1. Introduction
The increasing global demand for wood and wood-based products by the furniture and construction industries leads to a significant consumption of wood raw materials. The use of fast-growing tree species and the efficient valorisation of alternative lignocellulosic raw materials, such as agricultural biomass and recycled wood, in the production of wood-based panels represent viable and environmentally friendly approaches to address this problem [
1].
Due to its numerous favourable characteristics, such as durability, resistance to deformation, and excellent tensile strength, plywood is one of the main layered wood-based materials, widely used in furniture manufacturing, interior design, construction, packaging, etc. [
2,
3]. The main type of veneer used to produce plywood, glue-laminated details, and other types of laminated wood is rotary cut (peeled) veneer. These products are primarily applied in structural construction, roofing and flooring, the automotive industry, and aviation, as well as in furniture production.
In recent years, the furniture industry has begun to aim to use lightweight panels that have high mechanical characteristics [
4]. Modern technologies for producing wood-based panels allow the use of small-sized and lower-quality wood raw materials; however, the wood consumption is significant. The production of so-called lightweight furniture panels minimises the application of wood resources and reduces carbon emissions. Currently, there is no standard classifying lightweight panels depending on their density. Among the specialists in the field, the following classification is generally accepted: lightweight panels have a density ≤ 500 kg∙m
−3; very lightweight panels have density values ≤ 350 kg∙m
−3; and ultra-lightweight panels are characterised by densities ≤ 200 kg∙m
−3 [
5]. These panels also have some disadvantages, including their high price, which results in the increased cost of the final product, difficulty in processing with woodworking machines, poor edging quality, installation and fitting problems, etc. In general, lightweight panels can be manufactured entirely of light materials and multilayer panels that have outer layers made of high-density materials with high strength characteristics and inner layer(s) composed of lighter and lower strength materials [
5].
Poplar wood is preferred for producing plywood due to its advantages of being a fast-growing wood species with a relatively low price, good workability and dimensional stability, environmental friendliness, a light color that facilitates dying, etc. In plywood manufacturing, poplar is often used as a substitute for the commonly used beech and birch wood [
6,
7,
8]. Plywood manufacturing technology is associated with significant quantities of waste and by-products, such as peeler cores. It has been established that the volumes of waste peeler cores in the production of veneer and plywood vary from 1% to 30% depending on the average diameter of the logs [
9,
10,
11]. At present, only a very small percentage of peeler cores is used for manufacturing value-added products [
12,
13], while the predominant part is mainly used for the production of energy, wood chips, and other applications with a low economic value, such as packaging, pallets, etc. Currently, there is no well-established approach for the effective and rational utilisation of these by-products of plywood manufacturing in the furniture and construction industries.
The aim of this research was to investigate the feasibility of using poplar peeler cores as a by-product of plywood production in the development of lightweight hybrid plywood panels and determine their main physical and mechanical properties in order to assess their suitability for application in the furniture and construction industries. A simplified method for cutting peeler cores as an alternative to other cutting methods described in our previous research was presented [
12,
13].
3. Results and Discussion
Minimal wood losses were found according to the accepted methodology for cutting the peeler cores into sections. The waste from this type of cutting resulted mainly in the form of shavings and two or three offcuts at either end of each peeler core. When cutting the peeler cores into sections with a thickness of 12 mm (
Figure 1a), the quantitative yield reached 72%. When the peeler cores were cut into sections with thicknesses of 22 mm and 32 mm, the quantitative yields also increased to 78% (
Figure 1b) and 80%, respectively. The results showed very low wood consumption—from 20 to 28%. However, these yields are significantly higher compared to other methods for the utilisation of peeler cores [
12], and the technique is maximally simplified.
The physical properties of hybrid plywood panels fabricated with different ratios of peeler cores sections in the core layer are presented in
Table 2.
The obtained results show that the density of the hybrid plywood panels varied between 304 and 378 kg∙m
−3. These density values are significantly lower compared to conventionally produced poplar plywood [
18,
19,
20,
21,
22]. The density decreased almost linearly with the decrease in the ratio of peeler core sections used in the core layer. There was a slight decrease in the density of the panels that had the same thickness and the same ratio of peeler core sections when replacing the UF adhesive (panel type B—313 kg∙m
−3) with the PF adhesive (panel type C—309 kg∙m
−3). This difference can be explained by the lower glue consumption when using PF resin.
The use of beech veneers for the face layers (panel type I) resulted in increased density by 17% compared to the hybrid plywood panels fabricated from poplar (panel type C). Based on the results obtained, all of the types of hybrid plywood panels produced with peeler core sections in the core layer can be classified as lightweight panels [
5].
The TS values (
) in all of the studied series of hybrid plywood were about 1%. These small values might be explained with the structure of the plywood panels produced, i.e., only 2 veneer sheets in the face layers. In addition, the wood fibre direction of the peeler core sections in the core layer of the panels was perpendicular to the panel plane [
23].
The WA values of the hybrid plywood panels ranged from 21.7 to 28.9%. Generally, two types of trends were observed. Firstly, it was observed that plywood with lower peeler core sections exhibited generally lower water absorption. This phenomenon can be attributed to the reduced volume of wood materials per unit, leading to a smaller area exposed to water. Consequently, the decreased surface area exposure contributed to the observed lower water absorption in such plywood samples. Furthermore, plywood samples constructed with beech as face veneers demonstrated lower water absorption in comparison to those with poplar face veneers. This can be attributed to the higher density of beech as opposed to poplar, resulting in a more compact structure that limits the extent of water absorption in the plywood.
The summarised test results of the MOE and MOR values and the deformation behaviour of the laboratory-fabricated hybrid plywood types with a thickness of 20 mm are shown in
Figure 5,
Figure 6 and
Figure 7.
The obtained MOE values for all series of the hybrid plywood varied significantly (
Figure 5). Notably, when determining the limit of the MOE and MOR values in the directions parallel and perpendicular to the direction of the wood fibres of the plywood, no significant differences were found. The number and location of the peeler core sections in the core layer of the panels played a substantial role in the mechanical performance. For this reason, the results of the mechanical characteristics in both directions (parallel and perpendicular) are summarised and presented together.
The highest MOE values were observed for panel type A—3088 N·mm−2. The hybrid plywood of panel type B reached an average MOE value of 2659 N·mm−2, or 14% lower compared to panel type A. When the UF adhesive (panel type B) was replaced by PF resin (panel type C), the average MOE values reached 2567 N·mm−2, a slight decrease of 3%. The average MOE values for panel type D reached 2312 N·mm−2; as expected, reducing the number of peeler core sections in the core layer of the hybrid plywood resulted in lower MOE values for all types of panels produced.
The determined MOE values for panel type D varied in a wide range from 986 to 3666 N·mm−2. This might be attributed to small ratio (60%) of the peeler core sections used, leading to their non-uniform distribution in the core layer of the panels. Plywood samples featuring lower peeler core sections tend to exhibit increased voids due to the reduced filling area. These voids may serve as weak points, contributing to the initiation of failure during testing. Since the samples for the MOE were randomly selected, the occurrence of weak points under load is entirely unpredictable. Consequently, this randomness resulted in a wide range of values observed in the testing process.
Markedly, the laboratory-made panels exhibited high stiffness values, relatively close to those of medium-density fibreboards (MDF), compared to conventional wood-based panels used in the furniture industry [
24]. These high MOE values can be attributed to the structure of the core layer of the panels, i.e., the direction of the wood fibres of the peeler core sections was perpendicular to the plane of the plywood. This resulted in stresses close to splitting the wood rather than bending.
The results of the performed t-test on a series of hybrid plywood showed that when comparing panel type A and panel type B, the p-value = 0.01289; comparing panel type B and panel type C, the p-value = 0.67827; and comparing panel type C and panel type D, the p-value = 0.31005. In general, only in the first case were the results statistically significant; thus, with a decrease in the number of peeler core sections in the core layer, the MOE values did not change significantly.
The results obtained for the MOR values showed a similar trend to the MOE (
Figure 6).
The highest average MOR value of 17.9 N·mm−2 was determined for panel type A. The average MOR values decreased by 23% (13.7 N·mm−2) when the peeler core section ratio was 80% (panel type B). When replacing UF with PF resin in the panels that had the same number of peeler core sections in the core layer (panel type B and panel type C), a decrease in bending strength by 5% was observed (MOR = 13.0 N·mm−2). This might be attributed to the lower spread rate of PF adhesive (170 g.m−2), a more intensive absorption of the adhesive in the pores of the poplar wood and, last but not least, the secondary heat treatment. The face veneer sheets (1 and 2, and 4 and 5) were previously glued to create complete contact between them, and there were no gaps due to the lack of peeler core sections in the core layer. Additional heat treatment was subsequently performed to bond the peeler core sections to the double-face veneer sheets. In this case, although PF is resistant to thermal treatment, a partial thermal destruction of the adhesive seam may have occurred. Due to all the listed factors, there was a decrease in the strength characteristics of the hybrid plywood glued with PF. The MOR values of panel type D continued to decrease (MOR = 10.7 N·mm−2). Despite the large number of gaps, the strength characteristics were significantly high considering the low density (304 kg∙m−3) of these panels.
A comparison between panel type A and panel type B regarding the determined MOR values was carried out using a t-test. The results showed that for this pairing, the p-value = 0.05313; comparing panel type B and panel type C, the p-value = 0.72862; and comparing panel type C and panel type D, the p-value = 0.09364. All comparative analyses indicated no statistical significance. These results can be explained by the reductions in the number of peeler core sections in the core layer, which decreased the bending strength.
The bending deformation behaviour of hybrid plywood with a thickness of 20 mm is presented in
Figure 7.
When analysing the deformation behaviour and the load capacity of the different types of hybrid plywood with a thickness of 20 mm using the stress–strain relationships, it was found that the highest load capacity and limit stress was demonstrated by panel type A, or plywood with 100% filling bonded with UF adhesive. This type of plywood failed after an average stress of 0.7 MPa, and the deformation was about 20%. A slight drop in the maximum stress of approximately 16% was observed when the ratio of peeler core sections was reduced to 80%, in which case the maximum deformation before failure was about 15%. In the type C and type D panels, a subsequent drop in maximum stress to 0.5 MPa was observed, where the maximum strain before failure was maintained at about 15%.
Graphical representations of the mechanical characteristics (MOR and MOE) of the hybrid plywood panels manufactured with 30 mm thick poplar peeler core sections in the core layer are presented in
Figure 8,
Figure 9 and
Figure 10.
The trend in the MOE remained the same as that of hybrid plywood with a thickness of 20 mm (
Figure 8).
The highest MOE values of 2613 N·mm−2 were observed for panel type E. The decreased number of peeler core sections in panel type F and panel type H resulted in lower MOE values of 2180 N·mm−2 and 1451 N·mm−2, respectively.
The results of the conducted t-test on a series of hybrid plywood with a thickness of 30 mm displayed that when comparing panel type E and panel type F, the p-value = 0.13286; comparing panel type F and panel type G, the p-value = 0.41928; and comparing panel type F and panel type H, p-value = 0.41692. The results in all comparative analyses showed no statistical significance.
The determined average MOR values of the hybrid plywood fabricated with 30 mm thick poplar peeler core sections in the core layer are shown in
Figure 9. Similar to the panels made with 20 mm thick peeler core sections, the reduced number of sections in the core layer resulted in lower MOR values.
The highest MOR value was determined for panel type E. It can be seen that the bending strength of the hybrid plywood with a thickness of 30 mm decreased almost double compared to the panels with a thickness of 20 mm (panel type A). This can be explained by the fact that in the face layers, there were only two veneer sheets of the same wood type and thickness, and in the core layer, the distance between the face layers was increased from 12 to 22 mm. Almost all test specimens were destroyed in the veneer area during testing, and only a few of them in the area of contact between the veneer and the peeler core sections. For this reason, the tensile forces in the lower part of the panels increased with an increase in the distance from the axis of symmetry. Therefore, the ultimate strength of the veneer of a given wood species was reached at a lower load (for panel type A, Fmax = 613, and for panel type E, Fmax = 527 N).
The determined MOR value for panel type F was 7.5 N·mm−2; a reduction of 15% in bending strength was noticed. The difference was slightly less significant compared to the hybrid plywood with a thickness of 20 mm. Changing UF to PF adhesive (panel type G) with pre-bonding of the face veneer sheets again led to a slight decrease (9%), with an MOR = 6.8 N·mm−2. The average MOR value for panel type H, manufactured with the lowest number of peeler core sections in the core layers, was 6.8 N·mm−2.
The comparison between panel type E and panel type F regarding the determined MOR values was performed using a t-test. The results showed that the p-value = 0.13286; comparing panel type F and panel type G, the p-value = 0.41928; and comparing panel type F and panel type H, the p-value = 0.41692. The results in all comparative analyses exhibited no statistical significance.
Figure 10 illustrates the bending deformation behaviour of hybrid plywood with a thickness of 30 mm.
When analysing the stress–strain relationships, it was found that the plywood bonded with the UF adhesive and the highest number of peeler core sections in the core layer (panel type I) had the highest stress resistance within the limits of 0.5 MPa for the hybrid plywood with a thickness of 28 mm. The maximum deformation before failure for this plywood was about 12%. The decreased number of peeler core sections in the core layer (panel type F) resulted in a 25% decrease in the tensile strength. A maximum deformation before failure of about 11% was observed in this type of plywood.
Panel type G and Panel type H exhibited similar stress resistances of about 0.35 MPa and a maximum deformation before failure of approximately 14%.
The last series of panels (panel type I, panel type J, and panel type K) of hybrid plywood were made to determine if replacing the poplar face veneers with hardwood species would affect the physical and mechanical properties of the panels.
The obtained MOE results are shown in
Figure 11.
The average MOE values for hybrid plywood with a thickness of 18 mm (panel type I) were 4010 N·mm−2. Compared to panel type B, manufactured with the same thickness and number of peeler core sections but from poplar wood, the MOE values increased by approximately 33%. The density of hybrid plywood when using beech veneer in the face layer increased by only 13%. In the second type of hybrid plywood (panel type J), with the increase in thickness to 28 mm and the maximum number of peeler core sections, the MOE reached 2677 N·mm−2. Comparing it with the hybrid plywood with the same characteristics but with poplar veneer only (panel type E), the modulus of elasticity increased by 2% and the density by 6%, respectively. The MOE value obtained for panel type K was 1020 N·mm−2. The modulus of elasticity decreased by 30% compared to panel type H. This can be explained by the lower number of peeler core sections and the secondary burning of the PF resin in the production of panel type K.
A graphical representation of the bending strength values of the hybrid plywood panels fabricated with beech veneers in the face layers is presented in
Figure 12.
The results of the bending strength investigation showed a trend similar to the other series of hybrid plywood with the same thickness but with poplar wood veneer only. In panel type I (MOR = 18.7 N·mm−2), an increase of 27% was observed compared to panel type B, which had an MOR value of 10.3 N·mm−2. Panel type J showed a 14% increase compared to panel type E. The determined MOR value of panel type K was 3.8 N·mm−2.
Based on the results obtained for the physical and mechanical properties of all tested hybrid panels, it can be concluded that peeler cores can be utilised as a raw material for producing hybrid plywood. The density-to-strength ratios of this lightweight plywood were also very promising [
25]. Applying peeler cores as a filler in the core layer of hybrid lightweight plywood is rational and allows maximum utilisation. Another important fact is that the bonded hybrid plywood had excellent dimensional stability despite the small number of veneer sheets observed. This stability of the shape of the panels is a consequence of the orientation of the wood fibres of the washers. The larger number of washers provides significant assurance that when hardware or other fasteners are used, they will be securely clamped to the hybrid plywood. All this gives us a premise to claim that the manufactured hybrid plywood panels can be widely applied in the furniture industry as a construction material.
The deformation behaviour of hybrid plywood with a thickness of 18 and 28 mm is presented in
Figure 13.
When analysing the deformation behaviour of the laboratory-produced hybrid plywood, it was found that the panels with a thickness of 18 mm manufactured from beech (panel type I and panel type G) exhibited an average resistance to tension within the limits of 0.4 MPa but with a significant variation in the values of this indicator (from 0.25 to 0.95 MPa). The deformation at failure of these types of plywood ranged from 10 to 16%, but some of the samples had a deformation of more than 30%. The ultimate tensile strength of panel type A dropped significantly to 0.15 MPa, at a deformation range from 10% to 20%. Further, even using the beech veneer, the negative tendency to decrease the load capacity (tensile resistance) with the increase in the thickness of the hybrid plywood was confirmed.