Investigation of Heat Stepping Process for Epoxy-Amine Binders

It is determined that in order to create a protective coating with high physical, mechanical, and thermophysical characteristics, it is necessary to carry out the appropriate heat stepping during its formation. *e relevance of such processing mode use providing the increase of physical-mechanical and operational characteristics of epoxy material coatings due to the structure-forming processes in the material is substantiated.


Introduction
e reliability and durability of products based on epoxy oligomers depend on the thermal time hardening mode, the correct selection of which provides coatings with optimal service and technological properties.
It is proved that the heat treatment of composite materials significantly improves their physical and mechanical characteristics, including the matrix itself [1][2][3][4]. e possibility of further improvement of these characteristics is achieved by the automation of materials in the heat treatment process. As a rule, after product forming from the material based on cold hardening epoxy binders, it is kept for 24 hours at normal temperatures and then heat-treated at temperatures 393-403 K [5]. It is determined that the matrix crosslinking degree increases with the thermal treatment of the matrix [3,4]. e increase of the gel fraction yield during material formation is defined. At these temperatures, almost all physical units in the epoxy binder are destroyed [1]. In this case, the mobility of macromolecules increases, creating conditions for additional structuring in the matrix. e authors propose to carry out the epoxy material stepping in several stages [6,7]. It is proved that due to the creation of conditions under which the increase in the macromolecules mobility at temperatures higher than the glass transition temperature is observed, the structuring processes are refined. Such change in the conformational macromolecules set improves the physical and mechanical properties of the heat-treated material. e investigation of the influence of formed material stepping at temperatures below 393 K on the matrix properties during automatic temperature control is of great interest from the scientific and practical point of view when choosing heat treatment modes. e objective of this paper is to investigate the influence of the formed materials' stepping process for the improvement of the matrix properties by increasing the degree of crosslinking while improving the structuring processes in the binder.

Materials and Methods of Investigation
e epoxy diane oligomer of ED-20 grade (ISO 18280: 2010) polyethylene polyamine hardener is chosen as a binder for the investigation of heat stepping influence on the material properties. By binder (matrix), we mean a two-component mixture comprising epoxy resin and polyethylene polyamine. After hardening, as well as under the heat action, the processing forms samples for research. Such material is hardened at room temperature. e material forming is performed at 293 K for 24 hours. Ingredient ratio is ED-20-100 and 10 weight parts of polyethylene polyamine (PEPA), which corresponds to the stereochemical component ratio. en, the material is treated at temperature T � 393 K for t � 2 hours. e material is heat-treated according to the stepping heating and cooling modes. Polyethylene polyamine is used for epoxy resin crosslinking. Polyethylene polyamine is a binder component and is aligned with it. When aligned, polyethylene polyamine reveals the oxide groups of epoxy macromolecules. During chemical interaction of the opened epoxy groups between themselves, the polymeric grid from macromolecules is formed. Isothermal treatment improves the grid formation due to changes in the confirmation set of macromolecules and Bow Group increases the degree of binder crosslinking (matrix).
Nicolet 380 IR spectrometer ( ermo Electron Corporation, USA) is used to investigate the structuring processes. Compressed powder in the form of the film containing 1 mg of the investigated substance and 150 mg of KBr is used in the infrared spectrometer. e values of the limiting wetting angle are examined using the microscope of MBS-6 grade with "Olympus C-8080" camera. e physical sense of the investigated limiting wetting angle is to determine the geometric drops dimensions and their variations in time. It is proved by the investigations that after τ � 20. . . 25 min., the latter is almost unchanged. As the investigation duration extends, the change in the composites' wetting angle is within the error margin of the experiment. e composite destructive stress during bending is determined according to ASTM D 790-03. e investigating sample is placed on two supports loaded up to fracture and load and strain values are recorded. e elasticity modulus is determined according to ASTM D 790-03, and it is the stress ratio to the corresponding relative strain increment. In order to define the internal stresses of polymer composite material, the console method is used. e differences in the free end deviation of the fixed sample with the coating in time are determined. e sample hardening degree is determined by the gel fraction content (Soxhlet apparatus).
At least 5 tests are carried out for statistical analysis of the investigation results. e arithmetic mean value of all parallel experiments is determined, and the Student criterion is used to eliminate the false values.

Results and Discussion
According to IR spectroscopy, the conversion degree of epoxy groups during hardening by ED-20 polyethylene polyamine at 293 K for 24 hours is 62% (Table 1). Further spectra analysis reveals that the absorption bands of free amino groups completely disappear. e formation of a homogeneous structure throughout the whole polymer composite volume is defined by optical microscopy. e elasticity modulus of pure binder tensile strength is E � 47.60 MPa. After heat treatment at 393 K for 2 hours, the residual stresses in coatings are σ i �3.0-3.33 MPa. Further, the stepping is performed.
e results of such treatment effect on the binder properties are presented in Table 1. Within the next 10 days, the hardening degree determining by the content of the gel fraction increases by 10% and is 72%. As a result of structuring processes, the elasticity modulus increases by 9%, which is explained by the increase of the epoxy binder spatial grid density. Further increase in the crosslinking extent at the given temperature does not occur for 25-30 days.
e obtained results are in good agreement with the known data that while hardening the epoxy compositions at low temperatures up to 1/3 of epoxy groups does not react due to steric problems [8,9] and the occurrence of physical units at a temperature below the glass transition temperature (T c ) is T c � 393-395°K.
In order to ensure greater complete compositions hardening after 24 hours of exposure at 293 K, the sample heat treatment at 393 K using an automated device for heat treatment process control is carried out. e block diagram of the device is shown in Figure 1.
e device operates in the following way. e temperature in the furnace is measured by a thermocouple and is fed to the controller via the analog-digital converter, which, depending on the temperature value and set mode, outputs the control signal to the thermostat to increase or decrease the furnace heat. You are able to control the process by a personal computer that is connected to the controller by means of an interface converter. New heat treatment modes are also set new.
It is determined that with the increase of material formation temperature, the number of unreacted functional groups decreases, the composition structure formation degree increases, and the chemical grid with a greater degree of crosslinking volume is formed. It should be noted that in the grid formation at temperatures below T c , the structural processes in the binder are observed. However, as the result of reducing the chain section length between the crosslinking units, including those reduced by means of physical interaction, the binder macromolecule mobility and the structuring processes are reduced. With the increase of heat treatment temperature greater than 393 K, the speed of the crosslinking process increases significantly. Cohesive strength decreases due to the increase of internal stresses in the epoxy composite, as well as the occurrence of heterogeneous structure in the material. e increase of residual stresses at high adhesion of epoxy compositions to the metal surface causes protective coatings cracking, especially at the edges and, as a consequence, results in their separation.
For further improvement and support of high stability of operational and technological characteristics of epoxy composites in real conditions of long-term operation while choosing the optimum treatment mode, the composite heat stepping is also carried out taking into account the investigations of their hardening kinetics.
Based on the previous results of the investigations of the epoxy composites hardening kinetics, new modes of materials stepping heating are proposed ( Figure 2 and Table 2) taking into account isothermal effects, their intensity, and time of manifestation in the hardening process. e start of heating time (t 1 and t 2 ) and treatment duration (τ 1 and τ 2 ) are selected on the basis of the investigation results of epoxy composites mechanical loss tangent in the process of material forming into products [10]. e extremes on the dependence graph tg δ correspond to the material heat stepping modes. e correlation between these extremes and the heat treatment duration is also observed. e processing temperature (t) is chosen in the area T � 293 ÷ 353 K.
Due to the thermomechanical analysis and console method for elasticity modulus determination, it is possible to define the glass transition temperature (T S ) of epoxy composite materials investigated in the form of metal-based coatings by the nature of the stress changes curve [10]. Figure 3 shows the dependence of the internal stresses change on the temperature in the coatings based on epoxy resin and PEPA formed on the steel plate and hardened according to the specified heat treatment modes ( Figure 2 and Table 2).
It is evident from Figure 3 that the curves of temperature dependence of the internal stresses in coatings are nonmonotonic. e minimum stress corresponds to the epoxy composites' glass transition temperature. e maximum indicates the flow of additional structuring processes. erefore, the analysis of these results proves that the highest glass transition temperature corresponds to the coating on the basis of thermally treated composition no. 3. In this case, T S for coating treated under specified mode increases by 22 K compared to the coating maintained at room temperature.
Room temperature  2  20  100  35  30  313  303  3  20  100  35  30  333  303  4  0  100  35  30  333  313  5  -100  -30  -323  6  20  100  35  30  353  313  7 20 -180 -353 - Advances in Materials Science and Engineering e flow of structuring processes in the matrix is also confirmed by the change in their elasticity modulus under bending when the temperature changes ( Figure 4). For coating based on composition no. 3 (curve 3), the value of the elasticity modulus first sharply decreases, and then, it almost does not change with temperature. e horizontal area of this curve characterizes the conditionally equilibrium elastic modulus of the structured composite.
For coating material hardened at room temperature, the sharp decrease of the elasticity modulus under bending while changing the temperature (T � 393 K) is observed. But when the minimum value is reached, it starts to increase with further temperature rise. e module value asymptotically approaches the value of equilibrium elasticity modulus of the coating material formed on composition no. 2 basis.
It is determined that the heat treatment of epoxy coatings increases the material crosslinking degree. e value of the limiting wetting edge angle is an indicator of the crosslinking degree as the number of functional groups in the material decreases. e qualitative indicators of these processes are evaluated by the limiting wetting angle. e correlation of adhesion characteristics and the limiting wetting angle is also proved. ese results are in good agreement with the results of the paper [11]. e given data (Table 1) show that the minimum wetting angle corresponds to the composite crosslinked at 293 K for 24 hours and is 31°at a hardening rate of 62%. Increasing the crosslinking temperature and, relatively, the composition hardening degree increases the wetting angle. e increase of the wetting angle at treatment temperature rise can be explained by the decrease in the composite surface energy, associated with the decrease in the active functional group concentration being in good agreement with the materials of paper [11]. e composition is hardened at temperature 293 K for 72 hours and then heat-treated at temperature 393 K for 2 hours. Further, the stepping is performed according to the scheme shown in Figure 2, where T 1 is changed from 313 to 353 K at 20 K intervals and T 2 from 303 to 323 K at 10 K intervals.
It is determined that the composition formation at 293 K and subsequent heat treatment improves the impact toughness a � 8.7 kJ/m 2 to 9.25 kJ/m 2 , and the heat resistance increases by 17-18 K. It is proved that the increase in the temperature of additional stepping with T 1 � 313 K and T 2 � 303 K to T 1 � 353 K and T 2 � 323 increases the impact toughness to a � 9.45 kJ/mm 2 and heat resistance to 375 K.

Conclusions
e correlation dependence of the heat stepping modes with physical-mechanical and structural characteristics of the developed epoxy binders is proved. While creating composite materials with high operational properties, it is necessary to carry out the following thermal treatment, including stepping: expose time 24 hours at 293 K followed by heat treatment at temperature 393 K for 2 hours, then the material treatment at temperature 333 K for 35 minutes, then holding at temperature 293 K for 45 minutes, and further holding at 313 K for 30 min.
In future, we plan to investigate the effect of various organic modifiers and stepping on the modified matrix properties. e following material will be used as a binder for composites containing nanoadditives and discrete and longdimensional fibers.

Data Availability
e data used to support the findings of this study are available from the corresponding author upon request.

Conflicts of Interest
e authors declare that they have no conflicts of interest.  Table 1 (curve numbers correspond to composition numbers given in Table 2).