Characterisation of Hemp Fibres Reinforced Composites Using Thermoplastic Polymers as Matrices

Hemp fibres used as a reinforcing agent and three polymeric matrices (polypropylene, bicomponent, recycled polyester) were used to obtain composite materials by needle punching and heat pressing. The influence of the hemp/matrix ratio and the nature of the matrix on the properties of the composites were analysed. The obtained composites were characterised by physical–mechanical indices, thermal analysis (thermogravimetry (TG), differential thermogravimetry (DTG) and Differential Scanning Calorimetry (DSC)), Fourier Transform Infrared Spectroscopy (FTIR-ATR) analysis, Scanning Electron Microscopy (SEM) and Chromatic measurements. The mechanical properties of composites are influenced by both the hemp/matrix ratio and the nature of the matrix. The thermal stability of composites decreased as the amount of hemp increased (for the same mass losses, the decomposition temperature decreased significantly for composites containing a quantity of hemp greater than 50%). Regarding the nature of the matrix, for the same mass loss, the highest decomposition temperature was presented by the composites containing recycled polyester as matrix, and the lowest one was presented by composites containing polypropylene fibres as matrix. The FTIR and SEM analyses highlight the changes that occurred in the structure of the composite, changes determined both by the amount of hemp in the composite and by the nature of the matrix.


Introduction
In recent decades, due to their wide range of properties, composite materials have successfully replaced traditional materials such as metals, wood and plastics in many industrial fields: aerospace, automotive, energy, construction, marine, transportation, infrastructure, electronics and electrotechnics, agriculture, food, chemical, furniture, packaging, sports and recreation [1][2][3][4][5][6][7]. The rapid growth of the composite material market is closely related with performance limitations of traditional materials, such as the availability and the price. Composite materials combine the qualities of two or more materials with different properties in a product that has superior characteristics over the individual constituents. One constituent is called matrix, and embeds the other constituent, called the reinforcement. The reinforcement takes over the load and gives the composite material strength and rigidity, and the matrix binds the reinforcements together and transfers the load to and between the reinforcements. Polymer composites reinforced with natural lignocellulosic fibres are intensively studied as replacements in common applications for composites reinforced

Experimental Variants
In order to obtain composite materials, hemp fibres (H) as reinforcing agent and three types of thermoplastic polymer fibres as matrix were used: polypropylene (PP), bicomponent fibre (BI) and recycled polyester fibres (PES). Within each variant the percentage composition of the two components was modified from 0 to 100%. The coding and composition of the materials according to the experimental variants are presented in Table 2.

Composites Processing
The manufacturing process of composite materials consisted of the following steps:  In accordance with the specifications of EN 326-1 standard, type 2 samples (250 mm length, 25 mm width) were used for tensile testing. The distance between clamps was 150 mm and the testing speed was 2 mm/min as specified in SR EN ISO 527-4:2000 standard. The tensile test was performed on a ZWICK tensile tester (Ulm, Germany) at 23 • C according to ISO 527-4 standard. Five repetitions were done for each sample.

Thermogravimetric Analysis (TG/DTG)
The thermogravimetric measurements were performed using a Mettler Toledo TGA/SDTA 851 balance (Columbus, OH, US), allowing the simultaneous recording of the weight losses (TG) and the derivative thermogravimetric curves (DTG). The analysis was carried out under constant nitrogen flow (20 mL/min), at a heating rate of 10 • C/min. The heating scans were performed on 1.9-5.3 mg of sample in the temperature range 25-700 • C.

Differential Scanning Calorimetry (DSC)
The melting and crystallisation behaviour of the composites was studied using a Mettler Toledo DSC1 differential scanning calorimeter (Columbus, OH, US). The mass of samples encapsulated in aluminium pans with pierced lids to allow evaporation of the volatile components ranged between 2.2 and 5.4 mg. A nitrogen flow rate of 150mL/min was used. The sample was initially scanned from −60 to 200 • C or −60 to 300 • C at a heating rate of 10 K/min and followed by cooling with the same rate, and then it was rescanned in the same temperature interval. The crystallisation temperature (Tc), the crystallisation enthalpy (H c ), the melting temperature (Tm) and the melting enthalpy (H m ) were obtained from the heating-cooling-heating cycle of the sample. The crystallinity, X c (%), of the different compounds was obtained by Equation (1).
where in ∆H 0 m corresponds to the theoretical melting enthalpy of the fully crystalline polypropylene, whose value according to the literature's data is 207 J·g −1 , and w is the mass fraction of the filler [47].

Fourier Transform Infrared Spectroscopy
For the spectroscopic studies, a Bruker FTIR Vertex 70 spectrometer equipped with a diamond ATR (attenuated total reflection) device (Golden Gate; Bruker, Billerica, MA, USA) and ATR-FTIR (attenuated total reflection Fourier transform infrared) was used. The ATR-FTIR spectra were measured in the spectral range of 800-4000 cm −1 , by the accumulation of 64 scans.

Scanning Electron Microscopy
The scanning electron microscopy studies were performed on samples fixed on aluminium supports. The surface morphology of the uncoated samples was examined using an SEM-type Quanta 200 (FEI) (Hillsboro, OR, USA), operating at 20 kV with secondary electrons in the low vacuum mode (large-field detector (LFD)), the magnification being indicated on the micrographs.

Chromatic Measurements
Samples of composite materials were subjected to colour measurements performed on the entire spectrum of the visible range. The sample were evaluated for colour strength in terms of Kubelca-Munk equation [48] wherein "R" is the reflectance at sample complete opacity; "K" is the absorption coefficient; "S" is the scattering coefficient. A DATACOLOR SF-300 spectrophotometer (Lawrence Township, NJ, USA) was used for this purpose. The processing of the experimental data was performed with the help of some specialised software, Micromach R 2000.

Mechanical Properties
The mechanical properties of the fibres used as reinforcing agents, of the polymeric fibres used as matrices, and of the composite materials obtained from them are shown in Figures 1-3. The 100% hemp sample, which is a nonwoven material, has a much lower tensile strength (0.76 MPa) than composite materials. The tensile strengths of composite materials containing hemp fibre as a reinforcer increased as the content of the polymer matrix increased. The highest values were obtained for the composites that contain a quantity of hemp ranging between 30 and 50% (w/w), after which there was a slight decreasing tendency of the tensile strength. Regarding the nature of the matrix, the highest values of tensile strength were obtained for composite materials with polyester matrix (26.2 MPa), followed by composite materials with bicomponent fibre (23.77 MPa) and then by composite materials with polypropylene (20.33 MPa).
The elongation at break of the 100% hemp nonwoven material was approximately 71.5%, and this decreased in the composite materials as the hemp content increased. This decrease can be explained by the increased crystallinity of these composite materials ( Table 4). The elongations at break of the 100% polymer matrices are higher than those of the composite materials. PP has the highest value of elongation at break (14.1%), being followed by BI (12.5%) and afterthen by PES (8.3%). These values confirm the role of the reinforcing agent used in obtaining the composite materials. Samples of composite materials were subjected to colour measurements performed on the entire spectrum of the visible range. The sample were evaluated for colour strength in terms of Kubelca-Munk equation [48] R 2 ) R 1 ( S K 2   (2) wherein "R" is the reflectance at sample complete opacity; "K" is the absorption coefficient; "S" is the scattering coefficient. A DATACOLOR SF-300 spectrophotometer (Lawrence Township, NJ, USA) was used for this purpose. The processing of the experimental data was performed with the help of some specialised software, Micromach R 2000.

Mechanical Properties
The mechanical properties of the fibres used as reinforcing agents, of the polymeric fibres used as matrices, and of the composite materials obtained from them are shown in Figures 1-3. The 100% hemp sample, which is a nonwoven material, has a much lower tensile strength (0.76 MPa) than composite materials. The tensile strengths of composite materials containing hemp fibre as a reinforcer increased as the content of the polymer matrix increased. The highest values were obtained for the composites that contain a quantity of hemp ranging between 30 and 50% (w/w), after which there was a slight decreasing tendency of the tensile strength. Regarding the nature of the matrix, the highest values of tensile strength were obtained for composite materials with polyester matrix (26.2 MPa), followed by composite materials with bicomponent fibre (23.77 MPa) and then by composite materials with polypropylene (20.33 MPa).    The elongation at break of the 100% hemp nonwoven material was approximately 71.5%, and this decreased in the composite materials as the hemp content increased. This decrease can be explained by the increased crystallinity of these composite materials (Table 4). The elongations at break of the 100% polymer matrices are higher than those of the composite materials. PP has the highest value of elongation at break (14.1%), being followed by BI (12.5%) and afterthen by PES (8.3%). These values confirm the role of the reinforcing agent used in obtaining the composite materials.

TGA and DTG Analysis
The TGA and DTG thermograms of the hemp fibres used as reinforcers, of the various matrices (formed of polypropylene fibres, polyester fibres and bicomponent fibres) and of the composites obtained from them are presented in Figures 4-6.   The elongation at break of the 100% hemp nonwoven material was approximately 71.5%, and this decreased in the composite materials as the hemp content increased. This decrease can be explained by the increased crystallinity of these composite materials (Table 4). The elongations at break of the 100% polymer matrices are higher than those of the composite materials. PP has the highest value of elongation at break (14.1%), being followed by BI (12.5%) and afterthen by PES (8.3%). These values confirm the role of the reinforcing agent used in obtaining the composite materials.

TGA and DTG Analysis
The TGA and DTG thermograms of the hemp fibres used as reinforcers, of the various matrices (formed of polypropylene fibres, polyester fibres and bicomponent fibres) and of the composites obtained from them are presented in Figures 4-6.

TGA and DTG Analysis
The TGA and DTG thermograms of the hemp fibres used as reinforcers, of the various matrices (formed of polypropylene fibres, polyester fibres and bicomponent fibres) and of the composites obtained from them are presented in  Before analysing the thermal behaviour of composite materials, it is important to analyse the thermal behaviour of each component of the composite (Figure 4). When analysing the TG curve of hemp fibre, a mass loss of 7.3% was observed in the temperature range between 41 and 149 • C, which can be attributed to the loss of moisture from the surface of hemp fibre. In the range 149-303 • C, the mass losses were small (7.06%). The highest mass loss of 57.7% occurred within the temperature range of 303 • C to 376 • C, and can be attributed to the degradation of cellulose and hemicellulose (the rate of degradation is greatest at 359 • C). At temperatures between 376 • C and 498 • C and even higher, there was a new mass loss due to lignin degradation [49].
Regarding the DTG curve, the peak at 55 • C can be attributed to the moisture loss of the hemp fibre, while the sharp peak at 559 • C is due to the degradation of cellulose and hemicellulose. The peak at 446 • C can be attributed to lignin degradation. [47].
From the TG diagram of the polyester fibre, it is observed that it did not undergo significant changes up to the temperature of 399 • C. In the temperature range 399-461 • C, there was a significant degradation of the fibre (mass loss of 89.33%). Degradation continued up to temperature of 650 • C. From the DTG curve, it can be observed that the degradation rate reached its maximum at 434 • C.
By analysing the thermal behaviour of the bicomponent fibre, which is made of PP (cover) and polyester (core), it was observed that up to the temperature of 396 • C, there were no significant changes in terms of weight loss. A significant degradation of the fibre occurred in the range 396-462 • C (mass loss of 84.97%). The degradation continued in the range 462-664 • C, with a mass loss of 14.81%.       Before analysing the thermal behaviour of composite materials, it is important to analyse the thermal behaviour of each component of the composite (Figure 4). When analysing the TG curve of hemp fibre, a mass loss of 7.3% was observed in the temperature range between 41 and 149 °C, which can be attributed to the loss of moisture from the surface of hemp fibre. In the range 149-303 °C, the mass losses were small (7.06%). The highest mass loss of 57.7% occurred within the temperature range of 303 °C to 376 °C, and can be attributed to the degradation of cellulose and hemicellulose (the rate of degradation is greatest at 359 °C). At temperatures between 376°C and 498°C and even higher, there was a new mass loss due to lignin degradation [49].
Regarding the DTG curve, the peak at 55 °C can be attributed to the moisture loss of the hemp fibre, while the sharp peak at 559 °C is due to the degradation of cellulose and hemicellulose. The peak at 446 °C can be attributed to lignin degradation. [47].
From the TG diagram of the polyester fibre, it is observed that it did not undergo significant changes up to the temperature of 399 °C. In the temperature range 399-461 °C, there was a significant degradation of the fibre (mass loss of 89.33%). Degradation continued up to temperature of 650 °C. From the DTG curve, it can be observed that the degradation rate reached its maximum at 434 °C.
By analysing the thermal behaviour of the bicomponent fibre, which is made of PP (cover) and polyester (core), it was observed that up to the temperature of 396 °C, there were no significant changes in terms of weight loss. A significant degradation of the fibre occurred in the range 396-462 °C (mass loss of 84.97%). The degradation continued in the range 462-664 °C, with a mass loss of 14.81%.
The DTG curve of the bicomponent fibre indicates a maximum degradation at the temperature of 436 °C, which can be attributed to the degradation of the polypropylene component, and another one at 601 °C, probably due to the degradation of the polyester component.
From the TG diagram of the polypropylene fibre, it can be observed that a maximum degradation of the fibre occurred in the range 358-469 °C, with a mass loss of 98.14%. From the DTG curve, it can be observed that the maximum degradation of fibre took place at the temperature of 442 °C.
After analysing the TG curves of composite materials containing hemp as the reinforcing agent and polypropylene as the matrix (Figure 5), it can be observed that: in the The DTG curve of the bicomponent fibre indicates a maximum degradation at the temperature of 436 • C, which can be attributed to the degradation of the polypropylene component, and another one at 601 • C, probably due to the degradation of the polyester component.
From the TG diagram of the polypropylene fibre, it can be observed that a maximum degradation of the fibre occurred in the range 358-469 • C, with a mass loss of 98.14%. From the DTG curve, it can be observed that the maximum degradation of fibre took place at the temperature of 442 • C.
After analysing the TG curves of composite materials containing hemp as the reinforcing agent and polypropylene as the matrix (Figure 5), it can be observed that: in the first stage of degradation (between 25 and 150 • C), the mass loss increased with the increase in the hemp content, as would be expected, since the polypropylene matrix has a strong hydrophobic character and does not absorb moisture.
The thermal stability of the analysed composite materials decreased slightly with the increase in the hemp content used as reinforcing agent.
From the TG curves ( Figure 6) obtained for the composite materials containing 50% hemp and 50% matrix (PP, BI and PES), it can be noticed that the thermal stability of the samples decreased in the following order: composites with polyester fibre matrix > composites with bicomponent fibre matrix > composites with polypropylene matrix. For temperatures higher than 420 • C, the composites with polyester fibre matrix and the composites with bicomponent fibre matrix showed an almost similar behaviour. From the analysis of the DTG curves it can be observed that four peaks appear in the composite material with the PP matrix. The first peak that appears in the range 54-120 • C corresponds to the loss of moisture, while the peak at 342 • C corresponds to the degradation of hemp, the peak at 393 • C can be attributed to the degradation of lignin and PP, and the one at 465 • C corresponds to the degradation of PP. The temperature range indicated for the use of this composite is 20-120 • C.
For the samples with bicomponent fibre matrix, three peaks occurred. The peak in the range 48-95 • C can be attributed to the moisture loss of the hemp fibre. The peaks from 344 • C and 432 • C can be attributed to the degradation of the hemp fibre and to the polypropylene component of the bicomponent fibre.
Three peaks appear in the DTG diagram of the composite with a polyester matrix. The peak in the range 54-74 • C can be attributed to the moisture loss from the hemp fibre, the one at 344 • C corresponds to the degradation of the hemp fibre, and the peak at 435 • C can be attributed to the degradation of the polyester fibre in the composite material.
The most important thermogravimetric characteristics (T onset -the starting temperature of the step, T peak -the temperature corresponding to the maximum value of the mass loss, T endset -the ending temperature of each step and w%-the percentage mass loss corresponding to each interval) are listed in Table 3. Thermal stability increases as the amount of hemp in the composite decreases. For the same mass losses, the decomposition temperature decreased significantly for the composites that contain hemp in quantities higher than 50% (Table 4). Regarding the influence of the matrix on the thermal stability of the composite, it can be observed that the composite material with the polyester fibre matrix exhibited the highest thermal stability, being followed by the composite with a bicomponent fibre matrix. For the same mass losses, the decomposition temperatures of the composites decreased in the order of 50H50PES > 50H50BI > 50H50PP.

DSC Analysis
The DSC thermograms indicate the melting and crystallisation temperatures of the analysed samples (Figures 7-9). From the DSC curves (Figure 7a) corresponding to the heating process, it can be observed that the DSC curve of the hemp fibre shows a low endothermic peak around 63 • C, which corresponds to the decrease in moisture in the fibre. The DSC curve of polypropylene fibre presents an endothermic peak at 165 • C, while the DSC thermogram of the bicomponent fibre shows two peaks, the first one at 71 • C corresponding to the fibre in the mantle structure, and the second one at about 237 • C corresponding to the fibre core. In the case of the polyester fibre, the initial melting temperature is 235 • C, with a maximum of 239 • C and a final temperature of 243 • C. The DSC curves obtained in the cooling process (Figure 7b) indicate for hemp fibres an exothermic heat flow that is almost constant in the analysed temperature range. For the other fibres subjected to the cooling process, the crystallisation process takes place at 112 • C for polypropylene, at 166 • C for the bicomponent fibre and at 201 • C for the polyester fibre, respectively. Regarding the nature of the matrix derived from the analysed composites (Figure 8), from the DSC curves, it can be observed that the first peak appears at 62 °C for the composite 50H50BI, at 72 °C for the composite 50H50PP and at 78 °C for the composite 50H50PES. These peaks are assigned to the endothermic processes that correspond to the evaporation of moisture from the composite material. The second peak occurs at 159 °C for 50H50BI, at 166 °C for PP and 248 °C for polyester fibre, respectively. From the diagrams resulting from the cooling process, the exothermic crystallisation peaks appear at 115 °C for 50H50PP, at 113 °C for 50H50BI and at 197 °C for 50H50PES, respectively. The composite materials obtained from 25H75 PP and 50H50PP have a higher melting temperature compared to the melting temperature of PP, while composites obtained from 75H25 PP have a lower melting temperature compared to the melting temperature of PP fibres. This could be explained by an increased interaction between the PP matrix and the reinforcer for composites containing up to 50% H. These results are also correlated with the results obtained in the case of physical-mechanical indices when the tensile strength increases up to a composition of about 50% hemp fibres, after which it shows a decreasing tendency.  Regarding the influence of hemp fibre content (Figure 9a) in polypropylene fibre matrix composites, the DSC curves are consistent with the TGA curves. The first endothermic peak appears at 70 °C for composite 25H75PP, at 72 °C for composite 50H50PP and at 75 °C for composite 75H 25PP, respectively.  Regarding the influence of hemp fibre content (Figure 9a) in polypropylene fibre matrix composites, the DSC curves are consistent with the TGA curves. The first endothermic peak appears at 70 °C for composite 25H75PP, at 72 °C for composite 50H50PP and at 75 °C for composite 75H 25PP, respectively.  Regarding the nature of the matrix derived from the analysed composites (Figure 8), from the DSC curves, it can be observed that the first peak appears at 62 • C for the composite 50H50BI, at 72 • C for the composite 50H50PP and at 78 • C for the composite 50H50PES. These peaks are assigned to the endothermic processes that correspond to the evaporation of moisture from the composite material. The second peak occurs at 159 • C for 50H50BI, at 166 • C for PP and 248 • C for polyester fibre, respectively. From the diagrams resulting from the cooling process, the exothermic crystallisation peaks appear at 115 • C for 50H50PP, at 113 • C for 50H50BI and at 197 • C for 50H50PES, respectively. The composite materials obtained from 25H75 PP and 50H50PP have a higher melting temperature compared to the melting temperature of PP, while composites obtained from 75H25 PP have a lower melting temperature compared to the melting temperature of PP fibres. This could be explained by an increased interaction between the PP matrix and the reinforcer for composites containing up to 50% H. These results are also correlated with the results obtained in the case of physical-mechanical indices when the tensile strength increases up to a composition of about 50% hemp fibres, after which it shows a decreasing tendency.
Regarding the influence of hemp fibre content (Figure 9a) in polypropylene fibre matrix composites, the DSC curves are consistent with the TGA curves. The first endothermic peak appears at 70 • C for composite 25H75PP, at 72 • C for composite 50H50PP and at 75 • C for composite 75H 25PP, respectively.
From the diagram of the cooling process of the composite materials, we can observe an increase with a 2-3 • C increment in crystallisation temperature (Tc) of the composites compared to pure PP.
The crystallisation temperature of PP (112.5 • C read from the cooling curve of Figure 9b) suggests that PP is a semicrystalline polymer that exhibits a high tendency to crystalise.
The values of the crystallisation temperatures corresponding to the obtained composite materials are close. The difference between the crystallisation temperature of PP and the crystallisation temperatures of the obtained composites is around 3 • C, while the values of their crystallisation temperatures range between 112.5 and 115.55 • C.
This fact confirms that the hemp fibres acted as nucleation agents, and consequently the PP from the composite materials started to crystallise at a temperature higher than 112.5 • C, the surface of the hemp fibres constituting crystallisation centers for the polymeric matrix [50].
From Figures 7a and 9a and from Table 5, it can be noticed that during the heating process, a slight decrease in the melting temperature of the composite material, Tm, occurs, compared to the melting temperature of the polymeric matrix. This behaviour was previously reported by other researchers [51,52]. Table 5. DSC data for PP and its composites.  This decrease in the melting temperature can be explained by the incompatibility between the PP fibre, which has nepolar groups, and the hemp fibre, a hydrophillic lignocellulosic fibre (between the two types of fibres only weak interactions occurred).
A second scan for the composite samples was also performed (with a second heating). The results obtained from the interpretation of the curves recorded at the second heating, the glass transition temperatures included (T g ), have been inserted in the tables (Tables 5 and 6). Table 6. DSC data for hemp and its composites.

Sample
∆H m (J/g) * ∆H c (J/g) ∆H m (J/g) ** T g ( • C) *** For the composite materials obtained from PP and hemp, we can observe, on the one hand, an increase in the enthalpy of melting ∆H m, and on the other hand a decrease in the crystallinity as the hemp fibre content from the composite decreased. Regarding the enthalpy of crystallisation, the higher the degree of crystallinity of the composite material, the higher the amount of heat released [53,54]. Table 5 shows the values obtained for the crystallisation enthalpy ∆H c , the melting enthalpy ∆H m and the level of crystallinity Xc, calculated with Equation (1). The value obtained for the melting enthalpy ∆H m of PP is 74.4 J·g −1 , and close values were previously reported by other authors (∆Hm 74 (J·g −1 ) [55]. It can be noticed that the value of crystallinity Xc for PP (45.19%) is lower compared to the values of the crystallinity level for the composite materials, which vary from 77.23% to 46.58%. From the curve recorded at the second heating, it is clear that the melting temperature T m of pure PP was 164.74 • C, while the characteristic melting temperatures of the composite materials ranged from 161.58 • C to 163.20 • C. The values of the crystallinity level Xc corresponding to the heating process ranged between 40.85% and 68.94%. Both for the cooling process and the heating process, the values of the crystallinity level for the composite materials were higher than the crystallinity level of pure PP used as matrix. These results could be explained by the nucleation effect exerted by the lignocellulosic hemp fibres on the PP matrix, during the manufacturing of the composite materials. The obtained results regarding the influence of the matrix type features on the composite materials containing 50% hemp and 50% polymer fibre are shown in Table 6.
The values for the melting enthalpy ∆Hm are higher for the polyester fibre than for the bicomponent fibre. Additionally, the values of the melting enthalpy ∆Hm of the composite materials obtained from these fibres are lower than those obtained for the polymer matrices.
The values of the glass transition temperature for recycled PES previously reported by other researchers range between 60 and 80 • C [56][57][58][59]. The Tg value obtained by us for recycled PES falls within this range.

FTIR Analysis
The FTIR spectra of the hemp and polypropylene, and of the composite materials for the wave numbers range (3600-600 cm −1 ), are shown in Figure 10a-e.
The broadband in the range 3429-3349 cm −1 is assigned to the stretching vibrations of the -OH groups belonging to the cellulose and hemicellulose from the hemp fibre [60].
The peaks located within the range 2963-2856 cm −1 in the FTIR spectra of the hemp, the polymeric fibres and the composite materials can be assigned to both types of stretching vibrations (symmetrical and asymmetrical) of the C-H bonds (CH 2 groups) from the hemp and from the polymeric fibres [61].
The absorption band located in the range 1733-1741 cm −1 corresponds to the stretching vibrations of the C=O bonds presented in the lignin, pectin and waxes contained by the hemp fibre. The intensity of this absorption band decreased with the decrease in the hemp content in the composite materials wherein polypropylene was used as the matrix. In the case of polyester fibres, of the bicomponent fibres and of the composite materials containing these fibres as matrices, the peaks located at 1713 cm −1 , 1717 cm −1 , 1715 cm −1 and 1719 cm −1 are due to stretching vibrations of the group C=O from the polyester.
The intensity of the absorption band around 1640 cm −1 , attributed to the bending vibrations of O-H bonds from the adsorbed water molecules, decreased once the amount of polypropylene from the composites had increased. This is due to the fact that by decreasing the amount of hemp there are fewer "free" hydroxyl groups engaged in the formation of the hydrogen bonds [62].
The peak detected at 1426 cm −1 in the FTIR spectrum of hemp corresponds to the bending vibrations of C-H bonds from the CH and CH 2 groups of cellulose, hemicellulose and lignin. The peak recorded at 1457 cm −1 in the FTIR spectrum of PP and in the FTIR spectra of the composites that contain PP corresponds to the bending vibrations of C-H bonds from the CH 2 and CH 3 groups of propylene [63]. The peak located at 1315 cm −1 in the FTIR spectrum of the hemp, attributed to the rocking vibrations of the C-H bonds from the CH 2 groups of cellulose, was not found in the FTIR spectra of the rigid composites that contain hemp [64]. The peak recorded at 1026 cm-1 in the FTIR spectrum of hemp, attributed to the stretching vibrations of the C-O bonds (C-O-C glycosidic linkages from cellulose and hemi-cellulose, C-OH phenolic groups from lignin and C-O-C ether linkages from lignin, respectively), decreased greatly in intensity as the amount of hemp in the composites decreased [65]. The decrease in the peak intensity once the PP/H ratio had increased may be due to the steric hindrance that occurs as the amount of PP in the composite increases. The band located around 1094 cm −1 in the FTIR spectra of the polyester fibres, bicomponent fibres and hemp containing composites is attributed to the stretching vibrations of the C-O bonds from the ester groups of polyester, as well as to the stretching vibration of the C-O bonds from the ether groups of cellulose, hemicellulose and lignin. The peak located around 898 cm −1 is characteristic of the glycosidic β-linkage from the cellulose and hemicellulose. The peak detected around 872 cm −1 is attributed to the stretching vibrations of the C-O bond from the polyester. The peak recorded around 840 cm −1 is assigned to the out-of-plane stretching vibrations of the C-H bonds from the aromatic rings present in the lignin [65]. The presence of the peaks located at 721, 723 and 725 cm −1 is related to the out-of-plane stretching vibrations of the C-H bonds from the aromatic ring [66]. The values of the glass transition temperature for recycled PES previously reported by other researchers range between 60 and 80 °C [56][57][58][59]. The Tg value obtained by us for recycled PES falls within this range.

FTIR Analysis
The FTIR spectra of the hemp and polypropylene, and of the composite materials for the wave numbers range (3600-600 cm −1 ), are shown in Figure 10a  The broadband in the range 3429-3349 cm −1 is assigned to the stretching vibrations of the -OH groups belonging to the cellulose and hemicellulose from the hemp fibre [60].
The peaks located within the range 2963-2856 cm −1 in the FTIR spectra of the hemp, the polymeric fibres and the composite materials can be assigned to both types of stretching vibrations (symmetrical and asymmetrical) of the C-H bonds (CH2 groups) from the hemp and from the polymeric fibres [61].
The absorption band located in the range 1733-1741 cm −1 corresponds to the stretching vibrations of the C=O bonds presented in the lignin, pectin and waxes contained by the hemp fibre. The intensity of this absorption band decreased with the decrease in the hemp content in the composite materials wherein polypropylene was used as the matrix. In the case of polyester fibres, of the bicomponent fibres and of the composite materials containing these fibres as matrices, the peaks located at 1713 cm −1 , 1717 cm −1 , 1715 cm −1 and 1719 cm −1 are due to stretching vibrations of the group C=O from the polyester.
The intensity of the absorption band around 1640 cm −1 , attributed to the bending vibrations of O-H bonds from the adsorbed water molecules, decreased once the amount of polypropylene from the composites had increased. This is due to the fact that by decreasing the amount of hemp there are fewer "free" hydroxyl groups engaged in the formation of the hydrogen bonds [62].
The peak detected at 1426 cm −1 in the FTIR spectrum of hemp corresponds to the bending vibrations of C-H bonds from the CH and CH2 groups of cellulose, hemicellulose

SEM Analysis
The SEM images of the hemp fibres, polymeric fibres and composite materials are presented in Figure 11.
The matrices of PP, PES and BI, the reinforcing agent, and the obtained composite materials were morphologically investigated. The images were recorded at 1000× and 5000×.
From Figure 11a it can be observed that the size of the hemp fibres is about 50 µm and their surface is rough. PP and PE matrices (Figure 11b,c) have a specific compact, homogeneous structure. In the case of the BI matrix, it can be observed that the fibres have a size of approximately 20-30 µm, and the surface of the fibres is smooth. In order to highlight the influence of the matrix, the morphology of the composite materials with 50% reinforcing agent (hemp) and 50% matrix (PP) was analysed (Figure 11f,h,i). From a morphological point of view, good adhesion between components implies a compact structure, in which the reinforcing agent is evenly distributed in the matrix. In Figure 11e-g, the influence of the hemp percentage on the morphology of the H-PP composite can be observed. At a rate of 25-50% hemp, it can be noticed that the fibres are well integrated into the PP matrix. When the percentage of hemp increases to 75%, some of the fibres are not embedded in the matrix. The results indicated by the SEM images are also confirmed by the physico-mechanical tensile strengths, which increased in the first stage for the composites that contain up to about 50% hemp, and after that they exhibited a decreasing tendency. The matrices of PP, PES and BI, the reinforcing agent, and the obtained composite materials were morphologically investigated. The images were recorded at 1000× and 5000×.
From Figure 11a it can be observed that the size of the hemp fibres is about 50 μm and their surface is rough. PP and PE matrices (Figure 11b,c) have a specific compact, homogeneous structure. In the case of the BI matrix, it can be observed that the fibres have a size of approximately 20-30 μm, and the surface of the fibres is smooth. In order to highlight the influence of the matrix, the morphology of the composite materials with 50% reinforcing agent (hemp) and 50% matrix (PP) was analysed (Figure 11 f,h,i). From a morphological point of view, good adhesion between components implies a compact structure, in which the reinforcing agent is evenly distributed in the matrix. In Figures 11 e-g, the influence of the hemp percentage on the morphology of the H-PP composite can be observed. At a rate of 25-50% hemp, it can be noticed that the fibres are well integrated into the PP matrix. When the percentage of hemp increases to 75%, some of the fibres are not embedded in the matrix. The results indicated by the SEM images are also confirmed by the physico-mechanical tensile strengths, which increased in the first stage for the composites that contain up to about 50% hemp, and after that they exhibited a decreasing tendency.

Chromatic Measurements
Chromatic measurements of composite materials were performed on the entire visible spectrum and were evaluated by colour intensity (K/S). The obtained results are presented in graphic form in Figure 12. Following the processes of obtaining composite materials, the initial mixture underwent a series of chromatic changes. Under the action of temperature and pressure, the chemical fibre (PP, BI or PES) melted and diffused throughout the mass of hemp fibre.

Chromatic Measurements
Chromatic measurements of composite materials were performed on the entire visible spectrum and were evaluated by colour intensity (K/S). The obtained results are presented in graphic form in Figure 12. Following the processes of obtaining composite materials, the initial mixture underwent a series of chromatic changes. Under the action of temperature and pressure, the chemical fibre (PP, BI or PES) melted and diffused throughout the mass of hemp fibre. By cooling, a homogeneous material is obtained whose chromatic characteristics will be influenced by the ratio between the hemp fibre and matrix. In all the analysed variants, the colour intensity of the samples increased with the increase in hemp fibre content, and decreased with the increase in the polymeric fibre content used as matrices.