| Literature DB >> 35591327 |
Dorota Dziurka1, Marcin Kuliński1, Adrian Trociński1, Radosław Mirski1.
Abstract
Numerous studies have shown that the geometry of micro-joints significantly affects the strength of the so joined timber element. The bending strength increases by creating a larger bonding area by increasing the length of the wedge joint. Although this type of joint has been successfully used for many years, it can still be troublesome to make. For these reasons, the present study investigated an easy-to-fabricate wedge joint, which we folded during the beams' formation and glued with the same adhesive as the individual lamellas. Although the research has not fully answered all the questions relevant to both scientific and technological curiosity, it indicates the great potential of this solution. Following the principle adopted in the ongoing wood optimisation work, we concluded that the beams of the target cross-section should be produced, and it should only be possible to cut them to a certain length. In this approach, we only removed defects at critical points for the beam structure and, in this way, up to 30% of the timber processed could be saved or better utilised.Entities:
Keywords: strength properties; structural beams; structural glulam elements; timber
Year: 2022 PMID: 35591327 PMCID: PMC9105998 DOI: 10.3390/ma15092992
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.748
Figure 1The binding system proposed in this study.
Figure 2Measuring device: (a) the scheme of the manufactured beam, (b) photo.
Quality of lumber used in the research and determined by the measurement of the modulus of elasticity.
| Type of Beam | Characteristic | Number of Lamella (Counts from the Tension Zone) | |||||||
|---|---|---|---|---|---|---|---|---|---|
| Lam. 1 | Lam. 2 | Lam. 3 | Lam. 4 | Lam. 5 | Lam. 6 | Lam. 7 | Lam. 8 | ||
| M | Em (kN/mm2) | 16.36 | 15.51 | 15.48 | 17.73 | 17.26 | 17.21 | 17.65 | 15.41 |
| SD (kN/mm2) | 0.30 | 0.44 | 0.33 | 0.14 | 0.18 | 0.20 | 0.18 | 0.31 | |
| v (%) | 1.86 | 2.85 | 2.14 | 0.79 | 1.04 | 1.14 | 1.02 | 2.04 | |
| UK | Em (kN/mm2) | 13.24 | 16.08 | 16.15 | 17.63 | 17.18 | 17.21 | 17.66 | 15.73 |
| SD (kN/mm2) | 0.49 | 0.78 | 0.44 | 0.13 | 0.12 | 0.15 | 0.14 | 0.49 | |
| v (%) | 3.72 | 4.88 | 2.73 | 0.74 | 0.70 | 0.89 | 0.80 | 3.11 | |
| Δ | EmM − EmUK | 3.13 | −0.56 | −0.67 | 0.10 | 0.09 | 0.00 | −0.01 | −0.31 |
M—beams composed of 8 layers of the primary yield; UK—beams composed of 7 layers of the primary yield and one sideboard; Em—modulus of elasticity; SD—standard of deviation; v—coefficient of variation.
Figure 3Static bending strength in a 4-point test for manufactured beams.
Statistical analysis of bending strength.
| t * | df ** | p *** | Standard Deviation | Standard Deviation | Levene’s | Levene’s df | Levene’s p |
|---|---|---|---|---|---|---|---|
| 1.999 | 13 | 0.066956 | 4.949 | 3.861 | 0.164888 | 13 | 0.691301 |
* t—value of the Student’s t-test, ** df—the number of degrees of freedom, *** p—Probability value.
Figure 4Failure of joint in beam-type UK.
Figure 5Modulus of elasticity of manufactured beams.
Student’s t-test for the modulus of elasticity, Levene’s analysis of variance.
| t | df | p | Standard Deviation | Standard Deviation UK | Levene’s | Levene’s df | Levene’s p |
|---|---|---|---|---|---|---|---|
| 1.54087 | 13 | 0.14733 | 0.46856 | 0.87850 | 1.7212 | 13 | 0.21224 |
Statistical analysis of the moisture content of beams.
| t | df | p | Standard Deviation | Standard Deviation UK | Levene’s | Levene’s df | Levene’s p |
|---|---|---|---|---|---|---|---|
| −0.63937 | 13 | 0.53369 | 1.2782 | 1.2051 | 0.58921 | 13 | 0.456442 |
Figure 6Moisture content of manufactured beam types.
The values of normal stresses acting on individual lamellas.
| Force | Mg_max (kN·m) | Beam Type | Lam_1 | Lam_2 | Lam_3 | ||||
|---|---|---|---|---|---|---|---|---|---|
| Top * | Axis ** | Top | Axis | Top | Axis | Bottom *** | |||
| Normal Stresses (N/mm2) | |||||||||
| 121 | 67.2 | UK | 35.0 | 32.3 | 29.7 | 25.1 | 20.5 | 15.9 | 11.3 |
| 134 | 74.4 | M | 35.0 | 30.6 | 26.3 | 21.9 | 17.5 | 13.1 | 8.8 |
| 191.5 | 106.3 | M | 50.0 | 43.8 | 37.5 | 31.3 | 25.0 | 18.8 | 12.5 |
*—upper surface of the lamella, **—in the axis of the lamella, ***—lower surface of the lamella.
Figure 7ANOVA analysis of the tensile strength of adhesive joints.
Figure 8View of the tensile specimen (cross-section approx. 20 × 20 mm).