
Subject: Chemistry and Materials Science  -   Materials Science and Technology

1. Introduction

Actions to combat climate change and its impacts are urgent for all countries. The transport sector, accounting for around one-fifth of global CO2 emissions, remains a focus for decarbonization. Despite the COVID-19 pandemic causing a significant decline in global emissions, the transport sector still produced nearly seven gigatons of carbon emissions in 2020. With economic recovery, transport demand is expected to rise, potentially increasing emissions if no interventions are taken [1].
On one hand, prioritizing public transport over private vehicles is critical for decarbonizing transport. Investing in high-quality, low-emission public transport improves equity by providing accessibility, especially for those who cannot afford private vehicles, and positively impacts safety. Public transport users have the lowest per capita emissions among motorized modes but suffer higher air pollution levels. Electrifying public transport, particularly in developing countries, is a priority [1].
In the US and Canada, the role of public transportation in sustainability and equity is gaining attention, with the electrification of buses being key to achieving energy transformation and equity goals [2]. The EU is also making significant progress, with the Netherlands leading in electric bus adoption and other countries like Luxembourg, Sweden, and Germany following suit under the European Green Deal, which aims to reduce net greenhouse gas emissions by at least 55% by 2030 [3].
Electrified public transport promotes energy equity, addressing environmental justice concerns in marginalized communities affected by air pollution. Deploying electric buses in these areas provides cleaner and healthier transportation options [2]. Despite impressive growth in the electrification of public transport in the EU and US over the last decade, more work is needed to transition fully from diesel-powered buses and rail networks to electric alternatives [3].
Successful implementations in cities like Amsterdam, London, Barcelona, Glasgow, and New York highlight the environmental and societal benefits of this transition. Continued global and national commitments to sustainability, infrastructure investment, and collaborative efforts are laying the foundation for a cleaner, greener future in urban transport [3].
At the early stages of electrification (2009-2013), electric vehicles technologies were not widely tested, and technical specifications varied among manufacturers. Public transport operators gained critical understanding from small-scale pilots, learning to specify vehicle and charging needs to fit their operational requirements [1].
European capitals have extensive bus and tram networks, with frequent service throughout the day and night [4]. Trolleybuses, drawing power from dual overhead wires, are a key part of this infrastructure. Early trolley shoes made from cast iron were not ideal due to abrasiveness, leading to the development of carbon/metal composites, which offer similar mechanical and electrical properties to copper but with improved mechanical properties [4,5].
On the other hand, aviation is one of the biggest pollutants today which represents the 11.6% of the total transport emissions, being a serious threat due to the proximity of the vehicles to the ozone layer. To tackle this problem, several studies are being carried out in various topics such new aircraft architectures, lighter materials, new clean fuels and electrification of major systems, including propulsion. The adoption of electric propulsion in the regional aircraft would entail significant advantages in several areas. The most transcendent benefit is the reduction of nitrogen oxides (NOx) and carbon (CO, CO2) emissions due to the independency of fuels. Along with it, the noise produced by the airplane’s turbofans will be significantly minimized [6].
Electric motors in aerospace are not new. The Airbus A380 was the first commercial aircraft to apply them across multiple onboard systems and had four variable frequency electrical generators each delivering 150kVA. Today the Boeing 787 is one of the most electric airliners, with 1.5MW of onboard power and a bleed less environmental control architecture – both provided by Collins Aerospace.
The most novel aspect of increasing the use of motors in aerospace applications lies in evolving them into a primary propulsive power source [7].
The core of the motor and the electronics were developed few years ago, and since then it has been all about proving the development, working with the regulator and proving the compliance. The next stage will be writing the test plans and getting them approved. At the moment, nothing is certified for a passenger commercial aircraft [8].
Carbon/metal composites are used in various industrial fields, including high-voltage capacitors [9], and offer advantages like lightweight, corrosion resistance, and design flexibility in high-voltage applications [10]. In the automotive and aviation industries, these composites provide superior strength and hardness, are economical, and can be heat-treated for various applications [11,12].
The experiments conducted in this research aimed at the technological processing of electro-graphitic material to obtain a carbon/metal composite material that could be used as a current collector material for high current electric engines. The characteristics of the materials need to closely match the specifications required for a semi-finished product necessary for manufacturing finished products used in the operation of traction motors, especially those used in equipping public transport vehicles.
The novelty of this work is the presentation of the new innovative technological process for obtaining the carbon/metal composite material used in the manufacture of sliding contacts for current collector heads, as well as the characteristics obtained for this material.

2. Materials and Methods

Within this chapter, the development of composite materials for sliding contacts is described. Four types of materials have been developed for testing by using different raw materials and different techniques and an assessment was made in order to determine which of those four materials is more suitable for the application. Thus, option 1 which has 2 variants includes Pitch as binder but uses two types of graphite as “lubricant”: granulated graphite and flakes. Option 2 was using a phenol-formaldehyde resin (commercially known as Novolac) as binder and granulated graphite as “lubricant”. Finally, option 3 is using Novolac as binder but graphite chemically coated with copper.

2.1. Option 1: Composite Obtained by Mechanical Mixing of Graphite and Copper Powders with Carbon Binder (Coal Tar Pitch)

In this option, a composite was developed in which the bond between the carbon particles and the metallic particles is achieved through a carbon binder – coal tar pitch.
The raw materials used were:
-
Option 1 A: (CNS)
Raw material Quantity [% wt.]
Granulated natural graphite (>100 μm) 18
Electrolytic copper powder 60
Sn powder 7
Molybdenum disulfide (MoS₂) 5
Coal tar pitch 10
-
Option 1 B: (CFS)
Raw material Quantity [% wt.]
Flake natural graphite 18
Electrolytic copper powder 60
Sn powder 7
Molybdenum disulfide (MoS₂) 5
Coal tar pitch 10
Figure 1. Flow sheet for obtaining Cu/Graphite/Pitch composite material (CNS/CFS).
Figure 1. Flow sheet for obtaining Cu/Graphite/Pitch composite material (CNS/CFS).
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2.2. Option 2 (CGN): In This Option, an Isotropic Structure Composite Was Developed in Which the Bond between the Carbon Particles and the Metallic Particles Is Achieved through an Organic Binder – Novolac. To Achieve Better Compactness and Structural Uniformity, the Powder Mixture Was Coated with the Binder

The raw materials used were:
Raw material Quantity [% wt.]
Granulated natural graphite (>100 μm) 15
Electrolytic copper powder 60
Sn powder 7
Novolac (which includes 5% HMTA) 18
For cross-linking the binder, 5% HMTA (hexamethylenetetramine) was added relative to the Novolac.
Figure 2. Flow sheet for obtaining Cu/Novolac/Graphite composite material (CGN).
Figure 2. Flow sheet for obtaining Cu/Novolac/Graphite composite material (CGN).
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2.3. Option 3 (CGA): Material Obtained from Composite Powder (Graphite Chemically Coated with Copper) with Organic Binder – Novolac

In this option, a composite was created in which the bonding of graphite particles with copper is physical in nature. The addition of the binder aimed to densify and increase hardness without the metal forming a continuous network.
Globally, research is ongoing regarding the chemical deposition of metals on graphite to obtain advanced composites. Such a study was presented at the conference [13].
The method used for chemically plating graphite with copper involves a series of steps, which are presented below (Figure 3).
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resulting metallic Cu which bonds with the graphite. The bonding is realized by the π electrons of graphite which allows the forming of the metallic layer on the surface.
After it is obtained the metal plated graphite powder is used as raw material for composite manufacturing as follows:

3. Results and Discussion

All the obtained composite materials have been characterized from structural and mechanical point of view and the results are shown as follows:
From mechanical point of view, the following characteristics have been determined: initial density (before thermal treatment), final density (after thermal treatment), electrical resistivity, hardness, mechanical strength and the results are shown in Table 1.
The density of the material was calculated after the measurements of their dimensions and weighing them on an electronic balance provided by Kern, model ALT 220-4NM.
Electrical resistivity was measured by using M9115 Electrical Resistivity System provided by Grace Instruments.
HB hardness was measured by using EMCO-Test M4C025G3M apparatus
As it can be assessed from Table 1, the materials’ density increases after the thermal treatment and GCA shows the highest value. Also, CGA shows the highest value for mechanical strength and the lowest value for electrical resistivity, meaning that CGA material is the most resistant one, the denser and has the highest electrical conductivity, allowing thus electric current to pass more rapidly leading to a lower heating of the material.
From structural point of view, all 4 obtained materials have been analyzed under optical microscope at 50x. The device was provided by AXIO and is fitted with a Lumix photo camera.
As it can be observed from Figure 5, all the materials show high homogenization and structural integrity. Moreover, after the thermal treatment there are no visible pores within the structure of the material.
Also, functional characterization has been made within the lab and the following characteristics have been determined: electric discharge both at working and maximum imposed current, friction coefficient and mechanical wear after 1000 hours of work. The setup, as it can be seen in Figure 6 consisted of an array of equipment measuring the electrical parameters and also an equipment ensuring the equivalent force of the real equipment fitted on the trolleybus. Also, a copper wire similar to the ones used for trolleybus lines was continuously moved for 1000 hours while the above-mentioned apparatus was applying the force.
Table 2 is showing the electric discharge and the applied electric load of each of the samples.
Table 3 is showing the friction coefficient ant mechanical wear after 1000 working hours and, as expected graphite-based materials, CNS and CFS shows the lowers friction coefficient but the highest wear. This is correlated to their lower mechanical strength. In the meantime, CGN is showing the lowest mechanical wear even though its friction coefficient is several times higher than graphite-based materials.
Other researches have been focused on alloying the copper either with Al-Sn/Si and/or Pb and after that inserting the alloy within the material of the sliding contact [14].
Even though, the obtained materials have shown similar hardness as the one studied within this paper, the testing of the materials have been made only for 27 km and no discharge testing have been made.
Figure 7 is showing a comparison of the HB wickers hardness of the materials studies here and the ones studied by other papers.
As it can be observed from Figure 7, the HB hardness properties of the materials obtained within this paper are more uniform varying from 912 to 1017 MPa, while the ones obtained by other papers are too apart varying from 622 to 1193 MPa.
As mentioned, even though other studied materials show better mechanical properties, they haven’t been tested for such long distance and, as shown in paper [14], they already had mechanical wear. While the materials studied within this paper showed mechanical wear varying from 13 to 38 mm after 1000 working hours.
Moreover, currently, the sliding contacts commonly used are made of cast iron which has high mechanical and wear resistance but which during the electrical discharge forms small iron debris which, in time lead to mechanical wear of the copper wire, making it very expensive to replace. Even though the materials studied within this paper can form copper debris during an electric discharge, these debris have similar mechanical properties as the wire and does not wear it out, making them more suitable and less costly to use.

4. Conclusions

Analyzing the characteristics of the composites, it can be concluded that:
  • Although they have similar hardness values, the four materials exhibit different coefficients of friction, determined under identical conditions, depending on each one's chemical composition and processing method, as follows:
  • Materials with a pitch binder that also contain molybdenum disulfide as a lubricant have much lower coefficients of friction than those with a Novolac binder that contain no other lubricant besides graphite.
  • The composite made of copper-plated graphite powder has the highest coefficient of friction, which can be explained by the fact that the graphite can no longer act as a lubricant due to the coating.
  • From the perspective of mechano-electrical wear, it can be said that although they have similar hardness and mechanical strength, the materials wear differently depending on electrical conductivity and voltage drop, as follows:
  • The copper-graphite pitch composites (CNS and CFS), which have the highest electrical resistivity and voltage drop, wear the most.
  • The copper-graphite-Novolac (CGN) composite exhibits the lowest wear, having quite high electrical resistivity but the lowest voltage drops.
  • Regarding the composite based on copper-plated graphite powder, the relatively high wear is due to the fact that, despite having very low electrical resistivity, the phenomenon of copper migration from the network occurs much more easily.
  • These results shown within the paper are obtained within the lab. Therefore, testing in real life conditions is needed in order to correctly assess if the developed material which shows the most promising perspectives in suitable for the end purpose of the work.

Author Contributions

Authors individual contributions “Conceptualization, RM; methodology, RM and RE.; validation RM, RE and DE; formal analysis DE.; investigation, RE; resources, RM.; data curation, RE and DE; writing—original draft preparation, RM.; writing—review and editing, RM.; All authors have read and agreed to the published version of the manuscript.

Funding

This work was carried out through the “Nucleu” Program within the National Research Development and Innovation Plan 2022-2027, carried out with the support of MCID, project no. PN23.12.01.01

Acknowledgments

The authors would like to acknowledge the administrative support of Romanian Research and Development Institute for Gas Turbines, COMOTI.

Conflicts of Interest

The authors declare no conflicts of interest

References

  1. The World Bank, 2021. “Electrification of Public Transport: A Case Study of Shenzhen Bus Group.” World Bank, Washington, DC. License: Creative Commons Attribution CC BY 3.
  2. Bryan Jungers, Could electrifying public transportation be the key to achieving energy equity goals? , 2008 - 2024 E Source Companies LLC, February 21, 2024,.
  3. Heliox Energy, How have countries around the world electrified public transport? , July 10, 2023.
  4. Available online:. Available online: https://visitbucharest.today/bucharest-public-transport/ (accessed on 15 March 2024).
  5. Available online:. Available online: https://en.wikipedia.org/wiki/Trolleybus (accessed on 5 September 2023).
  6. P. Alvarez, M. Satrústegui, M. Martinez-Iturralde “Review of High Power and High Voltage Electric Motors for Single-Aisle Regional Aircraft”, IEEE Access, 2022. [CrossRef]
  7. J. Roper “The advances in motor technology driving the development of electric aircraft”, Aerospace Testing International, 04.2023.
  8. R. Armesmith “Electric motors for aircraft”, E-Mobility Engineering, 2024.
  9. Ching-Fang Liu, Yu-Chien Liu, Tien-Yu Yi, and Chi-Chang Hu Carbon materials for high-voltage supercapacitors, Carbon, Volume 145, April 2019, Pages 529-548.
  10. Satish Bhalerao, Nitin Ambhore, and Munjadas Kadam, Polymer Matrix Composite in High Voltage Applications: A Review, Biointerface reaesarch in applied chemistry, Volume 12, Issue 6, 2022, 8343 – 8352.
  11. Three D Metals, 5 Advantages High Carbon Steel Brings to the Automotive Industry, January 26, 2024.
  12. Achour, B; Ouinas, D; Touahmia, M ; Boukendakdji Buckling of Hybrid Composite Carbon/Epoxy/Aluminum Plates with Cutouts, Engineering, Technology and Applied Science Research, vol. 8, feb. 2018, pp: 2393-2398.
  13. Tsiskarishvili R. “Study of the process of copper plating graphite by chemical method”, Proceedings of National Academy f Sciences of Belarus, April 2013, 39(3-4), pp: 184-188,.
  14. Shyrokov V.V., Vasylenko Y.I., Khlopyk O.P. Frenchko M.S., “Development of antifriction Aluminum-base alloys and compositions for sliding current collectors”, Materials Science, vol 42, no.6, 2006.
Figure 3. Flow sheet for obtaining Cu plated graphite.
Figure 3. Flow sheet for obtaining Cu plated graphite.
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Figure 4. Flow sheet for obtaining Cu plated graphite/Novolac composite material (CGA).
Figure 4. Flow sheet for obtaining Cu plated graphite/Novolac composite material (CGA).
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Figure 5. Images of the obtained materials.
Figure 5. Images of the obtained materials.
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Figure 6. Schematic of functional characterization setup.
Figure 6. Schematic of functional characterization setup.
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Figure 7. Comparison with other studied materials.
Figure 7. Comparison with other studied materials.
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Table 1. Mechanical characteristics for the obtained composites.
Table 1. Mechanical characteristics for the obtained composites.
Material Initial density,
[g/cm3]
Final density,
[g/cm3]
Electrical resistivity,
[µΩm]
Hardness HB10/40
[kgf/mm2]
Mechanical strength,
[MPa]
CNS 3,4 3,6 157 107,6 32,7
CFS 3,4 3,6 151 100 30,5
CGN 3,0 3,2 100 93 25
CGA 3,6 3,7 7,5 99 38
Table 2. Electric discharge and electric load.
Table 2. Electric discharge and electric load.
Material Electric load (min/max) J,
[A/cm2]
Electric discharge 2Ue,
[V]
CNS 25 2
50 3,20
CFS 25 3,40
50 5,03
CGN 25 1.2
50 1.93
CGA 25 1.2
50 2.04
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